You completely overlooked the 1910 Coanda plane, using a 4 cylinder engine to drive a fan, with fuel injected and ignited aft of the fan. While it is not clear whether the plane actually flew, it did lead Henri Coanda to note and explore the tendency of the flame to cling to the sides of the fuselage. Now we are well aware of the Coanda effect.
Fuck off coanda didn't do shit in 1910 but a shrouded propeller. After jet power was established, he tried to leech off some relevance by showing clearly more recently fabricated bullshit plans where he added in airstream combustion which he tried to sell as his original plans.
The all first motorjet engine was built by Henri Coanda in 1910: this engine was installed in a monoplane aircraft and tested from Coanda himself: it works well but Coanda was surprised from the power and the plane did crash during take off.Coanda was not seriously injured but did stop the experiences…Coanda had the help from the Gustave Eiffel and the mathematician Henri Painleve…
Coanda said he was distracted by the jet exhaust flow clinging to and charring the mahogany sides of the aircraft fuselage. In his distraction, he fail to notice the wall of the city, Paris, in the airplane's path. Crashing into the city wall resulted in his temporary arrest as an Anarchist Saboteur and being enjoined from involvements with aircraft. His distraction, however, resulted in his first description of laminar flow (Coandă effect) and the founding of the science of fluidics.
@@RealTechZen When I set up a ventilation fan to cool my apartment, I take care that the air-flow runs parallel to the longest wall. A tiny desk-fan keeps a huge apartment feeling light and airy without any drafts. Thank you, Monsieur Coanda!
@@EngineeringFun Technically that is not a jet since there was no fuel injection and no high speed thrust generated by thermal cycle...it was a ducted fan + compressor + a nozzle
@@electricaviationchannelvid7863 , @My Opinion Doesn't Matter - It DID have fuel injected in the compressed air volume. Actually that's how the now famous Coanda effect was developed, despite the deflectors near fuselage, the flames licked the fuselage after a certain speed. The numbers if I remember well were 80kg thrust without fuel injection and 220kg with injection (not sure of the precise numbers). The accident in which his jet crashed and burned was because of the unexpected high thrust after the fuel was turned on. The Romanian man was a professional designer with Bristol and not a pilot. He intended to only taxi the plane and didn't know how to pilot a plane. Read about this guy from less biased sources than Wikipedia. I studied him extensively in college and personally saw his creations with detailed blueprints at the Dimitrie Leonida technical museum in Bucharest when I visited as a student. There are many articles and detailed plans about his planes and there is also a motor jet sled he created. There is plenty of misinformation floating around (including from some YT channels!!) because some people who made similar stuff decades later wanted to be first in history books. Just think about this, only 7 years after the Wright brothers' flight with a stick and canvass contraption, at the time when stick and canvas was still state of the art this guy has a plane without any canvas (all mahogany plywood) and without the bracing wires AND with jet propulsion. Gustave Eiffel, the designer of Eiffel Tower, once said about Henri Coanda: “This boy was born 30, maybe 50 years earlier.” adabarbu.medium.com/henri-coand%C4%83-a-romanian-inventor-a8a301162e80
@@pork_cake This is why Wankel-Rotary engines should have been used ; they have 1/10 the # of parts , and break much less often . They also produce over twice the hp. as four-stroke engines , per-pound .
@@Prof.Megamind.thinks.about.it. the breaking part is debatable, however if they were used more we definitely could have solved the issues and had extremely reliable, compact, and powerful rotaries.
@@finlaymcdiarmid5832 That may be true , but the airlines require compact power and extreme reliability . Rotaries fit this bill much better than piston-engines .
so in other words - some of the jets' plusses and all of the piston engine's negatives. Super expensive super complicated and only marginally better in some scenarios. Deadend.
Very interesting, thank you. The various compound engines in the 40s are really fascinating. But when you look at so much complexity for 12% gain there are many other options.
This sounds like an interesting engine option to use in a fictional, dieselpunk-themed story setting while also reserving the early turbojet engines as something being experimented on in the background of the said story setting. Said early turbojet research could also be part of a story plot device alongside WW2 research projects like radar, radios, cryptography and early computers, rocketry, etc.
I've been waiting for a video on the VRDK and motorjets in general. I believe if used a little earlier in the war and with more optimization, the tech would have had a nice 3-5yr period of being the best powerplant.
this time flight uploads before i go to work. another good day in the books. but on another note something makes me think these would be deafening.. im getting thunderscreech vibes *edit* 12.5% increase in efficiency 🔥🔥
When I was a kid I read a book on building flying model planes (wires only - decades before RC was common.) One design was a model F-86 with a similar set-up turning an internal ducted fan, but without the fire, of course. Woulda made balsa wood planes - interesting.
I think it's funny how people drone on about complexity. The piston engine has soldiered on faithfully in so many apps and for 100 yrs in aircraft. Its numerical parts complexity is now just a given. They can all be made very well and not have to run at their ragged metallurgical edge to get the thermal efficiency; as does a turbine running almost at critical mass and can produce no meaningful power outside of that narrow parameter. On a more red neck note who would NOT want to fly in a Learjet that sounds like two Mclaren F1's in a dead heat either side of your cabin. Pod racers eat your heart out.
but the power to weight ratio of piston engines is shit...... so yeah, you dont have to run them ragged, but even running them ragged, jets still have a better power to weight. so they'll run long enough to get shot down by the faster planes.
I was thinking the same thing when I saw the title, but Coanda's experiments were more focused on recapturing the excess energy in the exhaust of a piston engine. No reheat, just fully expanding the exhaust. So while the motorjet uses the piston engine to replace the role of the turbine in a jet engine, Coanda used the piston engine to replace the compressor and combustion stages. TLDR: Coanda did the opposite of this, sorta
There are some new exciting developments being researched in rotary engines like the Wankel, and despite being a little less fuel efficient than pistons in their current state, rotaries are much smaller, much less complex. much lighter, and operate at much higher rpms... sounds like a better match for a Motorjet to me! Thanks for the excellent video Flight Dojo!
@@kieranh2005 Yes, when running at a _constant speed_ at their _sweet spot,_ the Wankel is very efficient indeed. They do not like being revved up and down. Mazda's new MX-30 hybrid in January will have a Wankel range extender. It will be easy to convert to hydrogen running. Japan is turning to a hydrogen economy, with hydrogen produced economically by helium gas cooled nuclear reactors.
@@johnburns4017 >They do not like being revved up and down. So they are good in something like a cheap kamikaze drone that flies at constant speed, attacks with quantity and where lower noise is an additional benefit as it reduces detection.
Imagine a compound cycle engine where the shaft for the compressor and turbine was also the eccentric shaft for a rotary engine sandwiched in between them
When I saw the liquid piston engine, which is an inverted chamber and rotor of the Wankel rotary, I had the same thought. Why not exploit the weight advantage of the rotary and fuel efficiency of the otto cycle engine and produce a general aviation combined cycle engine with low gal/hr consumption under cruise, but high dash speed for fun.
@@electric_boogaloo496 Wankel engines tend to drive efficiency way down due to their elongated, oddly shaped combustion chamber, it behaves roughly like a engine with a very short stroke but wide bore, good for power, bad for efficiency
Or how about one which has two compressors the first a low pressure axial compressor which is powered by the more efficient piston engine (and also acts as a supercharger diverting a little air for the piston engine); and the second (centrifugal or axial) which is powered by a turbine. Perhaps dumping the exhaust of the piston engine into the inlet of the second compressor (the piston engine possibly running slightly fuel rich). Perhaps the combustor-can-flameholder things could run fuel rich to keep the temperature down but the lean air entering the entire combustion chamber would then meet the burning fuel rich air coming out the combustion cans and maybe ignite a secondary combustion? So the entire combustion chamber is burning, but at lower temperature than normal.
This looks like one of those times when you have established tech (piston engines) and new advanced tech (jet turbine engines) and there were a few engineers that understood one well and one not so well, and at that point, it was just natural for them to ask "What if?" and experiment. Each engine type has its pros and cons, and its own use and purpose. I call it scientific due diligence is seeing if it was possible to combine the strong points of each type into a single unit. Today, if you look hard enough on RUclips, you will find the occasional garage guy that took a turbo charger off a car and made a crude but functional jet engine out of it. I think this was a necessary phase of aviation technology we needed to look at, and a part of what makes aviation history so damn cool.
10% increase in fuel efficiency is a lot, but i wonder what practical applications this might have for hybrid/electric drives. Electric motors might need less gearing and with many short distance aircraft there might be a sweetspot in between a larger battery and the wight of an electrically driven motorjet to boost range? Kind of like an afterburner for electric aricraft, which would optimally use regenerative fuels or at least fill the gap towards heavier and mid ranged aircraft with better efficiencies? Great video, my jaw dropped when i saw the inline ice which even had enough thrust on its own to power the plane. It's a logic step to use the excess heat but the idea of basically putting an entire engine inside another is really amazing
Love your content as always. Just a note on the Russians late start into Jet/Rocket plane development. They did in fact fly the Bereznyak-Isayev BI-1 rocket powered interceptor in May of 42 with some success.
Thanks for this video, there isn't much out there about motorjets. I found them interesting because even today, with modern materials, temperature at the turbine blades is one of the biggest limiting factors in jet performance. Unfortunately, the tradeoffs don't appear to be worth it, and afterburners end up being a better solution for aircraft that need to go that fast. Maybe something will change, between a new interest in supersonic transportation and better battery technology, it might be possible.
My first visit to the Oshkosh convention was in 1974 and I recall a prototype on display that year or soon after of a one-half size F80 that used an automotive V8 driving an internal fan through a gearbox. I haven't seen or heard of it since then, and it wasn't ready to fly at that time, so I have no idea if it was successful. I suspect that that propulsion design would be less effective on a sport plane than a propeller would be, but the point of it was a jet-powered design without the high cost of a turbine power plant. It interested me a lot because it looked just like the fighter it replicated, only smaller.
Yup, ducted fan with afterburner is exactly the thing that came to mind. That is, if there's no turbine, isn't that like an afterburner, except that ignition in the jet's combustion chamber wasn't from an upstream turbojet. Or, am I totally confused.
The most practical combustion engine for the Motorjet might be the Wankel! Why?: small size, high rpm and excess burnt oil simply provide extra power to the jet engine stage! Great video!!
I have seen a homebuilt motorjet. Not based on the Campini design but the Tsu-11, the motorjet from the model 22 Ohka. It uses a McCulloch TC-6150-J-2 turbocharged flat-6 2 stroke engine to drive a similar compressor with side inlets. It is installed in a small plane similar to the model 22 but altered by shortening the nose and installing a fuel tank, and with a V-tail like a Bonanza. It can cruise on the piston engine only and can go exceptionally fast with the jet started. It occasionally appears at the local airport once in a great while. I have no idea about who built it or why, but I've seen it with the tail removed and the engine exposed.
Rolls Royce’s patent of 1995 has long since expired. If anyone thought there was any merit in the engine they would have done something about it by now. I won’t hold my breath.
@@lordgarion514 Robert, you completely missed the point. The flying wing and its inherent advantages was a dream for Jack Northrop, who died before he saw it come to fruition as computerized flight controls finally overcame some of the challenges the design faced. People told Jack Northrop that it wasn’t possible, the same way the original poster of this thread breezily dismisses the entire concept of a motorjet from his couch.
Thank you for the info on the Ohka "motorjet" version. I have seen a Smithsonian photo of their "motorjet" Ohka 22 (the Japanese Navy Air Research Bureau designation - the plain rocket version was Ohka 11) which designates the engine as a "Campani jet" engine. The Smithsonian photo states that their Ohka 22 was "recovered in Japan in 1945 -- I have seen a photo of an Ohka-22 sitting on an assembly trestle in a factory in Japan with piles of Ohka parts and partially assembled Ohka aircraft in the background -- this may (or may not) be the same motorjet Ohka. I'm interested in the Ohka because I have a photo taken of my father and his high school friend standing in front of an Ohka at Yontan airfield on Okinawa. The photo is framed to show his tent in the background. The photo showing my dad includes the Ohka with Identification number I-18. There are also photos around the Internet with good images showing the numbers I-10 and I-13. I was in contact with a correspondent who sent me a copy of two photos, one of his father helping to move Ohka I-10 along a dirt track on a low dolly and another of his father standing next to the rocket engine of I-10 with a date on the photo of 4 April, 1945. This correspondent says that he visited an aviation history museum in Chino, California, to see an Ohka that they have (had??) on display and a curation expert at the museum told him that the invading US troops found five Ohkas, fueled and armed, in a cave on Okinawa and they were removed to an open area at Yontan so that they could safely be disarmed. There are photos of I-18 with its external nose removed while the warhead is being removed. There are also photos showing the solid rocket fuel tubes being removed from an Ohka (this aircraft is not identified but the background surroundings seem to indicate that it is likely also I-18). I do not have any information about any other Ohkas that were captured on Okinawa.
Interesting. didn't the Junkers Jumo 004 turbojet used in the Me-262 fighter use a 2 cycle piston engine to start their compression cycle before transitioning to a 'pure' turbojet?
We built a compound cycle engine as an example and as a theoretical possible propulsion system for what is now known as the tomahawk cruise missile it was a V8 of about 250 CC's per cylinder running on compressed air produced over 1,000 horsepower! What made this particular compound cycle engine very interesting was a pair of clutches so you could use the turbine power to draw in more air and create more thrust as a conventional turbo shaft engine operates or with the flip of a switch you could add the turbines output to the crankshaft and make insane torque at the crankshaft. I believe it was an old German design from when they were having trouble creating a combuster section with materials of the day and lacking knowledge of modern engineering to create an air cushion between the flame and the metal so that the combustors did not melt through in a matter of seconds. All this contained in a 20-in diameter about 22 in Long it was actually very light, crazy powerful and produced a lot of thrust it was very efficient Considering it had all the modern engineering and materials made thrown at it. I don't know whatever happened to the test engine but it ran for 24 hours a number of times at Garrett Turbine Signal oil now Honeywell Phoenix Arizona.
I think its so cool that i knew the name Caproni before watching this video but never having known much about airplane history. I watched an animated film by studio Ghibli that features Caproni as a person of admiration for the main protagonist, a Japanese boy growing up and then working as an aerospace engineer in japan, before ww2. He meets Caproni in his dreams and they talk about wanting to build beautiful aircraft. I dont know how historically accurate Caproni or even the whole era is represented, but it does follow the life of the eventual designer of the zero fighter. Its called The Wind Rises, if your interested. Porco Rosso is another film by Ghibli, set in a fantasy world full of custom bi-planes and skypirates. Iv always wondered how flight would develop in a slower or different environment than history has already proven. Maybe we would see interesting designs like this developed more and become more common place as a form of personal transport completely reshaping the world as we know it. Thanks for this tidy video essay. I really enjoyed learning about this engine!
Try a small, compact, 3-rotor Wankel engine, mated directly (no gearbox) behind a 3-5 stage fan setup. Since a rotary engine runs best at about 5k RPM, you can mate it to fan, about 1.1m in diameter, which at 5k RPM would result in tip speeds, just below the speed of sound. Use cooling fins and air inlet in the duct for the engine. Route the fuel and electrical control lines through the struts. Use a jack-screw-mounted bulb in the exhaust nozzle to control exhaust airflow. If you can generate about 1000 lbs of thrust with such a setup, you could power a light GA plane with it.
The made a H block 2-stroke diesel engine like the Sabre for it at 75 litres, but resorted to a single boxer layout. The Nomad actually flew in an Avro Lincoln. Like all these types, turbo jets took over.
I honestly never knew about that version of the Ohka. The various Japanese suicide craft have always been of interest to me to the point where one of my cats is named Kaiten, yet I never heard of that version.
@@soggycracker5934 btw, the other cats are Harley aka WaccaCat (wacca is Latin for cow and she is black & white, wacca became vacca in later spoken Latin, you might know it as the root of the word vaccine), Maxwell aka General Taylor (he came with the name Maxwell, combined with my last name and he shares his name with one of the most famous American generals of the 20th century) and Luna the Lunatic (she came with the name Luna the rest is self explanatory). I got Kaiten & Harley as kittens, I adopted Luna & Maxwell from friends who were moving. Also I chose Kaiten because it sounds a lot like 'kitten' & BakaCat is both a nod to a nickname the Ohka apparently had as well as a nod to one of the names I commonly use, bakaman. (which itself is both meant to be amusing as well as being a nod to Socrates when he said that while people think him smart, he really knows nothing.) Yeah, I like to overthink way too many things.
in the 60's i recall pop science magazines doing storys about putting big Buick engines in Sabre jets on a guy hobby basis.cold jets i think they were called.
@@wingracer1614 Because only a few countries are able to produce turbine blades and they keep the metallurgy secret at an overpriced level...With a motorjet or electric compound motorjet you do not need that part but still able to achieve high speed thrust as well self launch capability vs. a pulse jet engine...
Gille St Hillaire designed a positive displacement motor called the Quasi Turbine. It is 1/5 the size and weight of a piston engine. The engine is empty in the centre and could house a transmission or generator. Multiple units can be ganged together like Wankle. Rotating eliminated vibration and this airplanes could be lighter again
I have always wanted to build an aircraft for GA that uses a piston engine to power a ducted fan but it will have many stages to the fan each spinning faster.
perhaps the Liquid Piston X3 mini engine could perform better at this task, being far more power dense while having the efficiency bonuses of internal combustion. they had a demonstration aircraft proving hybrid electric operation, with in flight starting and stopping, so perhaps an "Electro-Turbo-Motor-Jet" would be possible ahahaha
Just wouldn't make much sense. Now, a compressor that can be shifted to electrical power, mounted to a zeppelin or blimp that carries solar cells? That could work. But just hydrogen? Makes more sense to run a normal jet straight off of hydrogen.
The problem with powering a compressor with anything but a turbine on the same shaft is immense power that is needed. For instance a model turboshaft engine gives out about 5-6 kW of shaft power weighing 3-4 kgs. So to power its compressor one would need about 9-12 kW motor. And most likely a gearbox as the compressor wheel should rotate at about 100k rpm speed. It did make sense at the time when there wasn't much experience in combustion chambers designing and turbo jet engines in general so it was easier to control and tune the prototypes separately for the turbine and the compressor sides but once their performances are balanced there is no point to put anything in between.
So two totally different power trains powered by two totally different fuels, one of which is expensive, heavy and inefficient for aircraft use where weight and efficiency are everything? Yeah that sounds like a winner
Yes, it would work, the Caproni Campini could fly on fan only and then turn on the burner for extra thrust. If you used an alkaline fuel cell (which is being developed for the Piaseki Helicopter) the cooling requirements of 250C could be used to preheat the air before the burner. Motor jets could work, the reason Caprioni's didn't was the primitive nature of the piston engine which lacked an effective super charger.
Later versions of the Duplex Cyclone had a turbine coupled with the crankshaft. As a Turbo-compound engine the emphasis was on power recovery from the exhaust, not jet thrust. It saw quite widespread use though.
In the late 1930s/1940 the NACA was developing a transonic motor jet called "Jakes Jeep", it used a Pratt Whitney R-1535 radial. The man driving the program was Eastman Jacobs. He is famous for perfecting the laminar flow wing technology that went into the P-51 Mustang as well as developing the NACA 4 and 5 digit wing profiles all sides used. "jake's Jeep" was meant to reach around 550mph. It had a V tail to limit the problems of shock wave impingement on the tail while the laminar flow wing gave a high Mach Limit. All pretty good for 1939/1940. "Jakes Jeep" evolved into the Bell X-1 that first broke the sound barrier. The Bell X-1 also initially had a V tail. With US engine technology and supercharging technology Jakes Jeep would have worked. -There is a sad side note to this. When information of the Whittle turbojets was transmitted the US Happ Arnold, Head of the USAAF, did not transmit it to the NACA. -The Resulting Bell X-59 was a failure as the wings were not only too thick but failed to use the Laminar Flow wings already coming in on the P-51. Eastman Jocobs was so heartbroken he left NACA though some say it was because the innovative engineer had diverted NACA funds into plasma research in an attempt to realize thermonuclear fusion.
I assume the weight penalty is only worth it if we return to giant aircraft (An-225, 747, A380, etc). As long as we aim for smaller, that weight difference is too much of the overall mass budget of a design.
Why not electric transmission to eliminate the gearbox. That also allows reduction of the size of the engine since temporary peak power for takeoff can be drawn from batteries while the engine can be sized smaller for cruise power
He S 50 was a Motorjet developed at Heinkel by Wunibald Kamm, with inherent better features than the Caproni, that actually was an afterburner reinforced version of Stipa duct fuselage. However, at Heinkel failed in obtaining enough cooling for the 2-Stroke engine, and never reached production. Gesund +
I remember reading, as a kid, that during WW2, the Russians had developed an aircraft that employed a piston engine & propeller, and a ram-jet. It reached ~350 mph on piston power, then the ram-jet would kick in.
From what I know about German engineers, and their love of insanely, needlessly complex and expensive overengineering of simple machines, I'd bet the German engineers watching this video experienced a markedly higher heart rate, increased respiration, and a far higher degree of interest when they saw this video.
And right now someone at BmW is probably feverishly designing a motorjet to fit in their various cars to continue the tradition of needlessly complex, unreliable cars.
Modern materials science is progressing at breakneck pace, so it's very possible internal combustion engines will become light enough for the combined cycle engine to become practical.
Rolls-Royce began working on a sleeve valve two stroke “sprint” engine aka Crecy. It was all about power at the expense of fuel consumption. Once it was running they realised it could be a great compressor stage for a jet engine. Ultimately, the turbojet was easier to develop so the Crecy was cancelled.
Sounds like an afterburner for a prop driven plane. Even if they can set it up to be efficient, is that gain in efficiency going to justify the increase in complexity, maintenance and reliability.
I think that this idea still has some validity. With modern piston engines and compressors you could create something that is both efficient at low speeds, and yet possesses turbojet performance for brief periods. All at a relatively low cost.
for example, for a suicide drone which flies low and slow and then activates sprint mode for the last few minutes? Hell lets not forget that huge reason why motorjets were terrible when they were made, was because nobody bothered making them "right". i.e. for example no correctly made airflow, that helps to keep whole system running.
There have been modern developments of a somewhat similar nature to the motorjet, the composite cycle jet engine, which uses a piston engine (of whatever nature) as a pre burner stage gas generator to increase the thermodynamic efficiency of the whole engine. But so far all variants I've seen use the piston engine as just a gas generator having no apparent use for the shaft power to the main jet engine, perhaps due to scale that power is relegated to running auxiliaries. I suspect using the piston engine as a gas generator in a motorjet would improve it's efficiency, running a very large compounded turbine after it but before the jet combustor would keep the metallurgy a non issue and you could have a reasonably efficient early propfan.
If the MTU concept adds efficiency at the cost of weight, it should work on a land-based turbine used to drive a generator. Those utility guys are really, really interested in efficiency. Today they use the output of a turbojet to boil water to make steam to drive a steam turbine, but the steam turbine is taking energy out on the low-temperature side of the cycle, which is less efficient. The MTU concept, if I understand properly, is proposing to take some energy out of the fuel on the high-temperature side of the turbojet cycle, by raising the initial temperature. That improves the Carnot efficiency!
The Napier Nomad of the late 1940's / early 1950's was a brillient implimentaion of a turbocompound engne that at the time offered record breaking fuel efficiency at the expence of horrendouse complexity en.wikipedia.org/wiki/Napier_Nomad. I came accross some drawings when I was an apprentice and the Nomad was much more advanced than the engines we were producing for the HS125 loco's. Unfortunately cheap oil and simple turbojets killed it stone dead. The Nomad was reall a gas turbine using a 2 stroke diesel engine as the combustion chamber with the net result of massive overall compression ratios. Power was taken from both the turbine and the engine via a compley hydraulic friction drive variable gearbox which overcame the matching problems described in the RR patent. Takeoff power could be supplimented with afterburning and water-methonal injection, it was a true beast.
Seems like a rotory engine would be a better option than a piston engine for this kind of layout. They are much smaller, lighter and simpler than a piston engine and they spin at a much higher rpm which I have to think would be better than the slower speed a piston engine needs to run at. They can also put out a lot of power when designed and built well. And are stackable so if you want a larger stack you just need a few longer tie rods and crankshaft and you can essentially bolt two or more engines together. The only downside is that when not built perfectly they can have reliability issues and the engine technology isn't nearly as far developed as piston engines.
What a very fascinating look such unusual aircraft types I really enjoyed it and I help me better understand how this type of aircraft works. But do the Ryan FR Fireball and the xf15c fall into the same category of a Motorjet aircraft?
>XF15C No. It had 2 separate engines, that could work independently. The idea behind motorjet is that the regular internal combustion engine works as both an engine for propeller and compressor for jet, meaning jet part can't work as its own thing, as at that point its just a combustion chamber with no air flow.
You completely overlooked the 1910 Coanda plane, using a 4 cylinder engine to drive a fan, with fuel injected and ignited aft of the fan. While it is not clear whether the plane actually flew, it did lead Henri Coanda to note and explore the tendency of the flame to cling to the sides of the fuselage. Now we are well aware of the Coanda effect.
yeah he also made a lot of claims about the planes, which many now suspect to be exaggerated, interesting plane nonetheless.
Fuck off coanda didn't do shit in 1910 but a shrouded propeller. After jet power was established, he tried to leech off some relevance by showing clearly more recently fabricated bullshit plans where he added in airstream combustion which he tried to sell as his original plans.
The all first motorjet engine was built by Henri Coanda in 1910: this engine was installed in a monoplane aircraft and tested from Coanda himself: it works well but Coanda was surprised from the power and the plane did crash during take off.Coanda was not seriously injured but did stop the experiences…Coanda had the help from the Gustave Eiffel and the mathematician Henri Painleve…
And ever since... all Romanians believe they were the first to invent the JET ENGINE :)))))
Coanda said he was distracted by the jet exhaust flow clinging to and charring the mahogany sides of the aircraft fuselage. In his distraction, he fail to notice the wall of the city, Paris, in the airplane's path. Crashing into the city wall resulted in his temporary arrest as an Anarchist Saboteur and being enjoined from involvements with aircraft. His distraction, however, resulted in his first description of laminar flow (Coandă effect) and the founding of the science of fluidics.
@@LHFX so are the British
@@RealTechZen When I set up a ventilation fan to cool my apartment, I take care that the air-flow runs parallel to the longest wall.
A tiny desk-fan keeps a huge apartment feeling light and airy without any drafts.
Thank you, Monsieur Coanda!
@@jerryjencik3879 Well... at least there's some legitimacy behind their claims.
Frank Whittle initially thought of a piston engine to power the compressor in the 20s, but realised it wasn't necessary - a man way ahead.
The first motorjet airplane: en.wikipedia.org/wiki/Coand%C4%83-1910
@@EngineeringFun Technically that is not a jet since there was no fuel injection and no high speed thrust generated by thermal cycle...it was a ducted fan + compressor + a nozzle
@@electricaviationchannelvid7863 Technically that is a jet.
@@electricaviationchannelvid7863 , @My Opinion Doesn't Matter - It DID have fuel injected in the compressed air volume. Actually that's how the now famous Coanda effect was developed, despite the deflectors near fuselage, the flames licked the fuselage after a certain speed. The numbers if I remember well were 80kg thrust without fuel injection and 220kg with injection (not sure of the precise numbers). The accident in which his jet crashed and burned was because of the unexpected high thrust after the fuel was turned on. The Romanian man was a professional designer with Bristol and not a pilot. He intended to only taxi the plane and didn't know how to pilot a plane. Read about this guy from less biased sources than Wikipedia. I studied him extensively in college and personally saw his creations with detailed blueprints at the Dimitrie Leonida technical museum in Bucharest when I visited as a student. There are many articles and detailed plans about his planes and there is also a motor jet sled he created. There is plenty of misinformation floating around (including from some YT channels!!) because some people who made similar stuff decades later wanted to be first in history books. Just think about this, only 7 years after the Wright brothers' flight with a stick and canvass contraption, at the time when stick and canvas was still state of the art this guy has a plane without any canvas (all mahogany plywood) and without the bracing wires AND with jet propulsion. Gustave Eiffel, the designer of Eiffel Tower, once said about Henri Coanda: “This boy was born 30, maybe 50 years earlier.” adabarbu.medium.com/henri-coand%C4%83-a-romanian-inventor-a8a301162e80
@@EngineeringFun Well, then I was wrong, sorry!
It’s rare that I see an aviation video with something I’ve never heard of and none of my books have referenced but today you rolled a Nat20.
Adding a pair of v10 engines to a turbofan sounds like a maintenance nightmare.
On the other hand, the maintenance guys would be able to find parts down at the junkyard 🤣
@@pork_cake
This is why Wankel-Rotary engines should have been used ; they have 1/10 the # of parts , and break much less often .
They also produce over twice the hp. as four-stroke engines , per-pound .
@@Prof.Megamind.thinks.about.it. the breaking part is debatable, however if they were used more we definitely could have solved the issues and had extremely reliable, compact, and powerful rotaries.
@@Prof.Megamind.thinks.about.it. they use much more fuel.
@@finlaymcdiarmid5832
That may be true , but the airlines require compact power and extreme reliability .
Rotaries fit this bill much better than piston-engines .
so in other words - some of the jets' plusses and all of the piston engine's negatives. Super expensive super complicated and only marginally better in some scenarios. Deadend.
Very interesting, thank you. The various compound engines in the 40s are really fascinating. But when you look at so much complexity for 12% gain there are many other options.
This channel absolutely rocks. Fact dense but lightly delivered.
This sounds like an interesting engine option to use in a fictional, dieselpunk-themed story setting while also reserving the early turbojet engines as something being experimented on in the background of the said story setting. Said early turbojet research could also be part of a story plot device alongside WW2 research projects like radar, radios, cryptography and early computers, rocketry, etc.
It's worth also noting the Campini had a turbojet design that used a water cooled turbine. So did the Germans (to overcome alloy problems)
I've been waiting for a video on the VRDK and motorjets in general. I believe if used a little earlier in the war and with more optimization, the tech would have had a nice 3-5yr period of being the best powerplant.
Whittle issued patent for its engine in 1930, with proper funding he could have working fighter in 1935.
this time flight uploads before i go to work. another good day in the books. but on another note something makes me think these would be deafening.. im getting thunderscreech vibes
*edit* 12.5% increase in efficiency 🔥🔥
When I was a kid I read a book on building flying model planes (wires only - decades before RC was common.) One design was a model F-86 with a similar set-up turning an internal ducted fan, but without the fire, of course. Woulda made balsa wood planes - interesting.
I think it's funny how people drone on about complexity. The piston engine has soldiered on faithfully in so many apps and for 100 yrs in aircraft. Its numerical parts complexity is now just a given. They can all be made very well and not have to run at their ragged metallurgical edge to get the thermal efficiency; as does a turbine running almost at critical mass and can produce no meaningful power outside of that narrow parameter. On a more red neck note who would NOT want to fly in a Learjet that sounds like two Mclaren F1's in a dead heat either side of your cabin. Pod racers eat your heart out.
but the power to weight ratio of piston engines is shit......
so yeah, you dont have to run them ragged, but even running them ragged, jets still have a better power to weight.
so they'll run long enough to get shot down by the faster planes.
@@lordgarion514 🙄🙄😊😉
Many thanks Flight Dojo, I was looking at Wulf II stepped piston engine last night. It's a delight to see another curious and unconventional engine.
Fascinating video...thanks..
the exhausts on the spitfire were angled rearwards to get some measure of thrust from the exhaust
1:27 didn't (Romanian) Henri Coandă try something like this in a plane in 1910?
He made a ducted fan.
I was thinking the same thing when I saw the title, but Coanda's experiments were more focused on recapturing the excess energy in the exhaust of a piston engine. No reheat, just fully expanding the exhaust. So while the motorjet uses the piston engine to replace the role of the turbine in a jet engine, Coanda used the piston engine to replace the compressor and combustion stages.
TLDR: Coanda did the opposite of this, sorta
@@thejohhny2943 no Coanda did made a real compressor with gasoline injection in the compressed air: this design is well known
There are some new exciting developments being researched in rotary engines like the Wankel, and despite being a little less fuel efficient than pistons in their current state, rotaries are much smaller, much less complex. much lighter, and operate at much higher rpms... sounds like a better match for a Motorjet to me! Thanks for the excellent video Flight Dojo!
At their peak they are relatively efficient in fuel use compared to a reciprocating piston engine. Everywhere else they suck.
@@kieranh2005
Yes, when running at a _constant speed_ at their _sweet spot,_ the Wankel is very efficient indeed. They do not like being revved up and down. Mazda's new MX-30 hybrid in January will have a Wankel range extender. It will be easy to convert to hydrogen running. Japan is turning to a hydrogen economy, with hydrogen produced economically by helium gas cooled nuclear reactors.
@@johnburns4017 >They do not like being revved up and down.
So they are good in something like a cheap kamikaze drone that flies at constant speed, attacks with quantity and where lower noise is an additional benefit as it reduces detection.
@@Poctyk
They also do just that.
Imagine a compound cycle engine where the shaft for the compressor and turbine was also the eccentric shaft for a rotary engine sandwiched in between them
When I saw the liquid piston engine, which is an inverted chamber and rotor of the Wankel rotary, I had the same thought. Why not exploit the weight advantage of the rotary and fuel efficiency of the otto cycle engine and produce a general aviation combined cycle engine with low gal/hr consumption under cruise, but high dash speed for fun.
@@electric_boogaloo496 Wankel engines tend to drive efficiency way down due to their elongated, oddly shaped combustion chamber, it behaves roughly like a engine with a very short stroke but wide bore, good for power, bad for efficiency
@@user-si5fm8ql3c liquid piston's take on the Wankel does solve the combustion chamber shape problem.
@@user-si5fm8ql3c
Not when burning hydrogen.
Or how about one which has two compressors the first a low pressure axial compressor which is powered by the more efficient piston engine (and also acts as a supercharger diverting a little air for the piston engine); and the second (centrifugal or axial) which is powered by a turbine. Perhaps dumping the exhaust of the piston engine into the inlet of the second compressor (the piston engine possibly running slightly fuel rich). Perhaps the combustor-can-flameholder things could run fuel rich to keep the temperature down but the lean air entering the entire combustion chamber would then meet the burning fuel rich air coming out the combustion cans and maybe ignite a secondary combustion? So the entire combustion chamber is burning, but at lower temperature than normal.
I was searching for this information as an aviation nerd and didn't find anything so thank you very much.
Great video man! Love this format with the voiceover and the various clips and pictures in the background!
This looks like one of those times when you have established tech (piston engines) and new advanced tech (jet turbine engines) and there were a few engineers that understood one well and one not so well, and at that point, it was just natural for them to ask "What if?" and experiment. Each engine type has its pros and cons, and its own use and purpose. I call it scientific due diligence is seeing if it was possible to combine the strong points of each type into a single unit.
Today, if you look hard enough on RUclips, you will find the occasional garage guy that took a turbo charger off a car and made a crude but functional jet engine out of it.
I think this was a necessary phase of aviation technology we needed to look at, and a part of what makes aviation history so damn cool.
Always love videos abou italian engines, theres way too little of them out there even though the italians were crazy as well.
Why was there a red image of Ba’al above the test tunnel in the first few couple of scenes?
10% increase in fuel efficiency is a lot, but i wonder what practical applications this might have for hybrid/electric drives. Electric motors might need less gearing and with many short distance aircraft there might be a sweetspot in between a larger battery and the wight of an electrically driven motorjet to boost range? Kind of like an afterburner for electric aricraft, which would optimally use regenerative fuels or at least fill the gap towards heavier and mid ranged aircraft with better efficiencies?
Great video, my jaw dropped when i saw the inline ice which even had enough thrust on its own to power the plane. It's a logic step to use the excess heat but the idea of basically putting an entire engine inside another is really amazing
What about the exhaust recovery turbine used on Boeing B-50? I do not know if that’s a motorjet but it added thrust.
Love your content as always. Just a note on the Russians late start into Jet/Rocket plane development. They did in fact fly the Bereznyak-Isayev BI-1 rocket powered interceptor in May of 42 with some success.
Congratulations on the growth of your channel, I can see how interesting it is. Subscribed!
Thanks for this video, there isn't much out there about motorjets. I found them interesting because even today, with modern materials, temperature at the turbine blades is one of the biggest limiting factors in jet performance. Unfortunately, the tradeoffs don't appear to be worth it, and afterburners end up being a better solution for aircraft that need to go that fast. Maybe something will change, between a new interest in supersonic transportation and better battery technology, it might be possible.
My first visit to the Oshkosh convention was in 1974 and I recall a prototype on display that year or soon after of a one-half size F80 that used an automotive V8 driving an internal fan through a gearbox. I haven't seen or heard of it since then, and it wasn't ready to fly at that time, so I have no idea if it was successful. I suspect that that propulsion design would be less effective on a sport plane than a propeller would be, but the point of it was a jet-powered design without the high cost of a turbine power plant. It interested me a lot because it looked just like the fighter it replicated, only smaller.
Excellent channel, excellent video!
Thanks for showing me this aircraft flay that’s the only early jet I’ve never seen a video of
Yup, ducted fan with afterburner is exactly the thing that came to mind. That is, if there's no turbine, isn't that like an afterburner, except that ignition in the jet's combustion chamber wasn't from an upstream turbojet. Or, am I totally confused.
The most practical combustion engine for the Motorjet might be the Wankel! Why?: small size, high rpm and excess burnt oil simply provide extra power to the jet engine stage! Great video!!
I have seen a homebuilt motorjet. Not based on the Campini design but the Tsu-11, the motorjet from the model 22 Ohka. It uses a McCulloch TC-6150-J-2 turbocharged flat-6 2 stroke engine to drive a similar compressor with side inlets. It is installed in a small plane similar to the model 22 but altered by shortening the nose and installing a fuel tank, and with a V-tail like a Bonanza. It can cruise on the piston engine only and can go exceptionally fast with the jet started. It occasionally appears at the local airport once in a great while. I have no idea about who built it or why, but I've seen it with the tail removed and the engine exposed.
Rolls Royce’s patent of 1995 has long since expired. If anyone thought there was any merit in the engine they would have done something about it by now. I won’t hold my breath.
Just like Jack Northrop and his silly flying wing.
@@brookeshenfield7156
The B-2 is one of the best bombers in the world.
it's a flying wing.....
@@lordgarion514 Robert, you completely missed the point. The flying wing and its inherent advantages was a dream for Jack Northrop, who died before he saw it come to fruition as computerized flight controls finally overcame some of the challenges the design faced.
People told Jack Northrop that it wasn’t possible, the same way the original poster of this thread breezily dismisses the entire concept of a motorjet from his couch.
Not necessarily, people only tend to copy and follow successful products rather than risk pioneering news ones from scratch
@@inventsc Jack Northrop pioneered the flying wing “from scratch” but died before his company could make it a reality.
Ive always loved the Italian WW2 and post war planes, beautiful lines
Thank you for the info on the Ohka "motorjet" version. I have seen a Smithsonian photo of their "motorjet" Ohka 22 (the Japanese Navy Air Research Bureau designation - the plain rocket version was Ohka 11) which designates the engine as a "Campani jet" engine. The Smithsonian photo states that their Ohka 22 was "recovered in Japan in 1945 -- I have seen a photo of an Ohka-22 sitting on an assembly trestle in a factory in Japan with piles of Ohka parts and partially assembled Ohka aircraft in the background -- this may (or may not) be the same motorjet Ohka.
I'm interested in the Ohka because I have a photo taken of my father and his high school friend standing in front of an Ohka at Yontan airfield on Okinawa. The photo is framed to show his tent in the background. The photo showing my dad includes the Ohka with Identification number I-18. There are also photos around the Internet with good images showing the numbers I-10 and I-13. I was in contact with a correspondent who sent me a copy of two photos, one of his father helping to move Ohka I-10 along a dirt track on a low dolly and another of his father standing next to the rocket engine of I-10 with a date on the photo of 4 April, 1945. This correspondent says that he visited an aviation history museum in Chino, California, to see an Ohka that they have (had??) on display and a curation expert at the museum told him that the invading US troops found five Ohkas, fueled and armed, in a cave on Okinawa and they were removed to an open area at Yontan so that they could safely be disarmed. There are photos of I-18 with its external nose removed while the warhead is being removed. There are also photos showing the solid rocket fuel tubes being removed from an Ohka (this aircraft is not identified but the background surroundings seem to indicate that it is likely also I-18). I do not have any information about any other Ohkas that were captured on Okinawa.
Interesting. didn't the Junkers Jumo 004 turbojet used in the Me-262 fighter use a 2 cycle piston engine to start their compression cycle before transitioning to a 'pure' turbojet?
We built a compound cycle engine as an example and as a theoretical possible propulsion system for what is now known as the tomahawk cruise missile it was a V8 of about 250 CC's per cylinder running on compressed air produced over 1,000 horsepower!
What made this particular compound cycle engine very interesting was a pair of clutches so you could use the turbine power to draw in more air and create more thrust as a conventional turbo shaft engine operates or with the flip of a switch you could add the turbines output to the crankshaft and make insane torque at the crankshaft.
I believe it was an old German design from when they were having trouble creating a combuster section with materials of the day and lacking knowledge of modern engineering to create an air cushion between the flame and the metal so that the combustors did not melt through in a matter of seconds.
All this contained in a 20-in diameter about 22 in Long it was actually very light, crazy powerful and produced a lot of thrust it was very efficient Considering it had all the modern engineering and materials made thrown at it.
I don't know whatever happened to the test engine but it ran for 24 hours a number of times at Garrett Turbine Signal oil now Honeywell Phoenix Arizona.
Would it be wrong to think of the N1 as a testbed?
Nice one - I had never heard of a motor jet!!
I'm new to this channel but I am definitely going to subscribe
is it possible to heat a air using electric heater and suck air using dc motor to run elecric fan engine ?
First time I've heard of this engine layout.
Thanks.
I think its so cool that i knew the name Caproni before watching this video but never having known much about airplane history. I watched an animated film by studio Ghibli that features Caproni as a person of admiration for the main protagonist, a Japanese boy growing up and then working as an aerospace engineer in japan, before ww2. He meets Caproni in his dreams and they talk about wanting to build beautiful aircraft. I dont know how historically accurate Caproni or even the whole era is represented, but it does follow the life of the eventual designer of the zero fighter. Its called The Wind Rises, if your interested. Porco Rosso is another film by Ghibli, set in a fantasy world full of custom bi-planes and skypirates.
Iv always wondered how flight would develop in a slower or different environment than history has already proven. Maybe we would see interesting designs like this developed more and become more common place as a form of personal transport completely reshaping the world as we know it. Thanks for this tidy video essay. I really enjoyed learning about this engine!
Try a small, compact, 3-rotor Wankel engine, mated directly (no gearbox) behind a 3-5 stage fan setup.
Since a rotary engine runs best at about 5k RPM, you can mate it to fan, about 1.1m in diameter, which at 5k RPM would result in tip speeds, just below the speed of sound.
Use cooling fins and air inlet in the duct for the engine.
Route the fuel and electrical control lines through the struts.
Use a jack-screw-mounted bulb in the exhaust nozzle to control exhaust airflow.
If you can generate about 1000 lbs of thrust with such a setup, you could power a light GA plane with it.
Wankels are less efficient
The Napier Nomad was also a very cool engine built on this principle.
The made a H block 2-stroke diesel engine like the Sabre for it at 75 litres, but resorted to a single boxer layout.
The Nomad actually flew in an Avro Lincoln. Like all these types, turbo jets took over.
I honestly never knew about that version of the Ohka. The various Japanese suicide craft have always been of interest to me to the point where one of my cats is named Kaiten, yet I never heard of that version.
Do you have one name for multiple cats?!? All with the same name!?!
Each cat is a hero and has a very specific mission
@@soggycracker5934 No, but I do tend to have multiple names for each cat. That one is also called BakaCat.
@@soggycracker5934 btw, the other cats are Harley aka WaccaCat (wacca is Latin for cow and she is black & white, wacca became vacca in later spoken Latin, you might know it as the root of the word vaccine), Maxwell aka General Taylor (he came with the name Maxwell, combined with my last name and he shares his name with one of the most famous American generals of the 20th century) and Luna the Lunatic (she came with the name Luna the rest is self explanatory). I got Kaiten & Harley as kittens, I adopted Luna & Maxwell from friends who were moving.
Also I chose Kaiten because it sounds a lot like 'kitten' & BakaCat is both a nod to a nickname the Ohka apparently had as well as a nod to one of the names I commonly use, bakaman. (which itself is both meant to be amusing as well as being a nod to Socrates when he said that while people think him smart, he really knows nothing.) Yeah, I like to overthink way too many things.
@@whyjnot420 My cat is named F#@ker. He's an asshole, but he's my asshole, and I love him.
You mite like to look at the Napier Nomad for a presentation, that would definitely add to this presentation
in the 60's i recall pop science magazines doing storys about putting big Buick engines in Sabre jets on a guy hobby basis.cold jets i think they were called.
Why no rotary (Star) piston motorjet?
I don't know the aero terminology but would base bleeding the wings help any?
Interresting that could be implemented in VTOL/STOL configuration. Maybe the F-35 B have that aplication to its wing lifting jets?
Sure you could do it but why? You're just making it heavier, less powerful and less efficient.
@@wingracer1614 Because only a few countries are able to produce turbine blades and they keep the metallurgy secret at an overpriced level...With a motorjet or electric compound motorjet you do not need that part but still able to achieve high speed thrust as well self launch capability vs. a pulse jet engine...
@@electricaviationchannelvid7863 OK but a country that can't build a proper jet engine can't build F35s either. So they buy them from the US.
Gille St Hillaire designed a positive displacement motor called the Quasi Turbine. It is 1/5 the size and weight of a piston engine. The engine is empty in the centre and could house a transmission or generator. Multiple units can be ganged together like Wankle. Rotating eliminated vibration and this airplanes could be lighter again
There is a mistake at 9:27. There is no turbine in the high pressure section. What you called the turbine is in fact the *radial* compressor section.
Was this the same as the turbofan aircraft engines?
Excellent work.
I have always wanted to build an aircraft for GA that uses a piston engine to power a ducted fan but it will have many stages to the fan each spinning faster.
You got my subscription with the title
Another great video
goated with the sauce, great video
perhaps the Liquid Piston X3 mini engine could perform better at this task, being far more power dense while having the efficiency bonuses of internal combustion. they had a demonstration aircraft proving hybrid electric operation, with in flight starting and stopping, so perhaps an "Electro-Turbo-Motor-Jet" would be possible ahahaha
So this is the direct inverse of a turboprop then?
reminds me of that weird prop-jet hybrid in the game IL-2 1946.
I wonder how it would be if you had a hybrid system. An Electric motor powering the compressor fan, that is powered by a fuel cell?
Just wouldn't make much sense. Now, a compressor that can be shifted to electrical power, mounted to a zeppelin or blimp that carries solar cells? That could work. But just hydrogen? Makes more sense to run a normal jet straight off of hydrogen.
The problem with powering a compressor with anything but a turbine on the same shaft is immense power that is needed. For instance a model turboshaft engine gives out about 5-6 kW of shaft power weighing 3-4 kgs. So to power its compressor one would need about 9-12 kW motor. And most likely a gearbox as the compressor wheel should rotate at about 100k rpm speed. It did make sense at the time when there wasn't much experience in combustion chambers designing and turbo jet engines in general so it was easier to control and tune the prototypes separately for the turbine and the compressor sides but once their performances are balanced there is no point to put anything in between.
So two totally different power trains powered by two totally different fuels, one of which is expensive, heavy and inefficient for aircraft use where weight and efficiency are everything? Yeah that sounds like a winner
Yes, it would work, the Caproni Campini could fly on fan only and then turn on the burner for extra thrust. If you used an alkaline fuel cell (which is being developed for the Piaseki Helicopter) the cooling requirements of 250C could be used to preheat the air before the burner. Motor jets could work, the reason Caprioni's didn't was the primitive nature of the piston engine which lacked an effective super charger.
Why not use an air cooled radial for compression?
Later versions of the Duplex Cyclone had a turbine coupled with the crankshaft. As a Turbo-compound engine the emphasis was on power recovery from the exhaust, not jet thrust. It saw quite widespread use though.
In the late 1930s/1940 the NACA was developing a transonic motor jet called "Jakes Jeep", it used a Pratt Whitney R-1535 radial. The man driving the program was Eastman Jacobs. He is famous for perfecting the laminar flow wing technology that went into the P-51 Mustang as well as developing the NACA 4 and 5 digit wing profiles all sides used. "jake's Jeep" was meant to reach around 550mph. It had a V tail to limit the problems of shock wave impingement on the tail while the laminar flow wing gave a high Mach Limit. All pretty good for 1939/1940. "Jakes Jeep" evolved into the Bell X-1 that first broke the sound barrier. The Bell X-1 also initially had a V tail. With US engine technology and supercharging technology Jakes Jeep would have worked.
-There is a sad side note to this. When information of the Whittle turbojets was transmitted the US Happ Arnold, Head of the USAAF, did not transmit it to the NACA.
-The Resulting Bell X-59 was a failure as the wings were not only too thick but failed to use the Laminar Flow wings already coming in on the P-51. Eastman Jocobs was so heartbroken he left NACA though some say it was because the innovative engineer had diverted NACA funds into plasma research in an attempt to realize thermonuclear fusion.
I assume the weight penalty is only worth it if we return to giant aircraft (An-225, 747, A380, etc). As long as we aim for smaller, that weight difference is too much of the overall mass budget of a design.
you omited the Coanda 1910 aircraft. It was powered by a motorjet engine too.
Exactly: it did crash at first test and Coanda did stop his experience
Why not electric transmission to eliminate the gearbox. That also allows reduction of the size of the engine since temporary peak power for takeoff can be drawn from batteries while the engine can be sized smaller for cruise power
How have I never come across this concept before... So thoroughly forgotten
He S 50 was a Motorjet developed at Heinkel by Wunibald Kamm, with inherent better features than the Caproni, that actually was an afterburner reinforced version of Stipa duct fuselage. However, at Heinkel failed in obtaining enough cooling for the 2-Stroke engine, and never reached production. Gesund +
I suggest you to study also Henri Coanda . Best regards
Well done! And thanks!
I remember reading, as a kid, that during WW2, the Russians had developed an aircraft that employed a piston engine & propeller, and a ram-jet. It reached ~350 mph on piston power, then the ram-jet would kick in.
Surprised Harry Ricardo didn’t get more of a mention with the crecy
From what I know about German engineers, and their love of insanely, needlessly complex and expensive overengineering of simple machines, I'd bet the German engineers watching this video experienced a markedly higher heart rate, increased respiration, and a far higher degree of interest when they saw this video.
And right now someone at BmW is probably feverishly designing a motorjet to fit in their various cars to continue the tradition of needlessly complex, unreliable cars.
Napier Nomad next then please!
Reminds me of the F 35 with the fan running off a shaft...interesting!
Modern materials science is progressing at breakneck pace, so it's very possible internal combustion engines will become light enough for the combined cycle engine to become practical.
Rolls-Royce began working on a sleeve valve two stroke “sprint” engine aka Crecy. It was all about power at the expense of fuel consumption. Once it was running they realised it could be a great compressor stage for a jet engine. Ultimately, the turbojet was easier to develop so the Crecy was cancelled.
Sounds like an afterburner for a prop driven plane. Even if they can set it up to be efficient, is that gain in efficiency going to justify the increase in complexity, maintenance and reliability.
so the ryan fireball was not technically one it just seems that way because they are not connected together they just are in the same airframe
So fascinating, amazing channel, I'm subscribing. Are you still going to buildt a ww1 plane when you reach 100k?
Can you include metric values in the future videos?
Just found the channel today✌
I agree. Ludicrous and cool!
I think that this idea still has some validity.
With modern piston engines and compressors you could create something that is both efficient at low speeds, and yet possesses turbojet performance for brief periods. All at a relatively low cost.
for example, for a suicide drone which flies low and slow and then activates sprint mode for the last few minutes?
Hell lets not forget that huge reason why motorjets were terrible when they were made, was because nobody bothered making them "right". i.e. for example no correctly made airflow, that helps to keep whole system running.
Excellent.
There have been modern developments of a somewhat similar nature to the motorjet, the composite cycle jet engine, which uses a piston engine (of whatever nature) as a pre burner stage gas generator to increase the thermodynamic efficiency of the whole engine. But so far all variants I've seen use the piston engine as just a gas generator having no apparent use for the shaft power to the main jet engine, perhaps due to scale that power is relegated to running auxiliaries.
I suspect using the piston engine as a gas generator in a motorjet would improve it's efficiency, running a very large compounded turbine after it but before the jet combustor would keep the metallurgy a non issue and you could have a reasonably efficient early propfan.
i would really like a video about the soviet Bi-1
If the MTU concept adds efficiency at the cost of weight, it should work on a land-based turbine used to drive a generator. Those utility guys are really, really interested in efficiency. Today they use the output of a turbojet to boil water to make steam to drive a steam turbine, but the steam turbine is taking energy out on the low-temperature side of the cycle, which is less efficient.
The MTU concept, if I understand properly, is proposing to take some energy out of the fuel on the high-temperature side of the turbojet cycle, by raising the initial temperature. That improves the Carnot efficiency!
Thank you
@Flight Dojo >>> 👍👍
Skip the subscribe begging: 1:15
The Napier Nomad of the late 1940's / early 1950's was a brillient implimentaion of a turbocompound engne that at the time offered record breaking fuel efficiency at the expence of horrendouse complexity en.wikipedia.org/wiki/Napier_Nomad. I came accross some drawings when I was an apprentice and the Nomad was much more advanced than the engines we were producing for the HS125 loco's. Unfortunately cheap oil and simple turbojets killed it stone dead.
The Nomad was reall a gas turbine using a 2 stroke diesel engine as the combustion chamber with the net result of massive overall compression ratios. Power was taken from both the turbine and the engine via a compley hydraulic friction drive variable gearbox which overcame the matching problems described in the RR patent. Takeoff power could be supplimented with afterburning and water-methonal injection, it was a true beast.
Seems like a rotory engine would be a better option than a piston engine for this kind of layout. They are much smaller, lighter and simpler than a piston engine and they spin at a much higher rpm which I have to think would be better than the slower speed a piston engine needs to run at. They can also put out a lot of power when designed and built well. And are stackable so if you want a larger stack you just need a few longer tie rods and crankshaft and you can essentially bolt two or more engines together. The only downside is that when not built perfectly they can have reliability issues and the engine technology isn't nearly as far developed as piston engines.
In the RC Airplane world we use EDFs Electric Ducted Fan in a wide variety of scale airplane models
Yep and their massive sub 5 minute endurance...
And at least one person has grafted on an afterburner. I don't recall how much added thrust he got, but he singed his plane's tail right proper.
The pressure ratio of an EDF is very low, hence any afterburner fitted to one will be hilariously inefficient. The flame looks cool though.
What a very fascinating look such unusual aircraft types I really enjoyed it and I help me better understand how this type of aircraft works. But do the Ryan FR Fireball and the xf15c fall into the same category of a Motorjet aircraft?
>XF15C
No. It had 2 separate engines, that could work independently.
The idea behind motorjet is that the regular internal combustion engine works as both an engine for propeller and compressor for jet, meaning jet part can't work as its own thing, as at that point its just a combustion chamber with no air flow.