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La animación es buena , pero en el diseño del motor veo muchos fallos el difusor de entrada es convergente , el compresor radial no se usa solo, el compresor es de dos caras pero es imposible que coja aire de dentro, y a la cámara de combustión le faltan muchas piezas.
That's how jet engines worked in 1948... Yet here you make it look like it's a modern 747 engine which is very false. This is a very very basic turbojet engine, in reality we use turbofan engines that are very much more efficient.
Cool animation, just one flaw, the fire is ideally only in the combuster can, not flying through the turbine as shown. I guess this is done this way in orange to show that it is hot gas, but if the fire extended out of the can and was blowing through the turbine, the turbine would soon fail.
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The gases will not leave out the inlet because of the high pressure forward of the combustion chamber. It is easier for the gases to escape out the rear end of the engine due to its construction. The gases will however escape out the inlet if the compressor fails to compress enough.
Because the pressure on the front side of the burner's is much higher than the pressure at the turbine, so the flow wants to go from high to low pressure thus going backwards through the turbine.
If you had a jet engine without the compressor (fans) spinning and you introduced fuel into the combustion chamber and lit it, that's exactly what would happen. You have to get the fan spinning fast enough before you start burning fuel. Then the air is moving so fast that it can not escape out the front. The burning and expanding air rushes out the back and drives the rear fan which is connected to the front, which continues to suck in more air and oxygen to continue the fuel burning.
Well, this engine uses a compressor which compress air by centrifugal flow.. it is quite light and simple, has low temperature, can build with low cost compare to axial flow-compressor... but not that powerful compare to axial flow engine..
The air which goes through engine doesn't stop when they become mixed and ignited with fuel. Important thing is that air and fuel is keep moving backward and ignition continues while they are moving. Imagine a water pipe goes through area with very high temperature. water will be boiled but it won't stop the flow.
Well, this engine uses a compressor which compress air by centrifugal flow.. it is quite light and simple, has low temperature, can build with low cost compare to axial flow-compressor...
Actually developed in parallel. The Germans were the first to go mainstream with the axial design while the British thought the jet engine was all a bit magical and overrated.
There is no one way valve or any kind of piping layout that restricts flow in either direction. The compressor is continuously pushing high pressure air into the combustion chamber, at the back of the combustion chamber (via turbine) is lower pressure, ambient air. The flow takes the natural path from high pressure to low pressure. Lookup compressor stall if you would like to see what happens when the flow does go backward.
question, how come, after compression, it de-compresses right away (because the combustion chamber seems to be wider then the inlet) or is the combustion chamber split into multiple sections to keep the pressure the 'same' (i used quotes, because I know the pressure will be even greater after being heated)
This is the first generation of british jet engines during WWII with radial (not axial) compression and separated combustion chambers like Rolls-Royce_Nene. The german Junkers Jumo 004 at this time had still separated chambers, but the more sophisticated axial compression, which lead to a much leaner silhouette with aerodynamic advantages.
