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Aside from early diesel engines, does anyone know of brayton-cycle engine that uses a positive displacement compressor rather than an aerodynamic one?
FredGarvin said:You know, I vauguely remember a paper detailing an engine concept that did have a piston on top of an axial compressor. IIRC believe the compression was supplemental. Let me see if I can hunt it down.
It was on a turbo jet IIRC. I still haven't found it. Still looking.NateTG said:I was actually wondering about something similar to turbo-fans, but with positive displacement. Still, that sounds zany.
FredGarvin said:Try doing a search on it and see what you can come up with. It's not what you were looking for, but it's kind of in the ball park.
Danger said:Jeez, Nate... I thought that you were just asking about the intake side. A positive displacement output? I wouldn't want to be anywhere near it.
Yeah. It's a new one. I need to change things around every once in a while. That's Lou and Andy from Little Britain. The best skit show EVER.Q_Goest said:Hey Fred - New avatar? Which one is Fred?
FredGarvin said:Yeah. It's a new one. I need to change things around every once in a while. That's Lou and Andy from Little Britain. The best skit show EVER.
A 'Jet' engine with positive displacement compressor is a type of jet engine that uses a positive displacement compressor to compress air before it enters the combustion chamber. This type of engine is typically used in small aircraft engines.
The engine works by drawing in air through an inlet, which is then compressed by the positive displacement compressor. The compressed air is then mixed with fuel and ignited in the combustion chamber. This creates a high-pressure, high-velocity exhaust that creates thrust to propel the aircraft forward.
One advantage is that it is more fuel-efficient than other types of jet engines. It also has a simpler design, which means it is easier to maintain and has a longer lifespan. Additionally, this type of engine can operate efficiently at low speeds, making it suitable for small aircraft.
One disadvantage is that it is not suitable for high-speed aircraft as it cannot produce as much thrust as other types of jet engines. It also has a lower power-to-weight ratio, meaning it may not be suitable for larger or heavier aircraft. Additionally, the positive displacement compressor can be prone to damage if foreign objects are sucked into the engine.
This type of engine differs from other jet engines in the way it compresses air. While other jet engines use a centrifugal compressor or axial compressor, a positive displacement compressor uses a piston or rotary mechanism to compress air. This results in a simpler and more efficient design, but with limitations on speed and power.