Gluhareff Pressure Jet
![]() | This article has multiple issues. Please help improve it or discuss these issues on the talk page. (Learn how and when to remove these messages)
|
The Gluhareff Pressure Jet (or tip jet) is a type of
Mechanism

Having no moving parts, the engine works by having a coiled pipe in the combustion chamber that superheats the fuel (propane) before being injected into the air-fuel inlet. In the combustion chamber, the fuel/air mixture ignites and burns, creating thrust as it leaves through the exhaust pipe. Induction and compression of the fuel/air mixture is done both by the pressure of propane as it is injected, along with the sound waves created by combustion acting on the intake stacks.[2]
The engine has three intake stages, which are sized according to the sound created by the combustion process when running. This has exactly the same effect as the
A 1949 reference to a very similar concept exists.[4] Although described as a ram jet, this version heats the fuel within a closed space to create the pressure for injection and compression of the entrained air in a similar manner to the Gluhareff design and is in all fundamental respects a pressure jet of the same type.
Advantages
- No moving parts, meaning very little wear.
- Simple throttling, via a valve in the fuel line.
- Clean burning and very low emissions, especially as it is designed to use propane which burns very cleanly.
- It is possible that the engine can be built at home from plans or a kit. These are already commercially available kits.
- Simple design means that engines can be incorporated into either a helicopter's rotor blades or a fixed-wing aircraft's wings or tailfins.
Disadvantages
- Engines need to be sonically tuned for maximum efficiency.
- Noise is very similar to that of a pulse jet engine, which could cause discomfort for passengers and people on the ground.
- Very high engine temperatures are a problem (the engine can glow bright orange which creates an obvious material problem).
- Difficult to mount due to operating temperatures, intake valve assembly, and fuel supply.
Applications
See also
References
- ^ Ronald Barrett. "Gluhareff Pressure Jet Engine" (PDF).
- ^ "US Patent#: US3093962A". 1963-06-18. Retrieved 2014-02-28.
- ^ Ronald Barrett. "Gluhareff Pressure Jet Engine" (PDF).
- ^ Paul Nikulka. "Jet Model Engine" (PDF).