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  2. Power Jets WU - Wikipedia

    en.wikipedia.org/wiki/Power_Jets_WU

    The combustion chamber was connected to the compressor outlet by a very large single spiral duct giving the engine an asymmetrical appearance. Whittle designed the centrifugal compressor to develop about 4:1 pressure ratio when, as far as he was aware, the best previously demonstrated performance in a single stage was about 2.5:1.

  3. Jet engine performance - Wikipedia

    en.wikipedia.org/wiki/Jet_engine_performance

    The type of jet engine used to explain the conversion of fuel into thrust is the ramjet.It is simpler than the turbojet which is, in turn, simpler than the turbofan.It is valid to use the ramjet example because the ramjet, turbojet and turbofan core all use the same principle to produce thrust which is to accelerate the air passing through them.

  4. Combustor - Wikipedia

    en.wikipedia.org/wiki/Combustor

    A combustor is a component or area of a gas turbine, ramjet, or scramjet engine where combustion takes place. It is also known as a burner, burner can, combustion chamber or flame holder. In a gas turbine engine, the combustor or combustion chamber is fed high-pressure air by the compression system. The combustor then heats this air at constant ...

  5. Components of jet engines - Wikipedia

    en.wikipedia.org/wiki/Components_of_jet_engines

    All jet engines require high temperature gas for good efficiency, typically achieved by combusting hydrocarbon or hydrogen fuel. Combustion temperatures can be as high as 3500K (5841F) in rockets, far above the melting point of most materials, but normal airbreathing jet engines use rather lower temperatures.

  6. Combustion instability - Wikipedia

    en.wikipedia.org/wiki/Combustion_instability

    For example, in rocket engines, such as the Rocketdyne F-1 rocket engine [7] in the Saturn V program, instabilities can lead to massive damage of the combustion chamber and surrounding components (see rocket engines). Furthermore, instabilities are known to destroy gas-turbine-engine components during testing. [8]

  7. Fuel control unit - Wikipedia

    en.wikipedia.org/wiki/Fuel_control_unit

    Adding fuel too quickly to increase power can damage the turbines due to excessive heat, or the sudden rise in combustion chamber pressure may cause a compressor stall. Another danger of too much fuel is a rich blow-out , where soaking the fire with fuel displaces the oxygen and lowers the temperature enough to extinguish the flame.

  8. Delta’s hidden profit center is repairing jet engines - AOL

    www.aol.com/finance/delta-hidden-profit-center...

    Delta is doubling down on its TechOps business, opening a brand new jet engine repair facility with partner Pratt & Whitney in Atlanta. Delta’s hidden profit center is repairing jet engines ...

  9. Combustion chamber - Wikipedia

    en.wikipedia.org/wiki/Combustion_chamber

    The combustion chamber in gas turbines and jet engines (including ramjets and scramjets) is called the combustor. The combustor is fed with high pressure air by the compression system, adds fuel and burns the mix and feeds the hot, high pressure exhaust into the turbine components of the engine or out the exhaust nozzle.

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