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  2. Components of jet engines - Wikipedia

    en.wikipedia.org/wiki/Components_of_jet_engines

    Diagram of a typical gas turbine jet engine. Air is compressed by the compressor blades as it enters the engine, and it is mixed and burned with fuel in the combustion section. The hot exhaust gases provide forward thrust and turn the turbines which drive the compressor blades. 1. Intake 2. Low pressure compression 3. High pressure compression ...

  3. 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 ...

  4. 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.

  5. Template:Jetspecs - Wikipedia

    en.wikipedia.org/wiki/Template:Jetspecs

    |combustion= Description of the combustion chambers, for example 10 flow combustion chambers with igniter plugs in chambers 3 and 10 |turbine= Description of the turbine, for example single-stage axial flow with 54 blades |fueltype= Fuel type, for example aviation kerosene with 1% lubricating oil |oilsystem= Description of the oil system.

  6. Turbojet - Wikipedia

    en.wikipedia.org/wiki/Turbojet

    Diagram of a typical gas turbine jet engine Frank Whittle Hans von Ohain. The turbojet is an airbreathing jet engine which is typically used in aircraft. It consists of a gas turbine with a propelling nozzle. The gas turbine has an air inlet which includes inlet guide vanes, a compressor, a combustion chamber, and a turbine (that drives the ...

  7. File:Jet engine.svg - Wikipedia

    en.wikipedia.org/wiki/File:Jet_engine.svg

    English: Diagram of a typical gas turbine jet engine (in English). Air is compressed by the fan blades as it enters the engine, and it is mixed and burned with fuel in the combustion section. The hot exhaust gases provide forward thrust and turn the turbines which drive the compressor fan blades.

  8. Jet engine - Wikipedia

    en.wikipedia.org/wiki/Jet_engine

    A jet engine is a type of reaction engine, discharging a fast-moving jet of heated gas (usually air) that generates thrust by jet propulsion. While this broad definition may include rocket , water jet , and hybrid propulsion, the term jet engine typically refers to an internal combustion air-breathing jet engine such as a turbojet , turbofan ...

  9. Flame holder - Wikipedia

    en.wikipedia.org/wiki/Flame_holder

    A flame holder is a component of a jet engine designed to help maintain continual combustion. In a scramjet engine the residence time of the fuel is very low and complete penetration of the fuel into the flow will not occur. To avoid these conditions flame holders are used. [1] All continuous-combustion jet engines require a flame holder. A ...