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  2. Bypass ratio - Wikipedia

    en.wikipedia.org/wiki/Bypass_ratio

    The turboprop at its best flight speed gives significant fuel savings over a turbojet even though an extra turbine, a gearbox and a propeller were added to the turbojet's low-loss propelling nozzle. [14] The turbofan has additional losses from its extra turbines, fan, bypass duct and extra propelling nozzle compared to the turbojet's single nozzle.

  3. Turboprop - Wikipedia

    en.wikipedia.org/wiki/Turboprop

    GE T64 turboprop, with the propeller on the left, the gearbox with accessories in the middle, and the gas generator (turbine) on the right. A turboprop is a gas turbine engine that drives an aircraft propeller. [1] A turboprop consists of an intake, reduction gearbox, compressor, combustor, turbine, and a propelling nozzle. [2]

  4. Compressor stall - Wikipedia

    en.wikipedia.org/wiki/Compressor_stall

    The Rolls-Royce Avon turbojet engine was affected by repeated compressor surges early in its 1940s development which proved difficult to eliminate from the design. Such was the perceived importance and urgency of the engine that Rolls-Royce licensed the compressor design of the Sapphire engine from Armstrong Siddeley to speed development.

  5. 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 ...

  6. Gas turbine - Wikipedia

    en.wikipedia.org/wiki/Gas_turbine

    For a turboprop engine there will be a particular balance between propeller power and jet thrust which gives the most economical operation. In a turbojet engine only enough pressure and energy is extracted from the flow to drive the compressor and other components. The remaining high-pressure gases are accelerated through a nozzle to provide a ...

  7. Turbojet - Wikipedia

    en.wikipedia.org/wiki/Turbojet

    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 compressor).

  8. Free-turbine turboshaft - Wikipedia

    en.wikipedia.org/wiki/Free-turbine_turboshaft

    Some large turboprop engines, such as the original Bristol Proteus and the modern TP400 have free turbines. The TP400 is a three-shaft design, with two compressor turbines and a separate power turbine. Where the turbine is at the rear of the engine, a turboprop engine requires a long drive shaft forwards to the propeller reduction gearbox. Such ...

  9. Jet engine - Wikipedia

    en.wikipedia.org/wiki/Jet_engine

    The dictionary definition of jet engine at Wiktionary; Media about jet engines from Rolls-Royce; How Stuff Works article on how a Gas Turbine Engine works; Influence of the Jet Engine on the Aerospace Industry; An Overview of Military Jet Engine History, Appendix B, pp. 97–120, in Military Jet Engine Acquisition (Rand Corp., 24 pp, PDF)

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