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  2. Components of jet engines - Wikipedia

    en.wikipedia.org/wiki/Components_of_jet_engines

    Each stage is a stationary ring of nozzle guide vanes followed by spinning blades. The gas is moving from left to right and the 2nd and 3rd vane rings have been removed to better show the blades. The first ring shows the shape of the vanes and how they turn the gas from the combustor into a tangential direction necessary to spin the bladed disc.

  3. General Electric T31 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_T31

    Data from General characteristics Type: Single Shaft Turboprop Length: 116in (295cm) including exhaust cone, but not the propeller Diameter: 37in (94cm) maximum overall Dry weight: 1980lb (898Kg) including accessories Components Compressor: 14-stage axial Combustors: 8 can combustion chambers Turbine: axial single-stage Fuel type: Kerosene Oil system: pressure spray Performance Maximum power ...

  4. Propelling nozzle - Wikipedia

    en.wikipedia.org/wiki/Propelling_nozzle

    The areas of both the propelling nozzle and turbine nozzle set the mass flow through the engine and the maximum pressure. While both these areas are fixed in many engines (i.e. those with a simple fixed propelling nozzle), others, most notably those with afterburning, have a variable area propelling nozzle.

  5. Turbine - Wikipedia

    en.wikipedia.org/wiki/Turbine

    A steam turbine with the case opened Humming of a small pneumatic turbine used in a German 1940s-vintage safety lamp. A turbine (/ ˈ t ɜːr b aɪ n / or / ˈ t ɜːr b ɪ n /) (from the Greek τύρβη, tyrbē, or Latin turbo, meaning vortex) [1] [2] is a rotary mechanical device that extracts energy from a fluid flow and converts it into useful work.

  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. Turbofan - Wikipedia

    en.wikipedia.org/wiki/Turbofan

    A turbine stage turns the gas from an axial direction and speeds it up (in the nozzle guide vanes) to turn the rotor most effectively ( rotor blades must produce high lift), the proviso being that this is done efficiently, ie with acceptable losses. [70]

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    This bestselling 'lightweight but sturdy' Shark vacuum is back in stock at Walmart and it's on sale for just $97

  9. Turbine blade - Wikipedia

    en.wikipedia.org/wiki/Turbine_blade

    The number of turbine stages can have a great effect on how the turbine blades are designed for each stage. Many gas turbine engines are twin-spool designs, meaning that there is a high-pressure spool and a low-pressure spool. Other gas turbines use three spools, adding an intermediate-pressure spool between the high- and low-pressure spool.