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  2. Category:Low-bypass turbofan engines - Wikipedia

    en.wikipedia.org/wiki/Category:Low-bypass...

    Pages in category "Low-bypass turbofan engines" The following 68 pages are in this category, out of 68 total. This list may not reflect recent changes. A.

  3. 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 ...

  4. Pratt & Whitney J52 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_J52

    (PW1212) 12,000 lbf (53 kN) thrust version of the J52-P-408 with an improved low pressure turbine (LPT) and faster acceleration. Designed for the EA-6B and was additionally marketed as an upgrade for the A-4. The J52-P-409 was also proposed as a cost-effective upgrade to the A-6E as an alternative to the A-6F Intruder II, [9] but was not purchased.

  5. Pratt & Whitney JT8D - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_JT8D

    The Pratt & Whitney JT8D is a low-bypass (0.96 to 1) turbofan engine introduced by Pratt & Whitney in February 1963 with the inaugural flight of the Boeing 727.It was a modification of the Pratt & Whitney J52 turbojet engine which powered the US Navy A-6 Intruder and A-4 Skyhawk attack aircraft.

  6. Turbojet - Wikipedia

    en.wikipedia.org/wiki/Turbojet

    It was designed to test the Whittle jet engine in flight, and led to the development of the Gloster Meteor. [10] The first two operational turbojet aircraft, the Messerschmitt Me 262 and then the Gloster Meteor, entered service in 1944, towards the end of World War II, the Me 262 in April and the Gloster Meteor in July. Only about 15 Meteor saw ...

  7. Turbofan - Wikipedia

    en.wikipedia.org/wiki/Turbofan

    One of the earliest turbofans was a derivative of the General Electric J79 turbojet, known as the CJ805-23, which featured an integrated aft fan/low-pressure (LP) turbine unit located in the turbojet exhaust jetpipe. Hot gas from the turbojet turbine exhaust expanded through the LP turbine, the fan blades being a radial extension of the turbine ...

  8. General Electric J79 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_J79

    The General Electric J79 is an axial-flow turbojet engine built for use in a variety of fighter and bomber aircraft and a supersonic cruise missile.The J79 was produced by General Electric Aircraft Engines in the United States, and under license by several other companies worldwide.

  9. Category:Turbojet engines - Wikipedia

    en.wikipedia.org/wiki/Category:Turbojet_engines

    Pages in category "Turbojet engines" The following 2 pages are in this category, out of 2 total. This list may not reflect recent changes. N. Nose bullet; P. PBS TJ80-120