Information om | Engelska ordet AFTERBURNING


AFTERBURNING

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Exempel på hur man kan använda AFTERBURNING i en mening

  • An enlarged Mirage II proposal was considered, as well as MD 610 Cavalier (3 versions), but was discarded in favour of a further-developed design, powered by the newly developed Snecma Atar afterburning turbojet engine, designated as the Mirage III.
  • It was powered by two afterburning Rolls-Royce Spey turbofan engines, as used in the British version of the F-4 Phantom II jet fighter.
  • To achieve this, the design included two Tumansky R-27 afterburning turbojets for cruise and four Rybinsk RD-36-35 turbojets for STOL performance.
  • In comparison, the afterburning Rolls-Royce Spey used a twenty chute mixer before the fuel manifolds.
  • The required power was supplied by a pair of afterburning Westinghouse XJ46-WE-02 turbojets, fed from intakes mounted high above the wings to avoid ingesting spray.
  • The General Electric/Rolls-Royce F136 was an afterburning turbofan engine being developed by General Electric, Allison Engine Company, and Rolls-Royce (Allison was subsequently acquired by Rolls-Royce) as an alternative powerplant to the Pratt & Whitney F135 for the Lockheed Martin F-35 Lightning II.
  • During the definition phase of what became the SEPECAT Jaguar ground attack aircraft, a separate partnership was formed between British aero-engine manufacturer Rolls-Royce and French helicopter engine specialist Turbomeca to develop the Adour, an afterburning turbofan engine, to power the aircraft.
  • The Pratt & Whitney F119, company designation PW5000, is an afterburning turbofan engine developed by Pratt & Whitney for the Advanced Tactical Fighter (ATF) program, which resulted in the Lockheed Martin F-22 Raptor.
  • J 29D – proposed fighter variant with afterburner; a single prototype was built to test the afterburning Ghost RM 2A turbojet with 27.
  • It was later adapted with an afterburner for supersonic designs, and in this form it was the world's first production afterburning turbofan, going on to power the F-111 and the F-14A Tomcat, as well as being used in early versions of the A-7 Corsair II without an afterburner.
  • Eleven preproduction IICs were used for operational evaluation and trials with SNECMA Atar 101C axial-flow turbojet and the afterburning Atar 101F.
  • In addition to production Mystère IVA, Dassault developed an upgraded Mystère IVB with either Rolls-Royce Avon (first two prototypes) or SNECMA Atar 101 (third prototype) afterburning engine and a radar ranging gunsight.
  • The first aircraft completed with only the SNECMA Atar 101F afterburning turbojet component of the planned turbo-ramjet powerplant.
  • Previous generations of Russian supersonic fighters such as the MiG-21 and MiG-23 used turbojets, but western fighters such as the F-111 and F-4K introduced the use of afterburning turbofans in the 1960s which were more efficient.
  • The problem was compounded by the need for a modest amount of afterburning (reheat) at take-off (and transonic acceleration).
  • A low-bypass-ratio (BPR) afterburning turbofan engine featuring a six-stage core high-pressure (HP) compressor with variable inlet guide vanes (IGVs), a three-stage low-pressure (LP) compressor with transonic blading, an annular combustion chamber, and cooled single-stage HP and LP turbines.
  • Armed with three 23mm cannons but no missiles, it was a faster upgraded MiG-15 fitted with an afterburning engine, and a radar-ranging gunsight reverse-engineered from the F-86A (as well as a new, more sharply swept wing to increase its critical Mach number, therefore top speed).
  • In 2015, Defence Minister Manohar Parrikar informed the Rajya Sabha that the Ghatak UCAV will be powered by a dry variant of the Kaveri afterburning turbofan engine, which will have a thrust of 52 kilonewtons.
  • In September 2017, a newly built J-20 prototype (numbered "2021") was flight testing with Chinese-made WS-10 Taihang engines, featuring sawtoothed serration edge on its afterburning nozzles.
  • Supplementary burning (reheat or afterburning) between the two turbines and in the tailpipe can also be used for additional thrust.


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