Military aircraft jet-engines
History
“After World War Two, piston engines continued to power civil airliners for many years, but in the field of military aircraft they were rapidly displaced by the gas turbine. Fighters and bombers switched to the turbojet, transports and maritime-patrol aircraft used turboprops, and helicopters benefited greatly from changing to turboshaft engines. The change meant more power for less weight, far greater reliability, no cooling problems and safer kerosene-type fuels.
With extraordinary reluctance, designers eventually recognized that the turbofan, offering a wide choice of bypass ratio (BPR - the mass flow of air in the bypass duct divided by that through the core), could with advantage replace the turbojet. In supersonic aircraft the need to minimize frontal area means that BPR is seldom as high as 1, and even then the installation must be done with great care. When the J79 turbojet of 79.63 kN thrust installed in the McDonnell Douglas F-4 Phantom was replaced in the British versions by the Rolls-Royce Spey turbofan of 91.25 kN the change made the aircraft slower in level flight, while giving improvements in take-off and climb performance!
Today the turbojet is almost extinct, except for some countries like China, where different criteria apply. Elsewhere, the trend has been towards achieving greater power with engines that are not only lighter but also smaller and dramatically simpler. For example, the Spey Mk 202, the engine of the RAF Phantoms, had a total of 17 stages of blading in the compressors (5+12 flow pressure+high pressure) and four stages of blading in the turbines (2+2). The next-generation RB. 199, engine of the Tornado, has 12 stages of compression (3+3+6) and again four stages of expansion through the turbines (1+1+2), whereas today’s Eurojet EJ200, engine of the Eurofighter, has only eight compressor stages (3+5) and two turbine stages (1+ 1).
(more…)
