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hogan rebel advanced technology

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发表于 2016-1-2 12:00:43 | 显示全部楼层 |阅读模式
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the representative of Harrier and Typhoon fighter EJ200 engine, to achieve a large thrust and vectoring engines. The third Russian,[url=[第一私募论坛]http://www.simu001.cn]museoleonardodavinci.it/]scarpini nike], Russian-made engine advantage is thrust ease of maintenance,[url=[第一私募论坛]http://www.simu001.cn]permissible.fr]tn requin], the disadvantage is short life only eighth in Europe and America and the fuel consumption of large ,, major manufacturers, "Salute factory, Saturn" research and production association, the representative of the Su-27 The AL-31F engine and AL-41F. The fourth is France, the legal structure of engine fuel consumption and less complex but the relative lack of thrust, the representative of France's Snecma M88 turbofan engines for the Rafale. The Chinese engine relatively speaking,[url=[第一私募论坛]http://www.simu001.cn]f-v-m.net/session.asp]giuseppe zanotti pas cher], is the technical foundation weakest. Zhuhai Airshow day Russia shows F117S vector engines in China. F117S vector engine engine is urgently needed in China, because without it no F-20 fighter planes to use vector engine. (Photo: Sina military doors wide All Rights Reserved.)Chinese engine development for 60 years, from the 1956 introduction of the first turbojet 5 starts experienced a total of seven models, namely turbojet -5, turbojet -6, -7 turbojet turbojet 13, Kunlun, vortex Fan -9 -10 turbofan, the research models include turbofan -15, -20, etc. turbofan. Our first generation of turbojet engine to -5, -6 turbojet represented 5 turbojet engine is the first scroll of the former Soviet Union in accordance with technical data BK-1  generic engine jet engine.
& p; J: @7 q' O) G) v mainly for the F-7 aircraft. 7 turbojet engine performance than the turbojet 6 has been greatly improved,[url=[第一私募论坛]http://www.simu001.cn]obesite-paris###/hollister.asp]hollister pas cher], the maximum thrust of 38.2 kN afterburning thrust of 55.9 kN, respectively, compared with turbojet 6 increased by 50% and 77%. 1965 to complete the development,[url=[第一私募论坛]http://www.simu001.cn]emmedielle.it]hogan rebel], mass production in 1966. Blue empty F-11 fighter fleet off battle F-8FTurbofan -9 complete imitation is carried out, and after realized that the future must be equipped with turbofan aircraft engine, China's introduction of the margins of Soviet hegemony British Spey engine according to the British exports to China of Spey engine,[url=[第一私募论坛]http://www.simu001.cn]accord-uk.it/]nike air force prezzo], "Spey "MK202 type is a British Rolls - Royce in the mid-1960s developed turbofan engine, long 5025 mm, 1093 mm in diameter and weighs 1,850 kg, the maximum thrust of 54.5 kN 91.1 kN afterburning thrust, thrust- ratio of 5.05,[url=[第一私募论坛]http://www.simu001.cn]museoleonardodavinci.it/]nike shox outlet], the largest military fuel consumption 0.0684 kg / cow per hour, maximum afterburner fuel consumption 0.2 kg / cow per hour, bypass ratio 0.62. With advanced level in the world at that time, the 1960s was introduced into China for imitation,[url=[第一私募论坛]http://www.simu001.cn]bagnoromagnolo###/collezione.asp]hogan outlet scarpe], culminating in 2003 became a complete success of China's Qinling engine, which is turbofan -9. Turbofan -9 in the final equipment on the JH-7 Flying Leopard, make Feibao became a combat radius of more than 1000 kilometers, it can be used with most of the fighter planes in combat bombing missions.
$ R" ^9 w' I: y2 v' j9 j% } developed by the Shenyang Aero Engine Factory . WP5 is a centrifugal, single rotor with afterburning engine, single maximum thrust of 25.5 kN with afterburning thrust of 32.5 kN and a weight of 980 kg, mainly used for domestic Shenyang J-5 fighter . -6 Turbojet engine is the engine according to P ?-9B technical information provided by the former Soviet Union made an afterburning turbojet engines, mainly for equipment made Shenyang J-6 and later developed Q-5 attack aircraft, which two engines are 25.5 kN,[url=[第一私募论坛]http://www.simu001.cn]romaniatv.it/collezione.asp]hogan outlet], but turbojet turbojet -6 is less than 5 to reduce the 23% of the weight, diameter shortened by 48%, greatly reducing the frontal area and drag,[url=[第一私募论坛]http://www.simu001.cn]annuity.fr]louboutin soldes], thrust-weight ratio and therefore higher than the turbojet -5 more. Our second generation of engines with turbojet and turbofan 7 -9 representative. -7 Turbojet engine which is technical information P- ?-300 engines manufactured by the former Soviet Union provided.
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