超级军网求教！！！留里卡AL-7、AL-21的资料。
来源：百度文库 编辑：超级军网 时间：2024/05/03 05:42:26
哪位老大给介绍介绍留里卡AL-7、AL-21的资料，谢谢！！！哪位老大给介绍介绍留里卡AL-7、AL-21的资料，谢谢！！！
AL-21F
http://salut.ru/ViewTopic.php?Id=670
In 1966 the enterprise embarked on the serial production of the 3rd generation AL-21F engines. These engines were installed and operated on Su-17M, Su-22, Su-24 and MiG-23B aircraft. Today AL-21F engines are operated on Su-22M4 and Su-24.
Once retired from aviation and after modifications and upgrading, the Al-21F3 engines are used to drive the industrial power generation and gas-transfer plants manufactured by FSUE «MMPP «Salut».
Maximum thrust, kgf 11250
Inlet diameter, mm 885
Maximum dimention, mm 1030
Length, mm 5340
Minimum specific fuel consumption, kg/kgf*h 0.76
Dry weight, kg 1580
Air consumption, kg/s 104
AL-21F
http://salut.ru/ViewTopic.php?Id=670
In 1966 the enterprise embarked on the serial production of the 3rd generation AL-21F engines. These engines were installed and operated on Su-17M, Su-22, Su-24 and MiG-23B aircraft. Today AL-21F engines are operated on Su-22M4 and Su-24.
Once retired from aviation and after modifications and upgrading, the Al-21F3 engines are used to drive the industrial power generation and gas-transfer plants manufactured by FSUE «MMPP «Salut».
Maximum thrust, kgf 11250
Inlet diameter, mm 885
Maximum dimention, mm 1030
Length, mm 5340
Minimum specific fuel consumption, kg/kgf*h 0.76
Dry weight, kg 1580
Air consumption, kg/s 104
http://en.wikipedia.org/wiki/Lyulka_AL-7
The AL-7 had supersonic airflow through the first stage of the compressor. TR-7 prototype developing 6,500 kgf (14,330 lbf, 63.7 kN) of thrust was tested in 1952, and the engine was initially intended for Ilyushin's Il-54 bomber. The afterburning version AL-7F was created in 1953. In 1957, Su-7 'Fitters' equipped with AL-7F exceeded Mach 2 at 18,000 m (70,900 ft), which lead to production of Su-7B and Su-9 'Fishpot' equipped with this engine. The engine was adopted for Tu-128P 'Fiddler' in 1960, and it was used in the AS-3 'Kangaroo' cruise missile. The Beriev Be-10 jet flying boat used a non-afterburning AL-7PB with stainless steel compressor blades.
Maximum Thrust:
67.1 kN (15,075 lbf) military power
98.1 kN (22,050 lbf) with afterburner
Overall pressure ratio: 9.5:1
Turbine inlet temperature: 860 °C (1,580 °F)
Specific fuel consumption: 98.9 kg/(h·kN) (0.97 lb/(h·lbf))
The AL-7 had supersonic airflow through the first stage of the compressor. TR-7 prototype developing 6,500 kgf (14,330 lbf, 63.7 kN) of thrust was tested in 1952, and the engine was initially intended for Ilyushin's Il-54 bomber. The afterburning version AL-7F was created in 1953. In 1957, Su-7 'Fitters' equipped with AL-7F exceeded Mach 2 at 18,000 m (70,900 ft), which lead to production of Su-7B and Su-9 'Fishpot' equipped with this engine. The engine was adopted for Tu-128P 'Fiddler' in 1960, and it was used in the AS-3 'Kangaroo' cruise missile. The Beriev Be-10 jet flying boat used a non-afterburning AL-7PB with stainless steel compressor blades.
Maximum Thrust:
67.1 kN (15,075 lbf) military power
98.1 kN (22,050 lbf) with afterburner
Overall pressure ratio: 9.5:1
Turbine inlet temperature: 860 °C (1,580 °F)
Specific fuel consumption: 98.9 kg/(h·kN) (0.97 lb/(h·lbf))
据有些老大曾说：在AL-21面前，R-29就是渣。麻烦哪为能给详细点地说说？[:a14:][:a15:]
AL-21似乎是苏24的发动机
5# veritas
是的，加10分！
不仅苏-24，苏-17/20/22也用该（系列）发动机。据说Su27在研发初期也是用AL-21的。
是的，加10分！
不仅苏-24，苏-17/20/22也用该（系列）发动机。据说Su27在研发初期也是用AL-21的。
一个单转子发动机，推比也不高，但超大的很多人评价比R-29高多了。
还听说AL-21参考了美国J-79,不知那位达人愿意科普一下?[:a15:]