AŠ-62IR
( & # 1040; & # 1064; -62 & # 1048; & # 1056;)
- the longest produced star engine in the USSR
The star nine-cylinder air-cooled AŠ-62IR engine was designed in the ADŠvecova design office ( & # 1054; & # 1050; & # 1041; & # 1040;. & # 1044;. & # 1064; & # 1074 ; & # 1077; & # 1094; & # 1086; & # 1074; & # 1072;). The first engine tests took place in May 1938 and a year later (May 11, 1939), the engine successfully passed the state tests and could be accepted into series production.
The AŠ-62IR version became the most mass-produced version of the M-62 engine, and a total of 3,500 units of this power unit were produced. Since 1942, in addition to the AŠ-62IR, other versions of the M-62 have not been mass-produced.
It was used on aircraft Lisunov Li-2 and Antonov An-2. It was also experimentally mounted on the German [Arl=/topic/view/6465] Arade Ar-196[/url].
Since 1956, the AŠ-62IR has been manufactured under license in China, where it bears the HS5 designation, and since 1960, in Poland, where it bears the ASz-62 designation. The Polish version of the Asz-62IR engine is designed with the requirements of the FAR-33 regulation. Further developments at WSK PLZ Kalisz in Poland resulted in engine versions K9-AA, K9-BA and K9-BB with a take-off power of 860 kW (1178 HP) and a rated power of 698 kW.
ASz-62IR are installed in the following aircraft:
Antonov An-2
de Havilland Canada DHC-3 (some machines)
PZL-106 Kruk (some variants)
PZL-Mielec M-18 Dromader
PZL M-24 Dromader Super (K-9AA)
In the USSR, it was produced in the following plants:
1938-40 - Race No. 24 ( & # 8470; 24)
1940-43 - Race No. 19 ( & # 8470; 19)
1944-50 - Race No. 36 ( & # 8470; 36)
1949-53 - Race No. 478 ( & # 8470; 478)
since 1952 - Race No. 154 ( & # 8470; 154)
TTD:
displacement (l): 29.87
cylinder volume (l): 3.31
compression ratio: 6.4: 1
engine weight (kg): 560
Engine Diameter [mm]: 1375
take-off mode:
- power: 745.7 kW (1000 hp)
at speed (rpm): 2200
nominal mode:
ground power: 611.5 kW (820 hp)
at speed (rpm): 2100
power at 1500 m: 1320 kW (840 hp)
at speed (rpm): 2100
sources:
www.airwar.ru
http://engine.aviaport.ru/issues/index.html
& # 1041; & # 1086; & # 1095; & # 1072; & # 1088; & # 1086; & # 1074; & # 1042;. & # 1045;., & # 1043; & # 1091; & # 1090; & # 1084; & # 1072; & # 1085; & # 1051;. & # 1044;.: & # 1040; & # 1074; & # 1080; & # 1072; & # 1094; & # 1080; & # 1086; & # 1085; & # 1085; & # 1099 ; & # 1081; & # 1084; & # 1086; & # 1090; & # 1086; & # 1088; & # 1040; & # 1064; -62 & # 1048; & # 1056;
Kotelnikov, Vladimir: Russian Piston Aero Engines. 2005
Edit: Janko PALIGA (data addition)
( & # 1040; & # 1064; -62 & # 1048; & # 1056;)
- the longest produced star engine in the USSR
The star nine-cylinder air-cooled AŠ-62IR engine was designed in the ADŠvecova design office ( & # 1054; & # 1050; & # 1041; & # 1040;. & # 1044;. & # 1064; & # 1074 ; & # 1077; & # 1094; & # 1086; & # 1074; & # 1072;). The first engine tests took place in May 1938 and a year later (May 11, 1939), the engine successfully passed the state tests and could be accepted into series production.
The AŠ-62IR version became the most mass-produced version of the M-62 engine, and a total of 3,500 units of this power unit were produced. Since 1942, in addition to the AŠ-62IR, other versions of the M-62 have not been mass-produced.
It was used on aircraft Lisunov Li-2 and Antonov An-2. It was also experimentally mounted on the German [Arl=/topic/view/6465] Arade Ar-196[/url].
Since 1956, the AŠ-62IR has been manufactured under license in China, where it bears the HS5 designation, and since 1960, in Poland, where it bears the ASz-62 designation. The Polish version of the Asz-62IR engine is designed with the requirements of the FAR-33 regulation. Further developments at WSK PLZ Kalisz in Poland resulted in engine versions K9-AA, K9-BA and K9-BB with a take-off power of 860 kW (1178 HP) and a rated power of 698 kW.
ASz-62IR are installed in the following aircraft:
Antonov An-2
de Havilland Canada DHC-3 (some machines)
PZL-106 Kruk (some variants)
PZL-Mielec M-18 Dromader
PZL M-24 Dromader Super (K-9AA)
In the USSR, it was produced in the following plants:
1938-40 - Race No. 24 ( & # 8470; 24)
1940-43 - Race No. 19 ( & # 8470; 19)
1944-50 - Race No. 36 ( & # 8470; 36)
1949-53 - Race No. 478 ( & # 8470; 478)
since 1952 - Race No. 154 ( & # 8470; 154)
TTD:
displacement (l): 29.87
cylinder volume (l): 3.31
compression ratio: 6.4: 1
engine weight (kg): 560
Engine Diameter [mm]: 1375
take-off mode:
- power: 745.7 kW (1000 hp)
at speed (rpm): 2200
nominal mode:
ground power: 611.5 kW (820 hp)
at speed (rpm): 2100
power at 1500 m: 1320 kW (840 hp)
at speed (rpm): 2100
sources:
www.airwar.ru
http://engine.aviaport.ru/issues/index.html
& # 1041; & # 1086; & # 1095; & # 1072; & # 1088; & # 1086; & # 1074; & # 1042;. & # 1045;., & # 1043; & # 1091; & # 1090; & # 1084; & # 1072; & # 1085; & # 1051;. & # 1044;.: & # 1040; & # 1074; & # 1080; & # 1072; & # 1094; & # 1080; & # 1086; & # 1085; & # 1085; & # 1099 ; & # 1081; & # 1084; & # 1086; & # 1090; & # 1086; & # 1088; & # 1040; & # 1064; -62 & # 1048; & # 1056;
Kotelnikov, Vladimir: Russian Piston Aero Engines. 2005
Edit: Janko PALIGA (data addition)
