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Lyulka AL-41
Lyulka was a USSR aero engine design bureau and manufacturer from 1938 to the 1990s, when manufacturing and design elements were integrated as NPO Saturn based at Rybinsk. The Lyulka design bureau had its roots in the "Kharkiv Aviation Institute" ( Ukrainian SSR ) where Arkhip Mikhailovich Lyulka Arkhip Mikhailovich Lyul'ka (''Russian'': Архи́п Миха́йлович Лю́лька, ''Ukrainian'': Архип Михайлович Люлька) (1908–1984) was a Soviet scientist and designer of jet engines, head of the OKB Lyulka, ... was working with a team designing the ''ATsN'' (Agregat Tsentralnovo Nadduva - Centralised supercharger) installation on the Petlyakov Pe-8 bomber. Lyul'ka was responsible for designing the first Soviet gas turbine engines. Preferring to steer away from copying captured German equipment, it succeeded in producing home grown engines. Engines References * Gunston, Bill. “The Osprey Encyclopaedia of Russian Aircraft 1875–1995”. L ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
NPO Saturn
UEC NPO Saturn, PJSC (russian: ОДК-Сатурн НПО) is a Russian aircraft engine manufacturer, formed from the mergers of Rybinsk Motors and Lyul'ka-Saturn (after Arkhip Mikhailovich Lyulka) in 2001. Saturn's engines power many former Eastern Bloc aircraft, such as the Tupolev Tu-154. Saturn holds a 50% stake in the PowerJet joint venture with Safran Aircraft Engines. The company, founded by Pavel Soloviev, has its headquarters in the town of Rybinsk. History UEC Saturn was established in 2001, following the merger of Rybinsk Motors and Lyulka-Saturn. Rybinsk Motors was established on 20 October 1916 as the Russian Renault automotive plant. In 1917 it started producing aviation engines for the Ilya Muromets aircraft. The company was nationalized in 1918. Rybinsk was originally known as the Kolesov Engine Design Bureau. Kolesov took over the organization from V.A. Dobrynin who founded it in the late 1930s or early 1940s. Under Kolesov's direction, the bureau designed turb ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Lyulka TR-2
Lyulka was a USSR aero engine design bureau and manufacturer from 1938 to the 1990s, when manufacturing and design elements were integrated as NPO Saturn based at Rybinsk. The Lyulka design bureau had its roots in the "Kharkiv Aviation Institute" ( Ukrainian SSR ) where Arkhip Mikhailovich Lyulka was working with a team designing the ''ATsN'' (Agregat Tsentralnovo Nadduva - Centralised supercharger) installation on the Petlyakov Pe-8 The Petlyakov Pe-8 (russian: Петляков Пе-8) was a Soviet heavy bomber designed before World War II, and the only four-engine bomber the USSR built during the war. Produced in limited numbers, it was used to bomb Berlin in August 1941. ... bomber. Lyul'ka was responsible for designing the first Soviet gas turbine engines. Preferring to steer away from copying captured German equipment, it succeeded in producing home grown engines. Engines References * Gunston, Bill. “The Osprey Encyclopaedia of Russian Aircraft 1875–1995”. Londo ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Sukhoi Su-7
The Sukhoi Su-7 ( NATO designation name: Fitter-A) is a swept wing, supersonic fighter aircraft developed by the Soviet Union in 1955. Originally, it was designed as a tactical, low-level dogfighter, but was not successful in this role. On the other hand, the soon-introduced Su-7B series became the main Soviet fighter-bomber and ground-attack aircraft of the 1960s. The Su-7 was rugged in its simplicity, but its Lyulka AL-7 engine had such high fuel consumption that it seriously limited the aircraft's payload, as even short-range missions required that at least two hardpoints be used to carry drop tanks rather than ordnance. Design and development Original Su-7 fighters On 14 May 1953, after Joseph Stalin's death, the Sukhoi OKB was reopened"Sukhoi Su-7." ''Sukhoi Company Museum.'' Retrieved: 28 January 2011 and by the summer, it ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Ilyushin Il-54
The Il-54 was a transonic bomber developed in the USSR in the 1950s. Only two examples were built before the project was abandoned. Design and development The Council of Ministers issued a directive to OKB-115, for a transonic bomber prototype to be submitted for State Acceptance Trials in July 1954. The design of this bomber went through several stages before settling on the final configuration. The Il-54, as built, had a very thin 45 degree swept wing with anhedral, which was shoulder-mounted on the fuselage. The Lyulka AL-7 engines were housed in slim, pylon mounted, pods at approximately 1/3 span. Because the wings and engine nacelles were too small to house a conventional undercarriage, the Il-54 used a bicycle undercarriage arrangement, with nose and main gear units on the centreline of the aircraft, at each end of the bomb bay. This arrangement meant a conventional rotating takeoff would be impossible. To enable the Il-54 to take off, in a reasonable runway length, the ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Beriev Be-10
The Beriev Be-10, also known as Izdelye M, (NATO reporting name: Mallow) was a twin engined, turbojet powered, flying-boat, patrol bomber built by the Soviet Union from 1955. The Be-10 is sometimes referred to as the M-10, though this designation is believed to apply only to the modified Be-10 that established 12 FAI world records in 1961, Bort no. ''40 Yellow'', still holding class records for speed and altitude. Design and development The Be-10 was designed in response to Council of Ministers of the Soviet Union directive No.2622-1105ss which called for a turbojet-powered flying boat for open-sea reconnaissance, bombing, torpedo attack and mine-laying. Stipulated performance was to include a maximum speed of and the ability to operate in wave heights of at wind speeds up to with submission for state acceptance trials in November 1955. OKB-49, under the leadership of Gheorgiy M. Beriev took up the challenge of designing and building the ''izdeliye M'' (Beriev OKB in-house ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Lyulka AL-7
The Lyulka AL-7 was a turbojet designed by Arkhip Mikhailovich Lyulka and produced by his Lyulka design bureau. The engine was produced between 1954 and 1970.Gunston 1989, p.100. Design and development 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 AL-7F version was created in 1953. In April 1956, the Sukhoi S-1 prototype, equipped with the AL-7F, exceeded Mach 2 at 18,000 m (70,900 ft), which led to the production of the Su-7 'Fitter' and Su-9 'Fishpot', equipped with this engine.Green, William and Gordon Swanborough. ''The Great Book of Fighters.'' St. Paul, Minnesota: MBI Publishing, 2001. . Later, the engine was adopted for the Tu-128 'Fiddler' in 1960, and for the AS-3 'Kangaroo' cruise missile. The Beriev Be-10 jet flying boat used a non-afterburning AL-7PB with ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
OKB-1 150
The OKB-1 150 was a jet bomber designed and produced in the Soviet Union from 1948. Development At the end of World War II, many German engineers were 'seconded' by the Soviet government to continue their advanced research under direct supervision of the USSR. One of the most significant German teams was OKB-1 (opytno-konstruktorskoye byuro – experimental design bureau) set up in GOZ-1 (Gosudarstvenny opytnyy zavod – state experimental plant) at Dubna near Moscow. OKB-1, with Dr. Brunolf Baade as chief designer, continued work on German-built aircraft such as the EF-131 and '140', which used many components of the two EF-131's, as well as design work on the stillborn EF 132 long-range bomber. By early 1948 Semyon Alekseyev had been appointed supervisor/chief warden/supervisor of OKB-1, with Dr. Brunolf Baade remaining as chief designer. This has caused confusion in the past with '150' being ascribed to Alekseyev and not OKB-1 (OKB-1 was not named after Baade for propagand ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Sukhoi Su-17 (1949)
The Sukhoi Su-17 (Aircraft R) was a prototype Soviet fighter. The name was later reused for an entirely different fighter-bomber, see Sukhoi Su-17. Development The Su-17 was designed to closely match the theoretical TsAGI calculations for supersonic performance. The aircraft had a 50° swept wing A swept wing is a wing that angles either backward or occasionally forward from its root rather than in a straight sideways direction. Swept wings have been flown since the pioneer days of aviation. Wing sweep at high speeds was first investigate ... fitted with air brakes and boosted controls. A unique feature was that in addition to an ejection seat, the entire nose section of the aircraft could separate from the rest of the airframe. The project was canceled with no flights due to problems with wing structure, ongoing difficulties with the development of the TR-3 engine, and the closure of the Sukhoi OKB. The only example was eventually used as a gunfire target. Specifications (S ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Yakovlev Yak-1000
The Yakovlev Yak-1000 was a Soviet supersonic technology demonstrator intended to evaluate the aerodynamic layout and field performance of the cropped delta wing discussed in captured German documents in combination with the new Lyulka AL-5 turbojet. The tandem undercarriage proved to be unsatisfactory and there were serious flight stability problems related to the delta wing, enough so that it never flew after an accident during taxiing tests. Background and description A June 1950 Council of Ministers directive ordered Yakovlev to develop a supersonic fighter that used the Lyul'ka AL-5 axial compressor turbojet. Based on a recommendation from one of TsAGI aerodynamicists, Yakovlev was directed to use the rhomboid or cropped delta-shaped wing covered in captured German research.Gordon, et al., pp. 184–185 The directive was extremely ambitious as it required the maximum speed to be Mach 1.7 at a time when the world speed record was barely over the sound barrier. This req ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Tupolev Tu-82
The Tupolev Tu-82 was a 1940s Soviet experimental swept-wing bomber. It was the first Soviet jet bomber with swept wings. Design and development Similar to the earlier Tupolev Tu-14 The Tupolev Tu-14 (NATO reporting name: Bosun) (USAF/ DOD reporting name: Type 35), was a Soviet twinjet light bomber derived from the Tupolev Tu-73, the failed competitor to the Ilyushin Il-28 'Beagle'. It was used as a torpedo bomber by the ..., the Tu-82 was designed to investigate the use of swept wings. Powered by two Klimov VK-1 engines, the Tu-82 first flew in February 1949. It achieved a top speed of 934 km/h and a ceiling of 14,000 m. Tupolev planned a larger combat version as the Tu-86, but it was not built. Specifications (Tu-82) See also References Notes Bibliography * * * {{Tupolev aircraft Tupolev aircraft, Tu-0082 1940s Soviet bomber aircraft Twinjets Aircraft first flown in 1949 ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Lavochkin La-190
The Lavochkin La-190, (a.k.a. Aircraft 190), was a swept wing jet fighter designed and manufactured by the Lavochkin Design Bureau from 1950. Design and development The La-190 was an all-metal aircraft with a bicycle undercarriage and mid set wings with 55° sweep at 1/4 chord. The afterburning, Lyul'ka AL-5 (TR-3A), axial flow turbo-jet engine was attached to the rear of the centre fuselage with the air intake at the extreme nose, and exhaust at the end of the rear fuselage. Access to the engine for maintenance and removal was gained by removing the rear fuselage aft of the wing. The bicycle main and nose undercarriages were housed entirely within the fuselage with wing mounted outriggers in small pods at the wingtips. To increase the angle of incidence of the aircraft, to 20–22°, for take-off and landing, the twin wheeled levered suspension main undercarriage could be shortened or "knelt". The swept wings were of medium taper with 2/3 span flaps / 1/3 span ailerons, and win ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
