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|align=left| 8-stage Axial flow compressor '''Turbojet'''
|align=left| 8-stage Axial flow compressor '''Turbojet'''
|align=left| 1,300 kg
|align=left| 1,300 kg
|align=left| Alekseyev I-211, Ilyushin Il-22, Sukhoi Su-10, Sukhoi Su-11
|align=left| [[Alekseyev I-211]], [[Ilyushin Il-22]], [[Sukhoi Su-10]], [[Sukhoi Su-11]]
|-
|-
|align=left| '''[[TR-1A]]'''
|align=left| '''[[TR-1A]]'''
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|align=left| '''[[TR-3/AL-5]]'''
|align=left| '''[[TR-3/AL-5]]'''
|align=center| {{avyear|1949}}
|align=center| {{avyear|1949}}
|align=left| 7-stage Axial-flow '''Turbojet
|align=left| 7-stage Axial-flow '''Turbojet'''
|align=left| 4,600 kg (at qualification in 1950)
|align=left| 4,600 kg (at qualification in 1950)
|align=left| Il-30, Il-46, Lavochkin 190, Tu-86, Yak-1000, Su-17(1949)
|align=left| [[Il-30]], [[Il-46]], [[Lavochkin Aircraft 190]], [[Tu-86]], [[Yak-1000]], [[Su-17]](1949), "[[Aircraft 150]]"
|-
|-
|align=left| '''[[Al-5/TR-3A]]'''
|align=left| '''[[Al-5/TR-3A]]'''
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|align=left| as above
|align=left| as above
|-
|-
|align=left| '''[[TR-1]]'''
|align=left| '''[[TR-7]]'''
|align=center| {{avyear|1946}}
|align=center| {{avyear|1950's}}
|align=left| Type
|align=left| supersonic compressor prototype '''Turbojet'''
|align=left| Type
|align=left|
|align=left| Type
|align=left| Prototype for AL-7
|-
|-
|align=left| '''[[TR-1]]'''
|align=left| '''[[AL-7]]'''
|align=center| {{avyear|1946}}
|align=center| {{avyear|1954}}
|align=left| Type
|align=left| 9-stage supersonic compressor '''Turbojet'''
|align=left| Type
|align=left| 6,500 kg
|align=left| Type
|align=left| [[Il-54]], Su-7B, Tu-98, Su
|-
|-
|align=left| '''[[TR-1]]'''
|align=left| '''[[TR-1]]'''

Revision as of 06:58, 11 May 2009

Lyul'ka
Company typeAero-engine Design Bureau
SuccessorNPO Saturn
HeadquartersMoscow, USSR
Key people
Arkhip Mikhailovich Lyulka

Lyul'ka was a USSR aero-engine design bureau / manufacturer from 1938 to The 1990's when manufacturing and design elements were integrated as NPO Saturn based at Rybinsk. The Lyul'ka design bureau had its roots in the Kharkov Aviation Institute where Artem M. Lyul'ka 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, he succeded in producing home grown engines.

Engines

Summary of engines built/designed by Lyul'ka
Model name Date Type Thrust (kg) / Power (eshp) Fitted to
RTD-1/VDR-2 Template:Avyear Two-stage centrifugal compressor Turbojet 500kg estimated Test-bed only
S-18/VDR-3 Template:Avyear Axial flow compressor Turbojet 1,250 kg Gu-VRD project
TR-1 Template:Avyear 8-stage Axial flow compressor Turbojet 1,300 kg Alekseyev I-211, Ilyushin Il-22, Sukhoi Su-10, Sukhoi Su-11
TR-1A Template:Avyear 8-stage Axial flow compressor Turbojet 1,500 kg
TR-2 Template:Avyear projected growth version of TR-1
TR-3/AL-5 Template:Avyear 7-stage Axial-flow Turbojet 4,600 kg (at qualification in 1950) Il-30, Il-46, Lavochkin Aircraft 190, Tu-86, Yak-1000, Su-17(1949), "Aircraft 150"
Al-5/TR-3A Template:Avyear as above as above as above
TR-7 Template:Avyear supersonic compressor prototype Turbojet Prototype for AL-7
AL-7 Template:Avyear 9-stage supersonic compressor Turbojet 6,500 kg Il-54, Su-7B, Tu-98, Su
TR-1 Template:Avyear Type Type Type
TR-1 Template:Avyear Type Type Type
TR-1 Template:Avyear Type Type Type
TR-1 Template:Avyear Type Type Type
TR-1 Template:Avyear Type Type Type


[[Category:]]