User:Petebutt/Sandbox: Difference between revisions
Appearance
Content deleted Content added
No edit summary |
No edit summary |
||
Line 48: | Line 48: | ||
|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]]''' |
||
Line 64: | Line 64: | ||
|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]]''' |
||
Line 74: | Line 74: | ||
|align=left| as above |
|align=left| as above |
||
|- |
|- |
||
|align=left| '''[[TR- |
|align=left| '''[[TR-7]]''' |
||
|align=center| {{avyear| |
|align=center| {{avyear|1950's}} |
||
|align=left| |
|align=left| supersonic compressor prototype '''Turbojet''' |
||
|align=left| |
|align=left| |
||
|align=left| |
|align=left| Prototype for AL-7 |
||
|- |
|- |
||
|align=left| '''[[ |
|align=left| '''[[AL-7]]''' |
||
|align=center| {{avyear| |
|align=center| {{avyear|1954}} |
||
|align=left| |
|align=left| 9-stage supersonic compressor '''Turbojet''' |
||
|align=left| |
|align=left| 6,500 kg |
||
|align=left| |
|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
Company type | Aero-engine Design Bureau |
---|---|
Successor | NPO Saturn |
Headquarters | Moscow, 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
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:]]