FIELD: engines and pumps.
SUBSTANCE: engine unit (1) comprises gas turbine engine (2), attachment pylon (4), and multiple engine suspension assemblies (6a, 6b, 8) arranged between pylon (4) and gas turbine engine (2). Solely multiple engine suspension assemblies (6a, 6b, 8) fix gas turbine engine (2) on pylon (4). Note here that every aforesaid assembly is attached to has turbine engine compressor casing (12).
EFFECT: engine longer life.
19 cl, 13 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT GAS TURBINE ENGINE PYLON | 2005 |
|
RU2381150C2 |
| AIRCRAFT ENGINE ASSEMBLY UNIT | 2005 |
|
RU2381148C2 |
| AIRCRAFT ENGINE ASSEMBLY | 2005 |
|
RU2381149C2 |
| AIRCRAFT POWER PLANT | 2006 |
|
RU2409505C2 |
| AIRCRAFT POWER PLANT | 2006 |
|
RU2401223C2 |
| AIRCRAFT ENGINE SUPPORT COMPRISING TWO TIE RODS WITH TRANSVERSE JOINTING ELEMENT | 2007 |
|
RU2433068C2 |
| AIRCRAFT POWER PLANT COMPRISING ENGINE SUSPENSION ASSEMBLIES SHIFTED DOWNWARD AT BLOWER HOUSING | 2009 |
|
RU2487057C2 |
| AIRCRAFT POWER PLANT BUILT AROUND TURBOJET WITH REINFORCING STRUCTURES CONNECTING FAN CASE WITH CENTRAL HOUSING | 2009 |
|
RU2485022C2 |
| AIRCRAFT TURBOJET ENGINE PYLON | 2006 |
|
RU2400401C2 |
| AIRCRAFT TURBOJET ENGINE ATTACHMENT STRUT | 2006 |
|
RU2399558C2 |
