FIELD: transport.
SUBSTANCE: proposed aircraft power plant 1 comprises turbojet angle 2, engine attachment strut 4, assemblies 6a, 6b, 8, 9 of engine suspension arranged between said strut and turbojet engine. Front assemblies 6a, 6b of engine suspension are secured on case 12 of turbojet engine fan in symmetry about the plane formed by lengthwise axis 5 of turbojet engine and its vertical axis Z. Note here that first and second front assemblies 6a, 6b can take up forces acting along lengthwise axis X and vertical axis Z of turbojet engine. Engine suspension rear assembly 9 can take up forces acting along axis Z of turbojet engine.
EFFECT: reduced friction between compressor vanes and engine central case, engine longer life.
17 cl
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT POWER PLANT | 2006 |
|
RU2401223C2 |
| 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 |
| AIRCRAFT POWER PLANT COMPRISING ENGINE AND ENGINE PYLON | 2006 |
|
RU2401222C2 |
| AIRCRAFT ENGINE ASSEMBLY UNIT | 2005 |
|
RU2381148C2 |
| AIRCRAFT POWER PLANT WITH ENGINE AND ATTACHMENT STRUT | 2006 |
|
RU2420430C2 |
| AIRCRAFT ENGINE ASSEMBLY | 2005 |
|
RU2381149C2 |
| AIRCRAFT ENGINE STUB | 2006 |
|
RU2406658C2 |
