FIELD: aircraft engineering.
SUBSTANCE: engine assembly unit (1) comprises turbojet engine (2), pylon (4), and multiple engine attachment elements (6a, 6b, 8) arranged between pylon (4) and turbojet engine (2). Said multiple elements comprises two suspension front units (6a, 6b) shifted relative each other along turbojet engine vertical axis (Z). Note here that first suspension unit (6a) can take up only those loads that act along engine crosswise axis (Y). Second front unit (6b) can take up only those forces that act along axes (Y) and (Z).
EFFECT: optimum distribution of loads taking transmitted from turbojet engine to pylon structure.
8 cl, 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT ENGINE ASSEMBLY | 2005 |
|
RU2381149C2 |
| AIRCRAFT TURBOJET ENGINE PYLON | 2006 |
|
RU2400401C2 |
| AIRCRAFT POWER PLANT COMPRISING ENGINE AND ENGINE PYLON | 2006 |
|
RU2401222C2 |
| AIRCRAFT POWER PLANT | 2006 |
|
RU2409505C2 |
| AIRCRAFT GAS TURBINE ENGINE PYLON | 2005 |
|
RU2381150C2 |
| AIRCRAFT ENGINE UNIT | 2005 |
|
RU2383473C2 |
| AIRCRAFT POWER PLANT BUILT AROUND TURBOJET WITH REINFORCING STRUCTURES CONNECTING FAN CASE WITH CENTRAL HOUSING | 2009 |
|
RU2485022C2 |
| AIRCRAFT POWER PLANT | 2006 |
|
RU2401223C2 |
| AIRCRAFT POWER PLANT COMPRISING ENGINE SUSPENSION ASSEMBLIES SHIFTED DOWNWARD AT BLOWER HOUSING | 2009 |
|
RU2487057C2 |
| AIRCRAFT TURBOJET ENGINE ATTACHMENT STRUT | 2006 |
|
RU2399558C2 |
