FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly to engine to fuselage pylon attachment. Suspension comprises front, rear and mid plane of suspension. Front plane is located at level of intermediate engine housing and joins it with pylon. Rear suspension plane is located at level of exhaust of engine housing and joins it with pylon. Intermediate plane is located between front and rear surfaces and comprises connection link between gas turbine engine and pylon. Connecting link is arranged with clearance on engine and not used at operating suspension of rear plane. Connecting link is connected with element made of flexible material, which provides said gap due to properties of elastic deformation.
EFFECT: higher safety of gas turbine engine suspension operation is achieved.
10 cl, 7 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE DESIGNED TO SECURE GAS TURBINE ENGINE TO AIRCRAFT | 2008 |
|
RU2388659C1 |
| TURBOJET HINGED TO AIRCRAFT PYLON | 2008 |
|
RU2487056C2 |
| ATTACHMENT OF TURBOJET TO AIRCRAFT | 2008 |
|
RU2487821C2 |
| AIRCRAFT DEVICE COMPRISING WING AND SUSPENSION PYLON | 2006 |
|
RU2398713C2 |
| FAN BODY SUPPORT FRAME MOUNTED AT NACELLE ATTACHMENT PYLON AND AIR INTAKE | 2008 |
|
RU2468963C2 |
| ISOSTATIC SUSPENSION OF A TURBOJET BY REAR DOUBLE SUPPORT | 2014 |
|
RU2682206C2 |
| GAS TURBINE ENGINE CONTAINING SUSPENSION MEANS | 2019 |
|
RU2784242C2 |
| FLYING LABORATORY FOR FLIGHT TESTS OF AIRCRAFT ENGINES AND OTHER OBJECTS OF AVIATION EQUIPMENT SUSPENDED FROM ENGINE PYLON OF AIRCRAFT | 2023 |
|
RU2814557C1 |
| TURBINE ENGINE PROVIDED WITH MEANS OF ABSORBING STRESSES FROM THRUST OF ENGINE THEREOF | 2014 |
|
RU2677312C2 |
| GAS TURBINE ENGINE SUSPENSION UNIT | 2019 |
|
RU2789803C2 |
