FIELD: transportation.
SUBSTANCE: proposed holding device has an upper tension bar, with a rigid fastener to a pylon, first and second tie rods. Each rod is joined to the engine using the first ball and socket joint on one side, and to a tension bar on the other side, using the second ball and socket joint. Each tie rod has a third spare joint, and the tie rods are interchangeable.
EFFECT: minimisation of the risk of error when assembling the device for joining an engine to the structure of an aircraft.
5 cl, 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| REAR HOLDING DEVICE OF AIRCRAFT ENGINE | 2004 |
|
RU2346856C2 |
| AIRCRAFT JET ENGINE SUSPENSION | 2006 |
|
RU2374142C2 |
| AIRCRAFT DEVICE COMPRISING WING AND SUSPENSION PYLON | 2006 |
|
RU2398713C2 |
| REAR SUSPENSION ASSEMBLY OF AIRCRAFT ENGINE WITH DOUBLE EYE, AND POWER PLANT CONTAINING SUCH ASSEMBLY | 2006 |
|
RU2435968C2 |
| AIRCRAFT ENGINE ATTACHMENT FRAME | 2005 |
|
RU2369529C2 |
| ATTACHMENT OF MULTISTAGE TURBOJET TO AIRCRAFT | 2009 |
|
RU2483004C2 |
| AIRCRAFT ENGINE ASSEMBLY | 2005 |
|
RU2381149C2 |
| GAS TURBINE ENGINE SUSPENSION UNIT | 2019 |
|
RU2789803C2 |
| DEVICE FOR TURBOJET ENGINE | 2011 |
|
RU2585368C2 |
| CONNECTION ELEMENT, CRAKE HOOK AND CRANE SUSPENSION | 2008 |
|
RU2458828C2 |
