FIELD: engines and pumps.
SUBSTANCE: non-twistable annular stator assembly of aircraft engine includes rigid annular support element, and at least one device for attachment of engine to aircraft. Engine attachment device includes housing made from composite material and rigidly fixed on annular support element, and rigid element enveloping the composite housing with tight fit to it and containing the connecting element to be attached to the aircraft.
EFFECT: invention allows decreasing the weight of annular stator assembly, thus maintaining its rigidity.
18 cl, 13 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FLYING VEHICLE | 1994 |
|
RU2126344C1 |
| FRONT FRAME FOR THRUST REVERSER WITH DEFLECTING CASCADES | 2010 |
|
RU2542165C2 |
| AIRCRAFT POWER PLANT | 2009 |
|
RU2499745C2 |
| AIRCRAFT GAS TURBINE ENGINE MOUNT BAR | 2010 |
|
RU2571680C2 |
| GAS TURBINE ENGINE SUPPORT POST ASSEMBLY | 2012 |
|
RU2606462C2 |
| METHOD OF AND DEVICE FOR INCREASING POWER OUTPUT OF GAS TURBINE BY WET COMPRESSION | 1997 |
|
RU2178532C2 |
| ATTACHMENT OF BLADES IN HOLDER OF COMPOSITE MATERIAL BY FIXATION | 2011 |
|
RU2583183C2 |
| UNIT OF STATOR OF GAS-TURBINE MOTOR AND PROCEDURE FOR REPAIR OF THIS UNIT; ALSO MOTOR COMPRISING THIS UNIT OF STATOR | 2005 |
|
RU2394161C2 |
| AIRCRAFT TURBO MACHINE ASSEMBLY AND AIRCRAFT TURBO MACHINE | 2010 |
|
RU2566617C2 |
| TURBOMACHINE MODULE EQUIPPED WITH RADIAL GAP IMPROVEMENT DEVICE | 2008 |
|
RU2472000C2 |
