FIELD: engines and pumps.
SUBSTANCE: thrust reverser making turbojet engine nacelle rear compartment section comprises front frame attached to nacelle fixed section to support movable cowling drive cylinders, and grids of deflecting vanes arranged along perimetre. Front frame has fixed part to secure it thereto and to support grids of deflecting vanes, and part arranged to displace along nacelle axis and supporting one of the ends of cowling drive power cylinders secured thereto. Front frame fixed and movable sections are furnished with locks for them to be locked and unlocked.
EFFECT: simplified cowling displacement in servicing.
11 cl, 10 dwg
Title | Year | Author | Number |
---|---|---|---|
TURBOJET ENGINE THRUST REVERSER | 2008 |
|
RU2450151C2 |
METHOD OF CONTROLLING THRUST REVERSER MOTORS | 2008 |
|
RU2451198C2 |
DETACHABLE AIR INTAKE FOR TURBOJET NACELLE | 2007 |
|
RU2451804C2 |
THRUST REVERSER | 2010 |
|
RU2546132C2 |
THRUST REVERSER | 2010 |
|
RU2522017C2 |
AUTOMATIC ADJUSTMENT METHOD OF ELECTRIC POWER CYLINDERS OF JET TURBINE ENGINE NACELLE | 2008 |
|
RU2459100C2 |
POD FOR JET TURBINE ENGINE | 2007 |
|
RU2442726C2 |
LOCKING/UNLOCKING DEVICE OF THRUST REVERSER, THRUST REVERSER CONTAINING SUCH DEVICE, AND AIRCRAFT ENGINE NACELLE EQUIPPED WITH SUCH THRUST | 2011 |
|
RU2576400C2 |
THRUST REVERSER DEVICE FIXED STRUCTURE AND TURBOJET ENGINE NACELLE HAVING SUCH DEVICE | 2013 |
|
RU2650982C2 |
TURBOJET ENGINE NACELLE REINFORCING STRUCTURE | 2011 |
|
RU2569725C2 |
Authors
Dates
2012-05-27—Published
2007-11-19—Filed