FIELD: engines and pumps.
SUBSTANCE: claimed thrust reverser comprises deflectors, moving cowl and inner panel. Moving cowl can translate along the nacelle from the closed position whereat it ensures the nacelle aerodynamic continuity and overlaps the deflectors to the open position whereat it opens the nacelle channel and said deflectors. Said inner panel can translate along the nacelle to turn the locking flaps. Moving cowl comprises the controlled nozzle section and locking means. The latter can interact with the additional locking means of said inner panel to connect mechanically said panel with moving cowl. Locking means or additional locking means comprises the locking latch fitted to thrust against resilient return mean to displace from the gripping position to free position. Said latch is retained at free position by means of the pin fitted at the thrust reverser fixed structure. Another invention of proposed set covers aircraft turbojet with above described assy.
EFFECT: simplified design.
12 cl, 12 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| BYPASS TURBOJET NACELLE | 2009 |
|
RU2499904C2 |
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| TURBOJET NACELLE REAR ASSEMBLY | 2010 |
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| THRUST REVERSER WITH AERODYNAMIC COUPLING FOR FRONT FRAME | 2011 |
|
RU2574118C2 |
| CONTROL SYSTEM FOR TURBOJET ENGINE NACELLE AND NACELLE EQUIPPED WITH SUCH SYSTEM | 2010 |
|
RU2531204C2 |
| TURBOJET NACELLE MOVING PANEL DRIVE SYSTEM | 2010 |
|
RU2521906C2 |
