Invention Grant
- Patent Title: Aviation gas turbine thrust reversing device
- Patent Title (中): 航空燃气轮机推力换向装置
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Application No.: US13979782Application Date: 2012-01-19
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Publication No.: US09328694B2Publication Date: 2016-05-03
- Inventor: Predrag Todorovic
- Applicant: Predrag Todorovic
- Applicant Address: DE
- Assignee: Rolls-Royce Deutschland Ltd & Co KG
- Current Assignee: Rolls-Royce Deutschland Ltd & Co KG
- Current Assignee Address: DE
- Agency: Shuttleworth & Ingersoll, PLC
- Agent Timothy J. Klima
- Priority: DE102011008917 20110119
- International Application: PCT/EP2012/000240 WO 20120119
- International Announcement: WO2012/097995 WO 20120726
- Main IPC: F02K1/72
- IPC: F02K1/72 ; F02K3/02 ; F02K1/64 ; F02K1/70 ; F02K1/76

Abstract:
The present invention relates to an aircraft gas turbine thrust-reversing device with an engine having an engine cowling, the rear area of which can be displaced in the axial direction of the engine from a closed forward thrust position into a rearwardly displaced thrust reversal position, resulting in an essentially annular free space towards a forward stationary area of the engine cowling, with the rear area of the engine cowling being functionally coupled to deflecting elements arranged in the forward thrust position within the front area of the engine cowling, with the deflecting elements during displacement of the rear area of the engine cowling being moveable on a partial-circular path facing the central axis of the engine and contactable by their rear end areas with a cowling of the core engine.
Public/Granted literature
- US20130318945A1 AVIATION GAS TURBINE THRUST REVERSING DEVICE Public/Granted day:2013-12-05
Information query
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