Invention Grant
- Patent Title: Turbofan engine comprising a series of rotary blades for blocking the stream of the bypass air
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Application No.: US16827021Application Date: 2020-03-23
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Publication No.: US11434849B2Publication Date: 2022-09-06
- Inventor: Antoine Cousin , Frédéric Ridray
- Applicant: Airbus Operations SAS
- Applicant Address: FR Toulouse
- Assignee: Airbus Operations SAS
- Current Assignee: Airbus Operations SAS
- Current Assignee Address: FR Toulouse
- Agency: Greer, Burns & Crain, Ltd.
- Priority: FR1903095 20190325
- Main IPC: F02K1/00
- IPC: F02K1/00 ; F02K1/72 ; F02K1/76

Abstract:
A turbofan engine with a nacelle including a runner translationally mobile between advanced and back-off positions to open a window between a stream and an outside, a plurality of blades, each rotatable on the runner between retracted and deployed positions, and a maneuvering system displacing each blade and comprising, for each blade, a shaft rotatable on the runner and to which the blade is fixed, and a toothed segment on the shaft, and a toothed arc rotatable on the runner about a longitudinal axis, the tooth arc teeth meshing with the toothed segment teeth, a slip translationally mobile on the runner in a plane at right angles to the longitudinal axis between first and second positions, a connecting rod mounted articulated between the slip and the toothed arc, a rib integral to the fixed structure, and a guiding U integral to the slip and which straddles the rib.
Public/Granted literature
- US20200378340A1 TURBOFAN ENGINE COMPRISING A SERIES OF ROTARY BLADES FOR BLOCKING THE STREAM OF THE BYPASS AIR Public/Granted day:2020-12-03
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