Invention Grant
- Patent Title: Turbofan engine comprising a set of rotatable blades for blocking off the bypass flow duct and redirecting the air flow
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Application No.: US17199960Application Date: 2021-03-12
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Publication No.: US11359542B2Publication Date: 2022-06-14
- Inventor: Pascal Gardes , Fabien Menou , Pascal Gougeon , Simon Vanderbauwede
- 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: FR2002535 20200316
- Main IPC: F02C6/20
- IPC: F02C6/20 ; F02C9/18 ; F04D29/52 ; F02K1/72 ; F02K1/64 ; F02K1/70

Abstract:
An engine including a motor and a nacelle and a duct between the nacelle and the motor. The nacelle includes a fixed structure, a mobile assembly that is mobile between an advanced position and a retracted position to define a window between the duct and the outside, and a plurality of blades that are mobile in rotation between a stowed position and a deployed position, each one extending on either side of its axis of rotation with a first arm and a second arm. In the stowed position, the first arm is outside the duct and the second arm is inside the nacelle, and where, in the deployed position, the first arm is across the duct and the second arm projects out of the nacelle. With such blades, the flow of air is optimally directed towards the front without it being necessary to provide cascades.
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