Invention Grant
- Patent Title: Bypass turbofan engine comprising a nacelle equipped with a translationally-mobile thrust-reversal system and with a fan case equipped with supports
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Application No.: US16656632Application Date: 2019-10-18
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Publication No.: US11136938B2Publication Date: 2021-10-05
- Inventor: Pascal Gardes , Frédéric Ridray , José Goncalves
- 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: FR1871256 20181022
- Main IPC: F02K1/72
- IPC: F02K1/72 ; B29C65/70 ; B29C65/78 ; B29C65/00 ; B29C65/48 ; B29L31/30 ; F02K1/54 ; F02K1/68

Abstract:
A bypass turbofan engine with a nacelle comprising a fan case and a thrust-reversal system. The fan case comprises an exterior wall, and the reversal system comprises a slider having an upstream frame, a downstream frame and a plurality of spars fixed between the upstream frame and the downstream frame, in which the slider is able to move between a forward position and a retracted position. The fan case comprises, at a rear edge of its exterior wall, a support. Each support comprises, for each spar, a shoe fixed to the exterior wall and positioned radially about the spar, and a skirt secured to the shoes and extending the rear edge, in which, in a forward position, the skirt bears around the downstream frame, and in which in a forward/retracted/intermediate position, the shoes are distant from the spars from the upstream frame.
Information query
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