Invention Grant
- Patent Title: Deflector provided with faces with different curvatures for a thrust reverser of an aircraft engine nacelle
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Application No.: US18129507Application Date: 2023-03-31
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Publication No.: US12012911B2Publication Date: 2024-06-18
- Inventor: Lauren Davis , Christophe Bourdeau , Frédéric Chelin
- Applicant: AIRBUS OPERATIONS (SAS)
- Applicant Address: FR Toulouse
- Assignee: AIRBUS OPERATIONS (S.A.S.)
- Current Assignee: AIRBUS OPERATIONS (S.A.S.)
- Current Assignee Address: FR Toulouse
- Agency: Nixon & Vanderhye P.C.
- Priority: FR 03682 2022.04.21
- Main IPC: F02K1/72
- IPC: F02K1/72

Abstract:
A deflector for an ejection structure of a thrust reverser is disclosed including a deflector plate configured to act on an aerodynamic flow, the deflector plate having a concave upstream face, a convex downstream face, an inlet end, and an outlet end. The upstream face and the downstream face of the deflector plate have different curved profiles, the deflector has a particular profile giving it properties allowing it to act effectively on the aerodynamic flow so as to enhance the performance of the thrust reverser in which it is mounted.
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