Invention Grant
- Patent Title: Aircraft turbomachine assembly comprising an articulated cowl
-
Application No.: US16658936Application Date: 2019-10-21
-
Publication No.: US11142327B2Publication Date: 2021-10-12
- Inventor: Christophe Labarthe , Jean Geliot
- 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: FR1871281 20181023
- Main IPC: B64D29/08
- IPC: B64D29/08 ; B64D29/06 ; B64D29/02 ; B64D27/26

Abstract:
A turbomachine assembly comprising a nacelle having an air inlet and comprising a structure. A forward hood is fixed to the structure and extends backwards from the air inlet. An articulated hood is arranged in the upper part of the nacelle and at the rear of the forward hood and comprises a front edge arranged at the front of the articulated hood. A rear edge is arranged at the rear of the articulated hood. A joint is disposed at the front edge between the articulated hood and the structure and ensures a displacement of the articulated hood between a closed position and an open position. A locking system is arranged at the rear edge, and is mobile between a locked position and an unlocked position, where in the closed position, the front edge is under the forward hood.
Information query