Invention Grant
- Patent Title: Turbojet engine nacelle
- Patent Title (中): 涡轮喷气发动机舱
-
Application No.: US13731150Application Date: 2012-12-31
-
Publication No.: US08845287B2Publication Date: 2014-09-30
- Inventor: Hervé Hurlin , Nicolas Dezeustre , Olivier Kerbler , François Gallet , Bertrand Desjoyeaux
- Applicant: Aircelle , SNECMA
- Applicant Address: FR Gonfreville l'Orcher
- Assignee: Aircelle
- Current Assignee: Aircelle
- Current Assignee Address: FR Gonfreville l'Orcher
- Agency: Brinks Gilson & Lione
- Priority: FR1055182 20100629
- Main IPC: F01D25/28
- IPC: F01D25/28 ; B64D29/08 ; F01D25/24 ; B64D29/06

Abstract:
A nacelle for a turbojet engine is provided that includes an air intake upstream from the turbojet engine, a middle section intended to surround a fan of the turbojet engine and its case, and a downstream section. The middle section is made from at least one aerostructure capable of ensuring external aerodynamic continuity of the nacelle, and the aerostructure is rigidly bound, so as to be able to be taken apart, to at least one surrounding fixed structure.
Public/Granted literature
- US20130121814A1 TURBOJET ENGINE NACELLE Public/Granted day:2013-05-16
Information query