Invention Grant
- Patent Title: Turbojet nacelle having a removable air intake structure
- Patent Title (中): 涡轮喷气发动机舱具有可拆卸的进气结构
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Application No.: US13203094Application Date: 2010-02-04
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Publication No.: US08899255B2Publication Date: 2014-12-02
- Inventor: Herve Jean Albert Mouton , Thomas Alain Christian Vincent
- Applicant: Herve Jean Albert Mouton , Thomas Alain Christian Vincent
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR0951154 20090224
- International Application: PCT/FR2010/050175 WO 20100204
- International Announcement: WO2010/097532 WO 20100902
- Main IPC: F02C7/04
- IPC: F02C7/04 ; B64D29/06 ; B64D33/02

Abstract:
A turbojet engine nacelle, including an air intake structure for directing an airflow towards a fan of the turbojet engine, a middle structure attached to the air intake structure for surrounding the fan of the turbojet engine, the air intake structure including an inner panel attached to the middle structure and defining a fixed structure with the middle structure, and an outer panel including an air intake lip at the end thereof opposite the middle structure, the outer panel being longitudinally translatably movable relative to the inner panel. The nacelle further includes at least one rod having one end attached onto a flange of the air intake lip and a mechanism rigidly connected to the middle structure for securing and locking the other end of each rod by applying a traction force thereon.
Public/Granted literature
- US20110308634A1 TURBOJET NACELLE HAVING A REMOVABLE AIR INTAKE STRUCTURE Public/Granted day:2011-12-22
Information query
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