Invention Grant
- Patent Title: Turbojet engine nacelle with downstream section
- Patent Title (中): 涡轮喷气发动机舱与下游段
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Application No.: US14524099Application Date: 2014-10-27
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Publication No.: US09341083B2Publication Date: 2016-05-17
- Inventor: Hazem Kioua , Vincent Peyron , Laurent Georges Valleroy
- Applicant: AIRCELLE
- Applicant Address: unknown Gonfreville l'Orcher
- Assignee: AIRCELLE
- Current Assignee: AIRCELLE
- Current Assignee Address: unknown Gonfreville l'Orcher
- Agency: Burris Law, PLLC
- Priority: FR1253902 20120427
- Main IPC: B64D29/06
- IPC: B64D29/06 ; F01D25/24 ; F02K1/72 ; B64D33/04
Abstract:
A turbofan engine nacelle has a downstream section which includes at least one front frame. The front frame is attached to a stationary portion of the nacelle, and the downstream section is provided with at least one rail or slide which extends in a longitudinal direction of the nacelle and is capable of engaging with at least one corresponding slide or rail of an attachment pylon of the turbofan engine. The front frame is connected to the rail or slide of the downstream section by means of at least one swiveled connecting rod.
Public/Granted literature
- US20150300204A1 TURBOJET ENGINE NACELLE WITH DOWNSTREAM SECTION Public/Granted day:2015-10-22
Information query
