Invention Grant
- Patent Title: Turbojet engine nacelle with variable ventilation outlet cross section
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Application No.: US13870369Application Date: 2013-04-25
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Publication No.: US09670798B2Publication Date: 2017-06-06
- Inventor: Guy Bernard Vauchel , Laurence Lemains
- Applicant: AIRCELLE
- Applicant Address: FR Gonfrieville l'Orcher
- Assignee: AIRCELLE
- Current Assignee: AIRCELLE
- Current Assignee Address: FR Gonfrieville l'Orcher
- Agency: Burris Law, PLLC
- Priority: FR1058712 20101025
- Main IPC: F02K1/46
- IPC: F02K1/46 ; F01D25/24 ; B64D29/00 ; B64D33/04 ; F02K1/38 ; F02K1/72

Abstract:
A turbojet engine nacelle includes a rear section having an internal structure. The internal structure surrounds a rear part of an engine compartment and delimits, with an ejection jet pipe, an outlet cross section for the ventilation of the engine compartment. The engine nacelle includes a moving element associated with a corresponding controller. The moving element is able to move between a withdrawn position in which the outlet cross section for ventilation is at a maximum and an engaged position in which the moving element partially reduces the outlet cross section for ventilation by comparison with the retracted position. The controller is capable of moving the moving element between the retracted and engaged positions.
Public/Granted literature
- US20130236294A1 TURBOJET ENGINE NACELLE WITH VARIABLE VENTILATION OUTLET CROSS SECTION Public/Granted day:2013-09-12
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