Invention Grant
- Patent Title: Nacelle rear assembly for a turbojet engine comprising a suspension cradle
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Application No.: US15654087Application Date: 2017-07-19
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Publication No.: US09856826B2Publication Date: 2018-01-02
- Inventor: Patrick Boileau
- Applicant: SAFRAN NACELLES
- Applicant Address: FR Gonfreville L'Orcher
- Assignee: SAFRAN NACELLES
- Current Assignee: SAFRAN NACELLES
- Current Assignee Address: FR Gonfreville L'Orcher
- Agency: Burris Law, PLLC
- Priority: FR1550492 20150121
- Main IPC: F02K1/72
- IPC: F02K1/72 ; F02C7/20 ; B64D29/06 ; B64D27/10 ; B64D27/16 ; F02K1/76

Abstract:
The present disclosure provides a rear nacelle assembly for a turbojet having at least one thrust reversal device to redirect air circulating from upstream to downstream in a flow path of a turbojet and a mast that connects the nacelle to a structure of an aircraft. In one form, the thrust reverser device includes a cradle having a first longeron and a second longeron extending longitudinally opposite sides of the mast. The first and second longeron each include a device for slideably guiding the cowl and the cascade. In another form, a rear portion and a front portion of the cradle connects to the mast by a rear connecting device and front connecting device, respectively, such that the cradle is adapted to follow the movements of the turbojet.
Public/Granted literature
- US20170321634A1 NACELLE REAR ASSEMBLY FOR A TURBOJET ENGINE COMPRISING A SUSPENSION CRADLE Public/Granted day:2017-11-09
Information query
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