Invention Grant
- Patent Title: Cascade thrust reverser for an aircraft turbojet engine
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Application No.: US14620543Application Date: 2015-02-12
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Publication No.: US09617955B2Publication Date: 2017-04-11
- Inventor: Vincent Peyron , Laurent Georges Valleroy , Franck Depoortere
- Applicant: AIRCELLE
- Applicant Address: FR Gonfreville l'Orcher
- Assignee: AIRCELLE
- Current Assignee: AIRCELLE
- Current Assignee Address: FR Gonfreville l'Orcher
- Agency: Burris Law, PLLC
- Priority: FR1257867 20120820
- Main IPC: F02K1/62
- IPC: F02K1/62 ; F02K1/72 ; F02K1/76

Abstract:
The present disclosure relates to a cascade thrust reverser providing that when a sliding cowl and a flap are in a direct jet position, a hook is held in engagement with another hook and the flap is immobilized inside of a housing of the sliding cowl by a stem of a telescopic connecting rod subjected to pre-stress generated by a compressed spring located in the body of the connecting rod. When the sliding cowl starts to slide from the direct jet position toward the reverse jet position, the hooks disengage each other and the stem engages with an extension in the body of the connecting rod, so that the flap is rotated from the direct jet position toward the reverse jet position due to the tensile force exerted by the stem.
Public/Granted literature
- US20160245229A1 CASCADE THRUST REVERSER FOR AN AIRCRAFT TURBOJET ENGINE Public/Granted day:2016-08-25
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