Invention Grant
US09109540B2 Airplane jet engine thrust reverser having gratings or cascades
有权
具有光栅或级联的飞机喷气发动机推力反向器
- Patent Title: Airplane jet engine thrust reverser having gratings or cascades
- Patent Title (中): 具有光栅或级联的飞机喷气发动机推力反向器
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Application No.: US13681210Application Date: 2012-11-19
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Publication No.: US09109540B2Publication Date: 2015-08-18
- Inventor: Guy Bernard Vauchel
- Applicant: AIRCELLE
- Applicant Address: FR Gonfreville L'Orcher
- Assignee: AIRCELLE
- Current Assignee: AIRCELLE
- Current Assignee Address: FR Gonfreville L'Orcher
- Agency: Brinks Gilson & Lione
- Priority: FR1053785 20100517
- Main IPC: F02K1/56
- IPC: F02K1/56 ; F02K1/62 ; F01D11/00 ; F02K1/72 ; F02K1/76

Abstract:
A cascade thrust reverser for an airplane dual flow jet engine nacelle is provided that includes a front frame holding a plurality of cascades, a cowling slidably mounted between a direct jet position and a reverse jet position. The cowl includes a substantially annular diaphragm that is placed edge-to-edge with the front frame and radially inside said cascades when said cowl is located in the direct jet position. Thrust reversal flaps are pivotably mounted onto the diaphragm, and cylinders for actuating the cowl are also provided. Upstream ends of the cylinders are mounted on a stationary portion of the nacelle, and the downstream ends of the cylinders are mounted on an upstream edge of the diaphragm.
Public/Granted literature
- US20130075493A1 AIRPLANE JET ENGINE THRUST REVERSER HAVING GRATINGS OR CASCADES Public/Granted day:2013-03-28
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