Invention Grant
- Patent Title: Integrated thrust reverser/pylon assembly
- Patent Title (中): 集成推力反向器/塔架总成
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Application No.: US12533334Application Date: 2009-07-31
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Publication No.: US08713910B2Publication Date: 2014-05-06
- Inventor: Alan Roy Stuart , John Robert Fehrmann
- Applicant: Alan Roy Stuart , John Robert Fehrmann
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agent William Scott Andes; Gary M. Hartman; Domenica N. S. Hartman
- Main IPC: F02K3/02
- IPC: F02K3/02 ; F02K1/00

Abstract:
Assembly for supporting a gas turbine engine comprises a support member including mounting sites for attachment to an associated aircraft. The support member includes integral slider tracks disposed on opposed sidewalls for selective engagement with a translatable cowl. The translatable cowl is translatable along the slider tracks to selectively cover and expose a cascade thrust-reversing structure. The cascade structure includes arcuate segments mounted in hinged relationship to the support member. Rearward translation of the translatable cowl to a service position permits the cascade structure to be opened for access to the core engine.
Public/Granted literature
- US20110023450A1 Integrated Thrust Reverser Assembly Public/Granted day:2011-02-03
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