Invention Grant
US08613398B2 Apparatus and methods for linear actuation of flow altering components of jet engine nozzle
有权
用于直线致动喷气发动机喷嘴的流动变化部件的装置和方法
- Patent Title: Apparatus and methods for linear actuation of flow altering components of jet engine nozzle
- Patent Title (中): 用于直线致动喷气发动机喷嘴的流动变化部件的装置和方法
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Application No.: US13163463Application Date: 2011-06-17
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Publication No.: US08613398B2Publication Date: 2013-12-24
- Inventor: David Patrick Calder , Pupinder Bhutiani
- Applicant: David Patrick Calder , Pupinder Bhutiani
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Global Patent Operation
- Agent Vivek P. Shankam
- Main IPC: B63H11/10
- IPC: B63H11/10 ; F02K1/00

Abstract:
A trans cowl for a jet engine includes a chevron coupled with a linear actuators. The chevron is movable by the linear actuator forward or aft to change a gas flow path formed by an core cowl and thrust reverser translating cowl. In a first position, the chevrons are disposed substantially parallel the gas flow path to attenuate drag and/or loss of engine thrust. In a second position, the chevrons are moved aft to project, or further project, into the gas flow path. In one embodiment, the linear actuator comprises a first component that is coupled with the outer cowl. A second component of the linear actuator is coupled with the chevron. When installed, the linear actuator can be coupled with a controller and an electrical power source. A position sensor coupled with the controller senses a position of the linear actuator and/or the chevron.
Public/Granted literature
- US20120321456A1 APPARATUS AND METHODS FOR LINEAR ACTUATION OF FLOW ALTERING COMPONENTS OF JET ENGINE NOZZLE Public/Granted day:2012-12-20
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