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

Apparatus and methods for linear actuation of flow altering components of jet engine nozzle
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.
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