|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||239/265.19; 060/771; 181/215|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 1 인용 특허 : 11|
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 t...
1. An apparatus for positioning a chevron, said apparatus comprising: a linear actuator;a chevron having a base end configured to fit within a corresponding channel on a translating cowl;a pair of guide members secured to the translating cowl and slidably engaged with opposite edges of the chevron,wherein the chevron is movable by the linear actuator forward or aft to change the position of the chevron relative to the gas flow path, andwherein the chevron comprises a slot that is sized and configured to receive a rotor of the linear actuator therein. 2. ...