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특허 상세정보

Aerospace vehicle yaw generating tail section

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-015/00    B64C-005/06   
미국특허분류(USC) 244/087; 244/055; 244/207
출원번호 US-0176516 (2011-07-05)
등록번호 US-8960599 (2015-02-24)
우선권정보 GB-1012675.3 (2010-07-29)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Oliff PLC
인용정보 피인용 횟수 : 0  인용 특허 : 29
초록

A tail section for an aerospace vehicle is provided. The tail section comprises a rudder which is movable about an axis to generate a yawing moment on the aerospace vehicle. The tail section further comprises a thruster having, in flow series, an air intake, an electrically powered device for accelerating the air received through the intake, and an air outlet which directs the accelerated air to increase the yawing moment generated by the rudder.

대표
청구항

1. A tail section for an aerospace vehicle, the tail section comprising: a rudder which is movable about an axis to generate a yawing moment on the aerospace vehicle;a thruster having, in flow series, an air intake, an electrically powered device for accelerating the air received through the intake, and an air outlet which directs the accelerated air to increase the yawing moment generated by the rudder; anda controller that, in response to a determination of an engine shutdown, performs automatic control to power the electrically powered device of the t...

이 특허에 인용된 특허 (29)

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