|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/75R ; 244/46 ; 244/327|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 10 인용 특허 : 0|
A body spoiler rotatably mounted within a recess formed within opposite sides of the forebody of a supersonic air vehicle and configured to conform with the fuselage of the vehicle. A sensor positioned close to the inlet of each engine powering the flight of the vehicle measures the pressure of the fluid entering the engine. If an engine on one side of the vehicle malfunctions, the pressure sensor sends a deploy signal to the body spoiler mounted on the same side of the vehicle. An actuator receives the deploy signal and rotates the spoiler through an an...
In an air vehicle powered by engines and being capable of moving within a fluid at supersonic speeds, a system for counterbalancing the yawing moment created by a malfunctioning engine positioned on one side of said vehicle, said system comprising: (a) a pressure detector located proximate the inlet to said engine, said detector capable of generating a signal when the pressure of the fluid entering said inlet reaches a predetermined value indicating engine malfunction; (b) at least one spoiler pivotably mounted on the forebody of said vehicle, said spoil...