Aircraft, missile, projectile or underwater vehicle with reconfigurable control surfaces
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F42B-015/01
출원번호
US-0077447
(2008-03-19)
발명자
/ 주소
Patel, Mehul
Ng, T. Terry
Cain, Alan B.
Sowle, Zak
DiCocco, Jack
출원인 / 주소
Orbital Research Inc.
대리인 / 주소
Brian M., Kolkowski
인용정보
피인용 횟수 :
2인용 특허 :
12
초록▼
The present invention relates to an aircraft, missile, projectile, or underwater vehicle with an improved control system and an improved control system for maneuvering an aircraft, missile, projectile, or underwater vehicle. More particularly, the present invention relates to an aircraft, missile, u
The present invention relates to an aircraft, missile, projectile, or underwater vehicle with an improved control system and an improved control system for maneuvering an aircraft, missile, projectile, or underwater vehicle. More particularly, the present invention relates to an aircraft, missile, underwater vehicle or projectile with removable control surfaces. The technical advantage of the removable control surface system (or “removable control surface”) over other systems is that the removable control surface system enables the aircraft, missile, underwater vehicle or projectile to have two or more design configurations, each configuration being tailored to the aircraft, missile, projectile, or underwater vehicle's specific stability or maneuverability requirements during a specific portion of the flight.
대표청구항▼
What is claimed is: 1. An aircraft, missile, underwater vehicle or projectile comprisinga body,a sensor or device for detecting a change in condition requiring increased maneuverability or increased stability, the sensor or device having an output, andat least two control surfaces,wherein one of the
What is claimed is: 1. An aircraft, missile, underwater vehicle or projectile comprisinga body,a sensor or device for detecting a change in condition requiring increased maneuverability or increased stability, the sensor or device having an output, andat least two control surfaces,wherein one of the at least two control surfaces is reduced or eliminated to increase maneuverability or increase stability by removing at least part of the one control surface based in part on the output of the sensor or device.
연구과제 타임라인
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이 특허에 인용된 특허 (12)
Harris Gordon L. (15719 Via De Santa Fe Rancho Santa Fe CA 92067-4751), Air launched munition range extension system and method.
Hopwell Brian L. (Preston GBX) Dale Nicholas C. (Preston GBX) Burns ; deceased Bryan R. A. (late of Treales GBX by Jean H. Burns ; administrator), Jettisonable aerodynamic control surfaces.
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