[특허]Target acquisition system

Target acquisition system 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F41G-003/22
출원번호	US-0787212 (1985-10-15)
발명자 / 주소	Avila Carl A. (Kent WA) Hack Kenneth W. (Seattle WA) Hibbert John A. (Federal Way WA)
출원인 / 주소	The Boeing Company (Seattle WA 02)
인용정보	피인용 횟수 : 48 인용 특허 : 0

초록 ▼

A target acquisition system for a mobile air defense system is capable of acquiring and engaging targets in rapid sequence while mounted on a moving vehicle. It incorporates a gyrostabilized turret drive system, an optical sight, a forward looking infrared scanner, an infared guided missile subsystem, an onboard computer, and system controls and displays. The turret drive will maintain a particular elevation and azimuth regardless of the motion of the vehicle on which the turret is mounted so that the target tracking system need not account for movement of the vehicle over the ground. The optical sight projects a set of reticles on a combining glass in front of the gunner, which shows the target on which the missile seeker is locked as well as the target at which the turret is pointed so that gunner can insure that the missile is locked on the correct target. Critical systems status signals are also displayed on the sight reticle by use of symbology so the gunner can monitor the key systems without taking his eyes off the target. The missile system controls eight missiles, two being activated at any one time, and notifies the gunner by an audio tone that the missile is locked onto a target and is ready to fire. The missile firing sequence is automatically controlled by the control electronics and inserts super elevation and lead angle automatically, and selects and activates the next missile to be fired without delay.

대표청구항 ▼

A heads-up sighting arrangement for a light air defense system having a turret including a cabin rotatably mounted on a base, an azimuth drive and azimuth control system for controlling a direction and speed of rotation of said cabin, a transparent canopy on said cabin and a height-adjustable seat within said cabin facing said transparent canopy for seating a gunner in a position to view airborne targets through said transparent canopy, and a munitions arm for mounting anti-aircraft munitions, said munitions arm being pivotally connected to the cabin for rotation therewith and for pivoting relative thereto about a horizontal axis so as to change an inclination of said munitions arm, a munitions arm elevation drive and elevation control system for controlling a direction and speed of pivoting of the munitions arm, such that the munitions arm may be aimed at and follow airborne targets by rotating the cabin and pivoting the munitions arm, said sight comprising: a sight arm pivotally mounted on a pivot point inside said cabin for rotation therewith and for pivoting about a horizontal axis within said cabin relative thereto, said sight arm being linked to said munitions arm for synchronous motion therewith under control of said gunner by use of said azimuth and elevation control systems; a transparent sight glass mounted on said sight arm between said height-adjustable seat and said transparent canopy in such a position that said gunner, sitting on said height-adjustable seat which has been adjusted to position a swivel axis of the gunner\s neck in line with a swivel axis of said sight arm, looking straight ahead through said transparent sight glass, will be looking in the same direction as said munitions arm is pointed, regardless of an angle of said munitions arm from the horizontal axis; an electro-optic sensor linked to said munitions arm to point in the same direction thereof, said electro-optic sensor producing signals indicative of targets within an angular and distance range of said electro-optic sensor; and projection means for receiving said signals and for producing and projecting indicia of the target sensed by said electro-optic sensor on said transparent sight glass in a position thereon indicative of a position of said sensed target relative to an aimed direction of said transparent sight glass, to enable the gunner to ensure that the electro-optic sensor is trained on the same target which he is viewing optically through said transparent sight glass.

이 특허를 인용한 특허 (48)

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Schmitz,John J.; Petrovich,Paul A.; Stormer,A. David; Washburn,Robert G., System and method for retrofit mechanism for motorizing a manual turret.
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Moraites, Stephen C.; McPhail, Shawn; Sobiski, Donald, System, method, and computer program product for indicating hostile fire.
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IPC	Description
A	생활필수품
A62	인명구조; 소방(사다리 E06C)
A62B	인명구조용의 기구, 장치 또는 방법(특히 의료용에 사용되는 밸브 A61M 39/00; 특히 물에서 쓰이는 인명구조 장치 또는 방법 B63C 9/00; 잠수장비 B63C 11/00; 특히 항공기에 쓰는 것, 예. 낙하산, 투출좌석 B64D; 특히 광산에서 쓰이는 구조장치 E21F 11/00)
A62B-1/08	.. 윈치 또는 풀리에 제동기구가 있는 것

내보내기 구분	파일저장 인쇄 메일전송
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저장형식	Text(ASCII format) Excel format PIAS분석(.xls)
메일정보	받는사람 (필수) @ 보내는사람 (선택) @ 제목 내용 KISTI 검색결과 이메일 서비스
안내	총 건의 자료가 검색되었습니다. 다운받으실 자료의 인덱스를 입력하세요. (1-10,000) 검색결과의 순서대로 최대 10,000건 까지 다운로드가 가능합니다. 데이타가 많을 경우 속도가 느려질 수 있습니다.(최대 2~3분 소요) 다운로드 파일은 UTF-8 형태로 저장됩니다. 파일의 내용이 제대로 보이지 않을실 때는 웹브라우저 상단의 보기 -> 인코딩 -> 자동선택 여부를 확인하십시오. ~ Text(ASCII format) Excel format

연합인증

Target acquisition system 원문보기

초록 ▼

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이 특허를 인용한 특허 (48)

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연합인증

Target acquisition system 원문보기

초록 ▼

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연구과제 타임라인

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이 특허를 인용한 특허 (48)

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특허 원문 보기

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