[특허]Survivability and mission flexibility enhancements for reconnaissance aircraft

Advanced Aerospace Technologies, Inc.

검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
검색연산자

검색연산자	기능	검색시 예
()	우선순위가 가장 높은 연산자	예1) (나노 (기계 \| machine))
공백	두 개의 검색어(식)을 모두 포함하고 있는 문서 검색	예1) (나노 기계) 예2) 나노 장영실
\|	두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색	예1) (줄기세포 \| 면역) 예2) 줄기세포 \| 장영실
!	NOT 이후에 있는 검색어가 포함된 문서는 제외	예1) (황금 !백금) 예2) !image
*	검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색	예) semi*
""	따옴표 내의 구문과 완전히 일치하는 문서만 검색	예) "Transform and Quantization"

과학기술 지식인프라 ScienceON

안녕하세요!
ScienceON 챗봇입니다.
궁금한 것은 저에게 물어봐주세요.

특허 상세정보

MyON담기

내보내기

Survivability and mission flexibility enhancements for reconnaissance aircraft

국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F42B-004/26
미국특허분류(USC)	244/170; 102/336; 102/351; 089/001.11
출원번호	US-0169425 (2002-06-28)
국제출원번호	PCT/US01/00033 (2001-01-02)
국제공개번호	WO01/50135 (2001-07-12)
발명자 / 주소	McDonnell, William R.
출원인 / 주소	Advanced Aerospace Technologies, Inc.
대리인 / 주소	Polster, Lieder, Woodruff & Lucchesi LC
인용정보	피인용 횟수 : 12 인용 특허 : 6

초록

대표
청구항
▼

A pod (34) containing sensors and/or targeting systems such as laser designators or range finders are hung on a cable (30) below an aircraft (12). The line (30) can be reeled in or out similar to towed decoys. This allows the aircraft (12) to operate above or in the cloud cover while the sensors/targeting equipment (34) are operating below the cloud cover to find the enemy forces. nd reel axle has a proximal end attached to the forward second reel flange and an opposing distal end, a second keyway being formed through the distal end of the second reel axle, the second keyway being configured for receiving a second drive key for engaging the forward second reel axle for rotation of the second reel. 6. A loading system according to claim 5 wherein the first and second keyways are formed with different geometric cross-sectional shapes. 7. A loading system according to claim 5 further comprising a portable power unit comprising: an electric motor disposed within a housing, the electric motor having an output shaft; a power cord in electrical communication with the electric motor, the power cord extending outside the housing and being connectable to an external power source; a first drive cylinder including opposing proximal and distal first drive cylinder ends, the distal first drive cylinder end extending outside the housing, the first drive cylinder also including a drive cylinder axis of rotation through the proximal and distal first drive cylinder ends, a first drive key formed at the distal first drive cylinder end and a cylindrical central passage through the proximal and distal first drive cylinder ends, the cylindrical central passage being coaxial with the drive cylinder axis of rotation, the first drive key being adapted for engagement with the first keyway; a second drive cylinder including opposing proximal and distal second drive cylinder ends, the distal second drive cylinder end extending outside the housing, the second drive cylinder also including a second drive key formed at the distal second drive cylinder end, at least a portion of the second drive cylinder being telescopically disposed within the central passage of the first drive cylinder, the second drive cylinder being configured for independent rotation within the central passage, the second drive key being adapted for engagement with the second keyway; and a power transmission arrangement connected to the output shaft of the electric motor and to the first and second drive cylinders, the power transmission arrangement being configured for applying rotational energy from the output shaft to selectively rotate the first drive cylinder, the second drive cylinder or both the first and second drive cylinders. 8. A loading system according to claim 7 wherein the electric motor is adapted to be powered by a 115 Volt, three phase DC power source. 9. A loading system according to claim 7 wherein the external power source is an electrical system of a ship and the power cord is adapted for connection to an electrical service station of the ship. 10. A loading system according to claim 7 wherein the external power source is an electrical system of an aircraft and the power cord is adapted for connection to an electrical outlet located on the aircraft structure. 11. A loading system according to claim 10 wherein the electric motor is adapted to be powered by an aircraft power source. 12. A loading system for loading a stores item onto a release unit attachable to an aircraft structure, the release unit comprising a release actuation assembly including an actuator arm, the loading system comprising: at least one hook pivotably mountable to the release actuation assembly, the at least one hook including a stores engagement portion configured for engaging a lifting structure of the stores item and an actuation portion configured for engagement by the actuator arm of the release actuation assembly to pivot the at least one hook and disengage the stores engagement portion from the lifting structure of the stores item; means for pivotably and removably mounting the at least one hook to the release actuation assembly; and means for lowering the at least one hook from the release unit for engagement with the lifting structure of the stores item and for raising the at least one hook into a position where the at least one hook can be mounte

이 특허에 인용된 특허 (6)

이 특허를 인용한 특허 피인용횟수: 12

IPC 상위 출원인

내보내기

상세정보
내보내기 구분	파일저장 인쇄 메일전송
구성항목	관리번호, 국가코드, 자료구분, 상태, 출원번호, 출원일자, 공개번호, 공개일자, 등록번호, 등록일자, 발명명칭(한글), 발명명칭(영문), 출원인(한글), 출원인(영문), 출원인코드, 대표IPC 관리번호, 국가코드, 자료구분, 상태, 출원번호, 출원일자, 공개번호, 공개일자, 공고번호, 공고일자, 등록번호, 등록일자, 발명명칭(한글), 발명명칭(영문), 출원인(한글), 출원인(영문), 출원인코드, 대표출원인, 출원인국적, 출원인주소, 발명자, 발명자E, 발명자코드, 발명자주소, 발명자 우편번호, 발명자국적, 대표IPC, IPC코드, 요약, 미국특허분류, 대리인주소, 대리인코드, 대리인(한글), 대리인(영문), 국제공개일자, 국제공개번호, 국제출원일자, 국제출원번호, 우선권, 우선권주장일, 우선권국가, 우선권출원번호, 원출원일자, 원출원번호, 지정국, Citing Patents, Cited Patents
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

과학기술 지식인프라 ScienceON

ScienceON Chatbot

특허 상세정보

Survivability and mission flexibility enhancements for reconnaissance aircraft

초록

대표
청구항
▼

이 특허에 인용된 특허 (6)

이 특허를 인용한 특허 피인용횟수: 12

IPC 상위 출원인

상세정보조회

원문조회

IPC 상세정보(version : 201201)

연구과제 성과물(0)

참여연구원의 다른 문헌(0)

처리중입니다.

잠시만 기다려주세요.

ScienceON Chatbot

특허 상세정보

Survivability and mission flexibility enhancements for reconnaissance aircraft

초록

대표청구항 ▼

이 특허에 인용된 특허 (6)

이 특허를 인용한 특허 피인용횟수: 12

IPC 상위 출원인

상세정보조회

원문조회

IPC 상세정보(version : 201201)

연구과제 성과물(0)

참여연구원의 다른 문헌(0)

처리중입니다.

잠시만 기다려주세요.

대표
청구항
▼