[특허]Aircraft wing fold actuation system

[미국특허] Aircraft wing fold actuation system 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B64C-003/56
출원번호	US-0556578 (2000-04-24)
발명자 / 주소	Russ David E.
출원인 / 주소	Hamilton Sunstrand Corporation
대리인 / 주소	Wood, Phillips, VanSanten, Clark & Mortimer
인용정보	피인용 횟수 : 27 인용 특허 : 1

초록 ▼

A wing fold actuation system (24) is provided for folding an outboard wing section (18) relative to an inboard wing section (16) between a deployed position (20) and a stored position (22). The system (24) includes an actuator (26) in the form of a geared rotary actuator (30) in combination with a four-bar linkage (32). A locking mechanism (28) is provided to lock the outboard wing section (18) in the deployed position (20), and includes a catch on the outboard wing section (18) that is engageable with a rotary latch (42) on the inboard wing section (16). A timing transmission (46) connects the rotary actuator (30) with the rotary latch (42) to time the rotation of the rotary latch (42) with respect to the movement of the outboard wing section (18) between the deployed and stored positions (20,22).

대표청구항 ▼

[ What is claimed is:] [1.]1. An aircraft wing fold actuation system for folding an outboard wing section relative to an inboard wing section between a deployed position and a stored position, the system comprising:a crank link pivoted to the inboard wing section at a first pivot point for rotation about an axis between first and second angular positions relative to the inboard wing section;a ground link extending between the inboard and outboard wing sections, the ground link being fixed to the inboard wing section to prevent relative movement therebetween, the outboard wing section being pivoted to the ground link at a second pivot point for movement between the deployed and stored positions, the second pivot point being spaced from the first pivot point;a follower link connected to the outboard wing section for movement therewith relative to the inboard wing section between the deployed and stored positions;a coupler link extending between the crank link and the follower link, the coupler link pivoted to the follower link at a third pivot point spaced from the second pivot point, the coupler link pivoted to the crank link at a forth pivot point spaced from the first and third pivot points, the crank and coupler links being within 5.degree. of crank link rotation of a toggle position with the crank link in the first position and the outboard wing section in the deployed position, the crank and coupler links being within 15.degree. of crank link rotation of another toggle position with the crank link in the second position and the outboard wing section in the stored position; andan actuator having an output drivingly connected to the second link to transmit torque to the second link to pivot the second link between the first and second positions.

이 특허에 인용된 특허 (1) 인용/피인용 타임라인 분석

Byford Frank (Washington WA), Control surface drive for folding wing aircraft.
상세보기

이 특허를 인용한 특허 (27) 인용/피인용 타임라인 분석

Himmelmann, Richard A.; Lang, David, Actuator with differential and brake.
상세보기
Degenholtz, Arthur; Mayer, Edward; Vaghela, Naresh P., Arrangement and associated system having an actuator and a tubular flap-drive member about the actuator.
상세보기
Good, Mark Steven; Lassen, Matthew August; Renzelmann, Michael E.; Gardner, Mark J.; Lesyna, Mark William; Hill, Brian Curtis; Tyler, Nicholas Seth, Backup system.
상세보기
Karem, Abe, Compact aircraft wing folding systems and methods.
상세보기
Kracke, Jeremy Alan George, Dual actuator drive assembly with synchronization shaft.
상세보기
Behar, Bruce W.; Flatt, James E.; Gurrola, David J.; Nguyen, Dan T., Electromechanical actuating assembly.
상세보기
Flatt, James E.; Gurrola, David J.; Behar, Bruce W.; Nguyen, Dan T., Electromechanical actuating assembly.
상세보기
Korya, Chetan; Bryant, Anthony; Harding, Matt; Brakes, David, Folding wing tip and rotating locking device.
상세보기
Santini, Gregory M.; Sakurai, Seiya, Horizontal folding wingtip.
상세보기
Santini, Gregory M.; Sakurai, Seiya, Horizontal folding wingtip.
상세보기
Flatt, James E., Jam tolerant electromechanical actuation systems and methods of operation.
상세보기
Flatt, James E., Jam tolerant electromechanical actuation systems and methods of operation.
상세보기
Flatt,James E., Jam tolerant electromechanical actuation systems and methods of operation.
상세보기
Flatt,James E., Jam tolerant electromechanical actuation systems and methods of operation.
상세보기
Kordel, Jan A.; Good, Mark S., Latching apparatus and methods.
상세보기
Easter, William Craig, Rapidly convertible hybrid aircraft and manufacturing method.
상세보기
Townsend, Keith; Fox, Stephen J., Rotary drive assembly for wing tip.
상세보기
Sakurai, Seiya; Kosko, Ryan W.; Santini, Gregory M., Swing wing tip system, assembly and method with dual load path structure.
상세보기
Lassen, Matthew A.; Ostrom, Nicholas A.; Weaver, Jared D.; Whitt, Daniel R., System for latching and locking a foldable airfoil.
상세보기
Good, Mark S.; Walker, Steven Paul; Lassen, Matthew A.; Pietersen, Quentin T., System for latching and locking a folding wing.
상세보기
Gronli, Timothy D., Velocity summing linear actuator.
상세보기
Lassen, Matthew August; Douglas, Chad Richard; Jones, Kelly Thomas; Kenning, Terence Boyd, Wing fold controller.
상세보기
Lassen, Matthew August; Good, Mark Steven, Wing fold controller.
상세보기
Fox, Stephen John; Sakurai, Seiya; Munsen, Victor A.; Noble, Jack S.; Skomorowski, John Tony, Wing fold system.
상세보기
Fox, Stephen John; Kordel, Jan A.; Townsend, Keith; Lassen, Matthew August; Gardner, Mark John; Good, Mark Steven, Wing fold system rotating latch.
상세보기
Good, Mark Steven; Kordel, Jan A.; Pietersen, Quentin Theodor; Walker, Steven Paul; Jones, Kelly Thomas; Lassen, Matthew August; Hansken, Rickie, Wing fold system with latch pins through multiple mating lugs.
상세보기
Schlipf, Bernhard; Hue, Xavier, Wing with retractable wing end piece.
상세보기

활용도 분석정보

상세보기

다운로드

내보내기

활용도 Top5 특허

해당 특허가 속한 카테고리에서 활용도가 높은 상위 5개 콘텐츠를 보여줍니다.
더보기 버튼을 클릭하시면 더 많은 관련자료를 살펴볼 수 있습니다.

내보내기 메뉴

내보내기 구분

파일저장
인쇄
메일전송

구성항목

기본정보
상세정보

관리번호, 국가코드, 자료구분, 상태, 출원번호, 출원일자, 공개번호, 공개일자, 등록번호, 등록일자, 발명명칭(한글), 발명명칭(영문), 출원인(한글), 출원인(영문), 출원인코드, 대표IPC

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

AI-Helper ※ AI-Helper는 을 사용합니다.

AI-Helper

안녕하세요, AI-Helper입니다. 좌측 "선택된 텍스트"에서 텍스트를 선택하여 요약, 번역, 용어설명을 실행하세요.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.

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

연합인증

[미국특허] Aircraft wing fold actuation system 원문보기