[특허]Automatic controls for airplane take-off and landing modes

Automatic controls for airplane take-off and landing modes 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	G05D-001/12
출원번호	US-0617621 (1975-09-29)
발명자 / 주소	Boyle James Alfred (Bellevue WA) Galins Peteris Adams (Renton WA) Gregoire Mark Charles (Issaquah WA) O\Toole Peter L. M. (Bellevue WA)
출원인 / 주소	The Boeing Company (Seattle WA 02)
인용정보	피인용 횟수 : 18 인용 특허 : 0

초록 ▼

A take-off and landing control device for automatic retraction of flaps upon stowing landing gear and upon attaining a predetermined airspeed and of indicating distance from brake release during take-off, and for an automatic decelerating approach with flaps extending as a function of distance from touchdown with automatic throttle cutback and automatic stabilizer trim in response to flap location maintaining an essentially constant angle of attack.

대표청구항 ▼

A device for controlling a flight pattern of an aircraft during take-off comprising: means for automatically retracting flaps in response to a sensed predetermined airspeed after stowing landing gear, said means comprising: means for comparing a voltage proportional to a preselected airspeed with a voltage proportional to airspeed from a central air data computer to impart a command voltage, and means for retracting the flaps upon the command voltage being received by the servo-amplifier, wherein the means for retracting the flaps in response to command voltage being received by the servo-amplifier comprises: a transfer valve controlled by the servo-amplifier, and a hydraulic motor driven by hydraulic fluid from the transfer valve; and means for determining and for indicating airplane position over a predetermined ground location at which point engine thrust is cut back to reduce the noise of climb-out. A method of controlling a flight pattern of an aircraft during take-off and approach modes, the steps comprising: extending the flaps for take-off; entering a predetermined speed in a control panel; engaging an automatic flap mode to compare actual speed with the predetermined speed to retract the flaps with landing gear stowed and predetermined speed reached; arming an automatic signalling device to indicate reaching a preselected distance from the start of the take-off; cutting back on the throttle, during climbout, upon receiving the distance signal; selecting a distance interval from touchdown for a decelerating approach during the approach mode; arming the automatic flap control to extend the flaps in response to distance from touchdown; entering a predetermined lower limit of speed for the end of the decelerating approach; arming the automatic decelerating throttle controls to reduce thrust in response to sensed flap position; entering a bias to stabilizer position at point of initial deceleration, and arming an automatic trim control system to respond to sensed flap position in combination with bias modified initial stabilizer position.

이 특허를 인용한 특허 (18)

Wyrembek,Susanne; May,Peter; Muthreich,Klaus, Aerodynamic component for controlling a landing guide path of an aircraft.
상세보기
DeVlieg Garrett H. ; Mackness Robert F. ; Yamamoto David T., Aircraft stop-to-position autobrake control system.
상세보기
Milligan Mancil W. (Knoxville TN) Wilkerson H. Joe (Knoxville TN), Airplane take-off monitor with learning feature.
상세보기
Berens, Martin; Quell, Juergen; Kroeger, August, Automatic control of a high lift system of an aircraft.
상세보기
Villaume, Fabrice; Jourdan, Christophe; Jacob, Armand; Blondin, Vincent, Automatic take-off method and device for an airplane.
상세보기
Brandau William E. (Westwood NJ) Swern Frederic L. (Succasunna NJ) Moses Kurt (Dumont NJ), Control system.
상세보기
Berens, Martin, Control system for aircraft high lift devices and method for controlling the configuration of aircraft high lift devices.
상세보기
Ishihara, Yasuo; Johnson, Steve; Conner, Kevin J, Flaps overspeed advisory system.
상세보기
Van Boven, Machiel, Flight management process for an aircraft.
상세보기
Sauvinet, Frédéric, Method and device for generating an optimum aerodynamic configuration of an aircraft during a flight.
상세보기
Wyrembek,Susanne; May,Peter; Muthreich,Klaus, Method and device for steepening a landing approach of an aircraft.
상세보기
Sicre Jean-Luc (Meudon la Foret FRX) Gruaz Daniel (Le Chesnay FRX), Method and system for controlling the decelerated approach of an aerodyne.
상세보기
Ferro, Daniel; Van Boven, Machiel, Navigation system for an aircraft and associated command process.
상세보기
Boissenin, Stéphane; Rosay, Jacques, Procedure and device for improving the maneuverability of an aircraft during the approach to landing and flare-out phases.
상세보기
Boissenin, Stéphane; Rosay, Jacques, Procedure and device for improving the maneuverability of an aircraft during the approach to landing and flare-out phases.
상세보기
Buchholz, Robert E.; Evans, Monte R.; Lee, Jonathan P.; Overton, Timothy G.; Thoreen, Adam M., Quiet landing attitude modifier for airplane.
상세보기
Chatrenet, Dominique; Mathieu, Gerard; Alonso, Fernando; Cart-Lamy, Martine, System for automatically controlling lift-augmentation devices of an aircraft during take-off.
상세보기
Delaplace,Franck; Buisson,Dominique, System for automatically controlling lift-enhancing devices of an aircraft, in particular wing leading edge slats.
상세보기

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
구성항목	기본정보 상세정보 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

연합인증

Automatic controls for airplane take-off and landing modes 원문보기

초록 ▼

대표청구항 ▼

연구과제 타임라인

이 특허를 인용한 특허 (18)

관련 콘텐츠

특허 원문 보기

IPC 상위 출원인

AI-Helper ※ AI-Helper는 오픈소스 모델을 사용합니다.

선택된 텍스트

연합인증

Automatic controls for airplane take-off and landing modes 원문보기

초록 ▼

대표청구항 ▼

연구과제 타임라인

전체(0) 논문(0) 특허(0) 보고서(0)

전체(0) 논문(0) 특허(0) 보고서(0)

이 특허를 인용한 특허 (18)

관련 콘텐츠

특허 원문 보기

IPC 상위 출원인

AI-Helper ※ AI-Helper는 오픈소스 모델을 사용합니다.

선택된 텍스트