[특허]Aircraft takeoff monitoring system

[미국특허] Aircraft takeoff monitoring system 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	G08B-021/00
출원번호	US-0480963 (1990-02-16)
발명자 / 주소	Arad Ady (P.O. Box 6408 FDR Station New York NY 10150)
인용정보	피인용 횟수 : 17 인용 특허 : 0

초록 ▼

The displays are provided for assisting a pilot in making critical decisions during the takeoff roll of the aircraft. The first of the displays includes four pointers which indicate, respectively, the maximum available acceleration of the aircraft, the minimum acceleration required to achieve a velocity V2 at 35 feet above the end of the runway with all engines operating, the minimum required acceleration which will allow the aircraft to accelerate to a critical velocity with all engines operating and complete a legal takeoff after loss of an engine at the critical velocity (V1), and the actual acceleration of the aircraft. The second display indicates the ability of the aircraft to safely complete the takeoff if an engine were to fail and the ability of the aircraft to stop safely if the pilot were to decide to abort the takeoff. The second display includes first and second sets of colored lights indicating clearly safe and unsafe conditions and a marginally safe condition for the continued takeoff and abort situations. The displays are driven by a microprocessor which is supplied with both specific and generalized data for the aircraft such that the variety of factors to be displayed can be calculated.

대표청구항 ▼

Apparatus for assisting a pilot of an aircraft during a takeoff roll on a runway comprising a display panel, maximum available acceleration indicator means (4) on said panel representing the maximum available acceleration of the aircraft, actual acceleration indicator means (6) on said panel for continuously indicating the real-time, actual acceleration of the aircraft, first minimum required acceleration indicator means (10) on said panel for continuously indicating the real-time minimum acceleration of the aircraft required to reach a critical velocity at a real time position on the runway, means for continuously determining the real time position on the runway, said real time position on the runway being continuously subject to change depending on changing conditions during the takeoff roll, and second minimum required acceleration indicator means (8) or continuously indicating the real-time minimum acceleration required to reach said critical velocity with all engines of the aircraft operating, to lose an engine at said critical velocity, and to complete a legal takeoff with said one engine inoperative.

이 특허를 인용한 특허 (17) 인용/피인용 타임라인 분석

Millard Wayne C.,CAX ; Millard Carl W.,CAX ITX L5S 1B2, Aircraft takeoff acceleration indicator system.
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Millard Wayne C.,CAX ; Millard Carl W,CAXITX L5S 1B2, Aircraft takeoff velocity indicator system.
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Palmer Steven D., Apparatus for measuring lift forces based upon differential pressure between surfaces of an aircraft.
상세보기
Ian Amos CA, Apparatus to calculate dynamic values for pressure density in an aircraft.
상세보기
Naimer, Hubert; Krohn, Patrick Gerald; Glaze, Patrick Kemp; Jorgensen, John Russell, Display generation system.
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Naimer, Hubert; Krohn, Patrick Gerald; Glaze, Patrick Kemp; Jorgensen, John Russell, Display generation system.
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Chen,Yu; Liu,Yun Ping; Chen,Sung Yuan; Chin,Min Chih, Display processing switching construct utilized in information device.
상세보기
Johnson, Steve; Ishihara, Yasuo; Conner, Kevin J, Flight deck display systems and methods for visually indicating low speed change conditions during takeoff and landing.
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Shaw, Robert L., Low cost flight instrumentation system.
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Palmer Steven D., Method and apparatus for flight parameter monitoring and control.
상세보기
Palmer Steven D., Method and apparatus for measuring forces based upon differential pressure between surfaces of an aircraft.
상세보기
Lemoult, Frederic; Demortier, Jean-Pierre; Pitard, Fabien; Betouret, Damien; Marani, Frederic; Lacaze, Isabelle; De Menorval, Jean-Louis; Marchand, Gael; Ott, Adrien; Wachenheim, Maxime, Method for detecting an error in input of one of the takeoff parameters into a flight management system.
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Palmer Steven D., Method for flight parameter monitoring and control.
상세보기
Burns, Timothy Donal Paul; Gannon, Aaron James; Kolbe, Dashiell Matthews; Wargacki, Darrin Walter; Moeller, Gerhard Walter, Methods for derated thrust visualization.
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Villaume,Fabrice; Godard,Eric; Chabe,David, Process and device for aiding the driving of a vehicle running over the ground.
상세보기
Horne, Thomas; Landers, Thomas; Mayo, John, Runway takeoff monitor.
상세보기
Gurusamy, Saravanakumar; Karmakar, Nirupam; Malviya, Pramod Kumar; Krishnamurthy, Prithvi, System and method of displaying airspeed information for an aircraft.
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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

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[미국특허] Aircraft takeoff monitoring system 원문보기