[특허]Control signal transmitting apparatus, particularly for aircraft

[미국특허] Control signal transmitting apparatus, particularly for aircraft 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	H04B-009/00
출원번호	US-0293277 (1981-08-17)
우선권정보	DE-3032918 (1980-09-02); DE-3111722 (1981-03-25)
발명자 / 주소	Wendt Hans J. (Buxtehude DEX)
출원인 / 주소	Messerschmitt-Boelkow-Blohm Gesellschaft mit beschraenkter Haftung (Munich DEX 03)
인용정보	피인용 횟수 : 40 인용 특허 : 1

초록 ▼

A control system for controlling, for example, the operation of an aircraft or any other system requiring a flow of data back and forth between controlling and controlled units of the system, comprises a passive, multiply intermeshed conductor network (20, 24) of light conductors (11, 12). This network transmits control signals in the form of digital light signals from a control signal source, such as a control stick (9) in the cockpit of an aircraft or spacecraft, to respective controlled servo-units (14). The transmission system includes signal processors (10) including mixers (15) and information devices (16, 17, 18) interposed between the control signal source and the network (24) which is connected to the addressable controlled units, e.g., servo-units. The system is powered by a power supply device comprising several energy sources which may be switched on selectively as required. Such energy sources include the propulsion plant, for example, of an aircraft, an auxiliary turbine (112), a slip wind turbine (120) and an electric battery (128). Each energy source is connected to a measuring and switching unit (106, 115, 124, 131) through redundant transmission units (110) three of which are connected in parallel to one another and to the network (24). The transmission units (110) are further connected through the network (24) to a testing device (135) for monitoring and controlling the connected units or components.

대표청구항 ▼

In a system for transmitting control signals from a control source providing controlling signals to controlled units through signal light conductor network means operatively interconnecting said control source and said controlled units, wherein a number of light conductors form redundant connection paths between said control source and said controlled units, the improvement comprising a first plurality of longitudinal light conductors and a further plurality of cross light conductors repeatedly intermeshing said longitudinal light conductors for forming said light conductor network means with a multitude of passive closed circuit paths intermeshed with one another so that controlling signals can pass from said control source to a controlled unit even if some of these circuit paths should fail, said control source comprising means for producing said controlling signals in the form of digital light signals, signal processor means (10) including signal mixing means (15) and information processing means (16, 17, 18) operatively connected to said light conductor network means for addressing and actuating said controlled units.

이 특허에 인용된 특허 (1) 인용/피인용 타임라인 분석

Martin ; Donald L. ; Yanke ; David B., Signal selection apparatus for redundant signal sources.
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이 특허를 인용한 특허 (40) 인용/피인용 타임라인 분석

Bernier, Alan T., Aircraft electrical power distribution network.
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Richter, Martin; Lücken, Peter, Aircraft having a vertical lift system.
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Najmabadi Kioumars ; Evans Monte R. ; Coleman Edward E. ; Bleeg Robert J. ; Breuhaus Richard S. ; Anderson Dorr Marshall ; Nelson Timothy A., Aircraft pitch-axis stability and command augmentation system.
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Stoner, Paul Douglas, Apparatus and method pertaining to light-based power distribution in a vehicle.
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Stoner, Paul Douglas; Vlad, Ovidiu Gabriel, Apparatus and method pertaining to light-based power distribution in a vehicle.
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Stoner, Paul Douglas; Vlad, Ovidiu Gabriel, Apparatus and method pertaining to provision of a substantially unique aircraft identifier via a source of power.
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Zavidniak, Martin P.; Shabra, Dale J., Communication system and method employing line replaceable equipment racks on an aircraft.
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De Rammelaere, Werner; Laperche, Jean-Claude; Rebut, Mathieu; Berthe, Benoit; Hintze, Hartmut; Krittian, Sebastian, Control system for an aircraft.
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Brownjohn, Nicholas; Osternack, Stefan; Poulain, Stéphane; Valancogne, Xavier; Fischer, Nils, Data network, aircraft or spacecraft, and method.
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Tichborne, Franklin; Lam, Joseph K-W; Masters, Simon; Parmenter, David, Data transmission network.
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Schievelbusch, Bernd, Device for detecting synchronous errors of high-lift surfaces on aircraft.
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Szuchy Nicholas C. (Babylon NY) Caserta Anthony (Huntington NY), Discrete strain sensor.
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Rizzotti ; III Alfred E. (New Rochelle NY), Electrical control system.
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Szuchy Nicholas C. (Babylon NY), Fiber optic aircraft load relief control system.
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Vidal Pierre-Albert,FRX ; Woirin Eddy Gaston Jean,FRX ; Massimi Jean-Maxime,FRX ; Ressent Philippe Louis,FRX, Flight control device for an aircraft, in particular a helicopter.
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Foote, Peter David; Stace, Christopher; Laycock, Leslie Charles, Heat distribution in a distributed lighting apparatus.
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Endicott,Eric, High density fiber optic output interface and system.
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Ivie,Lovell Brent; Gilstrap,Daniel; Howard,R. Brent; Bowden,Grant; Johnson,Dave, Information communication systems.
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Oyama Masumi (Tokyo JPX), Information medium for communicating data and/or a selectable control transfer program between the medium end and extern.
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Mitani, Yoichi; Tamaru, Masahiro; Ikarashi, Reiichi; Isobe, Taisei, Integrated electronic system mounted on aircraft.
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Stirling, Andrew J.; Pendergast, Simon E.; Parmar, Harivaden A., Local communication system.
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Elberbaum, David, Method and apparatus for connecting AC powered switches, current sensors and control devices via two way IR, fiber optic and light guide cables.
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Elberbaum, David, Method and apparatus for connecting AC powered switches, current sensors and control devices via two way IR, fiber optic and light guide cables.
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Elberbaum, David, Method and apparatus for connecting AC powered switches, current sensors and control devices via two way IR, fiber optic and light guide cables.
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Stoner, Paul Douglas, Method and apparatus for handling data and aircraft employing same.
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Stoner, Paul Douglas; Vlad, Ovidiu Gabriel, Method and apparatus for handling data and aircraft employing same.
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Hoy Robert S. ; Grai Timothy J. ; Hozeska Robert J., Method of non-intrusive testing for a process control interface system having triply redundant remote field units.
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Roth, Michael, System, apparatus and method for controlling an aircraft.
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Griffith, Scot E., Systems and methods for arbitrating sensor and actuator signals in a multi-channel control system.
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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] Control signal transmitting apparatus, particularly for aircraft 원문보기

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[미국특허] Control signal transmitting apparatus, particularly for aircraft 원문보기

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이 특허에 인용된 특허 (1) 인용/피인용 타임라인 분석

이 특허를 인용한 특허 (40) 인용/피인용 타임라인 분석

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