Device for the recognition of residual synchronization errors of multiple slats of flaps placed next to each other in aircraft
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
G01R-031/00
G01R-031/08
B64C-009/28
출원번호
US-0445417
(2003-05-27)
우선권정보
DE-0023495 (2002-05-27)
§371/§102 date
20040428
(20040428)
발명자
/ 주소
Schievelbusch, Bernd
Winkelmann, Christoph
출원인 / 주소
Liebherr-Aerospace Lindenberg GmbH
대리인 / 주소
Dilworth&
인용정보
피인용 횟수 :
4인용 특허 :
7
초록▼
A device for the recognition of residual synchronization errors of multiple slats or flaps placed next to each other in an aircraft. The device includes a current carrying wire that runs through the slats or flaps. This wire is fastened at one end in the area of the gap between the slats or flaps an
A device for the recognition of residual synchronization errors of multiple slats or flaps placed next to each other in an aircraft. The device includes a current carrying wire that runs through the slats or flaps. This wire is fastened at one end in the area of the gap between the slats or flaps and, on the other side, run through a cutting device. A detector can be used to detect and indicate the change in resistance when the wire is cut.
대표청구항▼
1. Device for the recognition of residual synchronization errors of multiple slats or flaps placed next to each other in aircraft,characterized in that, a current-carrying wire is fed through the slats or flaps arranged next to each other, where such wire is fastened at one end in the area of the ga
1. Device for the recognition of residual synchronization errors of multiple slats or flaps placed next to each other in aircraft,characterized in that, a current-carrying wire is fed through the slats or flaps arranged next to each other, where such wire is fastened at one end in the area of the gap between the slats or the flaps and on the other side fed through a cutting device and that, by means of a detector, the change in resistance can be detected when the wire is cut. 2. Device according to claim 1, characterized in that, the cutting device consists of an annular cutter.3. Device according to claim 2, characterized in that, the distance between wire and the cutter is selected in such a manner that the relative movement caused by wing flexing and installation tolerances between the slats or flaps arranged next to each other does not cause the wire to be cut.4. Device according to claim 3, characterized in that, the fastening of the wire at one end is done with at least one clamping screw.5. Device according to claim 2, characterized in that, the fastening of the wire at one end is done with at least one clamping screw.6. Device according to claim 1, characterized in that, the distance between wire and the cutter is selected in such a manner that the relative movement caused by wing flexing and installation tolerances between the slats or flaps arranged next to each other does not cause the wire to be cut.7. Device according to claim 6, characterized in that, the fastening of the wire at one end is done with at least one clamping screw.8. Device according to claim 6, wherein said wire extends across the gap or interval between adjacent flaps.9. Device according to claim 8, wherein said cutting device is mounted upon each said flap except an initial flap.10. Device according to claim 6, wherein said cutting device is mounted upon each said flap except an initial flap.11. Device according to claim 1, characterized in that, the fastening of the wire at one end is done with at least one clamping screw.12. Device according to claim 1, wherein said cutting device is situated on a sidewall of a flap.13. Device according to claim 12, wherein said flap sidewall comprises a bushing through which said wire runs and upon which said cutting device, which is constituted by an annular cutter, is mounted.14. Device according to claim 13, additionally comprising a bushing mounted upon a sidewall of an adjacent flap and through which said wire runs, such that said wire is cut when said adjacent flaps fail to move with synchronicity.15. Device according to claim 14, wherein said wire is secured to said adjacent flap by at least one clamping screw extending through said respective bushing.16. Device according to claim 13, wherein said wire extends across the gap or interval between adjacent flaps.17. Device according to claim 16, wherein said cutting device is mounted upon each said flap except an initial flap.18. Device according to claim 1, wherein said wire extends across the gap or interval between adjacent flaps.19. Device according to claim 18, wherein said cutting device is mounted upon each said flap except an initial flap.20. Device according to claim 1, wherein said cutting device is mounted upon each said flap except an initial flap.
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이 특허에 인용된 특허 (7)
Caferro Joseph S. (Seattle WA) Tomassi Hector V. (Renton WA), Auxiliary airfoil lost motion detector and actuator.
Lindstrom Jeffrey V. ; Reed R. David ; Platin Bradley E. ; Beyer Kevin W. ; Reusch David C., Method and apparatus for detecting skew and asymmetry of an airplane flap.
Moy, George; Padilla, Peter Angel; Renzelmann, Michael Edward; Gardner, Mark J.; Jokisch, Charles E.; Hanna, William Suhail; Selby, Eric J.; Barr, Mark A.; Amorosi, Stephen Roger, Slat skew detection system.
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