[미국특허]
Locking device comprising a telescopic connecting rod equipped with return means
원문보기
IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0673912
(2008-08-12)
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등록번호 |
US-8641370
(2014-02-04)
|
우선권정보 |
FR-07 05938 (2007-08-20) |
국제출원번호 |
PCT/EP2008/060586
(2008-08-12)
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§371/§102 date |
20110329
(20110329)
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국제공개번호 |
WO2009/043635
(2009-04-09)
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발명자
/ 주소 |
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출원인 / 주소 |
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대리인 / 주소 |
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인용정보 |
피인용 횟수 :
1 인용 특허 :
4 |
초록
▼
The present invention relates to a locking device (10) designed to fixedly attach a first element (9a) to a second element, comprising a locking member (12) intended to equip the first element, an additional locking element intended to equip the second element, and a control handle (13) connected to
The present invention relates to a locking device (10) designed to fixedly attach a first element (9a) to a second element, comprising a locking member (12) intended to equip the first element, an additional locking element intended to equip the second element, and a control handle (13) connected to the locking member via transmission means, characterized in that the transmission means comprise a telescopic connecting rod (15) designed to oscillate freely between a minimum extension position and a maximum extension position, and means for returning the telescopic connecting rod to its position of maximum extension, said return means being placed in a prestressed state when the control handle is in the closure position.
대표청구항
▼
1. A locking device designed for fixedly attaching a first element to a second element, said locking device comprising: a locking member intended for equipping the first element,a complementary locking member intended for equipping the second element, anda control handle connected to the locking mem
1. A locking device designed for fixedly attaching a first element to a second element, said locking device comprising: a locking member intended for equipping the first element,a complementary locking member intended for equipping the second element, anda control handle connected to the locking member by transmission means, characterized in thatwherein the transmission means comprise a telescopic connecting rod designed to oscillate freely between a position of minimum extension and a position of maximum extension and, on the-other-hand, means for the return of the telescopic connecting rod toward a position of maximum extension, said return means being placed in a prestressed state when the control handle is in the closing position. 2. The locking device as claimed in claim 1, wherein the telescopic connecting rod comprises a first rod fitted into a second rod. 3. The locking device as claimed in claim 2, wherein the return means comprise at least one spring integrated in the telescopic connecting rod. 4. The locking device as claimed in claim 3, thatwherein the spring has a first end fastened in an end of the first rod fitted in the second rod, and a second end fastened in the second rod. 5. The locking device as claimed in claim 2, wherein a pin fastened transversely in the second rod passes through two slots formed in a lateral surface of the first rod. 6. The locking device as claimed in claim 1, wherein the control handle is designed so as to be capable of being displaced alternately from a stable opening position, in which the locking member is open, to a stable locking position, in which the locking member is closed, passing through an unstable intermediate phase where the locking member is closed. 7. The locking device as claimed in claim 6, wherein the return member is designed so as to be capable, during the intermediate phase, of returning the control handle in the direction of its opening position if said control handle is freed of any external stress. 8. A turbojet engine nacelle comprising: a front air inlet section,a middle section intended for surrounding a blower of the turbojet engine, anda rear section formed from at least two half-shells held in a closing position by means of locking assemblies arranged along a junction line located in the lower part,wherein at least one of these locking assemblies comprises a locking device as claimed in claim 1. 9. The turbojet engine nacelle (1) as claimed in claim 8, wherein at least the locking device is arranged in front of the junction line. 10. An aircraft, comprising at least one nacelle as claimed in claim 8.
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Melcher Joseph C. (Auburn WA), Apparatus for latching two parts together.
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Daniels Dyrk L., Counterbalance mechanism for inwardly and upwardly opening plug-type airplane cargo doors.
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Norris, James R., Cowling latch system.
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Bourne William R. ; Dessenberger Arthur W. ; Jackson Frank T., Extended reach latch.
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Mercier, Claude, Latching actuation mechanism for nacelle mounted latching system.
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