[특허]Flush-mounted latching assembly

The Boeing Company

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특허 상세정보

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내보내기 페이스북 공유 트위터 공유 카카오톡 공유

Flush-mounted latching assembly

특허상세정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	E05C-019/00
미국특허분류(USC)	292/001; 292/DIG.37
출원번호	US-0198767 (2008-08-26)
등록번호	US-8201856 (2012-06-19)
발명자 / 주소	Etling, Keith A.
출원인 / 주소	The Boeing Company
대리인 / 주소	Armstrong Teasdale LLP
인용정보	피인용 횟수 : 0 인용 특허 : 18

초록

A latch assembly for a door is provided. The latch assembly includes a force actuated locking mechanism having a depressable actuator, a sleeve coupled to an inside surface of the door, wherein the sleeve includes a cylindrical opening configured to receive at least a portion of the force actuated locking mechanism therein and maintain the force actuated locking mechanism with respect to the door. The latch assembly also includes a flexible membrane oriented such that the depressable actuator is operable through the flexible membrane.

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1. A latch assembly for a door coupled to an aircraft skin, said assembly comprising: a force actuated locking mechanism comprising: a depressable actuator; anda flexible membrane, said depressable actuator operable through said flexible membrane; anda sleeve coupled to an inside surface of the skin, said sleeve comprising a cylindrical opening configured to receive at least a portion of said force actuated locking mechanism therein and maintain a position of said force actuated locking mechanism with respect to the door. 2. A latch assembly in accordance with claim 1, wherein said force actuating mechanism comprises a ball lock latch. 3. A latch assembly in accordance with claim 1, wherein the aircraft skin comprises an aperture, said force actuated mechanism substantially axially aligned with said aperture when received within said sleeve, said actuator at least partially received within said aperture. 4. A latch assembly in accordance with claim 3, wherein said force actuated locking mechanism comprises a flange configured to be received within a door aperture substantially axially aligned with said aperture of said aircraft skin. 5. A latch assembly in accordance with claim 1, wherein said flexible membrane is configured to form a seal around said latch assembly. 6. A latch assembly in accordance with claim 1, wherein said sleeve further comprises a flange extending radially outward from said sleeve, said receptacle flange coupled to an inside surface of the door. 7. A latch assembly in accordance with claim 1, further comprising a fairing compound comprising an aperture substantially axially aligned with said force actuated locking mechanism. 8. A latch assembly in accordance with claim 7, wherein said fairing compound is configured to form a substantially smooth surface between said flexible membrane and the door. 9. A system comprising: an aircraft skin;an access door including an aperture that extends between a door inner surface and a door outer surface; anda latch assembly comprising: a force actuated locking mechanism comprising: a depressable actuator; anda flexible membrane, said depressable actuator operable through said flexible membrane; anda sleeve coupled to an inside surface of the aircraft skin, said sleeve comprising a cylindrical opening configured to receive at least a portion of said force actuated locking mechanism therein and maintain a position of said force actuated locking mechanism with respect to the access door. 10. A system in accordance with claim 9, wherein said force actuating mechanism comprises a ball lock latch. 11. A system in accordance with claim 9, wherein said force actuated locking mechanism comprises a flange configured to be received within said aperture. 12. A system in accordance with claim 9, wherein said flexible membrane is configured to form a seal around said latch assembly. 13. A system in accordance with claim 9, wherein said sleeve comprises a flange extending radially outward from said sleeve, said receptacle flange coupled to said door inner surface. 14. A system in accordance with claim 9, further comprising a fairing compound comprising an aperture substantially axially aligned with said force actuated locking mechanism. 15. A system in accordance with claim 14, wherein said fairing compound is configured to form a substantially smooth surface between said flexible membrane and the door. 16. A method for fabricating a latch assembly for a door, the method comprising: extending an aperture between a door inner surface and a door outer surface;coupling a receptacle along the door inner surface, the receptacle configured to receive at least a portion of a force actuated locking mechanism therein;slidably inserting the force actuated locking mechanism into the receptacle;covering the door outer surface with a fairing compound such that the inserted force actuated locking mechanism is fixedly held within the receptacle; andforming a substantially smooth surface between a flexible membrane and one of the door inner surface and the door outer surface. 17. A method in accordance with claim 16, wherein forming a substantially smooth surface further comprises sealing the latch assembly within the receptacle such that the latch assembly is protected from external contaminants. 18. A method in accordance with claim 16, wherein coupling a receptacle along the door inside surface further comprises: extending a flange radially outward from a sleeve configured to receive the force actuated locking mechanism therein;coupling the flange to the door inner surface. 19. A method in accordance with claim 18, further comprising axially aligning the force actuated locking mechanism within the aperture. 20. A method for fabricating a latch assembly for an aircraft door, the method comprising: extending an aperture between a door inner surface and a door outer surface;axially aligning a force actuated locking mechanism within the aperture;coupling a receptacle along the door inside surface, the receptacle configured to receive at least a portion of a force actuated locking mechanism therein, and further comprising extending a flange radially outward from a sleeve configured to receive the force actuated locking mechanism therein;coupling the flange to the door inner surface;slidably inserting the force actuated locking mechanism into a receptacle coupled along the door inner surface;covering the door outer surface with a fairing compound such that the inserted force actuated locking mechanism is fixedly held within the receptacle; andforming a substantially smooth surface between a flexible membrane and one of the door inner surface and the door outer surface to facilitate sealing the latch assembly within the receptacle such that the latch assembly is protected from external contaminants.

이 특허에 인용된 특허 (18)

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Flush-mounted latching assembly

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이 특허에 인용된 특허 (18)

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특허 상세정보

Flush-mounted latching assembly

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이 특허에 인용된 특허 (18)

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