Mounting system for attaching a box in a compartment of an aircraft galley
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
E05B-065/46
B64D-011/04
출원번호
US-0140772
(2009-11-23)
등록번호
US-9199738
(2015-12-01)
우선권정보
DE-10 2008 064 084 (2008-12-19)
국제출원번호
PCT/EP2009/008327
(2009-11-23)
§371/§102 date
20110926
(20110926)
국제공개번호
WO2010/078885
(2010-07-15)
발명자
/ 주소
Tan, Joyce
Pangalila, Iwan
Henshaw, Robert
출원인 / 주소
Airbus Operations GmbH
대리인 / 주소
Taft Stettinius & Hollister LLP
인용정보
피인용 횟수 :
0인용 특허 :
2
초록▼
A mounting system (10) for attaching a box (14) in a compartment (12) of an aircraft galley comprises a first guide device set up for engaging with a complementary second guide device designed on the box (14) when the box (14) is inserted into the compartment (12) of the aircraft galley, and further
A mounting system (10) for attaching a box (14) in a compartment (12) of an aircraft galley comprises a first guide device set up for engaging with a complementary second guide device designed on the box (14) when the box (14) is inserted into the compartment (12) of the aircraft galley, and further set up for securing the box (14) against movement in the compartment (12) of the aircraft galley in a direction (P) perpendicular to a longitudinal axis (L) of the compartment (12) of the aircraft galley when the device is engaged with the complementary second guide device designed on the box (14). The mounting system (10) further comprises a locking mechanism set up for securing the box (14) against movement in the compartment (12) of the aircraft galley in a direction parallel to the longitudinal axis (L) of the compartment (12) of the aircraft galley.
대표청구항▼
1. A mounting system for attaching a box in a compartment of an aircraft galley, comprising: a first guide device on the mounting system formed by an elongate rail extending in a longitudinal direction along a bottom of the compartment with recessed cavities formed on either side thereof,a second gu
1. A mounting system for attaching a box in a compartment of an aircraft galley, comprising: a first guide device on the mounting system formed by an elongate rail extending in a longitudinal direction along a bottom of the compartment with recessed cavities formed on either side thereof,a second guide device connected along the bottom of the box having a pair of projections formed on either side thereof;wherein the projections and the recessed cavities are complementary in shape such that second guide device slidingly engages within the elongate rail of the first guide device when box is inserted into or removed from the compartment of the aircraft galley;wherein engagement of the first and second guide devices permits movement of the box only along the longitudinal direction within the compartment of the aircraft galley;a locking mechanism for selectively securing the box against movement in the compartment of the aircraft galley in the longitudinal direction; andan unloading device having an actuating handle and a slider connected to the actuating handle being displaceable parallel to the longitudinal direction in the compartment of the aircraft galley, wherein the slider is constructed with a portion to engage with a rear wall of the box to slide the box out of the compartment of the aircraft galley and the first and second guide devices are no longer engaged when the unloading device is actuated. 2. Mounting system according to claim 1, characterized in that the first guide device is disposed on a carrier element, which is devised to support a base element of the box when the first guide device is in engagement with the complementary second guide device formed on the box. 3. Mounting system according to claim 1, characterized in that the first guide device and the complementary second guide device formed on the box form a dovetail joint. 4. Mounting system according to claim 1, characterized in that the locking mechanism comprises a first locking unit having a first number of bars, wherein the bars of the first locking unit are devised in a locking position to secure a number, corresponding to the first number of bars, of boxes accommodated one behind the other in the compartment of the aircraft galley against movement in the compartment of the aircraft galley in a direction parallel to the longitudinal axis of the compartment of the aircraft galley. 5. Mounting system according to claim 4, characterized in that the first locking unit comprises a coupling device, which couples the bars of the first locking unit in such a way to one another that upon a movement of a first bar into a locking position the remaining bars are likewise moved into a locking position and that upon a movement of the first bar into an unlocking position the remaining bars are likewise moved into an unlocking position. 6. Mounting system according to claim 4, characterized in that the first and/or the second locking unit comprises/comprise a blocking mechanism and is/are movable between a first and a second position, wherein the blocking mechanism in the first position of the first and/or the second locking unit enables a movement of a bar of the first and/or the second locking unit into a locking position and in the second position of the first and/or the second locking unit blocks a movement of the bar of the first and/or the second locking unit into a locking position. 7. Mounting system according to claim 6, characterized in that the blocking mechanism of the first locking unit comprises at least one blocking projection, which in the second position of the first locking unit interacts in such a way with a bar of the first locking unit that a movement of the bar into a locking position is blocked and which in the first position of the first locking unit upon a movement of the bar into a locking position is received in a recess that is formed in the bar. 8. Mounting system according to claim 6, characterized in that the blocking mechanism of the second locking unit comprises at least one blocking projection, which in the second position of the second locking unit interacts in such a way with a bar of the second locking unit that a movement of the bar into a locking position is blocked and which in the first position of the second locking unit upon a movement of the bar into a locking position is received in a recess that is formed in the bar. 9. Mounting system according to claim 6, characterized in that the first and the second locking unit are connected to one another by a transmission, which is devised to move the second locking unit into its second position, in which the blocking mechanism of the second locking unit blocks a movement of a bar of the second locking unit into a locking position, when the first locking unit is moved into its first position, in which the blocking mechanism of the first locking unit enables a movement of a bar of the first locking unit into a locking position, and which is further devised to move the first locking unit into its second position, in which the blocking mechanism of the first locking unit blocks a movement of a bar of the first locking unit into a locking position, when the second locking unit is moved into its first position, in which the blocking mechanism of the second locking unit enables a movement of a bar of the second locking unit into a locking position. 10. Mounting system according to claim 9, characterized in that the transmission comprises a lever, which is pivotable about a centre line and is connected at a first end to the first locking unit and at a second end to the second locking unit, so that a linear movement of the first locking unit in a first direction is converted by the lever into a movement of the second locking unit in a second, opposite direction to the first direction. 11. Mounting system according to claim 6, characterized in that the mounting system further comprises a detection device for detecting the size of a box accommodated in the compartment of the aircraft galley as well as an actuating device, wherein the actuating device is devised in dependence upon the size, detected by the detection device, of the box accommodated in the compartment of the aircraft galley to move either the first or the second locking unit into its first position, in which the blocking mechanism of the first or the second locking unit enables a movement of a bar of the first and/or the second locking unit into a locking position. 12. Mounting system according to claim 1, characterized in that the locking mechanism comprises a second locking unit having a second number of bars, wherein the bars of the second locking unit are devised in a locking position to secure a number, corresponding to the second number of bars, of boxes accommodated one behind the other in the compartment of the air-craft galley against movement in the compartment of the aircraft galley in a direction parallel to the longitudinal axis of the compartment of the aircraft galley. 13. Mounting system according to claim 12, characterized in that the second locking unit comprises a coupling device, which couples the bars of the locking unit in such a way to one another than upon a movement of a first bar into a locking position the remaining bars are likewise moved into a locking position and that upon a movement of the first bar into an unlocking position the remaining bars are likewise moved into an unlocking position. 14. Aircraft galley comprising: a basic body, in which at least one compartment for receiving a box is formed, anda mounting system according to claim 1.
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이 특허에 인용된 특허 (2)
Resch ; Jr. Alvin Charles (Two Rivers WI), Gang luck assembly for cabinet drawers.
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