IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0399172
(2009-03-06)
|
등록번호 |
US-8118258
(2012-02-21)
|
우선권정보 |
DE-10 2008 013 790 (2008-03-12) |
발명자
/ 주소 |
- Mosler, Michael
- Neumann, Andreas
- Landes, Benjamin
|
출원인 / 주소 |
|
대리인 / 주소 |
Lerner, David, Littenberg, Krumholz & Mentlik, LLP
|
인용정보 |
피인용 횟수 :
3 인용 특허 :
16 |
초록
▼
The invention relates to a separation element for separating a first space from a second space in an aircraft. The separation element can be affixed between a ceiling region of the cabin, a hatrack in the ceiling region of the cabin, and between a movable space separation device. Furthermore, as a r
The invention relates to a separation element for separating a first space from a second space in an aircraft. The separation element can be affixed between a ceiling region of the cabin, a hatrack in the ceiling region of the cabin, and between a movable space separation device. Furthermore, as a result of attachment between the ceiling region, the hatrack and the movable space separation device, the separation element is connectable in a lightproof manner to the ceiling region, and in a lightproof manner to the hatrack. Furthermore, the separation element is designed in such a manner that it is connectable in a lightproof manner to the movable space separation device.
대표청구항
▼
1. A separation element for creating a first space and a second space in an aircraft having a hatrack associated with a suspension device, the separation element comprising: a first edge having a first edge surface conforming to the suspension device;a second edge having a second edge surface confor
1. A separation element for creating a first space and a second space in an aircraft having a hatrack associated with a suspension device, the separation element comprising: a first edge having a first edge surface conforming to the suspension device;a second edge having a second edge surface conforming to the hatrack;wherein, when the separation element is installed in the aircraft, the first edge and the second edge reduce the propagation of light between the first space and the second space and the hatrack and the suspension device;a covering hood associated with the second edge, the covering hood covering at least a portion of the hatrack when the separation element is installed such that it is ensured that opening of the hatrack is no longer possible. 2. The separation element of claim 1, wherein the first edge comprises a geometrically variable sealing medium forming the first edge surface, the first edge surface having a positive fit with the suspension device. 3. The separation element of claim 2, wherein the geometrically variable sealing medium reduces light propagation between the first space and the second space during relative movement of the separation element and the suspension device. 4. The separation element of claim 1, wherein the second edge comprises a geometrically variable sealing medium forming the second edge surface, the second edge surface having a positive fit with the hatrack device. 5. The separation element of claim 4, wherein the geometrically variable sealing medium reduces light propagation between the first space and the second space during relative movement of the separation element and the hatrack device. 6. The separation element of claim 4, wherein the first geometrically variable sealing medium and the second geometrically variable sealing medium are the same mediums. 7. The separation element of claim 1, wherein the first edge comprises a first geometrically variable sealing medium forming the first edge surface and the second edge comprises a second geometrically variable sealing medium forming the second surface. 8. The separation element of claim 1, wherein the separation element further includes a separation device, the separation element further comprising a third edge conforming to the separation device. 9. The separation element of claim 1, wherein a contour of the covering hood conforms to a contour of the hatrack and the second edge of the separation element. 10. The separation element of claim 1, wherein the separation element is formed from two spaced apart parallel elements. 11. A separation system for separating a space of an aircraft into a first space and a second space at a position where the aircraft includes a suspension device of a moveable space separation device, the separation system comprising: a separation element;a covering hood;the separation element comprising a first edge having a first edge surface conforming to the suspension device of the moveable space separation device;the separation element comprising a second edge having a second edge surface conforming to the hatrack;the separation element comprising a third edge having a third a third edge surface conforming to the movable space separation device;wherein a contour of the covering hood conforms to the second edge of the separation element;wherein the covering hood is either integrated in the hatrack as a replacement of a hatrack flap or is installed on an existing hatrack such that it is ensured that opening of the hatrack is no longer possible, andwherein the contour of the covering hood closes off, having positive fit, with the contour of the second edge surface of the separation element in such a manner that propagation of light between the first space and the second space is reduced. 12. The separation system of claim 11, wherein said first edge is formed from a geometrically variable sealing medium to seal the edge against the suspension device and the second edge is formed from a geometrically variable sealing medium to seal the second edge against the hatrack. 13. The separation system of claim 11, comprising a separation device, wherein the separation device is moveable. 14. The separation system of claim 11, comprising a separation device, wherein the separation device is one of a wall and a curtain. 15. The separation system of claim 11, wherein the hatrack includes an opening mechanism covered by the hood. 16. The separation system of claim 11, wherein the separation system further comprises a partition element, the partition element extending into the hatrack orthogonally to the contour of the hood. 17. An aircraft comprising: a fuselage having a longitudinal axis;a suspension device associated with the fuselage;a hatrack supported by the suspension device, the hatrack extending along the longitudinal axis of the aircraft;a separation element, the separation element separating the fuselage into a first space and a second space, the separation element having a first surface associated with the suspension device and a second surface associated with the hatrack, the two surfaces inhibiting the propagation of light between the first space and the second space between the suspension device and the hatrack;a covering hood associated with the separation element, the covering hood covering at least a portion of the hatrack when the separation element is installed such that it is ensured that opening of the hatrack is no longer possible. 18. The aircraft of claim 17, further comprising a separation device, the separation device aligned transverse to said longitudinal axis of said fuselage, the separation device associated with a third surface of said separation element.
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