ATE490908T1 - JOINT COVERING IN AIRPLANES - Google Patents
JOINT COVERING IN AIRPLANESInfo
- Publication number
- ATE490908T1 ATE490908T1 AT05022132T AT05022132T ATE490908T1 AT E490908 T1 ATE490908 T1 AT E490908T1 AT 05022132 T AT05022132 T AT 05022132T AT 05022132 T AT05022132 T AT 05022132T AT E490908 T1 ATE490908 T1 AT E490908T1
- Authority
- AT
- Austria
- Prior art keywords
- cover
- gap
- aircraft
- airplanes
- elements
- Prior art date
Links
- 239000013013 elastic material Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/066—Interior liners
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Plates (AREA)
- Sealing Devices (AREA)
- Diaphragms And Bellows (AREA)
- Tires In General (AREA)
Abstract
The cover for a gap (5) between a first (3) and a second (4) element in an aircraft has a cover section (2) to cover the gap, and a clamping element (6) for the fastening of the cover on a third element in such a way that the first and second elements are movable relative to one another. The first and second elements are interior components of an aircraft. The cover section consists of an elastic material and in the relaxed state has a curvature. After the assembly of the cover in the gap the cover section lies on the front side on the first and second element under tension. Independent claims are also included for the following: (A) a use for the gap cover which is in an aircraft; and (B) an aircraft equipped with the aforesaid gap cover.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US61813004P | 2004-10-13 | 2004-10-13 | |
| DE102004049893A DE102004049893B4 (en) | 2004-10-13 | 2004-10-13 | Joint cover in aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE490908T1 true ATE490908T1 (en) | 2010-12-15 |
Family
ID=36128779
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT05022132T ATE490908T1 (en) | 2004-10-13 | 2005-10-11 | JOINT COVERING IN AIRPLANES |
Country Status (2)
| Country | Link |
|---|---|
| AT (1) | ATE490908T1 (en) |
| DE (2) | DE102004049893B4 (en) |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102006017241B4 (en) | 2006-04-12 | 2017-11-23 | Airbus Operations Gmbh | Level gap cover for cabin linings |
| DE102007013904A1 (en) | 2007-03-22 | 2008-09-25 | Airbus Deutschland Gmbh | Spaltabdeckvorrichtung |
| US7578453B1 (en) | 2008-02-15 | 2009-08-25 | Kohler Co. | Handshower assembly |
| DE102008061381A1 (en) * | 2008-12-10 | 2010-06-24 | Siemens Aktiengesellschaft | Interior trim of a vehicle |
| DE102011120762A1 (en) | 2011-12-09 | 2013-06-13 | Airbus Operations Gmbh | Cover device and aircraft area with cover device |
| US9180823B2 (en) * | 2013-05-15 | 2015-11-10 | Embraer S.A. | Adaptive decorative trim assemblies for vehicle cabin interiors |
| DE102017125299A1 (en) | 2017-10-27 | 2019-05-02 | Airbus Operations Gmbh | Gap cover between cabin monuments, in particular for a passenger cabin of an aircraft |
| DE102019119558A1 (en) * | 2019-07-18 | 2021-01-21 | Recaro Aircraft Seating Gmbh & Co. Kg | Sealing device |
| EP4461637A1 (en) | 2023-05-12 | 2024-11-13 | Airbus Operations GmbH | A cover for a transition from a lining to a monument |
| EP4524031A1 (en) * | 2023-09-12 | 2025-03-19 | Airbus Operations GmbH | Aircraft interior lining arrangement, longitudinal gap cover, interior panel and installation method |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4067155A (en) * | 1975-08-28 | 1978-01-10 | Grefco, Inc. | Sealing system |
| US5014934A (en) * | 1989-06-30 | 1991-05-14 | The Boeing Company | Removable seal for discontinuities in aircraft skin |
| US5065960A (en) * | 1990-02-05 | 1991-11-19 | Northrop Corporation | Gap filler for advanced aircraft to reduce radar detectability |
| GB2287517B (en) * | 1994-03-14 | 1997-04-30 | Kenneth Barry Wilson | Panel assembly system |
| DE9406302U1 (en) * | 1994-04-18 | 1995-05-18 | ABET GmbH, 32051 Herford | Trim part for vehicles or airplanes |
| US5695154A (en) * | 1995-08-21 | 1997-12-09 | Northrop Grumman Corporation | Gap filler device |
| DE19709374C2 (en) * | 1997-03-07 | 1999-06-02 | Daimler Chrysler Aerospace | Fastening device for fixing ceiling components in an aircraft |
| US6712316B2 (en) * | 2002-08-01 | 2004-03-30 | The Boeing Company | Snap-on sidewall assembly |
-
2004
- 2004-10-13 DE DE102004049893A patent/DE102004049893B4/en not_active Expired - Fee Related
-
2005
- 2005-10-11 DE DE502005010646T patent/DE502005010646D1/en not_active Expired - Lifetime
- 2005-10-11 AT AT05022132T patent/ATE490908T1/en active
Also Published As
| Publication number | Publication date |
|---|---|
| DE102004049893A1 (en) | 2006-04-27 |
| DE502005010646D1 (en) | 2011-01-20 |
| DE102004049893B4 (en) | 2010-07-01 |
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