CN205916334U - Civil aviation aircraft cabin screen subassembly - Google Patents
Civil aviation aircraft cabin screen subassembly Download PDFInfo
- Publication number
- CN205916334U CN205916334U CN201620927004.9U CN201620927004U CN205916334U CN 205916334 U CN205916334 U CN 205916334U CN 201620927004 U CN201620927004 U CN 201620927004U CN 205916334 U CN205916334 U CN 205916334U
- Authority
- CN
- China
- Prior art keywords
- curtain
- main cabin
- fastener
- snap
- commercial aircraft
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
The utility model provides a civil aviation aircraft cabin screen subassembly, includes: well screen, side screen to and bonding fixing device. Service area and main cabin passenger district before the main cabin can effectively be separated in well screen (1) and side screen (2) of redesign installation, satisfies the requirement of security and airworthiness, has saved the dear cost of other purchase compartment, locker simultaneously, has improved the space of preceding service area and has felt and the comfort level.
Description
Technical field
The present invention relates to a kind of commercial aircraft main cabin curtain assembly.
Background technology
In aircraft, generally existing the curtain assembly installed, and reaches each service area of separation, or separates first-class cabin, commercial affairs
Cabin and the purpose of economy class.Service area before aircraft is separated with back occupant area, commonly used is arranged as: left side passenger
Dividing plate/compartment or locker are installed before area, central gangway (facilities such as kitchen are typically installed on right side) installs every curtain.But
For the improved science and technology removing first-class cabin, business class and all becoming economy class, because seat becomes many, former locker and dividing plate
Cannot install in the original location it is therefore desirable to install curtain assembly additional in aircraft forward.
Content of the invention
The present invention is in order to overcome the shortcomings of above technology, there is provided a kind of avoid installing extra genuine dividing plate/compartment or
The commercial aircraft main cabin curtain assembly of locker.
The present invention overcomes its technical problem be the technical scheme is that
A kind of commercial aircraft main cabin curtain assembly, comprising:
In every curtain, its upper end is slidably mounted on cabin ceiling in left-right direction by carriage, its right-hand end lead to
Cross fixing device to be removably fixed on the sidewall paneling of kitchen；
Every curtain, its upper end is slidably mounted on cabin ceiling in left-right direction by carriage, its left-hand end for side
It is removably fixed on the sidewall paneling of main cabin by fixing device；And
Adhering fixture, in being respectively arranged at every the left-hand end of curtain and side every curtain right-hand end, for will in every
Curtain and side are adhesively fixed every curtain；
Septum curtain is all made using aviation cloth every curtain with side.
Above-mentioned carriage includes inlaying some embedding nuts being fixed on cabin ceiling, is fixed on edge by screw
On embedding nut and in left-right direction horizontally disposed slide rail and be slidably mounted on some slide assemblies in slide rail, septum
The fixed fabric bar that curtain and side are sutured by its upper end respectively every curtain hangs on slide assemblies lower end.
Above-mentioned fixing device include being arranged in every the snap-fastener of curtain right-hand end and be arranged on the sidewall paneling of kitchen and with
The snap-fastener of the corresponding connection of snap-fastener.
Above-mentioned fixing device includes being arranged at side and every the snap-fastener of curtain left-hand end and is arranged on the sidewall paneling of main cabin
And the snap-fastener of connection corresponding with snap-fastener.
Above-mentioned adhering fixture include being arranged in every the male and female band public affairs face and be arranged at side every curtain of curtain left-hand end
The male and female band generatrix of right-hand end.
Every curtain in tying up for the ease of bundle, also include the fixing band being made up of aviation cloth being arranged on the sidewall paneling of kitchen
ⅱ.
For convenience by be fixed on the left of passageway every curtain, also include being installed on side on the right side of curtain by aviation cloth system
The fixing band becoming.
Above-mentioned slide rail is made up of aircraft aluminum.
Correctly operate for the ease of flight crew, above-mentioned slide rail is pasted with indicative label.
In order to improve positioning precision, also include the fixing band being vertically arranged, during the upper and lower ends of described fixing band are sutured in
On curtain, the collar slides and is set in fixing band, and described snap-fastener is fixed on the collar, and described fixing band and the collar are by boat
Empty cloth is made.
The invention has the beneficial effects as follows: redesign in installing every curtain 1 and side before curtain 2 effectively can separate main cabin
Service area and main cabin passenger area, meet the requirement of safety and airworthiness, save simultaneously other buying compartment, locker high
Expensive cost, improves spatial impression and the comfort level of front service area.
Brief description
Fig. 1 is the perspective view of the present invention；
Fig. 2 is the main structure diagram of the present invention；
Fig. 3 is the slide rail portion structure schematic diagram of the present invention；
Fig. 4 is the fixing band portion structure schematic diagram of the present invention；
In figure, 1. in every curtain 2. side every curtain 3. kitchen sidewall paneling, 4. main cabin sidewall paneling, 5. snap-fastener 6. snap-fastener
7. fixing band 10. cabin ceiling, 11. fixing band, 12. collar 13. snap-fastener of male and female band public affairs face 8. male and female band generatrix 9.
The indicative label 20. of 14. embedding nut, 15. screw, 16. slide rail, 17. fixed fabric bar, 18. slide assemblies 19. is pressed
The fixing band of button 21..
Specific embodiment
The present invention will be further described for 1 to accompanying drawing 4 below in conjunction with the accompanying drawings.
A kind of commercial aircraft main cabin curtain assembly, comprising: in every curtain 1, its upper end pass through carriage along right and left
To being slidably mounted on cabin ceiling 10, its right-hand end is removably fixed on kitchen sidewall paneling 3 by fixing device；Side
Every curtain 2, its upper end is slidably mounted on cabin ceiling 10 in left-right direction by carriage in face, and its left-hand end is passed through to fix
Device is removably fixed on main cabin sidewall paneling 4；And adhering fixture, in being respectively arranged at every curtain 1 left-hand end with
And side is every the right-hand end of curtain 2, for by be adhesively fixed every curtain 2 every curtain 1 and side；In all adopt every curtain 2 with side every curtain 1
Aviation cloth is made.In redesign installation, every curtain 1 and side, service area and main cabin before curtain 2 can effectively separate main cabin are taken advantage of
Objective area, meets the requirement of safety and airworthiness, saves other buying compartment, the cost of the costliness of locker simultaneously, improves
The spatial impression of front service area and comfort level.
Further, carriage can be following structure, it include inlaying be fixed on some on cabin ceiling 10
Embedding nut 14, be fixed on embedding nut 14 by screw 15 and in left-right direction horizontally disposed slide rail 16 and slide peace
Be loaded on some slide assemblies 18 in slide rail 16, in the fixed fabric that sutured by its upper end respectively every curtain 2 every curtain 1 and side
Bar 17 hangs on slide assemblies 18 lower end.In simple every curtain 2 installing/dismounting every curtain 1 and side.Fixing device can be as follows
Structure, it include being arranged in every the snap-fastener 13 of curtain 1 right-hand end and be arranged on kitchen sidewall paneling 3 and with snap-fastener 13
The snap-fastener 20 of corresponding connection, by the snapping of snap-fastener 13 and snap-fastener 20 can conveniently will in every curtain 1 and kitchen side
Wallboard 3 is connected.Fixing device can be following structure, and it includes being arranged at the snap-fastener 6 every curtain 2 left-hand end for the side
And be arranged on main cabin sidewall paneling 4 and connection corresponding with snap-fastener 6 snap-fastener 5, by snap-fastener 6 and snap-fastener 5
Snapping, can facilitate and side is fixed on main cabin sidewall paneling 4 every curtain 2.Bonding can be following structure, its fixing device bag
Include the male and female band public affairs face 7 and be arranged at the male and female band generatrix 8 every curtain 2 right-hand end for the side every curtain 1 left-hand end in being arranged at, pass through
Male and female band public affairs face 7 and male and female with generatrix 8 bonding can achieve in every curtain 1 and side after curtain 2 is connected to the screening coordinating gap
Gear, bonded structure is simple, easy to use.
The fixing band 21 being made up of aviation cloth being arranged on kitchen sidewall paneling 3 can also be included, and install
In the fixing band 9 being made up of aviation cloth every curtain 2 right side for the side.Fixing band 21 can will pull open after in every
Curtain 1 carries out bundle and ties up, and fixing band 9 can by be fixed on the left of passageway every curtain 11, improve the convenience of use.Slide rail
16 are made up of aircraft aluminum, and it is lightweight and intensity is big, meets the requirement of the intensity of curtain assembly.Can paste on slide rail 16
There is indicative label 19, indicative label 19 is printed on the operating procedure every curtain, to guarantee that flight crew correctly operates.Can also wrap
Include the fixing band 11 being vertically arranged, the upper and lower ends of fixing band 11 be sutured on curtain 1, the collar 12 slide be set in fixing band
On 11, snap-fastener 13 is fixed on the collar 12, and fixing band 11 and the collar 12 are made by aviation cloth.Because the collar 12 can
To slide up and down in fixing band 11, such that it is able to adjust the high and low position of snap-fastener 13, every the cloth of curtain 1 in preventing
The situation that the snap-fastener 13 that sagging deflections cause cannot fasten to snap-fastener 20 occurs.
Claims (10)
1. a kind of commercial aircraft main cabin curtain assembly is it is characterised in that include:
In be slidably mounted in left-right direction on cabin ceiling (10) by carriage every curtain (1), its upper end, its right-hand end
It is removably fixed on kitchen sidewall paneling (3) by fixing device；
Every curtain (2), its upper end is slidably mounted on cabin ceiling (10) in left-right direction by carriage, on the left of it for side
End is removably fixed on main cabin sidewall paneling (4) by fixing device；And
Adhering fixture, every the right-hand end every curtain (2) of left-hand end and side of curtain (1) in being respectively arranged at, for will in
It is adhesively fixed every curtain (2) every curtain (1) and side；
Septum curtain (1) is all made using aviation cloth every curtain (2) with side.
2. commercial aircraft main cabin curtain assembly according to claim 1 it is characterised in that: described carriage includes
Inlay some embedding nuts (14) being fixed on cabin ceiling (10), be fixed on embedding nut (14) by screw (15)
And horizontally disposed slide rail (16) and be slidably mounted on some slide assemblies (18) in slide rail (16) in left-right direction, described
In the fixed fabric bar (17) that sutured by its upper end respectively every curtain (2) every curtain (1) and side hang on slide assemblies (18)
Lower end.
3. commercial aircraft main cabin curtain assembly according to claim 1 it is characterised in that: described fixing device bag
Include in being arranged at every curtain (1) right-hand end snap-fastener (13) and be arranged at kitchen sidewall paneling (3) upper and with snap-fastener (13) phase
The corresponding snap-fastener (20) connecting.
4. commercial aircraft main cabin curtain assembly according to claim 1 it is characterised in that: described fixing device bag
Include be arranged at side every the snap-fastener (6) of curtain (2) left-hand end and be arranged at main cabin sidewall paneling (4) upper and with snap-fastener (6) phase
The corresponding snap-fastener (5) connecting.
5. commercial aircraft main cabin curtain assembly according to claim 1 it is characterised in that: described adhering fixture
Including in being arranged at every the male face of male and female band (7) of curtain (1) left-hand end and to be arranged at side female every the male and female band of curtain (2) right-hand end
Face (8).
6. commercial aircraft main cabin curtain assembly as claimed in any of claims 1 to 5 it is characterised in that: also
Including the fixing band (21) being made up of aviation cloth being arranged on kitchen sidewall paneling (3).
7. commercial aircraft main cabin curtain assembly as claimed in any of claims 1 to 5 it is characterised in that: also
Including being installed on the fixing band (9) being made up of aviation cloth on the right side of curtain (2) for the side.
8. commercial aircraft main cabin curtain assembly according to claim 2 it is characterised in that: described slide rail (16) is by navigating
Empty aluminium is made.
9. commercial aircraft main cabin curtain assembly according to claim 2 it is characterised in that: described slide rail (16) is upper viscous
Post indicative label (19).
10. commercial aircraft main cabin curtain assembly according to claim 3 it is characterised in that: also include being vertically arranged
Fixing band (11), the upper and lower ends of described fixing band (11) be sutured on curtain (1), the collar (12) slide be set in fixation
On band (11), described snap-fastener (13) is fixed on the collar (12), and described fixing band (11) and the collar (12) are by aviation cloth
Material is made.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620927004.9U CN205916334U (en) | 2016-08-24 | 2016-08-24 | Civil aviation aircraft cabin screen subassembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620927004.9U CN205916334U (en) | 2016-08-24 | 2016-08-24 | Civil aviation aircraft cabin screen subassembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205916334U true CN205916334U (en) | 2017-02-01 |
Family
ID=57871281
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620927004.9U Expired - Fee Related CN205916334U (en) | 2016-08-24 | 2016-08-24 | Civil aviation aircraft cabin screen subassembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205916334U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106081120A (en) * | 2016-08-24 | 2016-11-09 | 山东太古飞机工程有限公司 | Commercial aircraft main cabin curtain assembly |
-
2016
- 2016-08-24 CN CN201620927004.9U patent/CN205916334U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106081120A (en) * | 2016-08-24 | 2016-11-09 | 山东太古飞机工程有限公司 | Commercial aircraft main cabin curtain assembly |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170201 Termination date: 20200824 |