CN104290910B - A kind of console side panel of aircraft business class seat - Google Patents
A kind of console side panel of aircraft business class seat Download PDFInfo
- Publication number
- CN104290910B CN104290910B CN201410564993.5A CN201410564993A CN104290910B CN 104290910 B CN104290910 B CN 104290910B CN 201410564993 A CN201410564993 A CN 201410564993A CN 104290910 B CN104290910 B CN 104290910B
- Authority
- CN
- China
- Prior art keywords
- side panel
- console
- business class
- contiguous block
- class seat
- 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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- Chair Legs, Seat Parts, And Backrests (AREA)
- Vehicle Step Arrangements And Article Storage (AREA)
- Passenger Equipment (AREA)
Abstract
The invention discloses a kind of console side panel of aircraft business class seat, comprise: the first side panel and the second side panel, one end of described the first side panel is to intersect vertically with one end of described the second side panel and is connected, and be provided with a U-shaped opening in junction, described U-shaped opening connects extraneous console, the other end of described the first side panel is installed with a square holder, described holder inner hollow, and be provided with multiple fixing holes at edge, the other end of described the second side panel is provided with rotatable contiguous block, described contiguous block is provided with installing hole, by the way, the present invention can make console side panel arrangement simple, easy for installation, and arbitrarily adjusting seat angle, making passenger can obtain more comfortable sitting posture enjoys.
Description
Technical field
The present invention relates to a kind of seat parts, particularly a kind of console side panel of aircraft business class seat.
Background technology
Along with improving constantly of science and technology, people's living standard also improves gradually, aircraft is favored by consumer extensively as the most quick, the comfortable remote vehicles simultaneously, and people are in airplane, seat one of the vitals that is absolutely necessary, its stability requires very high, can directly affect the comfortableness of passenger's airplane, and in existing seat component part, the console side panel arrangement using is too dull, comparatively inconvenience, designs inadequate hommization when rotated, and the comfortableness that people take is also poor. .
Summary of the invention
The technical problem that the present invention mainly solves is to provide a kind of console side panel of aircraft business class seat, can make console side panel arrangement simple, easy for installation, and random adjusting seat angle, makes passenger can obtain more comfortable sitting posture and enjoys.
For solving the problems of the technologies described above, the technical scheme that the present invention adopts is: the console side panel that a kind of aircraft business class seat is provided, comprise: the first side panel and the second side panel, one end of described the first side panel is to intersect vertically with one end of described the second side panel and is connected, and be provided with a U-shaped opening in junction, described U-shaped opening connects extraneous console, the other end of described the first side panel is installed with a square holder, described holder inner hollow, and be provided with multiple fixing holes at edge, the other end of described the second side panel is provided with rotatable contiguous block, described contiguous block is provided with installing hole.
In a preferred embodiment of the present invention, described fixed seating, can the installation of convenient operation people to console side panel in described the first side panel and the crossing medial surface of described the second side panel.
In a preferred embodiment of the present invention, described contiguous block is that hinged bolt is connected with described the second side panel, can play easy to maintenance, easily changeable effect.
In a preferred embodiment of the present invention, described holder is that hinged bolt is connected with described the first side panel, can play easy to maintenance, easily changeable effect.
In a preferred embodiment of the present invention, described the first side panel and described the second side panel surfaces are equipped with all not identical inner groovies of size, shape, in ensureing console side panel entirety, save lot of materials, reduce costs, and outward appearance is not dull, comparatively attractive in appearance.
The invention has the beneficial effects as follows: the present invention is by being provided with a U-shaped opening in the intersection of the first side panel and the second side panel, connect extraneous console by this U-shaped opening, can make side panel entirety arbitrarily to rotate, humanization designing, bring more comfortable sitting posture to enjoy to passenger, by only needing the installing hole on fixing hole and the contiguous block on mounting-fixing base can complete whole installation process, simple and fast.
Brief description of the drawings
Fig. 1 is the structural representation of the present invention in a preferred embodiment;
In accompanying drawing, the mark of each parts is as follows: 1, the first side panel, 2, the second side panel, 3, U-shaped opening, 4, holder, 5, contiguous block, 6, fixing hole, 7, installing hole.
Detailed description of the invention
Below in conjunction with accompanying drawing, preferred embodiment of the present invention is described in detail, thereby so that advantages and features of the invention can be easier to be it will be appreciated by those skilled in the art that, protection scope of the present invention is made to more explicit defining.
Refer to Fig. 1, the embodiment of the present invention comprises:
A kind of console side panel of aircraft business class seat, comprise: the first side panel 1 and the second side panel 2, one end of described the first side panel 1 is to intersect vertically with one end of described the second side panel 2 and is connected, and be provided with a U-shaped opening 3 in junction, described U-shaped opening 3 connects extraneous console, the other end of described the first side panel 1 is installed with a square holder 4, described holder 4 inner hollow, and be provided with multiple fixing holes 6 at edge, the other end of described the second side panel 2 is provided with rotatable contiguous block 5, and described contiguous block 5 is provided with installing hole 7.
Further, described holder 4 is positioned at described the first side panel 1 and the crossing medial surface of described the second side panel 2, consider the positioning datum while installation, described holder 4 is positioned to described the first side panel 1 and the crossing medial surface of described the second side panel 2, humanization designing, can the installation of convenient operation people to console side panel.
Further, described contiguous block 5 with described the second side panel 2 for hinged bolt is connected, can play easy to maintenance, easily changeable effect.
Further, described holder 4 with described the first side panel 1 for hinged bolt is connected, can play easy to maintenance, easily changeable effect.
Further, described the first side panel 1 and described the second side panel 2 surfaces are equipped with all not identical inner groovies of size, shape, in ensureing console side panel entirety, save lot of materials, reduce costs, and outward appearance are not dull, comparatively attractive in appearance.
Be different from prior art, the present invention has disclosed a kind of console side panel of aircraft business class seat, be formed by connecting by adopting the first side 1 plate and the second side panel 2 to intersect vertically, and be provided with U-shaped opening 3 in junction, when mounted, first operating personnel aim at console by U-shaped opening 3, be fixed installation, again the first side panel 1 is aimed to backrest afterwards, holder 4 is fixed on backrest by fixing hole 6, again the second side panel 2 is aimed to cushion position, be arranged on by the installing hole 7 on contiguous block 5 on the cushion edge of seat, complete after installation, in the time of adjusting seat angle, whole side panel can rotate along U-shaped opening 3, the contiguous block 5 being simultaneously arranged on the second side panel 2 rotates thereupon, ensure the Stability Analysis of Structures of side panel entirety, not fragile, global design hommization, bring more comfortable sitting posture to enjoy to passenger.
The foregoing is only embodiments of the invention; not thereby limit the scope of the claims of the present invention; every equivalent structure or conversion of equivalent flow process that utilizes description of the present invention and accompanying drawing content to do; or be directly or indirectly used in other relevant technical fields, be all in like manner included in scope of patent protection of the present invention.
Claims (5)
1. the console side panel of an aircraft business class seat, it is characterized in that, comprise: the first side panel and the second side panel, one end of described the first side panel is to intersect vertically with one end of described the second side panel and is connected, and be provided with a U-shaped opening in junction, described U-shaped opening connects extraneous console, the other end of described the first side panel is installed with a square holder, described holder inner hollow, and be provided with multiple fixing holes at edge, the other end of described the second side panel is provided with rotatable contiguous block, and described contiguous block is provided with installing hole.
2. the console side panel of a kind of aircraft business class seat according to claim 1, is characterized in that, described fixed seating is in described the first side panel and the crossing medial surface of described the second side panel.
3. the console side panel of a kind of aircraft business class seat according to claim 1, is characterized in that, described contiguous block is that hinged bolt is connected with described the second side panel.
4. the console side panel of a kind of aircraft business class seat according to claim 1, is characterized in that, described holder is that hinged bolt is connected with described the first side panel.
5. the console side panel of a kind of aircraft business class seat according to claim 1, is characterized in that, described the first side panel and described the second side panel surfaces are equipped with all not identical inner groovies of size, shape.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410564993.5A CN104290910B (en) | 2014-10-22 | 2014-10-22 | A kind of console side panel of aircraft business class seat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410564993.5A CN104290910B (en) | 2014-10-22 | 2014-10-22 | A kind of console side panel of aircraft business class seat |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104290910A CN104290910A (en) | 2015-01-21 |
| CN104290910B true CN104290910B (en) | 2016-05-25 |
Family
ID=52310915
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410564993.5A Expired - Fee Related CN104290910B (en) | 2014-10-22 | 2014-10-22 | A kind of console side panel of aircraft business class seat |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104290910B (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5485976A (en) * | 1994-01-12 | 1996-01-23 | Weber Aircraft, Inc. | Plastic bottom diaphragm for aircraft seat |
| CN102056799A (en) * | 2008-05-07 | 2011-05-11 | 齐姆有限公司 | Kit for seat rows in aircraft |
| CN103201174A (en) * | 2010-10-18 | 2013-07-10 | 祖迪雅克座椅法国公司 | Passenger seating assemblies and aspects thereof |
| CN204223185U (en) * | 2014-10-22 | 2015-03-25 | 苏州华冲精密机械有限公司 | A kind of control desk side panel of aircraft business class seat |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2694323B1 (en) * | 2011-04-05 | 2021-11-03 | Safran Seats | Adjustable seat |
| US8782835B2 (en) * | 2012-03-20 | 2014-07-22 | Be Aerospace, Inc. | Seat cushion with integrated seat frame attachment structure |
-
2014
- 2014-10-22 CN CN201410564993.5A patent/CN104290910B/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5485976A (en) * | 1994-01-12 | 1996-01-23 | Weber Aircraft, Inc. | Plastic bottom diaphragm for aircraft seat |
| CN102056799A (en) * | 2008-05-07 | 2011-05-11 | 齐姆有限公司 | Kit for seat rows in aircraft |
| CN103201174A (en) * | 2010-10-18 | 2013-07-10 | 祖迪雅克座椅法国公司 | Passenger seating assemblies and aspects thereof |
| CN204223185U (en) * | 2014-10-22 | 2015-03-25 | 苏州华冲精密机械有限公司 | A kind of control desk side panel of aircraft business class seat |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104290910A (en) | 2015-01-21 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| 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: 20160525 Termination date: 20161022 |