CN104290910A - Console side plate of business class seat of airplane - Google Patents
Console side plate of business class seat of airplane Download PDFInfo
- Publication number
- CN104290910A CN104290910A CN201410564993.5A CN201410564993A CN104290910A CN 104290910 A CN104290910 A CN 104290910A CN 201410564993 A CN201410564993 A CN 201410564993A CN 104290910 A CN104290910 A CN 104290910A
- Authority
- CN
- China
- Prior art keywords
- side panel
- side plate
- control desk
- seat
- business class
- 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.)
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Abstract
The invention discloses a console side plate of a business class seat of an airplane. The console side plate comprises a first side plate and a second side plate, one end of the first side plate is connected with one end of the second side plate in a perpendicular intersection manner, and a U-shaped opening is arranged at the joint of the first side plate and the second side plate. The U-shaped opening is connected with an external console, a square fixing seat is fixedly mounted at the other end of the first side plate, the fixing seat is hollow inside and is provided with fixing holes at the edges, the other end of the second side plate is provided with a rotatable connecting block, and the connecting block is provided with a mounting hole. According to the above technical scheme, the console side plate is simple in structure and convenient to mount, angle of the seat can be optionally adjusted, and a passenger can feel more comfortable when sitting on the seat.
Description
Technical field
The present invention relates to a kind of seat parts, particularly a kind of control desk side panel of aircraft business class seat.
Background technology
Along with improving constantly of science and technology, the living standard of people also improves gradually, aircraft is extensively subject to consumers as the remote vehicle the most quick, comfortable simultaneously, and people are while airplane, seat is absolutely necessary one of vitals, its stability requires very high, directly can affect the traveling comfort of passenger's airplane, and in existing seat component part, the control desk side panel arrangement used is too dull, comparatively inconvenience when rotated, design inadequate hommization, the traveling comfort that people take is also poor.。
Summary of the invention
The technical matters that the present invention mainly solves is to provide a kind of control desk side panel of aircraft business class seat, and control desk side panel arrangement can be made simple, easy for installation, and can random adjusting seat angle, makes passenger can obtain more comfortable sitting posture enjoyment.
For solving the problems of the technologies described above, the technical scheme that the present invention adopts is: the control desk side panel providing a kind of aircraft business class seat, comprise: the first side panel and the second side panel, one end of described first side panel is connected in intersecting vertically with one end of described second side panel, and a U-shaped opening is provided with in junction, described U-shaped opening connects extraneous control desk, the other end of described first side panel is installed with a square permanent seat, described permanent seat inner hollow, and be provided with multiple fixed orifice at edge, the other end of described second side panel is provided with rotatable contiguous block, described contiguous block is provided with mounting hole.
In a preferred embodiment of the present invention, the medial surface that described fixed seating intersects in described first side panel and described second side panel, can convenient operation people to the installation of control desk side panel.
In a preferred embodiment of the present invention, described contiguous block and described second side panel are that hinged bolt is connected, and can play easy to maintenance, easily changeable effect.
In a preferred embodiment of the present invention, described permanent seat and described first side panel are that hinged bolt is connected, and can play easy to maintenance, easily changeable effect.
In a preferred embodiment of the present invention, described first side panel is equipped with all not identical inner groovy of size, shape with described second side panel surfaces, while guarantee control desk 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, extraneous control desk is connected by this U-shaped opening, side panel entirety can be made arbitrarily to rotate, humanization designing, more comfortable sitting posture is brought to enjoy to passenger, whole installation process can be completed, simple and fast by only needing the fixed orifice on mounting-fixing base and the mounting hole on contiguous block.
Accompanying drawing explanation
Fig. 1 is the present invention's structural representation in a preferred embodiment;
In accompanying drawing, the mark of each parts is as follows: 1, the first side panel, the 2, second side panel, and 3, U-shaped opening, 4, permanent seat, 5, contiguous block, 6, fixed orifice, 7, mounting hole.
Detailed description of the invention
Below in conjunction with accompanying drawing, preferred embodiment of the present invention is described in detail, can be easier to make advantages and features of the invention be readily appreciated by one skilled in the art, thus more explicit defining is made to protection scope of the present invention.
Refer to Fig. 1, the embodiment of the present invention comprises:
A kind of control desk side panel of aircraft business class seat, comprise: the first side panel 1 and the second side panel 2, one end of described first side panel 1 is connected in intersecting vertically with one end of described second side panel 2, and a U-shaped opening 3 is provided with in junction, described U-shaped opening 3 connects extraneous control desk, the other end of described first side panel 1 is installed with a square permanent seat 4, described permanent seat 4 inner hollow, and multiple fixed orifice 6 is provided with at edge, the other end of described second side panel 2 is provided with rotatable contiguous block 5, and described contiguous block 5 is provided with mounting hole 7.
Further, described permanent seat 4 is positioned at the medial surface that described first side panel 1 and described second side panel 2 intersect, consider positioning datum during installation, described permanent seat 4 is positioned at the medial surface that described first side panel 1 and described second side panel 2 intersect, humanization designing, can convenient operation people to the installation of control desk side panel.
Further, described contiguous block 5 is connected for hinged bolt with described second side panel 2, can play easy to maintenance, easily changeable effect.
Further, described permanent seat 4 is connected for hinged bolt with described first side panel 1, can play easy to maintenance, easily changeable effect.
Further, described first side panel 1 is equipped with all not identical inner groovy of size, shape with described second side panel 2 surface, while guarantee control desk side panel entirety, saves lot of materials, reduce costs, and outward appearance is not dull, comparatively attractive in appearance.
Be different from prior art, present invention is disclosed a kind of control desk 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 U-shaped opening 3 is provided with in junction, when mounted, first U-shaped opening 3 is aimed at control desk by operating personal, be fixed installation, again the first side panel 1 is aimed at backrest afterwards, permanent seat 4 is fixed on backrest by fixed orifice 6, again the second side panel 2 is aimed at cushion position, be arranged on the cushion edge of seat by the mounting hole 7 on contiguous block 5, after completing installation, when adjusting seat angle, whole side panel can rotate along U-shaped opening 3, the contiguous block 5 be simultaneously arranged on the second side panel 2 rotates thereupon, ensure the Stability Analysis of Structures of side panel entirety, not fragile, unit design hommization, more comfortable sitting posture is brought to enjoy to passenger.
The foregoing is only embodiments of the invention; not thereby the scope of the claims of the present invention is limited; every utilize specification sheets of the present invention and accompanying drawing content to do equivalent structure or equivalent flow process conversion; 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 control desk 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 first side panel is connected in intersecting vertically with one end of described second side panel, and a U-shaped opening is provided with in junction, described U-shaped opening connects extraneous control desk, the other end of described first side panel is installed with a square permanent seat, described permanent seat inner hollow, and be provided with multiple fixed orifice at edge, the other end of described second side panel is provided with rotatable contiguous block, and described contiguous block is provided with mounting hole.
2. the control desk side panel of a kind of aircraft business class seat according to claim 1, is characterized in that, the medial surface that described fixed seating intersects in described first side panel and described second side panel.
3. the control desk side panel of a kind of aircraft business class seat according to claim 1, is characterized in that, described contiguous block and described second side panel are that hinged bolt is connected.
4. the control desk side panel of a kind of aircraft business class seat according to claim 1, is characterized in that, described permanent seat and described first side panel are that hinged bolt is connected.
5. the control desk side panel of a kind of aircraft business class seat according to claim 1, it is characterized in that, described first side panel is equipped with all not identical inner groovy of size, shape with described second side panel surfaces.
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 true CN104290910A (en) | 2015-01-21 |
| CN104290910B 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 (6)
| 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 |
| US20120256457A1 (en) * | 2011-04-05 | 2012-10-11 | Jeremy Cailleteau | Adjustable seat |
| CN103201174A (en) * | 2010-10-18 | 2013-07-10 | 祖迪雅克座椅法国公司 | Passenger seating assemblies and aspects thereof |
| US20130247303A1 (en) * | 2012-03-20 | 2013-09-26 | Be Aerospace, Inc. | Seat cushion with integrated seat frame attachment structure |
| 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 |
-
2014
- 2014-10-22 CN CN201410564993.5A patent/CN104290910B/en not_active Expired - Fee Related
Patent Citations (6)
| 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 |
| US20120256457A1 (en) * | 2011-04-05 | 2012-10-11 | Jeremy Cailleteau | Adjustable seat |
| US20130247303A1 (en) * | 2012-03-20 | 2013-09-26 | Be Aerospace, Inc. | Seat cushion with integrated seat frame attachment structure |
| 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 |
|---|---|
| CN104290910B (en) | 2016-05-25 |
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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 |