CN204223185U - A kind of control desk side panel of aircraft business class seat - Google Patents
A kind of control desk side panel of aircraft business class seat Download PDFInfo
- Publication number
- CN204223185U CN204223185U CN201420612438.0U CN201420612438U CN204223185U CN 204223185 U CN204223185 U CN 204223185U CN 201420612438 U CN201420612438 U CN 201420612438U CN 204223185 U CN204223185 U CN 204223185U
- Authority
- CN
- China
- Prior art keywords
- side panel
- control desk
- business class
- contiguous block
- utility
- 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.)
- Withdrawn - After Issue
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Abstract
The utility model discloses a kind of control desk side panel 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, by the way, the utility model can make control desk side panel arrangement simple, easy for installation, and can random adjusting seat angle, make passenger can obtain more comfortable sitting posture to enjoy.
Description
Technical field
The utility model 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.。
Utility model content
The technical matters that the utility model mainly solves is to provide a kind of control desk side panel of aircraft business class seat, control desk side panel arrangement can be made simple, easy for installation, and can random adjusting seat angle, make passenger can obtain more comfortable sitting posture and enjoy.
For solving the problems of the technologies described above, the technical scheme that the utility model 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 the utility model preferred embodiment, 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 the utility model preferred embodiment, described contiguous block and described second side panel are that hinged bolt is connected, and can play easy to maintenance, easily changeable effect.
In the utility model preferred embodiment, described permanent seat and described first side panel are that hinged bolt is connected, and can play easy to maintenance, easily changeable effect.
In the utility model preferred embodiment, 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 beneficial effects of the utility model are: the utility model 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 utility model 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 utility model is described in detail, to make advantage of the present utility model and feature can be easier to be readily appreciated by one skilled in the art, thus more explicit defining is made to protection domain of the present utility model.
Refer to Fig. 1, the utility model embodiment 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, the utility model discloses 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 embodiment of the present utility model; not thereby the scope of the claims of the present utility model is limited; every utilize the utility model specification sheets 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 utility model.
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 |
|---|---|---|---|
| CN201420612438.0U CN204223185U (en) | 2014-10-22 | 2014-10-22 | A kind of control desk side panel of aircraft business class seat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420612438.0U CN204223185U (en) | 2014-10-22 | 2014-10-22 | A kind of control desk side panel of aircraft business class seat |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204223185U true CN204223185U (en) | 2015-03-25 |
Family
ID=52921306
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420612438.0U Withdrawn - After Issue CN204223185U (en) | 2014-10-22 | 2014-10-22 | A kind of control desk side panel of aircraft business class seat |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204223185U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104290910A (en) * | 2014-10-22 | 2015-01-21 | 苏州华冲精密机械有限公司 | Console side plate of business class seat of airplane |
-
2014
- 2014-10-22 CN CN201420612438.0U patent/CN204223185U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104290910A (en) * | 2014-10-22 | 2015-01-21 | 苏州华冲精密机械有限公司 | Console side plate of business class seat of airplane |
| CN104290910B (en) * | 2014-10-22 | 2016-05-25 | 苏州华冲精密机械有限公司 | A kind of console side panel of aircraft business class seat |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20150325 Effective date of abandoning: 20160525 |
|
| C25 | Abandonment of patent right or utility model to avoid double patenting |