CN104290909A - Center support plate of business class seat of airplane - Google Patents
Center support plate of business class seat of airplane Download PDFInfo
- Publication number
- CN104290909A CN104290909A CN201410564987.XA CN201410564987A CN104290909A CN 104290909 A CN104290909 A CN 104290909A CN 201410564987 A CN201410564987 A CN 201410564987A CN 104290909 A CN104290909 A CN 104290909A
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- CN
- China
- Prior art keywords
- hole
- via hole
- seat
- business class
- support plate
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- 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 center support plate of a business class seat of an airplane. The center support plate is mounted right below the seat and comprises a body, the surface of the body is provided with a plurality of via holes and mounting holes. The via holes including the first via hole, the second via hole, the third via hole, the fourth via hole, the fifth via hole and the sixth via hole which are different in size and shape, U-shaped connecting rods are arranged between the first via hole and the second via hole and between the third via hole and the fourth via hole as well as between the fifth via hole and the sixth via hole, and the mounting holes are arranged in the U-shaped connecting rods. According to the above technical scheme, high strength and flexibility can be guaranteed, materials are saved, and cost is reduced. After the center support plate is mounted below the seat, a passenger can feel more comfortable.
Description
Technical field
The present invention relates to a kind of aircraft seat accessory, particularly a kind of center brace panel of aircraft business class seat.
Background technology
Along with improving constantly of science and technology; people's living standard also improves thereupon; thus aircraft to have become at present fashion, popular, the vehicle efficiently the most; and aircraft seat is requisite thing in whole aircraft, when people sit on the seat, because aircraft navigates by water in high-altitude; and usually can experience seat built on the sand; make that people's feel comparatively uncomfortable, the of long duration damage that will cause this seat, the progress that clearly such seat has been out of step with the times.
Summary of the invention
The technical matters that the present invention mainly solves is to provide a kind of center brace panel of aircraft business class seat, while its high strength of guarantee, high tenacity, can save material, reduce costs, and after being arranged on under-seat, passenger can bring very comfortable enjoyment.
For solving the problems of the technologies described above, the technical scheme that the present invention adopts is: the center brace panel providing a kind of aircraft business class seat, be arranged on immediately below seat, comprise: body, described body surface is provided with multiple through hole and mounting hole, described through hole comprises: size, the first through hole that shape is all not identical, second through hole, third through-hole, fourth hole, fifth hole and the 6th through hole, described first through hole and described second through hole, third through-hole and fourth hole and be equipped with U-shaped pipe link between fifth hole and the 6th through hole, described mounting hole site is on described U-shaped pipe link.
In a preferred embodiment of the present invention, described body adopts alloy steel to form, and body can be made to have higher hardness.
In a preferred embodiment of the present invention, the left side of described first through hole is provided with knock hole, is convenient to the installation between the present invention and aircraft seat, and improves the accuracy installed.
In a preferred embodiment of the present invention, described each U-shaped pipe link is positioned on same level cross section, ensures the stability of body further.
The invention has the beneficial effects as follows: the present invention is provided with all not identical through hole of multiple size, shape by adopting at body surface, not only save material, reduce costs, and be provided with U-shaped pipe link, ensure that body has original high strength and high tenacity performance, adopt the center brace panel of this structure to be arranged on after below aircraft seat simultaneously, comfortable enjoyment can be brought to passenger.
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, body, the 2, first through hole, the 3, second through hole, and 4, third through-hole, 5, fourth hole, 6, fifth hole, the 7, the 6th through hole, 8, mounting hole, 9, knock 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 center brace panel of aircraft business class seat, be arranged on immediately below seat, comprise: body 1, described body 1 surface is provided with multiple through hole and mounting hole 8, described through hole comprises: the first through hole 2, second through hole 3, third through-hole 4, fourth hole 5, fifth hole 6 and the 6th through hole 7 that size, shape are all not identical, described first through hole 2 and described second through hole 3, third through-hole 4 and fourth hole 5 and be equipped with U-shaped pipe link between fifth hole 6 and the 6th through hole 7, described mounting hole 8 is positioned on described U-shaped pipe link.
Wherein, described body 1 adopts alloy steel to form, and body 1 can be made to have higher hardness.
The left side of described first through hole 2 is provided with knock hole 9, is convenient to the installation between the present invention and aircraft seat, and improves the accuracy installed.
Described each U-shaped pipe link is positioned on same level cross section, makes body 1 after mounting, can fit tightly with seat, ensures the stability of body 1 further.
Be different from prior art, present invention is disclosed a kind of center brace panel of aircraft business class seat, adopt and offer the first through hole 2 on body 1 surface, second through hole 3, third through-hole 4, fourth hole 5, fifth hole 6 and the 6th through hole 7, save lot of materials, reduce costs, and each hole size, shape is all not identical, magnificent in appearance air, simultaneously at the first through hole 2 and the second through hole 3, third through-hole 4 and fourth hole 5, U-shaped pipe link is provided with between fifth hole 6 and the 6th through hole 7, according to mechanics principle, enough guarantee bodies 1 have original high strength and high tenacity performance, and when mounted, first positioned by knock hole 9, again by be positioned at mounting hole 8 on U-shaped pipe link by body accurately fixing with aircraft seat below, comfortable enjoyment is provided 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 (4)
1. the center brace panel of an aircraft business class seat, be arranged on immediately below seat, it is characterized in that, comprise: body, described body surface is provided with multiple through hole and mounting hole, described through hole comprises: the first through hole that size, shape are all not identical, the second through hole, third through-hole, fourth hole, fifth hole and the 6th through hole, described first through hole and described second through hole, third through-hole and fourth hole and be equipped with U-shaped pipe link between fifth hole and the 6th through hole, described mounting hole site is on described U-shaped pipe link.
2. the center brace panel of a kind of aircraft business class seat according to claim 1, is characterized in that, described body adopts alloy steel to form.
3. the center brace panel of a kind of aircraft business class seat according to claim 1, it is characterized in that, the left side of described first through hole is provided with knock hole.
4. the center brace panel of a kind of aircraft business class seat according to claim 1, is characterized in that, described each U-shaped pipe link is positioned on same level cross section.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410564987.XA CN104290909A (en) | 2014-10-22 | 2014-10-22 | Center support plate of business class seat of airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410564987.XA CN104290909A (en) | 2014-10-22 | 2014-10-22 | Center support plate of business class seat of airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104290909A true CN104290909A (en) | 2015-01-21 |
Family
ID=52310914
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410564987.XA Pending CN104290909A (en) | 2014-10-22 | 2014-10-22 | Center support plate of business class seat of airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104290909A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201284012Y (en) * | 2008-09-28 | 2009-08-05 | 航宇救生装备有限公司 | Energy-absorbing navigation seat |
| US20110068226A1 (en) * | 2005-09-06 | 2011-03-24 | Airbus Deutschland Gmbh | Modular seat system for a vehicle |
| US20120267931A1 (en) * | 2008-12-09 | 2012-10-25 | Wolfgang K, Llc | Adjustable aircraft seat |
| WO2013143701A2 (en) * | 2012-03-30 | 2013-10-03 | Sogeclair S.A. | Unitary panel for the floor of a vehicle, floor, and vehicle including such a unitary panel |
| CN203544373U (en) * | 2013-11-21 | 2014-04-16 | 山东太古飞机工程有限公司 | Table board for airplane passenger cabin |
| EP2855267A1 (en) * | 2012-05-24 | 2015-04-08 | Lufthansa Technik AG | Floor connection assembly of an aircraft seat |
| CN204279957U (en) * | 2014-10-22 | 2015-04-22 | 苏州华冲精密机械有限公司 | A kind of center brace panel of aircraft business class seat |
-
2014
- 2014-10-22 CN CN201410564987.XA patent/CN104290909A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110068226A1 (en) * | 2005-09-06 | 2011-03-24 | Airbus Deutschland Gmbh | Modular seat system for a vehicle |
| CN201284012Y (en) * | 2008-09-28 | 2009-08-05 | 航宇救生装备有限公司 | Energy-absorbing navigation seat |
| US20120267931A1 (en) * | 2008-12-09 | 2012-10-25 | Wolfgang K, Llc | Adjustable aircraft seat |
| WO2013143701A2 (en) * | 2012-03-30 | 2013-10-03 | Sogeclair S.A. | Unitary panel for the floor of a vehicle, floor, and vehicle including such a unitary panel |
| EP2855267A1 (en) * | 2012-05-24 | 2015-04-08 | Lufthansa Technik AG | Floor connection assembly of an aircraft seat |
| CN203544373U (en) * | 2013-11-21 | 2014-04-16 | 山东太古飞机工程有限公司 | Table board for airplane passenger cabin |
| CN204279957U (en) * | 2014-10-22 | 2015-04-22 | 苏州华冲精密机械有限公司 | A kind of center brace panel of aircraft business class seat |
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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 | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20150121 |