CN104290911A - Reinforcing footstand of business class seat of airplane - Google Patents
Reinforcing footstand of business class seat of airplane Download PDFInfo
- Publication number
- CN104290911A CN104290911A CN201410565201.6A CN201410565201A CN104290911A CN 104290911 A CN104290911 A CN 104290911A CN 201410565201 A CN201410565201 A CN 201410565201A CN 104290911 A CN104290911 A CN 104290911A
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- CN
- China
- Prior art keywords
- bracing frame
- support
- reinforcing
- 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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- Seats For Vehicles (AREA)
Abstract
The invention discloses a reinforcing footstand of a business class seat of an airplane. The reinforcing footstand comprises a bottom plate, a first support and a second support. The first support and the second support are transversely and fixedly mounted at the top end of the bottom plate, circular via holes and rectangular via holes are communicated to each other and arranged in the first support and second support, the rectangular via holes are transversely distributed in the first support, the circular via holes are longitudinally distributed in the second support, the peak of the first support is lower than the peak of the second support, and a smooth arc curve is formed between the first support and the second support. According to the above technical scheme, the reinforcing footstand is simple in structure and convenient to mount, stability of the seat can be improved, and comfortability of the seat can be enhanced.
Description
Technical field
The present invention relates to a kind of aircraft seat part, particularly a kind of reinforcing runners of aircraft business class seat.
Background technology
Along with the change in epoch and the progress of science and technology, the vehicle around us get more and more, and all bring great convenience to everyone life.The automobile of land, steamer in ocean, it aerial aircraft, substantially reduces the distance of people's contacts, and the wherein aircraft vehicle and extensively favoring by customer the most fast and easily, and people are when airplane, saddle horse in aircraft is absolutely necessary, and in the component part of numerous aircraft seat, its runners is single supporting bar structure, its stability is poor, makes its comfort property poor.
Summary of the invention
The technical matters that the present invention mainly solves is to provide a kind of reinforcing runners of aircraft business class seat, and structure is simple, easy for installation, and can increase seat stability, thus improves the comfort property of seat.
For solving the problems of the technologies described above, the technical scheme that the present invention adopts is: the reinforcing runners providing a kind of aircraft business class seat, comprise: base plate, first bracing frame and the second bracing frame, described first bracing frame and described second bracing frame are all laterally fixedly mounted on the top of described base plate, and inside is by the manhole be communicated with and rectangular through-hole composition, described rectangular through-hole is transverse distribution in described first bracing frame, described manhole is genesis analysis in described second bracing frame, the summit of described first bracing frame is lower than the summit of described second bracing frame, smooth type circular curve is formed between described first bracing frame and described second bracing frame.
In a preferred embodiment of the present invention, the bottom surface of described base plate is a plane, improves the stability of runners further.
In a preferred embodiment of the present invention, one end of described base plate transverse direction is provided with longitudinal positioning groove, reinforcing accuracy rate when mounted of making a reservation can be made to improve, and by this positioning groove, seat entirety is fixed on somewhere, ground, improves the stability of seat further.
In a preferred embodiment of the present invention, described first bracing frame and described second bracing frame surface are equipped with the pin-and-hole penetrating rectangular through-hole, for the further fixation between reinforcing runners of the present invention and external device.
The invention has the beneficial effects as follows: two bracing frames of the present invention's height are to replace the runners of single bracing frame in prior art, and structure is simple, easy for installation, and can increase seat stability, thus improve the comfort property of seat.
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 bracing frame, the 2, second bracing frame, and 3, positioning groove, 4, base plate, 5, manhole, 6, rectangular through-hole, 7, pin-and-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 reinforcing runners of aircraft business class seat, comprise: base plate 4, first bracing frame 1 and the second bracing frame 2, described first bracing frame 1 and described second bracing frame 2 are all laterally fixedly mounted on the top of described base plate 4, and inside forms by the manhole 5 be communicated with and rectangular through-hole 6, described rectangular through-hole 6 is transverse distribution in described first bracing frame 1, described manhole 5 is genesis analysis in described second bracing frame 2, the summit of described first bracing frame 1 is lower than the summit of described second bracing frame 2, smooth type circular curve is formed between described first bracing frame 1 and described second bracing frame 2.
Further, the bottom surface of described base plate 4 is a plane, makes runners can have better stability on the ground putting, thus improves further and be provided with the traveling comfort that this reinforces the seat of runners.
Further, one end of described base plate 4 transverse direction is provided with longitudinal positioning groove 3, reinforcing accuracy rate when mounted of making a reservation can be made to improve, and by this positioning groove 3, seat entirety is fixed on somewhere, ground, improves the stability of seat further.
Further, described first bracing frame 1 and described second bracing frame 2 surface are equipped with the pin-and-hole penetrating rectangular through-hole 6, for the further fixation between reinforcing runners of the present invention and external device.
Be different from prior art, present invention is disclosed a kind of reinforcing runners of aircraft business class seat, the present invention adopts two bracing frames to replace the mode of single bracing frame of the prior art, by offering manhole 5 for assembling with seat miscellaneous part and square through hole 6 in the middle of the first bracing frame 1 and the first bracing frame 2, manhole 5 in first bracing frame 1 and the second bracing frame 2 and rectangular through-hole 6 are arranged to the form of different directions distribution simultaneously, this can be made to reinforce runners after mounting, Impact direction can balance, when after the first bracing frame 1 and the second bracing frame 2 and extraneous assembling parts, utilize pin rod or field bolt to penetrate rectangular through-hole 6 to be fixed, with base plate 4 is placed on floor, and be fixed on the positioning by positioning groove 7, structure is simple, easy for installation, and can seat stability be increased, thus improve the comfort property of seat.
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 reinforcing runners of an aircraft business class seat, it is characterized in that, comprise: base plate, first bracing frame and the second bracing frame, described first bracing frame and described second bracing frame are all laterally fixedly mounted on the top of described base plate, and inside is by the manhole be communicated with and rectangular through-hole composition, described rectangular through-hole is transverse distribution in described first bracing frame, described manhole is genesis analysis in described second bracing frame, the summit of described first bracing frame is lower than the summit of described second bracing frame, smooth type circular curve is formed between described first bracing frame and described second bracing frame.
2. the reinforcing runners of a kind of aircraft business class seat according to claim 1, is characterized in that, the bottom surface of described base plate is a plane.
3. the reinforcing runners of a kind of aircraft business class seat according to claim 1, it is characterized in that, one end of described base plate transverse direction is provided with longitudinal positioning groove.
4. the reinforcing runners of a kind of aircraft business class seat according to claim 1, is characterized in that, described first bracing frame and described second bracing frame surface are equipped with the pin-and-hole penetrating rectangular through-hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410565201.6A CN104290911A (en) | 2014-10-22 | 2014-10-22 | Reinforcing footstand of business class seat of airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410565201.6A CN104290911A (en) | 2014-10-22 | 2014-10-22 | Reinforcing footstand of business class seat of airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104290911A true CN104290911A (en) | 2015-01-21 |
Family
ID=52310916
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410565201.6A Pending CN104290911A (en) | 2014-10-22 | 2014-10-22 | Reinforcing footstand of business class seat of airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104290911A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6749266B2 (en) * | 2001-11-21 | 2004-06-15 | B E Aerospace, Inc. | Locking collar for passenger seat back recline assembly |
| CN101492095A (en) * | 2008-12-17 | 2009-07-29 | 航宇救生装备有限公司 | Integral energy-absorbing aviation 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 |
| WO2013109751A1 (en) * | 2012-01-17 | 2013-07-25 | Zodiac Seats Us Llc | Passenger seat |
| CN203753410U (en) * | 2014-04-01 | 2014-08-06 | 湖北航宇嘉泰飞机设备有限公司 | Main structure of aero seat |
| CN104149980A (en) * | 2014-08-12 | 2014-11-19 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Magnesium alloy seat |
| CN204279959U (en) * | 2014-10-22 | 2015-04-22 | 苏州华冲精密机械有限公司 | A kind of reinforcing runners of aircraft business class seat |
-
2014
- 2014-10-22 CN CN201410565201.6A patent/CN104290911A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6749266B2 (en) * | 2001-11-21 | 2004-06-15 | B E Aerospace, Inc. | Locking collar for passenger seat back recline assembly |
| CN101492095A (en) * | 2008-12-17 | 2009-07-29 | 航宇救生装备有限公司 | Integral energy-absorbing aviation 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 |
| WO2013109751A1 (en) * | 2012-01-17 | 2013-07-25 | Zodiac Seats Us Llc | Passenger seat |
| CN203753410U (en) * | 2014-04-01 | 2014-08-06 | 湖北航宇嘉泰飞机设备有限公司 | Main structure of aero seat |
| CN104149980A (en) * | 2014-08-12 | 2014-11-19 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Magnesium alloy seat |
| CN204279959U (en) * | 2014-10-22 | 2015-04-22 | 苏州华冲精密机械有限公司 | A kind of reinforcing runners of aircraft business class seat |
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Legal Events
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|---|---|---|---|
| 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 |