CN215205388U - Mounting connecting piece for aviation seat - Google Patents
Mounting connecting piece for aviation seat Download PDFInfo
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- CN215205388U CN215205388U CN202120900390.3U CN202120900390U CN215205388U CN 215205388 U CN215205388 U CN 215205388U CN 202120900390 U CN202120900390 U CN 202120900390U CN 215205388 U CN215205388 U CN 215205388U
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- connecting piece
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Abstract
The utility model discloses an installation connecting piece for an aviation seat, which comprises a mounting plate, wherein one side of the top of the mounting plate is fixedly connected with a supporting plate, the top of the supporting plate is fixedly connected with a first connecting plate, the top of the first connecting plate is fixedly connected with two symmetrical mounting blocks, one side of the two mounting blocks is respectively provided with a first mounting hole, one end of the mounting plate is rotatably connected with a second connecting plate through a rotating shaft, the top of the second connecting plate is provided with a second mounting hole, the mounting plate comprises a wear-resistant layer, a first firm layer and a first base layer, the inner side of the wear-resistant layer is fixedly connected with the first firm layer, the installation connecting piece for the aviation seat has better wear resistance and firmness, the mounting connecting piece is not easy to break during use, the service life of the installation connecting piece is longer, the installation connecting piece has a supporting structure, and the stability between the structures of the installation connecting piece is better, so that the practicability of the mounting connecting piece is higher.
Description
Technical Field
The utility model relates to an aviation seat technical field specifically is an erection joint spare that aviation seat used.
Background
The seat is a piece of seating equipment with a backrest, some also with armrests, according to the classification of use: airport seat, car seat, bus seat, family's seat, dining room seat, children's safety seat, leisure seat etc. current one kind is used for the aviation seat on the aircraft, and the aviation seat need use erection joint spare to install.
The existing installing connecting piece does not have good wear resistance and firmness, is easy to break during use, has short service life, does not have a supporting structure, and has poor stability between the structures, so that the practicability of the installing connecting piece is poor.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a erection joint spare that aviation seat was used to solve current erection joint spare that proposes in the above-mentioned background art and do not have better wearability and tightness, easy breaking occur during the use, erection joint spare's life is shorter, and erection joint spare does not have bearing structure, and stability between the erection joint spare structure is relatively poor, makes the relatively poor problem of erection joint spare's practicality.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an erection joint spare that aviation seat used, includes the mounting panel, one side fixedly connected with backup pad at mounting panel top, the first connecting plate of top fixedly connected with of backup pad, the installation piece of two symmetries of top fixedly connected with of first connecting plate, two first mounting hole has all been seted up to one side of installation piece, the one end of mounting panel is rotated through the pivot and is connected with the second connecting plate, the second mounting hole has been seted up at the top of second connecting plate, the mounting panel includes wearing layer, first firm layer and first basic unit, the first firm layer of inboard fixedly connected with of wearing layer, the first basic unit of inboard fixedly connected with on first firm layer.
As a preferred technical scheme of the utility model, the first stabilizer plate of opposite side fixedly connected with at mounting panel top, one end of first stabilizer plate and one side fixed connection of backup pad.
As an optimized technical scheme of the utility model, it is provided with a plurality of support columns to fix between first stabilising plate and the backup pad.
As a preferred technical scheme of the utility model, the opposite side fixedly connected with second stabilising plate of backup pad, the one end of second stabilising plate and the bottom fixed connection of first connecting plate, the fixed stabilizing block that is provided with between second stabilising plate and the first connecting plate.
As an optimized technical scheme of the utility model, four evenly distributed screw thread posts of bottom fixedly connected with of mounting panel.
As an optimal technical scheme of the utility model, the third mounting hole has all been seted up to four corners at mounting panel top.
As an optimized technical scheme of the utility model, it is a plurality of the support column all includes the firm layer of second and second basic unit, the inboard fixedly connected with second basic unit on the firm layer of second.
Compared with the prior art, the beneficial effects of the utility model are that: erection joint spare has better wearability and tightness, is difficult for breaking occur when using, and erection joint spare's life is longer, and erection joint spare has bearing structure, and stability between the erection joint spare structure is better for erection joint spare's practicality is higher.
Drawings
Fig. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of the mounting plate structure of the present invention;
fig. 3 is a schematic view of the structure of the support pillar of the present invention.
In the figure: 1. mounting a plate; 2. a support plate; 3. a first connecting plate; 4. mounting blocks; 5. a first mounting hole; 6. a second connecting plate; 7. a second mounting hole; 8. a wear layer; 9. a first solid layer; 10. a first base layer; 11. a first stabilizer plate; 12. a support pillar; 13. a second stabilizing plate; 14. a threaded post; 15. a second solid layer; 16. a second base layer.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-3, the utility model provides a mounting connector for an aviation seat, which comprises a mounting plate 1, a supporting plate 2 fixedly connected to one side of the top of the mounting plate 1, a first connecting plate 3 fixedly connected to the top of the supporting plate 2, two symmetrical mounting blocks 4 fixedly connected to the top of the first connecting plate 3, a first mounting hole 5 formed on one side of each of the two mounting blocks 4, a second connecting plate 6 rotatably connected to one end of the mounting plate 1 through a rotating shaft, a second mounting hole 7 formed on the top of the second connecting plate 6, a wear-resistant layer 8 formed on the mounting plate 1, the wear-resistant layer comprises a first solid layer 9 and a first base layer 10, the first solid layer 9 is fixedly connected to the inner side of the wear-resistant layer 8, the first base layer 10 is fixedly connected to the inner side of the first solid layer 9, the wear-resistant layer 8 is made of silicon dioxide, the first solid layer 9 is made of metal chromium, and the first base layer 10 is made of stainless steel.
Preferably, the other side of the top of the mounting plate 1 is fixedly connected with a first stabilizing plate 11, and one end of the first stabilizing plate 11 is fixedly connected with one side of the supporting plate 2, so that the stability of the connecting piece can be maintained.
Preferably, a plurality of support columns 12 are fixedly arranged between the first stabilizing plate 11 and the support plate 2, so that the firmness of the connecting piece structure is enhanced.
Preferably, the other side fixedly connected with second stabilizer plate 13 of backup pad 2, the one end of second stabilizer plate 13 and the bottom fixed connection of first connecting plate 3, the fixed stabilizer that is provided with between second stabilizer plate 13 and the first connecting plate 3 has further strengthened the shock resistance of erection joint spare for erection joint spare's result of use is better.
Preferably, four evenly distributed threaded columns 14 are fixedly connected to the bottom of the mounting plate 1, so that the connection of the mounting connecting piece is facilitated.
Preferably, four corners at the top of the mounting plate 1 are provided with third mounting holes, so that the mounting work of the connecting piece is facilitated.
Preferably, the plurality of supporting columns 12 each include a second solid layer 15 and a second base layer 16, the second base layer 16 is fixedly connected to the inner side of the second solid layer 15, the second solid layer 15 is made of chromium metal, and the second base layer 16 is made of stainless steel, so that the supporting columns 12 are higher in mechanical strength and are not easy to break.
When in specific use, the utility model relates to an installation connecting piece for an aviation seat, firstly, the other side of a supporting plate 2 is fixedly connected with a second stabilizing plate 13, one end of the second stabilizing plate 13 is fixedly connected with the bottom of a first connecting plate 3, a stabilizing block is fixedly arranged between the second stabilizing plate 13 and the first connecting plate 3, the shock resistance of the installation connecting piece is further enhanced, the using effect of the installation connecting piece is better, the other side of the top of a mounting plate 1 is fixedly connected with a first stabilizing plate 11, one end of the first stabilizing plate 11 is fixedly connected with one side of the supporting plate 2, the stability of the connecting piece can be kept, a plurality of supporting columns 12 are fixedly arranged between the first stabilizing plate 11 and the supporting plate 2, the firmness degree between the connecting piece structures is enhanced, the plurality of supporting columns 12 comprise a second firm layer 15 and a second base layer 16, the inner side of the second firm layer 15 is fixedly connected with a second base layer 16, the second solid layer 15 is made of chromium metal, and the second base layer 16 is made of stainless steel, so that the support column 12 has higher mechanical strength and is not easy to break.
Although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments or portions thereof without departing from the spirit and scope of the invention.
Claims (7)
1. The utility model provides a erection joint spare that aviation seat was used, includes mounting panel (1), its characterized in that: one side fixedly connected with backup pad (2) at mounting panel (1) top, the first connecting plate (3) of top fixedly connected with of backup pad (2), the installation piece (4) of two symmetries of top fixedly connected with of first connecting plate (3), two first mounting hole (5) have all been seted up to one side of installation piece (4), the one end of mounting panel (1) is rotated through the pivot and is connected with second connecting plate (6), second mounting hole (7) have been seted up at the top of second connecting plate (6), mounting panel (1) includes wearing layer (8), first firm layer (9) and first basic unit (10), the first firm layer (9) of inboard fixedly connected with of wearing layer (8), the first basic unit (10) of inboard fixedly connected with of first firm layer (9).
2. A mounting attachment for an aircraft seat as defined in claim 1, wherein: the other side fixedly connected with at mounting panel (1) top has first stabilizer plate (11), one end of first stabilizer plate (11) and one side fixed connection of backup pad (2).
3. A mounting attachment for an aircraft seat as defined in claim 2, wherein: a plurality of supporting columns (12) are fixedly arranged between the first stabilizing plate (11) and the supporting plate (2).
4. A mounting attachment for an aircraft seat as defined in claim 1, wherein: the other side fixedly connected with second stabilizer plate (13) of backup pad (2), the one end of second stabilizer plate (13) and the bottom fixed connection of first connecting plate (3), it is provided with the stabilizing block to fix between second stabilizer plate (13) and first connecting plate (3).
5. A mounting attachment for an aircraft seat as defined in claim 1, wherein: the bottom fixedly connected with of mounting panel (1) has four even screw thread posts (14) of distribution.
6. A mounting attachment for an aircraft seat as defined in claim 1, wherein: and the four corners at the top of the mounting plate (1) are provided with third mounting holes.
7. A mounting link for an aerial seat as defined in claim 3, wherein: the supporting columns (12) comprise second solid layers (15) and second base layers (16), and the inner sides of the second solid layers (15) are fixedly connected with the second base layers (16).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120900390.3U CN215205388U (en) | 2021-04-28 | 2021-04-28 | Mounting connecting piece for aviation seat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120900390.3U CN215205388U (en) | 2021-04-28 | 2021-04-28 | Mounting connecting piece for aviation seat |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215205388U true CN215205388U (en) | 2021-12-17 |
Family
ID=79447418
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120900390.3U Active CN215205388U (en) | 2021-04-28 | 2021-04-28 | Mounting connecting piece for aviation seat |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215205388U (en) |
-
2021
- 2021-04-28 CN CN202120900390.3U patent/CN215205388U/en active Active
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