CN208360503U - The metal plate shell of aero seat and the connection structure of skeleton - Google Patents
The metal plate shell of aero seat and the connection structure of skeleton Download PDFInfo
- Publication number
- CN208360503U CN208360503U CN201820837497.6U CN201820837497U CN208360503U CN 208360503 U CN208360503 U CN 208360503U CN 201820837497 U CN201820837497 U CN 201820837497U CN 208360503 U CN208360503 U CN 208360503U
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- China
- Prior art keywords
- skeleton
- parts
- metal plate
- plate shell
- pipe
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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.)
- Expired - Fee Related
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- Connection Of Plates (AREA)
- Mutual Connection Of Rods And Tubes (AREA)
Abstract
The utility model connect needs the technical issues of drilling on carbon fiber pipe to solve the metal plate shell of aero seat in the prior art with skeleton, provides a kind of metal plate shell of aero seat and the connection structure of skeleton.Including metal plate shell and skeleton, skeleton is square, is interconnected by four L shape pipe fittings by two parts head and the tail;Pipe fitting is made of inner layer metal pipe and outer layer carbon fiber pipe, and the both ends of metal tube are exposed to outside carbon fiber pipe;There is insertion hole, metal tube is fixed by bolts into after inserting in the hole in two connectors of two parts;It is provided with the arc bound edge being coated in two parts at corresponding two parts of metal plate shell, arc bound edge is bolted on the middle interconnecting piece of two parts, avoids and drill on carbon fiber pipe.
Description
Technical field
The utility model relates to aero seat technical fields.
Background technique
Carbon fiber is high intensity, the new fiber materials of high modulus fibre of a kind of phosphorus content 95% or more.It is by piece
The organic fibers such as shape graphite microcrystal are piled up along fiber axial direction, through micro crystal graphite obtained from carbonization and graphitization processing
Material.Carbon fibre composite light weight, intensity are high, in the case where meeting structural member performance requirement, can subtract with metal phase ratio
Weigh 70%~80%;Carbon fibre composite also has good fatigue durability and corrosion resistance, and noise is small, vibration declines
Subtracting property is good, safety is good, is particularly suitable for production aero seat skeleton.
Aero seat has metal plate coverboard, is mounted on the cladding foam that support seat is used on skeleton.But carbon fiber
Skeleton and metal material coverboard between can not using be welded to connect, can only be bolted, still, the intensity of carbon fiber pipe
Greatly, hardness is high, and drilling easilys lead to skeleton and splits, and reduces the security performance of skeleton.
Utility model content
In order to solve the above-mentioned technical problem the utility model, redesigns the connection structure of metal plate shell and skeleton, no
Drilling can be achieved with metal plate shell on carbon fiber pipe and frame bolt is connected.
In order to achieve the above objectives, the technical solution of the utility model is as follows:
The metal plate shell of aero seat and the connection structure of skeleton, including metal plate shell and skeleton, the metal plate shell cover
It covers above the skeleton;The skeleton is square, is interconnected by four L shape pipe fittings by two parts head and the tail;The pipe
Part is made of inner layer metal pipe and outer layer carbon fiber pipe, and the both ends of the metal tube are exposed to outside the carbon fiber pipe;It is described
There is insertion hole, the metal tube is fixed by bolts into after inserting in the hole in two connectors of two parts;The metal plate shell
Body corresponds to the arc bound edge for being provided with and being coated in two parts at two parts, and the arc bound edge is bolted on institute
On the middle interconnecting piece for stating two parts.
Further, the cross section of the inner layer metal pipe is regular hexagon, two parts are inserted into the transversal of hole
Face is and the matched regular hexagon of the metal tube.
Further, the carbon fiber pipe is cylinder, it is entwined outside the metal tube by carbon cloth.
Further, being provided with one piece of height and the arc bound edge on the outer wall of the middle interconnecting piece of two parts
The circular bosses of thickness matching have screw thread hole in the circular bosses;The arc bound edge, which corresponds to, is provided with appearance at the circular bosses
The circular hole of the circular bosses insertion, after the arc bound edge is coated on the middle interconnecting piece of two parts, the circle
Boss is located in the circular hole, then is locked into screw thread hole with bolt and fixes the two.
Compared with prior art, the utility model has the beneficial effects that the arc bound edge of 1. metal plate shells is solid using bolt
It is scheduled in two parts of metal in skeleton, avoids and drill on carbon fiber pipe;2. skeleton uses the structure of four root canal part assembly,
Easy to produce and assembling;3. inner layer metal pipe is designed to hexagonal structure, relative position that both pipe fitting is inserted into after two parts compared with
For fixation, the position that adjustment pipe fitting and two parts is no longer needed in unit is locked automatically in subsequent bolt, it is raw convenient for the assembling of skeleton
It produces.
Detailed description of the invention
It, below will be to required in embodiment description in order to illustrate more clearly of the technical scheme in the embodiment of the utility model
Attached drawing to be used is briefly described.
Fig. 1 is the structural schematic diagram of the skeleton of aero seat disclosed in embodiment one;
Fig. 2 is the structural schematic diagram of two parts disclosed in embodiment one;
The structural schematic diagram of metal plate shell disclosed in Fig. 3 embodiment one;
The structural schematic diagram of two parts disclosed in Fig. 4 embodiment two;
The side view of metal plate shell disclosed in Fig. 5 embodiment two.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe.
Embodiment one
It is the skeleton of aero seat shown in Fig. 1, is square, passes through two parts, 2 head and the tail by four L shape pipe fittings 1
It interconnects.Every root canal part is made of the inner layer metal pipe 1a and outer layer carbon fiber pipe 1b that cross section is regular hexagon;Metal
The both ends of pipe are exposed to outside carbon fiber pipe;Carbon fiber pipe is cylinder, is entwined outside metal tube by carbon cloth.Referring to figure
2, the interior insertion hole 2a with regular hexagon of two connectors of two parts, metal tube is fixed by bolts into after inserting in the hole.
It is metal plate shell shown in Fig. 3, the arc bound edge 3b bent downward including panel 3a and four.Metal plate is coated
In the top of skeleton, four arc bound edges are respectively coated by its corresponding two parts, are locked into two parts finally by bolt
Metal plate shell is connected with skeleton in middle interconnecting piece 2b.
Embodiment two
After the assembling of skeleton and metal plate shell generally uses production line, metal plate shell to be coated on skeleton, to be transferred to
Subsequent processing is locked by automatic locking screw machine structure.Opposite position occurs in transfer process for metal plate shell and skeleton in order to prevent
It moves, so the way of the present embodiment is as follows by Primary Location and fastening is carried out between metal plate shell and skeleton:
Referring to fig. 4, one piece of height and arc bound edge thickness matching are provided on the outer wall of the middle interconnecting piece 2b of two parts
Circular bosses 2c, there is in circular bosses screw thread hole 2d.Referring to Fig. 5, arc bound edge correspond to be provided at circular bosses hold circular bosses insert
The circular hole 3c entered, after arc bound edge is coated on the middle interconnecting piece of two parts, circular bosses are located in circular hole, then with bolt
It is locked into screw thread hole and fixes the two.
Various modifications to these embodiments will be readily apparent to those skilled in the art, herein
Defined General Principle can be real in other embodiments without departing from the spirit or scope of the present utility model
It is existing.Therefore, the present invention will not be limited to the embodiments shown herein, and be to fit to it is disclosed herein
Principle and the consistent widest scope of features of novelty.
Claims (4)
1. the metal plate shell of aero seat and the connection structure of skeleton, which is characterized in that including metal plate shell and skeleton, the metal plate
Golden shell body is covered on above the skeleton;The skeleton is square, is interconnected by four L shape pipe fittings by two parts head and the tail
At;The pipe fitting is made of inner layer metal pipe and outer layer carbon fiber pipe, and the both ends of the metal tube are exposed to the carbon fiber
Pipe is outer;There is insertion hole, the metal tube is fixed by bolts into after inserting in the hole in two connectors of two parts;
The metal plate shell corresponds to the arc bound edge for being provided with and being coated in two parts at two parts, and the arc bound edge passes through spiral shell
Bolt is fixed on the middle interconnecting piece of two parts.
2. the metal plate shell of aero seat according to claim 1 and the connection structure of skeleton, which is characterized in that in described
The cross section of layer metal tube is regular hexagon, and the cross section in the insertion hole of two parts is and the metal tube matched positive six
Side shape.
3. the metal plate shell of aero seat according to claim 2 and the connection structure of skeleton, which is characterized in that the carbon
Fibre pipe is cylinder, is entwined outside the metal tube by carbon cloth.
4. the metal plate shell of aero seat according to claim 3 and the connection structure of skeleton, which is characterized in that described two
The circular bosses of one piece of height with the arc bound edge thickness matching, the boss are provided on the outer wall of the middle interconnecting piece of parts
There is screw thread hole in platform;The arc bound edge corresponds to the circular hole for being provided at the circular bosses and holding the circular bosses insertion, works as institute
It states after arc bound edge is coated on the middle interconnecting piece of two parts, the circular bosses are located in the circular hole, then with spiral shell
Bolt-lock is into fixing the two in screw thread hole.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201820837497.6U CN208360503U (en) | 2018-05-31 | 2018-05-31 | The metal plate shell of aero seat and the connection structure of skeleton |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201820837497.6U CN208360503U (en) | 2018-05-31 | 2018-05-31 | The metal plate shell of aero seat and the connection structure of skeleton |
Publications (1)
Publication Number | Publication Date |
---|---|
CN208360503U true CN208360503U (en) | 2019-01-11 |
Family
ID=64931098
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201820837497.6U Expired - Fee Related CN208360503U (en) | 2018-05-31 | 2018-05-31 | The metal plate shell of aero seat and the connection structure of skeleton |
Country Status (1)
Country | Link |
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CN (1) | CN208360503U (en) |
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2018
- 2018-05-31 CN CN201820837497.6U patent/CN208360503U/en not_active Expired - Fee Related
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
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: 20190111 |