CN208007301U - Aero seat storage bin cover board controls skeleton - Google Patents
Aero seat storage bin cover board controls skeleton Download PDFInfo
- Publication number
- CN208007301U CN208007301U CN201820253953.2U CN201820253953U CN208007301U CN 208007301 U CN208007301 U CN 208007301U CN 201820253953 U CN201820253953 U CN 201820253953U CN 208007301 U CN208007301 U CN 208007301U
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- China
- Prior art keywords
- cam
- shaft
- cover board
- storage bin
- bin cover
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Abstract
The utility model is related to aero seat storage bin cover boards to control skeleton, which is characterized in that including two pieces of supporting plates and shaft, two pieces of supporting plate intervals setting；Shaft both ends are connect with two pieces of supporting plates respectively；The shaft rotatably arranged with；It is set with convex block in the shaft；Described convex block one end, which is sleeved in the shaft and links with the shaft, to be arranged；Cam is provided on the supporting plate, the cam is rotatably arranged on the supporting plate；The cam has arc notch；Its other end is always positioned in the arc notch in the convex block rotation process；When the cam rotation, arc notch both ends can drive the convex block other end to rotate.Aero seat storage bin cover board in the utility model controls skeleton, cover board is mounted in shaft, between shaft and supporting rod.Cover board can will be put between the article axis of rotation and supporting rod in storage space after opening, and closing can be by the space-closed between supporting rod and shaft after cover board.
Description
Technical field
The utility model is related to a kind of aero seat storage bin cover boards to control skeleton.
Background technology
Aircraft is one of Modern Traffic main tool.Aircraft space is limited, as can improving the space availability ratio in aircraft, is
Cost-effective important channel.Aircraft seat is the important component on aircraft.In use, there are one below Chain cushion
Fixed space.As can the space below cushion is used, it is greatly improved the effective rate of utilization of aircraft space.Below cushion
Although space can be used for storing some essential items or some articles that are indispensable but being of little use.But if storing article, such as
Fruit is not provided with corresponding cover board, and the article of storage is easy for being scattered.If setting cover board, the opening of cover board and closes and becomes
Problem.
Utility model content
One of the purpose of this utility model is to provide a kind of aviation easy to use to overcome deficiency in the prior art
Seat storage bin cover board controls skeleton.
In order to achieve the above object, the utility model is achieved through the following technical solutions：
Aero seat storage bin cover board controls skeleton, which is characterized in that including two pieces of supporting plates and shaft, two pieces of branch
Frame plate interval is arranged；Shaft both ends are connect with two pieces of supporting plates respectively；The shaft rotatably arranged with；It is set in the shaft
There is convex block；Described convex block one end, which is sleeved in the shaft and links with the shaft, to be arranged；It is provided on the supporting plate convex
Wheel, the cam are rotatably arranged on the supporting plate；The cam has arc notch；In the convex block rotation process
Its other end is always positioned in the arc notch；When the cam rotation, arc notch both ends can drive the convex block another
End rotation.
One embodiment according to the present utility model further includes elasticity reset device, and the cam makes the bullet when rotating
Property resetting apparatus deformation and generate elastic deformation force, elastic deformation force makes the cam return.
One embodiment according to the present utility model, the elasticity reset device are extension spring.
One embodiment according to the present utility model, the cam are rotatably arranged in the supporting plate by axis pin
On；The axis pin and/or the cam rotatably arranged with.
One embodiment according to the present utility model is provided with connecting rod on the cam, and described connecting rod one end is plugged on institute
It states on cam, described extension spring one end is fixedly connected on the supporting plate, and the other end is connect with connecting rod；The cam and institute
When stating axis pin rotation, the extension spring stretcher strain is made by the connecting rod.
One embodiment according to the present utility model further includes supporting rod, and the supporting rod is arranged above the shaft
Aero seat storage bin cover board in the utility model controls skeleton, and cover board is mounted in shaft, is located at shaft
Between supporting rod.Cover board can will be put between the article axis of rotation and supporting rod in storage space after opening, and closing can after cover board
By the space-closed between supporting rod and shaft.It can control the rotation of shaft using cam, you can that realizes cover board beats on and off
It closes.Other structure can be arranged to connect with cam, so as to passenger operation cam.Extension spring is set to deform and produce after cam rotation
Raw elastic deformation force, can make cam automatically reset using the elastic deformation force of spring.Shaft is driven by convex block when cam return
It resets.Therefore, the utility model is easy to use, can effectively improve the effective rate of utilization of aircraft space.
Description of the drawings
FIG. 1 is a schematic structural view of the utility model.
Fig. 2 is that the utility model omits the structural schematic diagram after supporting rod.
Fig. 3 is the utility model partial structural diagram.
Specific implementation mode
The utility model is described in detail with reference to embodiment.
As shown in Figure 1, Figure 2 and Figure 3, aero seat storage bin cover board controls skeleton comprising two pieces of supporting plates 10 and turns
Axis 20, two pieces of supporting plates 10 interval setting；20 both ends of shaft are connect with two pieces of supporting plates 10 respectively；The shaft 20 can turn
It is arranged dynamicly.Convex block 30 is set in the shaft 20；30 one end of the convex block be sleeved in the shaft 20 and with described turn
The linkage setting of axis 20.Cam 40 is provided on the supporting plate 10, the cam 40 can rotationally be sleeved on axis pin around axis pin 44
On 44.Axis pin 44 is fixedly installed.By axis pin 44, cam 40 is rotatably arranged on supporting plate 10.The cam 40 has
Arc notch 41.Its other end is always positioned in the arc notch 41 in 30 rotation process of the convex block；40 turns of the cam
When dynamic, arc notch both ends 42 can drive 30 other end of the convex block to rotate.Connecting rod 45 is provided on cam 40.45 one end of connecting rod
It is plugged on cam 40.
The utility model further includes elasticity reset device, the cam 40 make when rotating the elasticity reset device deform and
Elastic deformation force is generated, elastic deformation force makes the cam 40 reset.One embodiment according to the present utility model, the elasticity
Resetting apparatus is extension spring 50.50 one end of the extension spring is fixedly connected on the supporting plate 10, the other end with it is described
Connecting rod 45 connects；When the cam 40 is rotated with the axis pin 44,50 stretcher strain of the extension spring is made by connecting rod 45.
One embodiment according to the present utility model, further includes supporting rod 60, and the supporting rod 60 is arranged in the shaft
44 tops.
When the utility model is used, it is the opening of storage space below aero seat between shaft 20 and supporting rod 60.Lid
Plate (not shown) one end is connected in shaft 20, and the other end is freely arranged.Cover board will be between supporting rod 60 and shaft 20
Closing can control the opening of storage space and close.Cam 40 is rotated by 30 drive shaft 20 of convex block, and the rotation of shaft 20 drives
Cover board rotates synchronously, and realizes the opening and closing of storage space.
Aero seat storage bin cover board in the utility model controls skeleton, and cover board is mounted in shaft, is located at shaft
Between supporting rod.Cover board can will be put between the article axis of rotation and supporting rod in storage space after opening, and closing can after cover board
By the space-closed between supporting rod and shaft.It can control the rotation of shaft using cam, you can that realizes cover board beats on and off
It closes.Other structure can be arranged to connect with cam, so as to passenger operation cam.Extension spring is set to deform and produce after cam rotation
Raw elastic deformation force, can make cam automatically reset using the elastic deformation force of spring.Shaft is driven by convex block when cam return
It resets.Therefore, the utility model is easy to use, can effectively improve the effective rate of utilization of aircraft space.
The embodiments of the present invention are only used for illustrating the utility model, do not constitute to right
Limitation, other substantially equivalent replacements that those skilled in that art are contemplated that, in scope of protection of the utility model
It is interior.
Claims (6)
1. aero seat storage bin cover board controls skeleton, which is characterized in that including two pieces of supporting plates and shaft, two pieces of holders
Plate interval is arranged；Shaft both ends are connect with two pieces of supporting plates respectively；The shaft rotatably arranged with；It is set in the shaft
Convex block；Described convex block one end, which is sleeved in the shaft and links with the shaft, to be arranged；It is provided with cam on the supporting plate,
The cam is rotatably arranged on the supporting plate；The cam has arc notch；Its in the convex block rotation process
The other end is always positioned in the arc notch；When the cam rotation, arc notch both ends can drive the convex block other end
Rotation.
2. aero seat storage bin cover board according to claim 1 controls skeleton, which is characterized in that further include elastic reset
Device, the cam make the elasticity reset device deform and generate elastic deformation force when rotating, elastic deformation force makes described convex
Wheel resets.
3. aero seat storage bin cover board according to claim 2 controls skeleton, which is characterized in that the elastic reset dress
It is set to extension spring.
4. aero seat storage bin cover board according to claim 3 controls skeleton, which is characterized in that the cam passes through pin
Axis is rotatably arranged on the supporting plate；The axis pin and/or the cam rotatably arranged with.
5. aero seat storage bin cover board according to claim 4 controls skeleton, which is characterized in that be arranged on the cam
There are connecting rod, described connecting rod one end to be plugged on the cam, described extension spring one end is fixedly connected on the supporting plate, separately
One end is connect with connecting rod；When the cam is rotated with the axis pin, the extension spring stretcher strain is made by the connecting rod.
6. aero seat storage bin cover board according to claim 1 controls skeleton, which is characterized in that further include supporting rod,
The supporting rod is arranged above the shaft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820253953.2U CN208007301U (en) | 2018-02-12 | 2018-02-12 | Aero seat storage bin cover board controls skeleton |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820253953.2U CN208007301U (en) | 2018-02-12 | 2018-02-12 | Aero seat storage bin cover board controls skeleton |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208007301U true CN208007301U (en) | 2018-10-26 |
Family
ID=63886732
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820253953.2U Active CN208007301U (en) | 2018-02-12 | 2018-02-12 | Aero seat storage bin cover board controls skeleton |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208007301U (en) |
-
2018
- 2018-02-12 CN CN201820253953.2U patent/CN208007301U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190624 Address after: No. 788 Shanlian Road, Baoshan City Industrial Park, Shanghai, 2004 Patentee after: GLOBAL ADVANCED TECHNOLOGY Group Ltd. Address before: Two Blocks 788 Shanlian Road, Baoshan District, Shanghai, 2004 Patentee before: SHANGHAI GAOBO AVIATION TECHNOLOGY CO.,LTD. |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230615 Address after: 200444 3rd floor factory building, Building 3, No. 788 Shanlian Road, Baoshan District, Shanghai Patentee after: Shanghai Gaobo Aviation Manufacturing Co.,Ltd. Address before: No. 788 Shanlian Road, Baoshan City Industrial Park, Shanghai, 2004 Patentee before: GLOBAL ADVANCED TECHNOLOGY Group Ltd. |
|
| TR01 | Transfer of patent right |