CN209870754U - Aviation seat adjusting device - Google Patents
Aviation seat adjusting device Download PDFInfo
- Publication number
- CN209870754U CN209870754U CN201920511855.9U CN201920511855U CN209870754U CN 209870754 U CN209870754 U CN 209870754U CN 201920511855 U CN201920511855 U CN 201920511855U CN 209870754 U CN209870754 U CN 209870754U
- Authority
- CN
- China
- Prior art keywords
- spring part
- aviation seat
- shock attenuation
- supporting shoe
- drive
- 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.)
- Expired - Fee Related
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Abstract
The utility model discloses an aviation seat adjusting device, including the aviation seat, aviation seat bottom fixed surface is provided with the shock attenuation spring part, and the shock attenuation spring part specifically is provided with a plurality of groups, shock attenuation spring part bottom fixed surface is provided with the backup pad, backup pad bottom one side is provided with the adjustment tank, backup pad bottom fixed surface is provided with the supporting shoe, and the supporting shoe specifically is provided with a plurality of groups. The utility model discloses a shock attenuation spring part can effectually alleviate the influence of external vibrations to the aircraft seat among the automobile driving process to improve personnel's of taking travelling comfort, through step motor, can effectually drive step screw and rotate, make and to drive the slider operation, and drive supporting shoe round trip movement under the drive of slider, pulley and slide rail simultaneously can reduce the frictional force of supporting shoe and adjustment tank inner wall again, make and advance to adjust the use to the aircraft seat easily, be fit for being extensively promoted and used.
Description
Technical Field
The utility model relates to an adjusting device, in particular to aviation seat adjusting device.
Background
The chair is a seat with a backrest and armrests. Ancient people sit on the ground without chairs, and the 'chair' originally is a wooden name.
A general aviation seat is not provided with an adjusting device, when a passenger needs to have a rest, the comfort of the aviation seat is poor, the adjustable aviation seat also appears in the prior art, but the problem of poor comfort still exists because the angle of the chair back of the aviation seat can only be adjusted.
SUMMERY OF THE UTILITY MODEL
The utility model discloses a main aim at provides an aviation seat adjusting device, through the shock attenuation spring part, can effectually alleviate the influence of external vibrations to aviation seat among the automobile driving process, thereby improve the travelling comfort of taking personnel, through step motor, can effectually drive step screw and rotate, make and to drive the slider operation, and drive the supporting shoe round trip movement under the drive of slider, pulley and slide rail simultaneously, can reduce the frictional force of supporting shoe and adjustment tank inner wall again, make and advance easily to adjust the use to aviation seat, can effectively solve the problem in the background art.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides an aviation seat adjusting device, includes the aviation seat, aviation seat bottom fixed surface is provided with the shock attenuation spring part, and the shock attenuation spring part specifically is provided with a plurality of groups, shock attenuation spring part bottom fixed surface is provided with the backup pad, backup pad bottom one side is provided with the adjustment tank, backup pad bottom fixed surface is provided with the supporting shoe, and the supporting shoe specifically is provided with a plurality of groups, adjustment tank outer wall one side fixed surface is provided with step motor, the adjustment tank inner chamber is provided with step screw, and step screw one end links to each other with the step motor output, step motor surface has concatenated the slider, and the slider passes through the support and links to each other with the supporting shoe, supporting shoe bottom fixed surface is provided with the pulley, adjustment tank inner chamber top.
Furthermore, a bearing is fixedly arranged on the surface of one side of the inner cavity of the adjusting groove, and one side of the bearing is movably connected with the stepping screw rod.
Further, a switch is fixedly arranged on one side surface of the aviation seat.
Further, a mounting plate is fixedly arranged on the surface of the bottom of the adjusting groove.
Further, the stepping motor is electrically connected with the switch through a lead.
Compared with the prior art, the utility model discloses following beneficial effect has:
1. through the shock attenuation spring part, can effectually alleviate the influence of external vibrations to aviation seat among the automobile driving process to can improve the travelling comfort of taking personnel, owing to set up multiunit shock attenuation spring part, and then improved aviation seat damping performance, through the backup pad, can effectually provide the support to the shock attenuation spring part.
2. When the aviation seat needs to be adjusted forwards and backwards, the stepping motor can be effectively controlled to operate through the switch, so that the stepping motor can drive the stepping screw to rotate, the sliding block can be driven to operate, and the two sides of the sliding block are connected with the supporting block through the support, so that the supporting block can be driven to operate under the operation of the sliding block.
3. And can reduce the frictional force of supporting shoe and adjustment tank inner wall again through the pulley for can advance to adjust easily and use, the slide rail can provide stable orbit again to the pulley simultaneously, makes the aviation seat more steady in accommodation process, through the bearing, can effectual improvement step-by-step screw rod pivoted stability, through the mounting panel, can effectually install the adjustment tank, and then can install the use to the aviation seat.
Drawings
Fig. 1 is the overall structure schematic diagram of the utility model relates to an aviation seat adjusting device.
Fig. 2 is the internal structure schematic diagram of the adjusting groove of the adjusting device for an aviation seat of the present invention.
Fig. 3 is a schematic side structure view of the utility model relates to an aviation seat adjusting device.
In the figure: 1. an airline seat; 2. a shock absorbing spring member; 3. a support plate; 4. an adjustment groove; 5. a support block; 6. a stepping motor; 7. a step screw; 8. a slider; 9. a pulley; 10. a slide rail; 11. a bearing; 12. a switch; 13. and (7) mounting the plate.
Detailed Description
In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.
As shown in fig. 1-3, the adjusting device for the aviation seat comprises an aviation seat 1, a damping spring part 2 is fixedly arranged on the surface of the bottom of the aviation seat 1, and the damping spring part 2 is provided with a plurality of groups, the surface of the bottom of the damping spring part 2 is fixedly provided with a supporting plate 3, an adjusting groove 4 is arranged at one side of the bottom of the supporting plate 3, a supporting block 5 is fixedly arranged on the surface of the bottom of the supporting plate 3, and a plurality of groups of supporting blocks 5 are arranged, a stepping motor 6 is fixedly arranged on the surface of one side of the outer wall of the adjusting groove 4, a stepping screw 7 is arranged in the inner cavity of the adjusting groove 4, one end of the stepping screw 7 is connected with the output end of the stepping motor 6, the surface of the stepping motor 6 is connected with a slide block 8 in series, and the sliding block 8 is connected with the supporting block 5 through a support, the bottom surface of the supporting block 5 is fixedly provided with a pulley 9, and the top surface of the inner cavity of the adjusting groove 4 is fixedly provided with a sliding rail 10.
As shown in fig. 1-3 in this embodiment, through shock attenuation spring part 2, can effectually alleviate the influence of external vibrations to aviation seat 1 among the automobile driving process, thereby improve the travelling comfort of taking personnel, through step motor 6, can effectually drive step screw 7 and rotate, make and to drive slider 8 operation, and drive supporting shoe 5 round trip movement under the drive of slider 8, pulley 9 and slide rail 10 simultaneously can reduce the frictional force of supporting shoe 5 and 4 inner walls of adjustment tank again, make and to advance easily to adjust the use to aviation seat 1.
Wherein, the surface of one side of the inner cavity of the adjusting groove 4 is fixedly provided with a bearing 11, and one side of the bearing 11 is movably connected with the stepping screw 7.
In this embodiment, as shown in fig. 2, the stability of the rotation of the stepping screw 7 can be effectively improved by the bearing 11.
Wherein, a switch 12 is fixedly arranged on one side surface of the aviation seat 1.
In this embodiment, as shown in fig. 1, the operation of the stepping motor 6 can be effectively controlled by the switch 12.
Wherein, the bottom surface of the adjusting groove 4 is fixedly provided with a mounting plate 13.
In the embodiment, as shown in fig. 1, the mounting plate 13 can effectively mount the adjustment groove 4, and thus the aircraft seat 1 can be mounted and used.
Wherein, the stepping motor 6 is electrically connected with the switch 12 through a lead.
It should be noted that, the utility model relates to an aviation seat adjusting device, during operation, when the passenger needs to have a rest, the influence of external vibration on the aviation seat 1 in the driving process of the automobile can be effectively reduced through the damping spring part 2, thereby improving the comfort of the passenger, because the damping spring parts 2 are arranged, the damping performance of the aviation seat 1 is improved, the damping spring part 2 can be effectively supported through the supporting plate 3, when the aviation seat 1 needs to be adjusted forwards and backwards, the stepping motor 6 can be effectively controlled to operate through the switch 12, so that the stepping motor 6 can drive the stepping screw 7 to rotate, thereby driving the slider 8 to operate, because the two sides of the slider 8 are connected with the supporting block 5 through the bracket, thereby the supporting block 5 can be driven to operate under the operation of the slider 8, and the friction force between the supporting block 5 and the inner wall of the adjusting groove 4 can be reduced through the pulley 9, the use of adjusting easily can advance, and slide rail 10 can provide stable orbit again to pulley 9 simultaneously for aviation seat 1 is more steady in accommodation process, through bearing 11, can effectual improvement step-by-step screw 7 pivoted stability, through mounting panel 13, can effectually install adjustment tank 4, and then can install aviation seat 1 and use.
The utility model relates to an aviation seat adjusting device, including aviation seat 1, shock attenuation spring part 2, backup pad 3, adjustment tank 4, supporting shoe 5, step motor 6, step screw 7, slider 8, pulley 9, slide rail 10, bearing 11, switch 12 and mounting panel 13, the part is the general standard component or the part that technical staff in the field knows, and its structure and principle all are this technical staff all can learn through the technical manual or learn through conventional experimental method.
The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (5)
1. An aircraft seat adjusting device, comprising an aircraft seat (1), characterized in that: the damping spring part (2) is fixedly arranged on the surface of the bottom of the aviation seat (1), a plurality of groups of damping spring parts (2) are specifically arranged, a supporting plate (3) is fixedly arranged on the surface of the bottom of each damping spring part (2), an adjusting groove (4) is arranged on one side of the bottom of each supporting plate (3), a supporting block (5) is fixedly arranged on the surface of the bottom of each supporting plate (3), a plurality of groups of supporting blocks (5) are specifically arranged on each supporting block, a stepping motor (6) is fixedly arranged on the surface of one side of the outer wall of each adjusting groove (4), a stepping screw rod (7) is arranged in the inner cavity of each adjusting groove (4), one end of each stepping screw rod (7) is connected with the output end of each stepping motor (6), a sliding block (8) is connected in series on the surface of each stepping motor (6), the, and a sliding rail (10) is fixedly arranged on the surface of the top of the inner cavity of the adjusting groove (4).
2. An aircraft seat adjustment device according to claim 1, wherein: and a bearing (11) is fixedly arranged on the surface of one side of the inner cavity of the adjusting groove (4), and one side of the bearing (11) is movably connected with the stepping screw rod (7).
3. An aircraft seat adjustment device according to claim 1, wherein: a switch (12) is fixedly arranged on the surface of one side of the aviation seat (1).
4. An aircraft seat adjustment device according to claim 1, wherein: and a mounting plate (13) is fixedly arranged on the surface of the bottom of the adjusting groove (4).
5. An aircraft seat adjustment device according to claim 1, wherein: the stepping motor (6) is electrically connected with the switch (12) through a lead.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920511855.9U CN209870754U (en) | 2019-04-15 | 2019-04-15 | Aviation seat adjusting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920511855.9U CN209870754U (en) | 2019-04-15 | 2019-04-15 | Aviation seat adjusting device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209870754U true CN209870754U (en) | 2019-12-31 |
Family
ID=68960192
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920511855.9U Expired - Fee Related CN209870754U (en) | 2019-04-15 | 2019-04-15 | Aviation seat adjusting device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209870754U (en) |
-
2019
- 2019-04-15 CN CN201920511855.9U patent/CN209870754U/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 |
Granted publication date: 20191231 Termination date: 20200415 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |