CN209889126U - Parallel and level guide rail for adjusting position of aviation seat - Google Patents
Parallel and level guide rail for adjusting position of aviation seat Download PDFInfo
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- CN209889126U CN209889126U CN201920634959.9U CN201920634959U CN209889126U CN 209889126 U CN209889126 U CN 209889126U CN 201920634959 U CN201920634959 U CN 201920634959U CN 209889126 U CN209889126 U CN 209889126U
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Abstract
The utility model relates to an aviation seat installs technical field, especially relate to an aviation seat is parallel and level guide rail for position control, comprising a base plate, the relative division has first mounting hole on the bottom plate, the relative fixed mounting has the guide rail on the bottom plate, be equipped with the slide in the guide rail, slide bottom fixed mounting has the gyro wheel, the bottom sets up the spout with gyro wheel complex in the guide rail, the slide is fixed with first support one end, the first support other end stretches out the guide rail and fixes with the mounting bracket, be equipped with first mounting panel in the mounting bracket, first mounting panel bottom is connected with the bottom in the mounting bracket through first spring, first mounting panel top is connected with the top in the mounting bracket through the second spring, first mounting panel top is fixed with second support one end, the second support other end runs through the mounting bracket and fixes with; the utility model provides a technical scheme can effectively overcome not having seat position control function that prior art exists, does not have the defect of removing shock-absorbing function.
Description
Technical Field
The utility model relates to an aviation seat installs technical field, especially relates to an aviation seat is parallel and level guide rail for position control.
Background
With the rapid development of social economy and the improvement of living standard of people, people use more and more airplanes, and the installation technology of the aviation seat becomes a hot spot of social research. A guide rail is a groove or ridge made of metal or other material that can bear, secure, guide and reduce friction of a moving device or equipment. Longitudinal grooves or ridges on the surface of the guide rail for guiding, fixing machine parts, special equipment, instruments, etc. The guide rail is also called as a slide rail, a linear guide rail and a linear slide rail, is used in the linear reciprocating motion occasion, has a rated load higher than that of a linear bearing, can bear a certain torque, and can realize high-precision linear motion under the condition of high load, but the traditional aviation seat is not provided with the guide rail, so that the seat position cannot be adjusted, the damping function is not provided, and the use is inconvenient, therefore, the development of the parallel and level guide rail for adjusting the position of the aviation seat is a key for solving the problems.
The utility model discloses a be convenient for aircraft inside seat of installation is disclosed in the utility model patent of No. CN 208630866U, 2019.03.22 on the grant notice day, including cabin ground, the top fixedly connected with guide rail on cabin ground, the spout has been seted up at the top of guide rail, the inside joint of guide rail has the slide, the top of slide extends to the outside and the fixedly connected with seat body of spout on the guide rail. This aircraft is inside with seat convenient to installation, through the support that sets up, under the effect of second spring, can drive the inserted bar and peg graft in the first inside that leads to the chamber and the second leads to the chamber, go on fixed to the connecting block, thereby effectually going on fixed to the seat body, the stability of seat body when taking has been guaranteed to the passenger, under the effect of first spring, when drawing out the inserted bar in leading to the chamber from first, branch shifts out right through the elasticity of first spring, the staff has made things convenient for the dismantlement of seat, the time has been saved, the efficiency of work has been improved, avoid the delay to the flight.
However, such an aircraft interior seat that is easy to install does not have a seat position adjusting function and a movement damping function.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
To the above-mentioned shortcoming that prior art exists, the utility model provides an aviation seat is parallel and level guide rail for position control can effectively overcome not having seat position control function that prior art exists, does not have the defect of removing shock-absorbing function.
(II) technical scheme
In order to achieve the above purpose, the utility model discloses a following technical scheme realizes:
a first mounting hole is formed in the bottom plate in a relatively-opened mode, a guide rail is fixedly mounted on the bottom plate in a relatively-installed mode, a sliding plate is arranged in the guide rail, idler wheels are fixedly mounted at the bottom of the sliding plate, a sliding groove matched with the idler wheels is formed in the bottom of the guide rail, the sliding plate is fixed to one end of a first support, and the other end of the first support extends out of the guide rail and is fixed to a mounting frame;
a first mounting plate is arranged in the mounting frame, the bottom of the first mounting plate is connected with the inner bottom of the mounting frame through a first spring, the top of the first mounting plate is connected with the inner top of the mounting frame through a second spring, the top of the first mounting plate is fixed with one end of a second support, the other end of the second support penetrates through the mounting frame and is fixed with one end of a damping rod, the other end of the damping rod is fixed with the second mounting plate, a second mounting hole is formed in the second mounting plate in a relatively opened mode, and a through hole matched with the second support is formed in the mounting frame;
the improved sliding plate structure is characterized in that an air cylinder is arranged on the bottom plate and fixed with the bottom plate through a third support, the end part of the air cylinder is fixed with one end of a fourth support, the other end of the fourth support stretches into the guide rail and is fixed with the sliding plate, and a controller is fixedly mounted on the bottom plate.
Preferably, the controller model is STM32F103, the controller is supplied power by small-size battery, the cylinder is connected with the controller electricity.
Preferably, the guide rails are arranged in two numbers, the distances between the guide rails and the two ends of the bottom plate are equal, and the guide rails and the air cylinders are arranged on the same straight line.
Preferably, two first supports are fixedly mounted on each sliding plate, and the distances from the first supports to the two ends of the sliding plate are equal.
Preferably, sixteen first springs are arranged at the bottom of each first mounting plate, and the first springs are distributed along the bottom of the first mounting plate in an array manner.
Preferably, four second springs are arranged in each mounting frame and are uniformly distributed along the circumferential direction.
(III) advantageous effects
Compared with the prior art, the utility model provides an aviation seat is parallel and level guide rail for position control has following beneficial effect:
firstly, the bottom plate and the machine body can be fixed through the bolts and the first mounting holes, the second mounting plate and the aviation seat are fixed through the bolts and the second mounting holes, the installation is convenient, when the position of the aviation seat needs to be adjusted, the controller is used for controlling the cylinder to work, the fourth support is used for driving the sliding plate to move in the guide rail, and therefore the position of the aviation seat is adjusted, the parallel and level guide rail for adjusting the position of the aviation seat has a seat position adjusting function, and the use and later maintenance of passengers are facilitated;
second, the aircraft seat is removing and the in-process of using, the shock-absorbing pole plays the first order and cushions absorbing effect, improve passenger comfort in use, first mounting panel, first spring, the second spring plays the absorbing function of second level, every first mounting panel bottom is equipped with first spring sixteen, first spring distributes along first mounting panel bottom array and sets up, make the atress of first spring even, improve the shock attenuation effect, be equipped with four of second spring in every mounting bracket, the second spring sets up along circumferencial direction evenly distributed, make the second spring atress even, further improve the shock attenuation effect, make passenger comfort in use further improve, thereby make the parallel and level guide rail for aircraft seat position control have removal shock-absorbing function, be favorable to improving passenger comfort in use.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is a schematic view of the overall structure of the present invention;
fig. 2 is a left side view of the structure of fig. 1 according to the present invention;
FIG. 3 is a schematic top view of the structure of FIG. 1 according to the present invention;
FIG. 4 is a schematic view of the connection structure between the slide plate and the first bracket of the present invention;
FIG. 5 is a schematic structural view of the mounting frame and the through hole of the present invention;
in the figure: 1. a base plate; 2. a first mounting hole; 3. a guide rail; 4. a slide plate; 5. a roller; 6. a chute; 7. a first bracket; 8. a mounting frame; 9. a first mounting plate; 10. a first spring; 11. a second spring; 12. a second bracket; 13. a through hole; 14. a shock-absorbing lever; 15. a second mounting plate; 16. a second mounting hole; 17. a third support; 18. a cylinder; 19. a fourth bracket; 20. and a controller.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.
A level guide rail for adjusting the position of an aviation seat is disclosed, as shown in figures 1 to 5, and comprises a bottom plate 1, wherein a first mounting hole 2 is formed in the bottom plate 1 in a relatively opposite mode, a guide rail 3 is fixedly mounted on the bottom plate 1 in a relatively opposite mode, a sliding plate 4 is arranged in the guide rail 3, a roller 5 is fixedly mounted at the bottom of the sliding plate 4, a sliding groove 6 matched with the roller 5 is formed in the bottom of the guide rail 3, the sliding plate 4 is fixed with one end of a first bracket 7, and the other end of the first bracket 7 extends out of the guide rail 3;
a first mounting plate 9 is arranged in the mounting frame 8, the bottom of the first mounting plate 9 is connected with the inner bottom of the mounting frame 8 through a first spring 10, the top of the first mounting plate 9 is connected with the inner top of the mounting frame 8 through a second spring 11, the top of the first mounting plate 9 is fixed with one end of a second support 12, the other end of the second support 12 penetrates through the mounting frame 8 and is fixed with one end of a shock-absorbing rod 14, the other end of the shock-absorbing rod 14 is fixed with a second mounting plate 15, a second mounting hole 16 is formed in the second mounting plate 15 in a relatively opened mode, and a through hole 13 matched with the second support 12 is formed;
the bottom plate 1 is provided with a cylinder 18, the cylinder 18 is fixed with the bottom plate 1 through a third support 17, the end part of the cylinder 18 is fixed with one end of a fourth support 19, the other end of the fourth support 19 extends into the guide rail 3 and is fixed with the sliding plate 4, and the bottom plate 1 is fixedly provided with a controller 20.
Specifically, the controller 20 is STM32F103, the controller 20 is powered by a small storage battery, and the air cylinder 18 is electrically connected with the controller 20; two guide rails 3 are arranged, the distances between the guide rails 3 and the two ends of the bottom plate 1 are equal, and the guide rails 3 and the air cylinders 18 are arranged on the same straight line; two first supports 7 are fixedly arranged on each sliding plate 4, and the distances from the first supports 7 to the two ends of the sliding plate 4 are equal; sixteen first springs 10 are arranged at the bottom of each first mounting plate 9, and the first springs 10 are distributed along the bottom of the first mounting plate 9 in an array manner; four second springs 11 are arranged in each mounting frame 8, and the second springs 11 are uniformly distributed along the circumferential direction.
When the seat is used, the bottom plate 1 and the machine body can be fixed through the bolts and the first mounting holes 2, the second mounting plate 15 and the aviation seat are fixed through the bolts and the second mounting holes 16, the installation is convenient, when the position of the aviation seat needs to be adjusted, the controller 20 is used for controlling the cylinder 18 to work, and the fourth support 19 is used for driving the sliding plate 4 to move in the guide rail 3, so that the position of the aviation seat is adjusted, the parallel and level guide rail for adjusting the position of the aviation seat has a seat position adjusting function, and the use and later maintenance of passengers are facilitated; aviation seat is removing and the in-process of using, shock-absorbing rod 14 plays first order shock attenuation effect, improve passenger comfort in use, first mounting panel 9, first spring 10, second spring 11 plays the second level absorbing function, every first mounting panel 9 bottom is equipped with first spring 10 sixteen, first spring 10 distributes along first mounting panel 9 bottom array and sets up, make first spring 10's atress even, improve the shock attenuation effect, be equipped with 11 four of second spring in every mounting bracket 8, second spring 11 sets up along circumferencial direction evenly distributed, make 11 atress of second spring even, further improve the shock attenuation effect, make passenger comfort in use further improve, thereby make the parallel and level guide rail for the regulation of aviation seat position have removal shock-absorbing function, be favorable to improving passenger comfort in use.
The present invention discloses the type of the controller 20, and the internal structure and the pin function of the electrical components involved in the present application are the common knowledge of those skilled in the art, and those skilled in the art have the ability to establish the circuit connection relationship between the electrical components.
The above embodiments are only used to illustrate the technical solution of the present invention, and not to limit it; although the present invention has been described in detail with reference to the foregoing embodiments, it will be understood by those skilled in the art; the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; such modifications and substitutions do not depart from the spirit and scope of the present invention in its corresponding aspects.
Claims (6)
1. The utility model provides an aviation seat is parallel and level guide rail for position control which characterized in that: the device comprises a bottom plate (1), wherein first mounting holes (2) are formed in the bottom plate (1) in a relatively-opened mode, guide rails (3) are fixedly mounted on the bottom plate (1) in a relatively-fixed mode, sliding plates (4) are arranged in the guide rails (3), idler wheels (5) are fixedly mounted at the bottoms of the sliding plates (4), sliding grooves (6) matched with the idler wheels (5) are formed in the bottoms of the guide rails (3), the sliding plates (4) are fixed with one ends of first supports (7), and the other ends of the first supports (7) extend out of the guide rails (3) and are fixed with mounting frames (8);
a first mounting plate (9) is arranged in the mounting frame (8), the bottom of the first mounting plate (9) is connected with the inner bottom of the mounting frame (8) through a first spring (10), the top of the first mounting plate (9) is connected with the inner top of the mounting frame (8) through a second spring (11), the top of the first mounting plate (9) is fixed with one end of a second support (12), the other end of the second support (12) penetrates through the mounting frame (8) and is fixed with one end of a shock absorption rod (14), the other end of the shock absorption rod (14) is fixed with a second mounting plate (15), a second mounting hole (16) is formed in the second mounting plate (15) in a relatively-opened mode, and a through hole (13) matched with the second support (12) is formed in the mounting frame (8);
be equipped with cylinder (18) on bottom plate (1), cylinder (18) are fixed with bottom plate (1) through third support (17), cylinder (18) tip is fixed with fourth support (19) one end, fourth support (19) other end stretches into guide rail (3) and is fixed with slide (4), fixed mounting has controller (20) on bottom plate (1).
2. The flush rail for adjusting the position of an aircraft seat according to claim 1, wherein: the controller (20) model is STM32F103, controller (20) are supplied power by small-size battery, cylinder (18) and controller (20) electrical connection.
3. The flush rail for adjusting the position of an aircraft seat according to claim 1, wherein: the guide rail (3) are provided with two, the distance between the guide rail (3) and the two ends of the bottom plate (1) is equal, and the guide rail (3) and the cylinder (18) are arranged on the same straight line.
4. The flush rail for adjusting the position of an aircraft seat according to claim 1, wherein: every fixed mounting has two first support (7) on slide (4), first support (7) are apart from the distance of slide (4) both ends and are equal.
5. The flush rail for adjusting the position of an aircraft seat according to claim 1, wherein: sixteen first springs (10) are arranged at the bottom of each first mounting plate (9), and the first springs (10) are distributed along the bottom of the first mounting plate (9) in an array manner.
6. The flush rail for adjusting the position of an aircraft seat according to claim 1, wherein: every be equipped with second spring (11) four in mounting bracket (8), second spring (11) set up along circumferencial direction evenly distributed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920634959.9U CN209889126U (en) | 2019-05-06 | 2019-05-06 | Parallel and level guide rail for adjusting position of aviation seat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920634959.9U CN209889126U (en) | 2019-05-06 | 2019-05-06 | Parallel and level guide rail for adjusting position of aviation seat |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209889126U true CN209889126U (en) | 2020-01-03 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920634959.9U Active CN209889126U (en) | 2019-05-06 | 2019-05-06 | Parallel and level guide rail for adjusting position of aviation seat |
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| Country | Link |
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| CN (1) | CN209889126U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111571304A (en) * | 2020-05-25 | 2020-08-25 | 重庆工业职业技术学院 | High-precision electromechanical integrated control device |
| CN114771843A (en) * | 2022-06-16 | 2022-07-22 | 中国飞机强度研究所 | Seat vibration damping system in aviation aircraft manufacturing and vibration damping method thereof |
-
2019
- 2019-05-06 CN CN201920634959.9U patent/CN209889126U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111571304A (en) * | 2020-05-25 | 2020-08-25 | 重庆工业职业技术学院 | High-precision electromechanical integrated control device |
| CN114771843A (en) * | 2022-06-16 | 2022-07-22 | 中国飞机强度研究所 | Seat vibration damping system in aviation aircraft manufacturing and vibration damping method thereof |
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