Aero seat control mechanism convenient to operate
By designing a storage slot and a motor-driven gear system, the touch screen of the aviation seat is hidden in the storage slot, which solves the aesthetics and mistouch problems caused by exposure of the control mechanism in the prior art, and improves the operation convenience of the seat and Passenger comfort.
Patent Information
- Application Number
- CN202421651030.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-07-12
- Publication Date
- 2024-12-20
- Estimated Expiration
- 2034-07-12
AI Technical Summary
The existing aviation seat control mechanism has shortcomings in hiding and storage, which leads to damage to the aesthetics of the armrests. Passengers cannot hide when they do not need to use functions, which may lead to accidental changes in seat settings when they are accidentally touched and increase passengers' uneasiness.
An aviation seat control mechanism including a storage groove, a motor, a driving gear, a driven gear, a sliding groove, a sliding block, a threaded rod and a screw rod are designed. The driving gear meshs the driven gear and drives the screw rod to rotate through the motor. , the threaded block drives the touch screen into or out of the storage slot, providing hidden space, and limits the movement trajectory through the sliding block, supporting the touch screen to avoid damage.
It realizes the hiding of the touch screen, keeps the handrails clean and beautiful, avoids mist touching, and improves the practicality of the control mechanism and the user experience of the passenger.
Smart Images
Figure CN222202897U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of aviation seat control mechanisms, in particular to an aviation seat control mechanism which is easy to operate. Background Art
[0002] Airline seat control mechanisms refer to a group of mechanical or electronic devices used to adjust various functions of airline seats (such as backrest angle, leg rest, headrest, etc.). In modern airline seat designs, these control mechanisms are often integrated into the touch screen on the armrest to facilitate intuitive and convenient operation by passengers.
[0003] The current design of the control mechanism of the airline seat does have some shortcomings, especially in terms of hidden storage. These control mechanisms are usually directly exposed on the surface of the armrest, which not only destroys the overall aesthetics of the armrest, but also makes it impossible for passengers to hide these functions when they do not need to use them, making it look messy. At the same time, during the flight, since the touch screen is exposed, passengers may accidentally change the seat settings by accidentally touching these control mechanisms, causing unnecessary trouble. In addition, for those passengers who seek privacy and a quiet environment, these exposed control mechanisms undoubtedly increase their sense of uneasiness. Therefore, we propose an easy-to-operate airline seat control mechanism. Utility Model Content
[0004] The purpose of the utility model is to provide an easy-to-operate aviation seat control mechanism to solve the problems mentioned in the background technology. The current aviation seat control mechanism design does have some shortcomings, especially in terms of hidden storage. These control mechanisms are usually directly exposed on the armrest surface, which not only destroys the overall aesthetics of the armrest, but also makes it impossible for passengers to hide these functions when they do not need to use them, making it look messy. At the same time, during the flight, since the touch screen is exposed, passengers may accidentally change the seat settings due to accidental touches on these control mechanisms, causing unnecessary trouble. In addition, for passengers who seek privacy and a quiet environment, these exposed control mechanisms undoubtedly increase their sense of uneasiness.
[0005] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: an easy-to-operate aviation seat control mechanism, comprising a seat body, armrests are fixedly installed on the front and rear surfaces of the seat body, a storage groove is provided on one side of the top of the armrest arranged at the front end, a touch screen is provided on one side of the storage groove, a transmission groove is provided on the bottom of the storage groove, a screw rod is provided in the center of the transmission groove, a threaded block is threadedly connected to one side of the surface of the screw rod, a motor is fixedly installed on one side of the top of the storage groove, a driving gear is provided at the lower end of the motor, a driven gear is fixedly installed on one side of the surface of the screw rod, sliding grooves are provided at the front and rear ends of one side of the top of the storage groove, two sliding blocks are fixedly installed on the top of the touch screen, and a supporting ball is rollingly installed on one side of the lower end of the touch screen.
[0006] Compared with the prior art, the beneficial effects of the utility model are:
[0007] The easy-to-operate aviation seat control mechanism is designed with a storage slot, a motor, a driving gear, a driven gear, a sliding slot, a sliding block, a threaded rod and a lead screw. The motor drives the driving gear to mesh with the driven gear to rotate, so that the threaded block drives the touch screen to move as the lead screw rotates, and the touch screen can enter or move out of the storage slot, providing a hidden space for the touch screen. When the passenger is not using the touch screen, it can be stored in the storage slot to keep the armrest surface clean and beautiful while preventing the passenger from accidentally touching the touch screen. The sliding of the sliding block in the sliding slot can limit the moving trajectory of the touch screen, thereby improving the practicality of the aviation seat control mechanism. The design of the supporting ball is used to support the touch screen to prevent the touch screen from being damaged by downward pressure when moving out of the storage slot, thereby facilitating operation. BRIEF DESCRIPTION OF THE DRAWINGS
[0008] Figure 1 It is a schematic diagram of the structure of the utility model;
[0009] Figure 2 This is a structural sectional view of the handrail of the utility model;
[0010] Figure 3 This is a structural stereogram of the touch screen of the utility model;
[0011] Figure 4 This is a top view of the structure of the touch screen of the utility model;
[0012] Figure 5 It is the front view of the structure of the utility model.
[0013] In the figure: 1. seat body; 2. armrest; 3. touch screen; 4. storage slot; 5. transmission slot; 6. motor; 7. driving gear; 8. driven gear; 9. sliding slot; 10. sliding block; 11. supporting ball; 12. threaded block; 13. screw rod. DETAILED DESCRIPTION
[0014] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.
[0015] See also Figure 1-4 The utility model provides a technical solution: an aviation seat control mechanism that is easy to operate, comprising a seat body 1, armrests 2 are fixedly installed on the front and rear surfaces of the seat body 1, a storage groove 4 is opened on one side of the top of the armrest 2 arranged at the front end, a touch screen 3 is arranged on one side of the storage groove 4, a transmission groove 5 is opened at the bottom of the storage groove 4, a screw rod 13 is arranged at the center of the transmission groove 5, a threaded block 12 is threadedly connected to one side of the surface of the screw rod 13, a motor 6 is fixedly installed on one side of the top of the storage groove 4, a driving gear 7 is arranged at the lower end of the motor 6, a driven gear 8 is fixedly installed on one side of the surface of the screw rod 13, sliding grooves 9 are opened on the front and rear ends of one side of the top of the storage groove 4, two sliding blocks 10 are fixedly installed on the top of the touch screen 3, and a supporting ball 11 is rollingly installed on one side of the lower end of the touch screen 3.
[0016] The two ends of the screw rod 13 are movably connected to the bearings fixedly installed at the centers of the two sides of the inner wall of the transmission groove 5, respectively, so as to support the screw rod 13 when it rotates.
[0017] One side of the touch screen 3 penetrates into the interior of the storage groove 4 , and the upper end of the threaded block 12 penetrates into the interior of the transmission groove 5 and is fixedly connected to one side of the bottom of the touch screen 3 , and the touch screen 3 is driven to move by the threaded block 12 .
[0018] The motor 6 is fixedly connected to an output shaft through an output end at the bottom thereof, and the lower end of the output shaft is fixedly connected to the center of the top of the driving gear 7 , and the driving gear 7 is driven by the motor 6 to mesh with the driven gear 8 to rotate.
[0019] The driving gear 7 and the driven gear 8 are both configured in a conical structure. The driving gear 7 and the driven gear 8 are meshed and connected. The driving gear 7 rotates to mesh with the driven gear 8 and drives the screw rod 13 to rotate.
[0020] The two sliding blocks 10 are respectively located below the two sliding grooves 9. The upper ends of the two sliding blocks 10 extend into the interior of the two sliding grooves 9 and are slidably connected to the inner walls of the sliding grooves 9. The sliding blocks 10 slide inside the sliding grooves 9 to limit the horizontal movement of the touch screen 3.
[0021] The number of the supporting balls 11 is three, and the lower ends of the three supporting balls 11 are in contact with the upper end surface of the armrest 2 , so as to support the touch screen 3 .
[0022] Working principle: After the passenger adjusts the airline seat through the touch screen 3, the control button on the front surface of the armrest 2 is pressed to control the motor 6 to rotate. The motor 6 drives the driving gear 7 to engage the driven gear 8 to rotate, so that the driven gear 8 drives the screw 13 to rotate. At this time, the threaded block 12 drives the touch screen 3 to move horizontally into the storage slot 4. The supporting ball 11 at the bottom of the touch screen 3 supports the moving touch screen 3. At the same time, the touch screen 3 drives the sliding block 10 at the top to slide in the sliding slot 9 until the touch screen 3 moves to the storage slot 4. The operation is convenient.
[0023] In summary: the easy-to-operate aviation seat control mechanism, through the design of the storage slot 4, motor 6, active gear 7, driven gear 8, sliding slot 9, sliding block 10, threaded block 12 and screw rod 13, the motor 6 drives the active gear 7 to engage the driven gear 8 to rotate, so that the threaded block 12 drives the touch screen 3 to move with the rotation of the screw rod 13, so that the touch screen 3 can enter or move out of the storage slot 4, providing a hidden space for the touch screen 3, when the passenger is not using the touch screen 3, it can be stored in the storage slot 4 to keep the surface of the armrest 2 clean and beautiful while preventing the passenger from accidentally touching the touch screen 3, the sliding of the sliding block 10 in the sliding slot 9 can limit the moving trajectory of the touch screen 3, thereby improving the practicality of the aviation seat control mechanism, the design of the support ball 11 is used to support the touch screen 3 to prevent the touch screen 3 from being damaged by downward pressure when moving out of the storage slot 4, and convenient operation.
[0024] It should be noted that, in this article, relational terms such as first and second, etc. are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variants thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements includes not only those elements, but also other elements not explicitly listed, or also includes elements inherent to such process, method, article or device.
[0025] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.
Claims
1. An easy-to-operate aviation seat control mechanism, comprising a seat body (1), characterized in that: The front and rear surfaces of the seat body (1) are both fixedly mounted with armrests (2); a storage groove (4) is provided on one side of the top of the armrest (2) arranged at the front end; a touch screen (3) is provided on one side of the storage groove (4); a transmission groove (5) is provided at the bottom of the storage groove (4); a screw rod (13) is provided at the center of the transmission groove (5); a threaded block (12) is threadedly connected to one side of the surface of the screw rod (13); a motor (6) is fixedly mounted on one side of the top of the storage groove (4); a driving gear (7) is provided at the lower end of the motor (6); a driven gear (8) is fixedly mounted on one side of the surface of the screw rod (13); sliding grooves (9) are provided at the front and rear ends of one side of the top of the storage groove (4); two sliding blocks (10) are fixedly mounted on the top of the touch screen (3); and a support ball (11) is rollingly mounted on one side of the lower end of the touch screen (3).
2. The easy-to-operate aviation seat control mechanism according to claim 1, characterized in that: The two ends of the screw rod (13) are respectively movably connected to bearings fixedly installed at the centers of the two sides of the inner wall of the transmission groove (5).
3. The easy-to-operate aviation seat control mechanism according to claim 1, characterized in that: One side of the touch screen (3) penetrates into the interior of the storage groove (4), and the upper end of the threaded block (12) penetrates into the interior of the transmission groove (5) and is fixedly connected to one side of the bottom of the touch screen (3).
4. The easy-to-operate aviation seat control mechanism according to claim 1, characterized in that: The motor (6) is fixedly connected to an output shaft via an output end at the bottom thereof, and the lower end of the output shaft is fixedly connected to the center of the top of the driving gear (7).
5. The easy-to-operate aviation seat control mechanism according to claim 1, characterized in that: The driving gear (7) and the driven gear (8) are both arranged in a conical structure, and the driving gear (7) and the driven gear (8) are meshingly connected.
6. The easy-to-operate aviation seat control mechanism according to claim 1, characterized in that: The two sliding blocks (10) are respectively located below the two sliding grooves (9), and the upper ends of the two sliding blocks (10) respectively extend into the interior of the two sliding grooves (9) and are slidably connected to the inner walls of the sliding grooves (9).
7. The easy-to-operate aviation seat control mechanism according to claim 6, characterized in that: The number of the supporting balls (11) is three, and the lower ends of the three supporting balls (11) are in contact with the upper end surface of the handrail (2).