Aviation teacher seat locking adjusting device

By combining locking pins and perforated locking channel steel with electromagnets and motor systems, the problems of instructor seats sliding on the track and locking failure were solved, achieving precise adjustment and stable locking of the seats and improving safety.

CN224023186UActive Publication Date: 2026-03-24ZHUHAI XIANG YI AVIATION TECH CO LTD
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-02-21
Publication Date
2026-03-24

AI Technical Summary

Technical Problem

The instructor seat in the existing full-motion flight training simulator slides in the front-to-back direction of the track, and the locking mechanism is prone to failure, resulting in safety hazards.

Method used

The system employs a combination of locking pins and perforated locking channel steel. The locking pins are raised and lowered by an electromagnet, and combined with a motor and gear rack system, the seat can be precisely adjusted and locked on the slide rail.

Benefits of technology

It effectively prevents the seat from sliding on the rail, ensuring safety, and enables precise adjustment and locking of the seat position, improving the stability and safety of the seat on the rail.

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Abstract

The utility model belongs to the technical field of aviation simulation devices, particularly relates to an aviation teacher seat locking adjusting device, and aims to solve the safety problem that a seat slides in the front-back direction of a track and cannot be locked. The sliding seat comprises a base, a sliding seat and a limiting assembly, wherein the sliding seat is used for installing the seat and is connected to the base in a sliding mode, and the limiting assembly is used for limiting the sliding position of the sliding seat on the base. According to the utility model, the movement of the seat on the base is limited through the limiting of the limiting rod and the base, so that the sliding of the seat on the base is effectively limited.
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Description

Technical Field

[0001] This utility model belongs to the technical field of aviation simulation devices, and specifically relates to an aviation instructor seat locking and adjustment device. Background Technology

[0002] In actual training, the instructor seats of existing full-motion flight training simulators have repeatedly slid in the forward and backward directions of the track, and the locking mechanism has failed, which poses a safety problem. Utility Model Content

[0003] In order to solve the above-mentioned problems in the prior art, namely the safety problem of locking mechanism failure when the instructor seat slides in the front and back direction of the track, this utility model provides an aviation instructor seat locking adjustment device.

[0004] This application discloses an aviation instructor seat locking and adjustment device, which adopts the following technical solution:

[0005] An aviation instructor seat locking adjustment device includes a base, a slide for mounting the seat, a slider and a slide rail connecting the base and the slide, and a locking component for locking the slide in a sliding position on the slide rail.

[0006] The locking assembly includes a locking pin, which is inserted into a perforated locking channel steel by lifting and lowering to restrict the sliding of the slide block on the slide rail.

[0007] Optionally, the base is equipped with two slide rails arranged in parallel; the slide includes a mounting base plate and a slider fixedly connected to the lower side of the mounting base plate, the lower side of the slider is provided with a receiving groove, and the slider is fastened to the slide rail; the seat is mounted on the upper side of the mounting base plate.

[0008] By adopting the above technical solution, the seat is installed on the slide rail, and the position of the seat can be adjusted along the slide rail, making the direction of seat movement controllable and making it easier to align the locking hole.

[0009] Optionally, the upper side of the base is provided with two protruding ridges, which are arranged in parallel, and the slide rail is arranged on the ridges.

[0010] Optionally, the slide rail is elongated and has grooves on both sides; a rod protrudes from the groove wall of the slider's receiving groove and is inserted into the groove.

[0011] By adopting the above technical solution, the connection between the insert rod and the groove enables the slider and the slide rail to be engaged in the vertical direction, thereby limiting the position of the slider on the slide rail and preventing the slider from flipping and detaching on the slide rail.

[0012] Optionally, baffles are provided at both ends of the slide rail.

[0013] By adopting the above technical solution, the baffle restricts the sliding of the slide block on the slide rail, preventing the slide block from sliding directly off the slide rail.

[0014] Optionally, the locking assembly includes a perforated locking channel steel mounted on a base; the perforated locking channel steel is Ω-shaped with a flat upper surface and is fixedly connected to the base; the upper surface of the perforated locking channel steel is provided with locking holes, and multiple locking holes are provided, which are arranged at equal intervals along the length of the perforated locking channel steel.

[0015] By adopting the above technical solution, the locking pin is inserted into the locking hole opened on the perforated locking channel steel, which facilitates locking with the base by plugging.

[0016] Optionally, the locking hole is elliptical or strip-shaped, and the locking pin is a round rod.

[0017] By adopting the above technical solution, the locking pin can be easily inserted into the locking hole.

[0018] Optionally, an electromagnet is installed on the mounting base plate, and a locking pin passes through the electromagnet. The locking pin is raised and lowered by energizing the electromagnet.

[0019] Optionally, a motor is fixedly connected to the mounting base, and a gear is fixedly connected to the output shaft of the motor. The motor drives the gear to rotate, and a rack arranged parallel to the slide rail is fixedly connected to the base, with the gear meshing with the rack.

[0020] By adopting the above technical solution, when it is necessary to adjust the position of the aviation instructor's seat, the staff can use the control panel on the seat to electrically control the locking pin to rise, then electrically move the seat to adjust its fore-and-aft position, and then electrically control the locking pin to descend and insert it into the perforated locking channel steel. The movement of the seat on the slide rail is restricted by the locking pin and the perforated locking channel steel, thereby effectively locking the seat on the slide rail.

[0021] The beneficial effects of this utility model are:

[0022] (1) The movement of the seat on the slide rail is locked by locking pins and locking channel steel with holes;

[0023] (2) By setting an electromagnet, it is convenient to drive the locking pin to rise and fall;

[0024] (3) By setting a motor, the seat can be moved electrically along the slide rail;

[0025] (4) By setting grooves and inserts, the slider can be effectively installed on the slide rail, preventing the slider from separating from the slide rail, thereby preventing the slide block installed on the slider from falling off. Attached Figure Description

[0026] Other features, objects, and advantages of this application will become more apparent from the following detailed description of non-limiting embodiments with reference to the accompanying drawings:

[0027] Figure 1 This is a schematic diagram of the aviation instructor seat locking adjustment device in this embodiment;

[0028] Figure 2 This is a schematic diagram of a slide mounted on a base in this embodiment;

[0029] Figure 3 This is a schematic diagram of the connection between the slide rail and the slider in this embodiment.

[0030] Explanation of reference numerals in the attached drawings: 1. Base; 11. Raised ridge; 2. Slide rail; 21. Groove; 3. Slide block; 31. Mounting base plate; 32. Slider; 33. Insert rod; 4. Locking assembly; 41. Locking channel steel with hole; 42. Locking pin; 43. Locking hole; 44. Electromagnet; 5. Motor; 6. Gear; 7. Rack. Detailed Implementation

[0031] The present application will now be described in further detail with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are for illustrative purposes only and are not intended to limit the scope of the invention. Furthermore, it should be noted that, for ease of description, only the parts relevant to the invention are shown in the accompanying drawings.

[0032] It should be noted that, unless otherwise specified, the embodiments and features described in this application can be combined with each other. This application will now be described in detail with reference to the accompanying drawings and embodiments.

[0033] This utility model provides an aviation instructor seat locking and adjustment device, referring to... Figures 1-3 The aviation instructor seat locking and adjustment device includes a base 1, a slide rail 2 fixedly connected to the base 1, a slide block 3 slidably connected to the slide rail 2, and a locking component 4 for fixing the seat position.

[0034] The base 1 is fixed on the ground, and two protruding ribs 11 are provided on the upper side of the base 1. The two protruding ribs 11 are arranged in parallel, and the slide rail 2 is arranged on the protruding ribs 11.

[0035] The slide rail 2 is long and narrow, with grooves 21 on both sides. When the slide rail 2 is installed on the protrusion 11, it supports the slide block 3 together with the protrusion 11, so that there is a gap between the slide block 3 and the base 1, which facilitates the slide block 3 to slide on the slide rail 2.

[0036] The slide block 3 includes a mounting base plate 31, with a seat mounted on the upper side of the mounting base plate 31 and a slider 32 fixedly connected to the lower side of the mounting base plate 31. The slider 32 is mounted on a slide rail 2 and has a receiving groove. The slider 32 is snapped onto the slide rail 2, connecting it from top to bottom. A rod 33 protrudes from the wall of the receiving groove of the slider 32 and inserts into a recess 21. The connection between the rod 33 and the recess 21 enables the slider 32 to engage with the slide rail 2 in the vertical direction, securing the slide block 3 on the slide rail 2 and preventing it from flipping off. Additionally, baffles can be installed at both ends of the slide rail 2 to limit the sliding of the slide block 3 and prevent it from slipping directly off the slide rail 2.

[0037] The locking assembly 4 includes a perforated locking channel steel 41 mounted on the base 1 and a locking pin 42 passing through the perforated locking channel steel 41. The perforated locking channel steel 41 is Ω-shaped with a flat upper surface. It is fixedly connected to the base 1 and arranged parallel to the slide rail 2, located below the mounting base plate 31. Multiple locking holes 43 are formed on the upper surface of the perforated locking channel steel 41, evenly spaced along its length. The locking holes 43 are elliptical or strip-shaped. The locking pin 42 passes through the locking holes 43, and its insertion and disengagement are achieved by lifting and lowering. An electromagnet 44 is mounted on the mounting base plate 31, and a locking pin 42 passes through the electromagnet 44. The locking pin 42 is raised and lowered by energizing and de-energizing the electromagnet 44. The locking pin 42 is a round rod.

[0038] In order to facilitate the movement of the seat on the base 1, a motor 5 is fixedly connected to the mounting base plate 31, and a gear 6 is fixedly connected to the output shaft of the motor 5. The motor 5 drives the gear 6 to rotate. In addition, a rack 7 arranged parallel to the slide rail 2 is fixedly connected to the base 1. The gear 6 meshes with the rack 7. When the motor 5 starts, it drives the gear 6 to rotate. When the gear 6 rotates, it drives the mounting base plate 31 to slide on the slide rail 2 along the length direction of the rack 7.

[0039] The method of using the aviation instructor seat locking adjustment device disclosed in this application embodiment is as follows: When it is necessary to adjust the position of the aviation instructor seat, the operator controls the electromagnet 44 to start through the operation panel on the seat. After the electromagnet 44 is started, it controls the locking pin 42 to rise and disengage from the locking hole 43. Then, the motor 5 is controlled to drive the mounting base plate 31 to move along the slide rail 2 to adjust the position of the seat. When the seat moves to the target position, the control button is released, the electromagnet 44 is de-energized, and the locking pin 42 is driven to descend and insert into the locking hole 43 on the perforated locking channel steel 41. The movement of the seat on the base 1 is locked by the insertion of the locking pin 42 and the perforated locking channel steel 41, thereby effectively locking the movement of the seat on the base 1.

[0040] The term "comprising" or any other similar term is intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus / device that comprises a list of elements includes not only those elements but also other elements not expressly listed, or elements inherent in such process, method, article, or apparatus / device.

[0041] The technical solution of this utility model has been described above with reference to the preferred embodiments shown in the accompanying drawings. However, it will be readily understood by those skilled in the art that the protection scope of this utility model is obviously not limited to these specific embodiments. Without departing from the principle of this utility model, those skilled in the art can make equivalent changes or substitutions to the relevant technical features, and the technical solutions after these changes or substitutions will all fall within the protection scope of this utility model.

Claims

1. An in-flight instructor seat locking adjustment device, characterized by: The base (1), the slide (3) for installing the seat, the slide block (32) and the slide rail (2) connecting the base (1) and the slide (3), and the locking assembly (4) for locking the sliding position of the slide (3) on the slide rail (2) are included. The locking assembly (4) includes a locking bolt (42) which is inserted into the locking hole (43) of the hole locking channel steel (41) to limit the sliding of the slide (3) on the slide rail (2).

2. An in-flight crew seat locking adjustment device as defined in claim 1, characterized in that: The base (1) is provided with two slide rails (2) arranged in parallel, the slide (3) includes a mounting bottom plate (31) and a slide block (32) fixedly connected to the lower side of the mounting bottom plate (31), the lower side of the slide block (32) is provided with a receiving groove, and the slide block (32) is buckled on the slide rail (2); the seat is mounted on the upper side of the mounting bottom plate (31).

3. An in-flight crew seat locking adjustment device as defined in claim 2, characterized in that: The upper side of the base (1) is provided with two parallel convex edges (11), and the slide rail (2) is arranged on the convex edge (11).

4. An in-flight crew seat locking adjustment device as defined in claim 2, wherein: The slide rail (2) is in the shape of a long strip, and grooves (21) are formed on both sides; the receiving groove of the slide block (32) is provided with a plug rod (33) protruding from the groove wall, and the plug rod (33) is inserted into the groove (21).

5. The in-flight crew seat locking adjustment device of claim 2, wherein: The slide rail (2) is provided with a baffle at both ends.

6. The in-flight crew seat locking adjustment device of claim 2, wherein: The locking assembly (4) includes a hole locking channel steel (41) mounted on the base (1); the hole locking channel steel (41) is in the shape of Ω, the upper surface is a plane, and the hole locking channel steel (41) is fixedly connected to the base (1); the upper surface of the hole locking channel steel (41) is provided with locking holes (43), and a plurality of locking holes (43) are arranged at equal intervals along the length direction of the hole locking channel steel (41). The locking bolt (42) is inserted into the locking hole (43) of the hole locking channel steel (41).

7. An in-flight crew seat locking adjustment device as defined in claim 6, characterized in that: The locking hole (43) is in the shape of an ellipse or a strip, and the locking bolt (42) is a round rod.

8. An in-flight crew seat locking adjustment device as defined in claim 2, wherein: The mounting bottom plate (31) is provided with an electromagnet (44), the locking bolt (42) is inserted into the electromagnet (44), and the locking bolt (42) is lifted by energizing the electromagnet (44).

9. An in-flight crew seat locking adjustment device as defined in claim 2, wherein: The mounting bottom plate (31) is fixedly connected with a motor (5), the output shaft of the motor (5) is fixedly connected with a gear (6), the motor (5) drives the gear (6) to rotate, and the base (1) is fixedly connected with a rack (7) arranged in parallel with the slide rail (2), and the gear (6) is engaged with the rack (7).