Aircraft maintenance site data transmission device

By designing a data transmission device for aircraft maintenance including a support frame, a fine-tuning head, a lower chuck, a lower tray, an electric telescopic rod and a mobile storage box, the problem of inconvenience in adjustment and storage of existing devices is solved, and more efficient use and data transmission is achieved.

CN222992609UActive Publication Date: 2025-06-17SICHUAN AIRLINES CO LTD
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Patent Information

Application Number
CN202422373388.1
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-09-28
Publication Date
2025-06-17
Estimated Expiration
2034-09-28

AI Technical Summary

Technical Problem

The existing data transmission device is not convenient for adjustment and support according to the needs of on-site maintenance of the aircraft and storage and movement after use, which affects the efficiency of use.

Method used

A data transmission device for on-site aircraft maintenance is designed, including an information body, a support frame, a fine-tuning head, a lower chuck, a lower support plate, an electric telescopic rod and a mobile storage box. Through the cooperation of these components, the information body can be flexible in support, angle adjustment and lifting, and stored and moved when not in use.

Benefits of technology

The device facilitates adjustment and support according to the needs of on-site maintenance of the aircraft and storage and movement after use, improving usage efficiency and ensuring the smooth progress of data transmission.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model relates to the technical field of electronic information assistance, in particular to an airplane maintenance site data transmission device which comprises an information machine body, a supporting frame is supported at the bottom of the information machine body, a fine adjustment head is assembled at the upper end of the supporting frame, a lower chuck is integrally arranged on the bottom wall of the supporting frame, and a lower supporting disc is assembled at the bottom of the lower chuck. An electric telescopic rod is assembled at the bottom of the lower supporting disc in a supporting mode, a movable storage box is assembled on the lower portion of the electric telescopic rod, universal wheels are assembled at the bottom of the movable storage box, side doors are assembled on the two sides of the movable storage box through hinges, and door locks are assembled on the sides of the side doors. According to the field maintenance requirements of the airplane, the support can be adjusted conveniently, and the storage and movement can be carried out after use.
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Description

Technical Field

[0001] The utility model relates to the technical field of electronic information assistance, and particularly relates to a data transmission device for aircraft maintenance sites. Background Technique

[0002] In the aircraft maintenance industry, efficient and accurate transmission of on-site maintenance data is crucial for ensuring the safe operation and maintenance quality of aircraft. With the continuous development of electronic information, there are more and more corresponding data processing and transmission machines. For example, special tablet computers and other corresponding machines can be used to record and process the corresponding maintenance data;

[0003] In this regard, Chinese Patent Application No.: CN202121674072.6 discloses a data transmitter for electronic information, which relates to the technical field of electronic information technology and includes a protective shell, a detection mechanism, a standing pile, and supporting feet. Two auxiliary heat dissipation devices are fixedly installed on the two side end faces of the protective shell. The auxiliary heat dissipation device includes a first heat dissipation mechanism and a second heat dissipation mechanism. There are multiple first heat dissipation mechanisms, and the multiple first heat dissipation mechanisms are evenly installed on the side end of the protective shell, and the outer ends of the multiple first heat dissipation mechanisms are plugged with the second heat dissipation mechanism;

[0004] However, the existing data transmission device is inconvenient to adjust the support according to the needs of aircraft on-site maintenance and to be stored and moved after use, which affects the use efficiency;

[0005] Therefore, in order to solve the above problems, a data transmission device for aircraft maintenance sites is proposed. Content of the Utility Model

[0006] The purpose of the utility model is to provide a data transmission device for aircraft maintenance sites to solve the problem that the existing data transmission device is inconvenient to adjust the support according to the needs of aircraft on-site maintenance and to be stored and moved after use, which affects the use efficiency as mentioned in the above background technique.

[0007] To achieve the above purpose, the utility model provides the following technical solution: A data transmission device for aircraft maintenance sites includes an information body, the bottom of the information body is supported by a support frame, a fine-tuning head is assembled at the upper end of the support frame, a lower chuck is integrally provided on the bottom wall of the support frame, a lower support plate is assembled at the bottom of the lower chuck, an electric telescopic rod is supported and assembled at the bottom of the lower support plate, a mobile storage box is assembled at the lower part of the electric telescopic rod, universal wheels are assembled at the bottom of the mobile storage box, and side doors are assembled on both sides of the mobile storage box through hinges, and door locks are assembled on the sides of the side doors.

[0008] As a further improvement of this solution, a flat chuck is assembled on the top of the fine-tuning head, and a lower support plate is assembled at the bottom of the flat chuck. The lower support plate is welded to the top of the fine-tuning head. An inner chuck is clamped inside the fine-tuning head. The inner chuck is fixed to the upper end of the support frame, and a locking pin is inserted into the side of the inner chuck in a threaded manner. The inner end of the locking pin abuts against the surface of the inner chuck.

[0009] As a further improvement of this solution, side buckles are fixed to the side of the lower support plate, and the three side buckles are distributed in a triangular shape. The inner side of the upper end of the side buckle is clamped on the side surface of the lower chuck.

[0010] As a further improvement of this solution, a limit pin is inserted through the side inner parts of the lower chuck and the lower support plate. The limit pin is threadedly connected to the lower support plate, and a pull rope is tied to the upper end of the limit pin. The pull rope is fixed to the outer wall of the lower support plate.

[0011] As a further improvement of this solution, an inner support plate corresponding to the lower support plate is assembled on one side inside the movable storage box. A lithium battery is assembled on the other side inside the movable storage box. Both the lithium battery and the inner support plate are located on the front side of the electric telescopic rod.

[0012] As a further improvement of this solution, a partition is provided between the bottom of the inner support plate, the lithium battery, and the electric telescopic rod. The upper and lower ends of the partition are fixed inside the movable storage box. Handles are symmetrically assembled on both sides of the top of the movable storage box.

[0013] As a further improvement of this solution, a charging component is assembled on one side inside the movable storage box close to the inner support plate. The inner support plate is electrically connected to a distribution box, and the distribution box is electrically connected to the electric telescopic rod. The distribution box is assembled on one side of the lithium battery, and the distribution box is electrically connected to the lithium battery.

[0014] Compared with the prior art, the beneficial effects of the present utility model are as follows: The present utility model is convenient for adjusting the support according to the needs of aircraft on-site maintenance and for storage and movement after use;

[0015] By providing a support frame, with the cooperation of the fine-tuning head, the lower chuck, the lower support plate, and the electric telescopic rod, the present utility model is convenient for the support and assembly of the information body. At the same time, with the cooperation of the fine-tuning head, it is convenient to finely adjust the use angle of the information body. Subsequently, with the telescopic movement of the electric telescopic rod, it is convenient to lift and use the information body, so as to facilitate the use according to the needs of aircraft on-site maintenance and not interfere with its data transmission, making the use more convenient. Through this design, the convenience and practicality of the data transmission device at the aircraft maintenance site are improved.

[0016] The utility model is provided with a movable storage box, in which an electric telescopic rod is assembled, so as to facilitate the storage of the electric telescopic rod when it is not in use. Meanwhile, with the cooperation of universal wheels, it is convenient to move and carry. At the same time, the information body can be stored and maintained under the opening and closing of the side door, making the information body safer and more convenient for subsequent use. Through this design, the convenience and practicability of the data transmission device at the aircraft maintenance site are improved. Brief Description of the Drawings

[0017] Figure 1 It is a front three-dimensional schematic view of the overall structure of the utility model;

[0018] Figure 2 It is a side three-dimensional schematic view of the overall structure of the utility model when it is extended and adjusted;

[0019] Figure 3 It is a top sectional three-dimensional schematic view of the partial structure of the movable storage box when the utility model is stored;

[0020] Figure 4 It is a side three-dimensional schematic view of the partial structure of the support frame of the utility model;

[0021] In the figure: 100, information body; 200, support frame; 210, fine adjustment head; 211, inner chuck; 212, locking pin; 220, lower chuck; 230, lower support plate; 231, side buckle; 232, limit pin; 233, pull rope; 240, electric telescopic rod; 250, flat chuck; 251, lower support plate; 300, movable storage box; 301, handle; 302, partition; 310, universal wheel; 320, side door; 321, door lock; 330, inner support plate; 340, charging component; 350, distribution box; 360, lithium battery. Detailed Description of the Embodiment

[0022] Next, the technical solutions in the embodiments of the present utility model will be clearly and completely described in conjunction with the drawings in the embodiments of the present utility model. Obviously, the described embodiments are only a part of the embodiments of the present utility model, rather than all the embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present utility model.

[0023] Please refer to Figures 1-4 , an embodiment provided by the present utility model:

[0024] An aircraft maintenance site data transmission device, including an information body 100, the bottom of the information body 100 is supported by a support frame 200, the upper end of the support frame 200 is equipped with a fine-tuning head 210, the bottom wall of the support frame 200 is integrally provided with a lower chuck 220, the bottom of the lower chuck 220 is equipped with a lower support plate 230, the bottom of the lower support plate 230 is supported and equipped with an electric telescopic rod 240, the lower part of the electric telescopic rod 240 is equipped with a mobile storage box 300, the bottom of the mobile storage box 300 is equipped with universal wheels 310, and both sides of the mobile storage box 300 are equipped with side doors 320 through hinges, and a door lock 321 is equipped on the side of the side door 320;

[0025] More specifically in this embodiment, a flat chuck 250 is assembled on the top of the fine-tuning head 210, and a lower support plate 251 is assembled on the bottom of the flat chuck 250. The lower support plate 251 is welded to the top of the fine-tuning head 210. An inner chuck 211 is clamped inside the fine-tuning head 210. The inner chuck 211 is fixed to the upper end of the support frame 200, and a locking pin 212 is threadedly inserted on the side of the inner chuck 211. The inner end of the locking pin 212 abuts against the surface of the inner chuck 211. Through this design, it is convenient for the auxiliary limit rotation of the fine-tuning head 210 and the support and assembly placement of the information body 100, making subsequent use more convenient;

[0026] More specifically in this embodiment, side buckles 231 are fixed on the side of the lower support plate 230, and the three side buckles 231 are distributed in a triangular shape. The inner side of the upper end of the side buckle 231 is clamped on the side surface of the lower chuck 220. Through this design, it is convenient for the limit clamping assembly of the lower side of the lower chuck 220, and it is also convenient for subsequent disassembly and assembly;

[0027] More specifically in this embodiment, a limit pin 232 is inserted through the sides of the lower chuck 220 and the lower support plate 230, and the limit pin 232 is threadedly connected to the lower support plate 230, and a pull rope 233 is tied to the upper end of the limit pin 232. The pull rope 233 is fixed to the outer wall of the lower support plate 230. Through this design, it is convenient for the stable assembly limit of the lower chuck 220 and the lower support plate 230, preventing falling off and rotation, and facilitating subsequent stable use;

[0028] More specifically in this embodiment, an inner support plate 330 corresponding to the lower support plate 230 is assembled on one side inside the mobile storage box 300, a lithium battery 360 is assembled on the other side inside the mobile storage box 300, and both the lithium battery 360 and the inner support plate 330 are located in front of the electric telescopic rod 240. Through this design, it is convenient for the internal assembly of the mobile storage box 300 and subsequent use;

[0029] More specifically, in this embodiment, a partition 302 is provided between the inner support plate 330, the lithium battery 360, and the bottom of the electric telescopic rod 240. The upper and lower ends of the partition 302 are fixed inside the mobile storage box 300. On both sides of the top of the mobile storage box 300, handles 301 are symmetrically assembled. Through this design, it is convenient to partition the inside of the mobile storage box 300 and facilitate subsequent side operation as needed.

[0030] More specifically, in this embodiment, a charging component 340 is assembled on one side of the mobile storage box 300 close to the inner support plate 330. The inner support plate 330 is electrically connected to a distribution box 350, and the distribution box 350 is electrically connected to the electric telescopic rod 240. The distribution box 350 is assembled on one side of the lithium battery 360 and is electrically connected to the lithium battery 360. Through this design, it is convenient to supply power to the electric telescopic rod 240 and the distribution box 350 for subsequent use.

[0031] Working principle: During assembly and use, the information body 100 is adjusted and supported according to the needs of the aircraft maintenance site. According to the use height, it is adjusted up and down in cooperation with the electric telescopic rod 240. Subsequently, the angle of the information body 100 is adjusted in cooperation with the fine-tuning head 210 and the inner chuck 211 and locked by the locking pin 212 for subsequent use and operation, facilitating the recording, transmission, and storage of relevant data at the aircraft maintenance site. Subsequently, when not in use, the limit pin 232 is unscrewed and the side buckle 231 is opened to facilitate the removal of the lower chuck 220. Subsequently, it is convenient to remove and store the support frame 200 and the information body 100 together. The door lock 321 is opened and the side door 320 is opened to facilitate placing the support frame 200 and the information body 100 inside the mobile storage box 300. At the same time, through the setting of the inner support plate 330, it is convenient to support and place the support frame 200 and the information body 100. The information body 100 can also be charged through the distribution box 350 for subsequent use. Through the locking of the door lock 321, it is convenient to maintain the information body 100, making the information body 100 safer and only accessible through the subsequent opening of the relevant key. Through the cooperation of the universal wheels 310 and the handle 301, it is convenient to move and transfer it. The operation ends here.

[0032] The above are only the preferred embodiments of the present utility model, and do not impose any form of limitation on the present utility model; any ordinary technician in the industry can smoothly implement the present utility model according to what is shown in the accompanying drawings of the specification and the above; however, any slight changes, modifications and equivalent changes made by those skilled in the art within the scope of the technical solution of the present utility model by using the technical content disclosed above are all equivalent embodiments of the present utility model; at the same time, any changes, modifications and evolutions made to the above embodiments based on the substantial technology of the present utility model are still within the protection scope of the technical solution of the present utility model.

Claims

1. An aircraft maintenance site data transmission device, comprising an information body (100), characterized in that: The bottom of the information machine body (100) is supported by a support frame (200), the upper end of the support frame (200) is equipped with a fine-tuning head (210), the bottom wall of the support frame (200) is integrally provided with a lower chuck (220), the bottom of the lower chuck (220) is equipped with a lower support plate (230), the bottom of the lower support plate (230) is supported and equipped with an electric telescopic rod (240), the lower part of the electric telescopic rod (240) is equipped with a mobile storage box (300), the bottom of the mobile storage box (300) is equipped with universal wheels (310), and side doors (320) are equipped on both sides of the mobile storage box (300) through hinges, and the side of the side door (320) is equipped with a door lock (321).

2. The aircraft maintenance site data transmission device according to claim 1, characterized in that: The top of the fine-tuning head (210) is equipped with a flat plate chuck (250), and the bottom of the flat plate chuck (250) is equipped with a lower support plate (251), the lower support plate (251) is welded to the top of the fine-tuning head (210), the fine-tuning head (210) is internally clamped with an inner clamp (211), the inner clamp (211) is fixed to the upper end of the support frame (200), and a locking pin (212) is threadedly inserted on the side of the inner clamp (211), and the inner end of the locking pin (212) abuts against the surface of the inner clamp (211).

3. The aircraft maintenance site data transmission device according to claim 1, characterized in that: The side of the lower support plate (230) is fixed with a side buckle (231), and three groups of side buckles (231) are distributed in a triangular shape, and the inner sides of the upper ends of the side buckles (231) are clamped on the side surface of the lower clamping plate (220).

4. The aircraft maintenance site data transmission device according to claim 1, characterized in that: A limit pin (232) is inserted through the sides of the lower chuck (220) and the lower support plate (230), and the limit pin (232) is threadedly connected to the lower support plate (230). A pull rope (233) is bolted to the upper end of the limit pin (232), and the pull rope (233) is fixed to the outer wall of the lower support plate (230).

5. The aircraft maintenance site data transmission device according to claim 1, characterized in that: An inner support plate (330) corresponding to the lower support plate (230) is mounted on one side of the mobile storage box (300), and a lithium battery (360) is mounted on the other side of the mobile storage box (300), and both the lithium battery (360) and the inner support plate (330) are located in front of the electric telescopic rod (240).

6. The aircraft maintenance site data transmission device according to claim 5, characterized in that: A partition (302) is provided between the inner support plate (330), the lithium battery (360) and the bottom of the electric telescopic rod (240), and the upper and lower ends of the partition (302) are fixed inside the mobile storage box (300), and handles (301) are symmetrically assembled on both sides of the top of the mobile storage box (300).

7. The aircraft maintenance site data transmission device according to claim 5, characterized in that: A charging assembly (340) is installed on a side of the mobile storage box (300) close to the inner support plate (330), and the inner support plate (330) is electrically connected to a distribution box (350), and the distribution box (350) is electrically connected to the electric telescopic rod (240), and the distribution box (350) is installed on one side of the lithium battery (360), and the distribution box (350) is electrically connected to the lithium battery (360).

Citation Information

Patent Citations

  • Data transmitter for electronic information

    CN215269325U