Aircraft maintenance tool box

Abstract

The utility model discloses an aircraft maintenance toolbox which comprises a box body and a cover body, one end of the cover body is connected with the box body through a rotating shaft, and the cutting assemblies are arranged in the box body and used for being combined and adjusted according to different maintenance tasks. The tool box further comprises a fastening assembly, the fastening assembly is used for ensuring that tools cannot shake and scatter in the transportation and use process, an illumination module is arranged at the lower end of the cover body, and a charging module is arranged at the bottom end of the box body. The utility model belongs to the technical field of aircraft maintenance, and particularly relates to an aircraft maintenance tool box.

Description

Technical Field

[0001] This utility model belongs to the field of aircraft maintenance technology, and in particular relates to an aircraft maintenance toolbox. Background Technology

[0002] A search revealed, for example, that patent CN218428270U discloses an aircraft maintenance toolbox, comprising two interlocking boxes, a retractor disposed within the boxes, and a fixing strap disposed within the boxes; the boxes are provided with a plurality of storage slots and a first hook; the retractor is connected to the fixing strap and retracts the fixing strap; the fixing strap is provided with a second hook, and when the fixing strap is unfolded, the fixing strap covers the opening of the storage slots, and the first hook and the second hook engage.

[0003] The aforementioned patent secures the tools by designing and installing fixing straps located inside the housing. However, different maintenance tasks require different combinations of maintenance tools, and the tools may shake and fall during transportation and use, greatly affecting maintenance efficiency and causing tool damage. Utility Model Content

[0004] The technical problem this invention aims to solve is that existing equipment requires different combinations of maintenance tools for different maintenance tasks, and these tools may shake and scatter during transportation and use.

[0005] To solve the above-mentioned technical problems, the present invention adopts the following technical solution: an aircraft maintenance toolbox, comprising a box body and a cover, one end of the cover being connected to the box body via a pivot, and a dividing component disposed within the box body, the dividing component being used for combination and adjustment according to different maintenance tasks; it also includes a fastening component, the fastening component being used to ensure that the tools do not shake or fall off during transportation and use, a lighting module being provided at the lower end of the cover, and a charging module being provided at the bottom of the box body.

[0006] Furthermore, the dividing component includes a enclosure, a positioning plate one, and a positioning plate two. The enclosure is fixed to the bottom of the box body. The positioning plate one is inserted between the enclosures. The positioning plate two is inserted between the enclosure and the positioning plate one. The upper end of the enclosure is provided with a plurality of positioning grooves one. The two ends of the positioning plate one and the positioning plate two are provided with positioning grooves two that match the positioning grooves one. The positioning plate one and the positioning plate two are respectively provided with positioning grooves three and four that match.

[0007] Furthermore, the fastening assembly includes a magnetic strip and an airbag. The magnetic strip is fixed to the bottom of the housing, and the airbag is located at the bottom of the cover. The airbag is connected to an air pump via a conduit. A microprocessor is located at the bottom of the housing. The magnetic strip is connected to the microprocessor via a wire, and the air pump is connected to the microprocessor via a wire. An inductive switch is located at the contact point between the cover and the housing, and the inductive switch is connected to the microprocessor via a wire.

[0008] Furthermore, the lighting module includes a lighting lamp and a photosensitive sensor. The lighting lamp is fixed to the bottom of the cover, and the photosensitive sensor is fixed to the inner wall of the box. The photosensitive sensor is connected to the microprocessor via a wire, and the lighting lamp is connected to the microprocessor via a wire.

[0009] Furthermore, the charging module includes a battery and a charging port. The battery is fixed to the bottom of the housing, and the charging port is fixed to the bottom of the housing. The charging port is connected to the battery via a wire.

[0010] Furthermore, the battery is connected to the microprocessor via wires, and the charging port is also connected to the microprocessor via wires.

[0011] Furthermore, the positioning plate one and positioning plate two are one or more sets, which can be combined and adjusted according to different maintenance tasks.

[0012] Furthermore, the edge of the cover is provided with a sealing ring that matches the upper end of the box.

[0013] Furthermore, the box and lid are made of high-strength, lightweight materials, which ensures that the toolbox is sturdy and durable, while also making it easy to carry and transport.

[0014] The beneficial effects of this utility model after adopting the above structure are as follows:

[0015] (1) Based on the type and quantity of aircraft maintenance tools, the size of the toolbox should be designed reasonably and a modular design should be adopted so that it can be combined and adjusted according to different maintenance tasks.

[0016] (2) The combination of magnetic strips and airbags ensures that the tools will not shake or fall during transportation and use.

[0017] (3) Install a lighting module inside the toolbox so that tools can be easily found even in low-light environments.

[0018] (4) The charging module at the bottom of the box provides a charging interface for power tools or electronic devices, using a USB interface or a dedicated charger interface, so that charging can be conveniently performed on-site. Attached Figure Description

[0019] The accompanying drawings are provided to further understand the present invention and form part of the specification. They are used together with the embodiments of the present invention to explain the present invention and do not constitute a limitation thereof.

[0020] Figure 1 This is a schematic diagram of the entire utility model. Figure 1 ;

[0021] Figure 2 This is a schematic diagram of the entire utility model. Figure 2 ;

[0022] Figure 3 This is an exploded view of the components of this utility model;

[0023] Figure 4 This is a schematic diagram of a partial section of this utility model.

[0024] In the attached diagram: 1. Box body, 2. Cover body, 3. Dividing assembly, 4. Fastening assembly, 5. Lighting module, 6. Charging module, 7. Enclosure, 8. Positioning plate one, 9. Positioning plate two, 10. Positioning groove one, 11. Positioning groove two, 12. Positioning groove three, 13. Positioning groove four, 14. Magnetic strip, 15. Airbag. Detailed Implementation

[0025] like Figure 1-2 As shown in Figure 4, an aircraft maintenance toolbox includes a box body 1 and a cover 2. One end of the cover 2 is connected to the box body 1 via a pivot, and a partition component 3 is disposed inside the box body 1. The partition component 3 is used for combination and adjustment according to different maintenance tasks. It also includes a fastening component 4, which is used to ensure that the tools do not shake or fall off during transportation and use. A lighting module 5 is provided at the lower end of the cover 2, and a charging module 6 is provided at the bottom of the box body 1.

[0026] The edge of the cover 2 is provided with a sealing ring that matches the upper end of the box 1. The box 1 and the cover 2 are made of high-strength, lightweight materials, which not only ensures the toolbox is sturdy and durable, but also makes it easy to carry and move.

[0027] like Figure 3 As shown, the dividing component 3 includes a barrier 7, a positioning plate 1 8, and a positioning plate 2 9. The barrier 7 is fixed to the bottom of the box body 1. The positioning plate 1 8 is inserted between the barriers 7, and the positioning plate 2 9 is inserted between the barrier 7 and the positioning plate 1 8. The upper end of the barrier 7 has several positioning grooves 10. The two ends of the positioning plates 1 8 and 2 9 have positioning grooves 2 11 that match the positioning grooves 1 10. The positioning plates 1 8 and 2 9 have corresponding positioning grooves 3 12 and 4 13 respectively.

[0028] Positioning plate 8 and positioning plate 9 are one or more sets, which can be combined and adjusted according to different maintenance tasks. The size of the toolbox is reasonably designed according to the type and quantity of aircraft maintenance tools, and a modular design is adopted so as to combine and adjust according to different maintenance tasks.

[0029] like Figure 3-4 As shown, the fastening assembly 4 includes a magnetic strip 14 and an airbag 15. The magnetic strip 14 is fixed to the bottom of the box 1, and the airbag 15 is located at the bottom of the cover 2. The airbag 15 is connected to the air pump through a conduit. A microprocessor is provided at the bottom of the box 1. The magnetic strip 14 is connected to the microprocessor through a wire, and the air pump is connected to the microprocessor through a wire. An induction switch is provided at the contact point between the cover 2 and the box 1. The induction switch is connected to the microprocessor through a wire.

[0030] The lighting module 5 includes a light and a photosensitive sensor. The light is fixed to the bottom of the cover 2, and the photosensitive sensor is fixed to the inner wall of the box 1. The photosensitive sensor is connected to the microprocessor via wires, and the light is connected to the microprocessor via wires. The charging module 6 includes a battery and a charging port. The battery is fixed to the bottom of the box 1, and the charging port is fixed to the bottom of the box 1. The charging port is connected to the battery via wires, and the battery is connected to the microprocessor via wires. The magnetic strip 14 and the airbag 15 work together to ensure that the tools will not shake or fall during transportation and use. The lighting module 5 is installed inside the toolbox so that the tools can be easily found in low-light environments. The charging module 6 at the bottom of the box 1, using a USB interface or a dedicated charger interface, provides a charging interface for power tools or electronic devices, facilitating charging at the repair site.

[0031] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions, and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents. In conclusion, if those skilled in the art, inspired by this description, design similar structural methods and embodiments without departing from the inventive spirit of the present invention, such designs should fall within the protection scope of the present invention.

Claims

1. An aircraft maintenance toolbox, characterized in that: The tool includes a housing and a cover, one end of which is connected to the housing via a pivot. It also includes a partition assembly inside the housing, which is used for combination and adjustment according to different maintenance tasks. The tool also includes a fastening assembly to ensure that it does not shake or fall off during transportation and use. The lower end of the cover is equipped with a lighting module, and the bottom of the housing is equipped with a charging module.

2. The aircraft maintenance toolbox according to claim 1, characterized in that: The edge of the cover is provided with a sealing ring that matches the upper end of the box. The box and the cover are made of high-strength, lightweight materials.

3. The aircraft maintenance toolbox according to claim 1, characterized in that: The partition component includes a fence, a positioning plate one, and a positioning plate two. The fence is fixed to the bottom of the box body. The positioning plate one is inserted between the fences. The positioning plate two is inserted between the fence and the positioning plate one. The upper end of the fence is provided with a plurality of positioning grooves one. The two ends of the positioning plate one and the positioning plate two are provided with positioning grooves two that match the positioning grooves one. The positioning plate one and the positioning plate two are respectively provided with positioning grooves three and four that match.

4. The aircraft maintenance toolbox according to claim 3, characterized in that: The positioning plate one and positioning plate two are one or more sets, which can be combined and adjusted according to different maintenance tasks.

5. The aircraft maintenance toolbox according to claim 1, characterized in that: The fastening assembly includes a magnetic strip and an airbag. The magnetic strip is fixed to the bottom of the box, and the airbag is located at the bottom of the cover. The airbag is connected to an air pump through a conduit. A microprocessor is located at the bottom of the box. The magnetic strip is connected to the microprocessor through a wire, and the air pump is connected to the microprocessor through a wire. An inductive switch is located at the contact point between the cover and the box, and the inductive switch is connected to the microprocessor through a wire.

6. The aircraft maintenance toolbox according to claim 5, characterized in that: The lighting module includes a lighting lamp and a photosensitive sensor. The lighting lamp is fixed to the bottom of the cover, and the photosensitive sensor is fixed to the inner wall of the box. The photosensitive sensor is connected to the microprocessor through wires, and the lighting lamp is connected to the microprocessor through wires.

7. An aircraft maintenance toolbox according to claim 5, characterized in that: The charging module includes a battery and a charging port. The battery is fixed to the bottom of the enclosure, and the charging port is fixed to the bottom of the enclosure. The charging port is connected to the battery via a wire.

8. An aircraft maintenance toolbox according to claim 7, characterized in that: The battery is connected to the microprocessor via wires, and the charging port is also connected to the microprocessor via wires.

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