Handheld tool for aircraft maintenance

Abstract

The utility model discloses a handheld tool for aircraft maintenance, which comprises a shell and a motor, the motor is fixedly mounted in the shell, the output end of the motor is connected with a screwdriver blade through a connector, and a track is fixedly mounted on the outer surface of the shell. The screw driver has the advantages that the suction cup and the connecting rod are adopted, when the aircraft shell is overhauled and disassembled, the screw driver head can be inserted into a cutter groove of a screw cap of the aircraft shell, then the suction cup and the surface of the aircraft shell are adsorbed and fixed, the motor can be started to drive the screw driver head to rotate, and then a screw is disassembled; the connecting rod and the suction cup resist torsion generated during rotation, workers are prevented from slipping out of the hands, maintenance and disassembly by the workers are greatly facilitated, use convenience is improved, meanwhile, the characteristic that the surface of an airplane shell is smooth is utilized, the suction cup is adopted for fixing, mounting and disassembly are convenient, fixing stability is high, the workers do not need to tightly abut against the device vigorously, and use is convenient. The use is more flexible and labor-saving.

Description

Technical Field

[0001] The utility model relates to the technical field of maintenance tools, in particular to a handheld tool for aircraft maintenance. Background Art

[0002] During aircraft cabin maintenance, it is often necessary to dismantle the aircraft's outer shell, such as the engine pylon, radome, and wings. The screws on the aircraft's outer shell are generally very tight.

[0003] After searching, it was found that the application number is CN201911096564.9, and the name is "A multifunctional maintenance tool for disassembling and assembling the shell of aviation equipment." This application addresses the problem that traditional aircraft disassembly and maintenance tools are mostly screw guns. When using screw guns to remove screws, maintenance personnel cannot hold the screw gun, and the handle of the screw gun rotates as a whole, making it impossible for maintenance personnel to hold and control the handle. This is quite troublesome for users. By providing a stop plate, a contact pad, a gripping rod, and a gripping sleeve, when using the device, the user aims the screwdriver at the screw, presses the contact pad against the shoulder, and holds the gripping sleeve on the gripping rod. In this way, the contact area between the aircraft body and the human body is increased. The stop plate and contact pad press against the shoulder, and the aircraft body does not rotate. In this way, the removal of screws from the aircraft shell becomes simple. However, this application still requires the worker to use the shoulder to apply a large amount of pressure, which is still quite laborious. At the same time, the pedal arrangement increases the overall volume and weight, making it more difficult to move. When the screw height is greater than the worker's shoulder, the shoulder cannot exert force, making removal more difficult. Further improvements can be made.

[0004] Currently, no effective solutions have been proposed for the problems in related technologies. Utility Model Content

[0005] (1) Technical problems solved

[0006] In view of the deficiencies in the prior art, the present invention provides a handheld tool for aircraft maintenance, which has the advantages of simple and compact structure, flexible use, labor saving and convenience, thereby solving the problems in the above-mentioned background technology.

[0007] (2) Technical solution

[0008] In order to achieve the advantages of simple and compact structure, flexible use, labor saving and convenience, the specific technical solutions adopted by the present invention are as follows:

[0009] A handheld tool for aircraft maintenance comprises a housing and a motor, wherein the motor is fixedly mounted inside the housing, and the output end of the motor is connected to a screwdriver head via a connector, and a track is fixedly mounted on the outer surface of the housing, a slider is slidably connected inside the track, and a connecting rod is hinged to the surface of the slider via a first hinge seat, and a suction cup is hinged to the other end of the connecting rod via a second hinge seat, and a handle is fixedly connected to the top surface of the housing via a handle rod.

[0010] Furthermore, a battery is fixedly installed inside the shell, and the battery is electrically connected to the motor through an electrical connection line.

[0011] Furthermore, a switch is fixedly mounted on the surface of the handlebar, and an output end of the switch is electrically connected to an input end of the motor.

[0012] Furthermore, the suction cups are arranged in two groups, and the suction cups are symmetrically arranged along the central axis of the shell.

[0013] Furthermore, the slider is a T-shaped structure, and the outer wall of the slider is polished.

[0014] Furthermore, the surface of the shell is densely and evenly provided with ventilation holes on one side of the motor.

[0015] (3) Beneficial effects

[0016] Compared with the prior art, the present invention provides a handheld tool for aircraft maintenance, which has the following beneficial effects:

[0017] (1) The present invention adopts a suction cup and a connecting rod. When inspecting and disassembling the aircraft shell, the screwdriver head can be inserted into the knife groove of the aircraft shell nut. Then, the suction cup is fixed to the surface of the aircraft shell by adsorption. The motor can be started to drive the screwdriver head to rotate, and then the screw can be removed. During the process of starting the motor, the connecting rod and the suction cup resist the torque generated during the rotation, preventing the staff from losing their hands, greatly facilitating the staff's inspection and disassembly, and improving the convenience of use. At the same time, the device takes advantage of the smooth surface of the aircraft shell and adopts a suction cup for fixing. It is easy to install and disassemble, and has high fixing stability. The staff does not need to tighten it vigorously, and it is more flexible and labor-saving to use.

[0018] (2) The utility model adopts a first hinge seat, a second hinge seat, a slider and a track. The slider can slide up and down along the track. The first hinge seat and the second hinge seat facilitate the up and down rotation of the connecting rod, thereby greatly facilitating the staff to move the housing and the screwdriver head up and down, and facilitating the upward movement of the screwdriver head to remove the screw when turning the screw, further improving the convenience of use. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the following briefly introduces the drawings required for use in the embodiments. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying any creative work.

[0020] Figure 1 This is a schematic diagram of the internal structure of a handheld tool for aircraft maintenance proposed by the utility model;

[0021] Figure 2 This is a front view of a handheld tool for aircraft maintenance proposed by the utility model;

[0022] Figure 3 This is a schematic diagram of the external structure of a handheld tool for aircraft maintenance proposed by the utility model;

[0023] Figure 4 It is a schematic diagram of the connection between the track and the slider proposed by the utility model.

[0024] In the picture:

[0025] 1. Housing; 2. Motor; 3. Battery; 4. Connector; 5. Screwdriver head; 6. Track; 7. Slider; 8. First hinge seat; 9. Connecting rod; 10. Second hinge seat; 11. Suction cup; 12. Handle bar; 13. Grip; 14. Switch. DETAILED DESCRIPTION

[0026] To further illustrate each embodiment, the present invention provides drawings, which are part of the disclosure of the present invention and are mainly used to illustrate the embodiments. They can be used in conjunction with the relevant descriptions in the specification to explain the operating principles of the embodiments. By referring to these contents, ordinary technicians in this field should be able to understand other possible implementation methods and the advantages of the present invention. The components in the figures are not drawn to scale, and similar component symbols are generally used to represent similar components.

[0027] According to an embodiment of the present utility model, a handheld tool for aircraft maintenance is provided.

[0028] The present invention will now be further described with reference to the accompanying drawings and specific embodiments. Figure 1-4As shown, a handheld tool for aircraft maintenance according to an embodiment of the present invention includes a shell 1 and a motor 2. The motor 2 is fixedly installed inside the shell 1, and the output end of the motor 2 is connected to a screwdriver head 5 through a connector 4. This is a common installation structure in the field and will not be described in detail here. A track 6 is fixedly installed on the outer surface of the shell 1, and a slider 7 is slidably connected inside the track 6. Both ends of the track 6 are closed structures to prevent the slider 7 from falling off, and a connecting rod 9 is hinged to the surface of the slider 7 through a first hinge seat 8, and the other end of the connecting rod 9 is hinged to a suction cup 11 through a second hinge seat 10. The top surface of the shell 1 is fixedly connected to a handle 13 through a handle rod 12, which is convenient for staff to hold. When inspecting and disassembling the aircraft shell 1, the screwdriver head 5 can be inserted into the knife groove of the nut of the aircraft shell 1, and then the suction cup 11 is connected to the aircraft shell 1. The surface of the shell 1 is adsorbed and fixed, and the motor 2 can be started to drive the screwdriver head 5 to rotate, and then the screw is removed. During the starting process of the motor 2, the connecting rod 9 and the suction cup 11 resist the torque generated during the rotation, preventing the staff from losing their hands, which greatly facilitates the staff to carry out maintenance and disassembly, and improves the convenience of use. At the same time, this device utilizes the smooth surface of the aircraft shell 1 and adopts the suction cup 11 for fixation. It is easy to install and disassemble, and the fixing stability is high. The staff does not need to tighten it vigorously, and it is more flexible and labor-saving to use. At the same time, the slider 7 can slide up and down along the track 6, and the first hinge seat 8 and the second hinge seat 10 facilitate the connecting rod 9 to rotate up and down, thereby greatly facilitating the staff to move the shell 1 and the screwdriver head 5 up and down, and conveniently move the screwdriver head 5 up to remove the screw when turning the screw, further improving the convenience of use.

[0029] In one embodiment, a battery 3 is fixedly installed inside the housing 1, and the battery 3 is electrically connected to the motor 2 through an electrical connection line. A switch 14 is fixedly installed on the surface of the handle rod 12, and the output end of the switch 14 is electrically connected to the input end of the motor 2. This is a common control structure and will not be described in detail here.

[0030] In one embodiment, two groups of suction cups 11 are arranged, and the suction cups 11 are symmetrically arranged along the central axis of the housing 1 to improve the stability of the fixation.

[0031] In one embodiment, the slider 7 is a T-shaped structure, and the outer wall of the slider 7 is polished to facilitate sliding up and down.

[0032] In one embodiment, the surface of the housing 1 is densely and evenly provided with ventilation holes on one side of the motor 2 to facilitate heat dissipation of the motor 2.

[0033] Working principle:

[0034] When inspecting and disassembling the aircraft shell 1, the screwdriver head 5 can be inserted into the knife groove of the nut of the aircraft shell 1. Then, the suction cup 11 is adsorbed and fixed to the surface of the aircraft shell 1, and the motor 2 can be started to drive the screwdriver head 5 to rotate, and then the screw is removed. During the starting process of the motor 2, the connecting rod 9 and the suction cup 11 resist the torque generated during rotation, preventing the staff from losing their hands, which greatly facilitates the staff to carry out inspection and disassembly and improves the convenience of use. At the same time, the device utilizes the smooth surface of the aircraft shell 1 and adopts the suction cup 11 for fixing. It is convenient to install and disassemble, and has high fixing stability. The staff does not need to tighten it vigorously, which is more flexible and labor-saving to use. At the same time, the slider 7 can slide up and down along the track 6, and the first hinge seat 8 and the second hinge seat 10 facilitate the connecting rod 9 to rotate up and down, thereby greatly facilitating the staff to move the shell 1 and the screwdriver head 5 up and down, and conveniently move the screwdriver head 5 up to remove the screw when turning the screw, further improving the convenience of use.

[0035] In the present invention, unless otherwise clearly stipulated and limited, the terms "install", "set", "connect", "fix", "screw" and the like should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integrated connection; it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium; it can be the internal connection of two elements or the interaction relationship between two elements. Unless otherwise clearly defined, ordinary technicians in this field can understand the specific meanings of the above terms in the present invention according to the specific circumstances.

[0036] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present invention should be included in the scope of protection of the present invention.

Claims

1. A handheld tool for aircraft maintenance, characterized in that: The invention comprises a housing (1) and a motor (2), wherein the motor (2) is fixedly mounted inside the housing (1), and the output end of the motor (2) is connected to a screwdriver head (5) via a connector (4), and a track (6) is fixedly mounted on the outer surface of the housing (1), a slider (7) is slidably connected inside the track (6), and a connecting rod (9) is hinged on the surface of the slider (7) via a first hinge seat (8), and the other end of the connecting rod (9) is hinged to a suction cup (11) via a second hinge seat (10), and a handle (13) is fixedly connected to the top surface of the housing (1) via a handle rod (12).

2. The handheld tool for aircraft maintenance according to claim 1, characterized in that: A battery (3) is fixedly installed inside the housing (1), and the battery (3) is electrically connected to the motor (2) via an electrical connection line.

3. The handheld tool for aircraft maintenance according to claim 1, characterized in that: A switch (14) is fixedly mounted on the surface of the handlebar (12), and an output end of the switch (14) is electrically connected to an input end of the motor (2).

4. The handheld tool for aircraft maintenance according to claim 1, characterized in that: The suction cups (11) are arranged in two groups, and the suction cups (11) are symmetrically arranged along the central axis of the housing (1).

5. The handheld tool for aircraft maintenance according to claim 1, characterized in that: The slider (7) is a T-shaped structure, and the outer wall of the slider (7) is polished.

6. The handheld tool for aircraft maintenance according to claim 1, characterized in that: The surface of the housing (1) is located on one side of the motor (2) and is densely and evenly provided with ventilation holes.

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