CN211073539U - Multifunctional tool kit for aircraft maintenance - Google Patents

Abstract

The utility model discloses a multifunctional tool kit is used in aircraft maintenance, the power distribution box comprises a box body, the diapire of box is fixed with four rubber pads, the diapire fixed mounting of box has solar panel, solar panel's roof fixedly connected with converter, the output of converter all is connected with the wire, two battery jars have been seted up in the box. The utility model discloses a converter will install the absorptive solar energy of solar panel on the box and convert the electric energy into and store in the battery, the problem that need look for external power source when using electrical apparatus instrument maintenance has been solved, the convenience of maintenance has effectively been improved, toughened glass protective material's protection casing both can prevent that external environment from leading to the fact the damage to solar panel simultaneously, also can not hinder solar panel absorption solar energy, and row and other instruments will be inserted to row groove and upper cover and separate, the security that the row used has effectively been guaranteed to insert, the debris has been avoided getting into and has caused the internal circuit short circuit in the row of inserting.

Description

Multifunctional tool kit for aircraft maintenance

Technical Field

The utility model relates to a toolbox technical field especially relates to an aircraft maintenance uses multi-functional toolbox.

Background

The multifunctional tool box for airplane maintenance is one box for holding various airplane maintenance tools. The method is mainly used for repairing, assembling and debugging the structure and accessories of the airplane body, testing the airplane to fly, diagnosing faults of the airplane, troubleshooting and the like.

Through the retrieval, chinese granted patent No. CN109129376A discloses a multifunctional tool case is used in aircraft maintenance, relate to toolbox technical field, including box and case lid, the positive top middle part fixedly connected with fixing device of box, the positive middle part of box is provided with the handle, the equal fixedly connected with universal wheel in a side four corners department of box, the another side bottom of box is provided with flexible handle, fixing device's upper surface middle part fixedly connected with button, the equal fixedly connected with in bottom both sides of button presses the depression bar, the trapezoidal slider of lower surface one end fixedly connected with of pressing the depression bar, fixing device's inside symmetry is provided with two slide bars, the upper surface and the equal fixedly connected with fixed block in lower surface middle part of slide bar, the positive middle part fixedly connected with triangle slider of slide bar, the one end fixedly connected with lug of slide bar, the.

The existing multifunctional tool box for airplane maintenance has the following defects: aircraft maintenance often need use power maintenance tool, and it is very inconvenient to insert external power supply when needing to use, moreover under different maintenance environment, also is difficult to find the external power supply that can use, even use external power supply through acting as go-between, and consuming time is long and complex operation.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving the problem in the background art and providing a multifunctional tool box for aircraft maintenance.

In order to achieve the above purpose, the utility model adopts the following technical scheme:

the utility model provides an aircraft maintenance uses multi-functional toolbox, includes the box, the diapire of box is fixed with four rubber pads, the diapire fixed mounting of box has solar panel, solar panel's roof fixedly connected with converter, the output of converter all is connected with the wire, two battery jars have been seted up in the box, two equal fixed battery, two of having placed in the battery jar the other end of wire all is connected with the input of battery, the roof fixedly connected with row's of inserting groove of battery jar, the row's of inserting inslot is installed and is inserted, two the output of battery all is connected with the input of inserting the row.

Preferably, a protective cover is fixed to the bottom wall of the box body and located below the solar panel.

Preferably, the protective cover is made of transparent tempered glass material.

Preferably, a round shaft is fixedly connected between the left side wall and the right side wall of the power strip groove, and an upper cover is rotatably sleeved on the outer wall of the round shaft.

Preferably, the diapire fixedly connected with inserted bar of upper cover, the fixed slot has been seted up to the preceding lateral wall in extension socket groove, the fixed slot interpolation is equipped with the expansion plate, the expansion plate integrated circuit board be equipped with the big or small position assorted socket of inserted bar.

Preferably, a baffle plate sliding in the fixing groove is fixed at one end of the expansion plate positioned in the fixing groove, vertical inward flanges are symmetrically fixed on the upper wall and the lower wall of the fixing groove, the distance between the two flanges is smaller than the length of the baffle plate, and an expansion spring sleeved on the outer wall of the expansion plate is fixed between the flanges and the baffle plate.

Compared with the prior art, this aircraft maintenance is with multi-functional toolbox's advantage lies in:

1. the solar energy absorbed by the solar panel arranged on the box body is converted into electric energy through the converter and stored in the storage battery, so that the problem that an external power supply needs to be searched when an electric appliance tool is used for maintenance is solved, and the convenience of maintenance is effectively improved;

2. the protective cover made of the toughened glass protective material can prevent the solar panel from being damaged by the external environment and can not prevent the solar panel from absorbing solar energy;

3. the power strip is separated from other tools by the power strip groove and the upper cover, so that the use safety of the power strip is effectively ensured, and the internal circuit short circuit caused by the fact that sundries enter the power strip is avoided;

to sum up, the utility model discloses a converter will install the absorptive solar energy of solar panel on the box and convert the electric energy to and store in the battery, the problem that need look for external power source when using electrical apparatus instrument maintenance has been solved, the convenience of maintenance has effectively been improved, toughened glass protective material's protection casing both can prevent that external environment from leading to the fact the damage to solar panel simultaneously, can not hinder solar panel absorption solar energy yet, and row of inserting groove and upper cover will be inserted and row and other instruments are separated, the security that row of inserting used has effectively been guaranteed, debris entering has been avoided and has been caused the internal circuit short circuit in the row of inserting.

Drawings

Fig. 1 is a front view of a multifunctional tool box for aircraft maintenance according to the present invention;

fig. 2 is a top view of the multifunctional tool box for aircraft maintenance according to the present invention;

fig. 3 is a side view of the structure of the multifunctional tool box part for aircraft maintenance according to the present invention.

In the figure: the solar photovoltaic power generation system comprises a box body 1, a rubber pad 2, a protective cover 3, a solar panel 4, a converter 5, a lead 6, a storage battery 7, an 8-socket groove, a round shaft 9, an upper cover 10, an 11-socket, an inserted rod 12, an expansion plate 13, an expansion spring 14 and a baffle 15.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.

Referring to fig. 1-3, a multifunctional tool box for aircraft maintenance comprises a box body 1, wherein four rubber pads 2 are fixed on the bottom wall of the box body 1, and the rubber pads 2 avoid friction between the box body 1 and the ground, so that the tool box is protected in a buffering manner.

The solar panel 4 is fixedly arranged on the bottom wall of the box body 1, the protective cover 3 is fixed on the bottom wall of the box body 1, the protective cover 3 is positioned below the solar panel 4, the protective cover 3 is made of transparent toughened glass material, the protective cover 3 made of toughened glass protective material can prevent the solar panel 4 from being damaged by the external environment and can not prevent the solar panel 4 from absorbing solar energy, the top wall of the solar panel 4 is fixedly connected with a converter 5, the output end of the converter 5 is connected with a lead 6, two battery grooves are arranged in the box body 1, storage batteries 7 are fixedly arranged in the two battery grooves, the other ends of the two lead 6 are connected with the input ends of the storage batteries 7, the top wall of each battery groove is fixedly connected with a socket groove 8, a socket 11 is arranged in the socket groove 8, the output ends of the two storage batteries 7 are connected with the input ends of the socket 11, the solar energy absorbed by the, the problem of need look for external power when using electrical apparatus instrument maintenance is solved, the convenience of maintenance has effectively been improved.

A round shaft 9 is fixedly connected between the left side wall and the right side wall of the power strip 8, an upper cover 10 is rotatably sleeved on the outer wall of the round shaft 9, an insert rod 12 is fixedly connected on the bottom wall of the upper cover 10, a fixing groove is formed in the front side wall of the power strip 8, an expansion plate 13 is inserted in the fixing groove, a socket matched with the insert rod 12 in size and position is clamped on the expansion plate 13, a baffle plate 15 sliding in the fixing groove is fixed at one end of the expansion plate 13 positioned in the fixing groove, vertical inward flanges are symmetrically fixed on the upper wall and the lower wall of the fixing groove, the distance between the two flanges is smaller than the length of the baffle plate 15, an expansion spring 14 sleeved on the outer wall of the expansion plate 13 is fixed between the flanges and the baffle plate 15, when maintenance is needed, the expansion plate 13 is pulled, the upper cover 10 is pulled, the power strip 11 can be used, after the use is finished, the expansion plate 13, extension spring 14 receives the extrusion to kick-back and promotes baffle 15 and remove in to the fixed slot, drives expansion plate 13 and removes in the fixed slot immediately, and then supports inserted bar 12 and carry out spacing fixed, and row's of inserting groove 8 and upper cover 10 will be inserted row 11 and other instruments and separate, have effectively guaranteed the security that row's of inserting 11 used, have avoided debris to get into and have caused the internal line short circuit in row's of inserting 11.

Further, unless otherwise specifically stated or limited, the above-described fixed connection is to be understood in a broad sense, and may be, for example, welded, glued, or integrally formed as is conventional in the art.

Now, the operation principle of the present invention is explained as follows:

the solar energy absorbed by the solar panel 4 installed on the box body 1 is converted into electric energy through the converter 5 to be stored in the storage battery 7, the problem that an external power supply needs to be found when an electric appliance tool is used for maintenance is solved, the maintenance convenience is effectively improved, meanwhile, the protective cover 3 made of the toughened glass protective material can prevent the external environment from damaging the solar panel 4, the solar panel 4 can not be prevented from absorbing the solar energy, the socket groove 8 and the upper cover 10 separate the socket 11 from other tools, the use safety of the socket 11 is effectively guaranteed, and the situation that sundries enter the socket 11 to cause internal circuit short circuit is avoided.

The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.

Claims (6)

1. The utility model provides an aircraft maintenance uses multi-functional toolbox, includes box (1), its characterized in that, the diapire of box (1) is fixed with four rubber pads (2), the diapire fixed mounting of box (1) has solar panel (4), the roof fixedly connected with converter (5) of solar panel (4), the output of converter (5) all is connected with wire (6), two battery jars have been seted up in box (1), two battery (7), two have all fixedly placed in the battery jar the other end of wire (6) all is connected with the input of battery (7), the roof fixedly connected with of battery jar inserts row groove (8), install row's of inserting (11), two in row's of inserting groove (8) the output of battery (7) all is connected with the input of row's of inserting (11).

2. Multifunctional toolbox for aircraft maintenance according to claim 1, characterized in that a protective cover (3) is fixed to the bottom wall of the box body (1), said protective cover (3) being located below the solar panel (4).

3. The multifunctional toolbox for aircraft maintenance according to claim 2, characterized in that the protective cover (3) is made of transparent tempered glass material.

4. The multifunctional toolbox for aircraft maintenance according to claim 1, wherein a circular shaft (9) is fixedly connected between the left and right side walls of the socket slot (8), and an upper cover (10) is rotatably sleeved on the outer wall of the circular shaft (9).

5. The multifunctional toolbox for aircraft maintenance according to claim 4, wherein an insert rod (12) is fixedly connected to the bottom wall of the upper cover (10), a fixing groove is formed in the front side wall of the socket groove (8), an expansion plate (13) is inserted into the fixing groove, and a socket matched with the insert rod (12) in size and position is clamped in the expansion plate (13).

6. The multifunctional toolbox for aircraft maintenance according to claim 5, wherein one end of the expansion plate (13) positioned in the fixing groove is fixed with a baffle plate (15) sliding in the fixing groove, the upper wall and the lower wall of the fixing groove are symmetrically fixed with vertical inward flanges, the distance between the two flanges is smaller than the length of the baffle plate (15), and an expansion spring (14) sleeved on the outer wall of the expansion plate (13) is fixed between the flanges and the baffle plate (15).

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