CN212020705U

CN212020705U - Small-size tool cabinet is used in aircraft engine maintenance

Info

Publication number: CN212020705U
Application number: CN201922488230.8U
Authority: CN
Inventors: 王茂恒
Original assignee: Feierde Aviation Equipment Manufacturing Shanghai Co ltd
Current assignee: Feierde Aviation Equipment Manufacturing Shanghai Co ltd
Priority date: 2019-12-30
Filing date: 2019-12-30
Publication date: 2020-11-27
Anticipated expiration: 2029-12-30

Abstract

The utility model belongs to the technical field of the tool cabinet, especially, a small-size tool cabinet is used in aircraft engine maintenance, the intelligent cabinet temperature adjusting device comprises a cabinet body, the cabinet body is one side open-ended rectangle box, the opening of the cabinet body passes through the baffle to be separated and constitutes top storehouse and bottom storehouse, the opening gomphosis in top storehouse is connected with the drawer, two electric screwdriver have been put in the drawer, there are first door and the second door that opens and shuts in the both sides of bottom storehouse through hinged joint, the avris fixed mounting of first door that opens and shuts has the three-layer rocker, all be equipped with the instrument draw-in groove on the three-layer rocker, equal gomphosis has the repair tools of adaptation with it. The utility model discloses a screw of different models on two electric screwdriver of drawer splendid attire dismouting aircraft engine respectively, the rocker corresponds the various repair tools of gomphosis through the instrument draw-in groove, is convenient for quick when the maintenance take and place, and the part splendid attire box avoids the part misuse through the renewal part that part location splendid attire hole location gomphosis corresponds, so promotes the convenience and the maintenance effect of maintenance.

Description

Small-size tool cabinet is used in aircraft engine maintenance

Technical Field

The utility model relates to a tool cabinet technical field specifically is an aircraft engine maintains and uses small-size tool cabinet.

Background

The aviation maintenance is to maintain and repair the aircraft and the technical equipment on the aircraft, keep and improve the feasibility of the aircraft, ensure the safety of the aircraft, is a precondition and a necessary condition for the use of the aircraft, and is also an important component of the aviation industry; the aircraft engine is the heart of the aircraft, the aircraft engine maintenance is a part of the aircraft maintenance, also is the important component part of the aviation aircraft work, the importance of the aircraft engine maintenance, mainly because the aircraft engine is a complicated machine composed of various types of parts and components, works in the working state of high temperature, high pressure, high rotating speed and severe environment which are constantly changed, requires light weight, large thrust, low oil consumption, reliable work, long service life and low cost, and the engine structure is constantly updated, so the proportion occupied by the aircraft engine maintenance is constantly increased; during the maintenance of the aircraft engine, various types of tools are used, and various parts on the aircraft engine are correspondingly assembled and disassembled, so that some devices are needed for auxiliary work, and the tool cabinet is most widely used.

The current tool cabinet for maintaining the aircraft engine has the following problems:

1. when the existing tool cabinet for maintaining the aircraft engine is operated, corresponding tools and parts cannot be found frequently, so that the maintenance efficiency is low, and the risk of mistakenly installing the parts exists.

2. The current tool cabinet for aircraft engine maintenance can not accurately observe the detached parts when performing maintenance operation, so that maintenance personnel can not quickly judge the use value of the tool cabinet.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

The utility model provides a not enough to prior art, the utility model provides an aircraft engine maintains and uses small-size tool cabinet has solved present aircraft engine maintains and uses tool cabinet when the operation, and corresponding instrument and part can not often be found to the maintenance personal to and can not carry out accurate observation to the part of pulling down, can't judge its use value's problem rapidly.

(II) technical scheme

In order to achieve the above object, the utility model provides a following technical scheme: a small tool cabinet for maintaining an aircraft engine comprises a cabinet body, wherein the cabinet body is a rectangular box body with an opening on one side, the opening of the cabinet body is divided into a top bin and a bottom bin through a partition plate, a drawer is connected with the opening of the top bin in an embedded mode, two electric screwdrivers are placed in the drawer, a first opening and closing door and a second opening and closing door are connected to two sides of the bottom bin through hinges, a three-layer swing frame is fixedly mounted on the side of the first opening and closing door, tool clamping grooves are formed in the three layers of swing frame, maintenance tools matched with the tool clamping grooves are embedded in the tool clamping grooves, two layers of part containing boxes are fixedly mounted on the side of the second opening and closing door, part positioning containing holes are formed in the two layers of part containing boxes, replacement parts are embedded in the part positioning containing holes in an all positioning mode, a power supply, an electric dust collector and a waste box are arranged at the bottom of an inner cavity, the power supply is electrically connected with the electric dust collector.

As an optimal technical scheme of the utility model, the insulating shock pad has been laid to the top surface of the cabinet body, the fixed microscope that has put of top surface of insulating shock pad.

As a preferred technical scheme of the utility model, the avris vertical fixation of the cabinet body has telescopic support rod, telescopic support rod's top fixedly connected with horizontal pole, the top hoist and mount of horizontal pole have the light.

As a preferred technical scheme of the utility model, the equal fixedly connected with universal removal wheel of four corners of cabinet body bottom, four the universal removal takes turns to and all is equipped with the brake block.

As a preferred technical scheme of the utility model, the instrument draw-in groove with the avris in part location splendid attire hole is all fixed and is provided with the data plate.

(III) advantageous effects

Compared with the prior art, the utility model provides an aircraft engine maintains and uses small-size tool cabinet possesses following beneficial effect:

1. this aircraft engine maintenance is with small-size tool cabinet through the screw of two electric screwdriver of drawer splendid attire difference dismouting aircraft engine on different models, the rocker corresponds the various repair tools of gomphosis through the instrument draw-in groove, is convenient for quick when the maintenance take and place, and the part splendid attire box avoids the part misuse through the renewal part that part location splendid attire hole location gomphosis corresponds, so promotes the convenience and the maintenance effect of maintenance.

2. This aircraft engine maintains uses small-size tool cabinet has laid insulating shock pad and has put the microscope at the top surface of the cabinet body, and insulating shock pad has insulating and shock-absorbing function, can prevent well that aircraft engine part from producing to collide with, and the microscope is used for looking over aircraft engine part's local detail, observes it and whether produces the damage to judge its use value.

Drawings

Fig. 1 is a development schematic view of the subjective structure of the present invention;

fig. 2 is the side-cut structure schematic diagram of the utility model.

In the figure: 1. a cabinet body; 2. carrying out top bin; 3. a bottom bin; 4. a drawer; 5. an electric screwdriver; 6. a first opening and closing door; 7. a second opening and closing door; 8. placing a frame; 9. a tool clamping groove; 10. placing the box; 11. a part positioning and containing hole; 12. a power source; 13. an electric vacuum cleaner; 14. a waste material box; 15. an insulating shock pad; 16. a microscope; 17. a telescopic strut; 18. a cross bar; 19. an illuminating lamp; 20. a universal moving wheel.

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. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Examples

Referring to the attached

drawings

1 and 2 of the specification, the utility model provides the following technical solutions: a small tool cabinet for maintaining an aircraft engine comprises a cabinet body 1, wherein the cabinet body 1 is a rectangular box body with an opening at one side, the opening of the cabinet body 1 is divided into a top bin 2 and a bottom bin 3 through a partition plate, a drawer 4 is embedded and connected with the opening of the top bin 2, two electric screwdrivers 5 are placed in the drawer 4, two sides of the bottom bin 3 are connected with a first opening and closing door 6 and a second opening and closing door 7 through hinges, three layers of swing frames 8 are fixedly arranged at the edge side of the first opening and closing door 6, tool clamping grooves 9 are respectively arranged on the three layers of swing frames 8, maintenance tools matched with the tool clamping grooves 9 are respectively embedded in the tool clamping grooves 9, two layers of part containing boxes 10 are fixedly arranged at the edge side of the second opening and closing door 7, part positioning containing holes 11 are respectively arranged in the two layers of part containing boxes 10, replacement parts are positioned and embedded in the part positioning containing holes 11, a power supply 12, a dust collector 13 and a waste material box, the power source 12 is electrically connected to the electric vacuum cleaner 13.

In the embodiment, two electric screwdrivers 5 respectively adopt a CDR120-LI bent handle type high-power impact screwdriver and a Bosch-GO straight handle type low-power electric screwdriver to correspondingly screw large-size screws and small-size screws on an aircraft engine, and are respectively used for disassembling and assembling screws of different types on the aircraft engine when the aircraft engine is maintained, various maintenance tools such as hammers, wrenches and the like are respectively embedded in three layers of swing frames 8 through tool clamping grooves 9, tools of each type are respectively embedded into clamping grooves matched with the tools, so that the tools can be conveniently and quickly taken and placed during maintenance, the problem that required tools cannot be found during maintenance and the maintenance efficiency and the maintenance effect are influenced is avoided, the two layers of part containing boxes 10 are respectively embedded with corresponding replacement parts through the part positioning containing holes 11 in a positioning way, when any part is required to be used, the part can be directly taken out from the corresponding part positioning containing holes 11, the parts are prevented from being used wrongly, meanwhile, the parts are prevented from being collided with each other to cause damage in the transportation process, the power supply 12 adopts a lithium iron phosphate battery pack or a lead-acid battery pack which have good explosion resistance, and explosion accidents are avoided; the electric dust collector 13 adopts a JYB-057 type rechargeable handheld high-power dust collector, can absorb dust and sundries in the gaps of an aircraft engine, improves the convenience and the effect of maintenance, and the waste material box 14 is used for containing the replaced scrapped parts, rags and other auxiliary tools.

Specifically, an insulating shock pad 15 is laid on the top surface of the cabinet body 1, and a microscope 16 is fixedly placed on the top surface of the insulating shock pad 15.

In this embodiment, insulating shock pad 15 adopts rubber pad or foam sponge, and the two all has insulating and absorbing function, can prevent aircraft engine part to produce well and collide with, and microscope 16 is used for looking over aircraft engine part's local detail, observes it and whether produces the damage to judge its use value, wherein, microscope 16 adopts SMB-008 binocular type, convenient to use and observation.

Specifically, the avris of the cabinet body 1 is vertically fixed with a telescopic supporting rod 17, the top end of the telescopic supporting rod 17 is fixedly connected with a cross rod 18, and the top end of the cross rod 18 is hung with a lighting lamp 19.

In this embodiment, telescopic strut 17 drives the top hoist and mount of horizontal pole 18 and has light 19, and night or when light is not enough, takes telescopic strut 17 out to turn on light 19 and throw light on to the aircraft part, then retract it and fold at daytime or at the removal in-process that need not to use, so that remove.

Specifically, four equal fixedly connected with universal removal wheels 20 in corner of the 1 bottom of the cabinet body, all be equipped with the braking vane on four universal removal wheels 20.

In this embodiment, the cabinet body 1 is flexibly moved in the airport through the universal moving wheels 20 so as to perform corresponding maintenance on different aircraft engines, and when the cabinet body 1 is moved to a position near a set aircraft engine, the cabinet body 1 is braked and stopped through the brake plates on the universal moving wheels 20 so as to take out a corresponding tool for safe maintenance operation.

Specifically, the sides of the tool clamping groove 9 and the part positioning containing hole 11 are both fixedly provided with nameplates.

In this embodiment, the avris of instrument draw-in groove 9 and part location splendid attire hole 11 is all fixed and is provided with the data plate, and the data plate is arranged in the model and the specification of the instrument of joint in each instrument draw-in groove 9 of record sign to and the model and the specification of the part of each part location splendid attire hole 11 splendid attire, and the staff of being convenient for is quick accurate selects required instrument and part, avoids mixing the aircraft engine maintenance problem who causes.

The electric screwdriver 5, the power source 12, the electric dust collector 13 and the microscope 16 in the present embodiment are known technologies that have been disclosed to be widely used in industrial production and daily life.

The utility model discloses a theory of operation and use flow: two electric screw drivers 5 are used for correspondingly screwing large-size screws and small-size screws on an aircraft engine, when the aircraft engine is maintained, the screws with different types on the aircraft engine are respectively disassembled and assembled, various maintenance tools such as hammers, wrenches and the like are all embedded in the three layers of swing frames 8 through the tool clamping grooves 9, tools of each type are all embedded into the clamping grooves matched with the tools, the tools are convenient to rapidly take and place during maintenance, the situation that required tools cannot be found during maintenance is avoided, the maintenance efficiency and the maintenance effect are influenced is avoided, the two layers of part containing boxes 10 are directly positioned and embedded with corresponding replacement parts through the part positioning containing holes 11, when any part is required to be used, the part can be directly taken out from the corresponding part positioning containing holes 11, the part is prevented from being mistakenly used, meanwhile, the parts are prevented from being collided with each other during transportation to cause damage, the power supply 12 adopts a lithium ion battery pack or a lead-, the two have good explosion resistance, so that the explosion accident is avoided; the electric dust collector 13 adopts a JYB-057 type rechargeable handheld high-power dust collector, can absorb dust and sundries in the gap of an aircraft engine, and improves the convenience and the effect of maintenance; insulating shock pad 15 has been laid to the top surface of the cabinet body 1, and microscope 16 has been put to insulating shock pad 15's top surface is fixed, and insulating shock pad 15 has insulating and absorbing function, can prevent aircraft engine part to produce well and collide with, and microscope 16 is used for looking over aircraft engine part's local detail, observes whether it produces the damage to judge its use value.

Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. The utility model provides an aircraft engine maintains uses small-size tool cabinet, includes the cabinet body (1), its characterized in that: the improved multifunctional wardrobe is characterized in that the wardrobe body (1) is a rectangular box body with an opening on one side, the opening of the wardrobe body (1) is divided by a partition plate to form a top bin (2) and a bottom bin (3), the opening of the top bin (2) is embedded and connected with a drawer (4), two electric screwdrivers (5) are placed in the drawer (4), two sides of the bottom bin (3) are connected with a first opening and closing door (6) and a second opening and closing door (7) through hinges, a three-layer swing frame (8) is fixedly installed on the side of the first opening and closing door (6), a tool clamping groove (9) is formed in each of the three layers of swing frames (8), maintenance tools matched with the tool clamping groove (9) are embedded in each tool clamping groove, two layers of part containing boxes (10) are fixedly installed on the side of the second opening and closing door (7), part positioning and part replacing holes (11) are formed in each part containing box (10), the bottom of the inner cavity of the bottom bin (3) is provided with a power supply (12), an electric dust collector (13) and a waste material box (14), and the power supply (12) is electrically connected with the electric dust collector (13).

2. A small tool cabinet for servicing an aircraft engine, as defined in claim 1, wherein: insulating shock pad (15) have been laid to the top surface of the cabinet body (1), microscope (16) have been fixed to put on the top surface of insulating shock pad (15).

3. A small tool cabinet for servicing an aircraft engine, as defined in claim 1, wherein: the avris of the cabinet body (1) is perpendicularly fixed with telescopic strut (17), the top fixedly connected with horizontal pole (18) of telescopic strut (17), the top hoist and mount of horizontal pole (18) have light (19).

4. A small tool cabinet for servicing an aircraft engine, as defined in claim 1, wherein: four equal fixedly connected with universal removal wheels (20) in corner of the cabinet body (1) bottom, four all be equipped with the braking vane on the universal removal wheel (20).

5. A small tool cabinet for servicing an aircraft engine, as defined in claim 1, wherein: the tool clamping groove (9) and the side of the part positioning containing hole (11) are both fixedly provided with nameplates.