CN205058016U - Be applied to tool bogie that aircraft engine disassembled operation - Google Patents
Be applied to tool bogie that aircraft engine disassembled operation Download PDFInfo
- Publication number
- CN205058016U CN205058016U CN201520844445.8U CN201520844445U CN205058016U CN 205058016 U CN205058016 U CN 205058016U CN 201520844445 U CN201520844445 U CN 201520844445U CN 205058016 U CN205058016 U CN 205058016U
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- China
- Prior art keywords
- support
- tool holder
- aircraft engine
- instrument
- hand push
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
The utility model relates to a be applied to tool bogie that aircraft engine disassembled operation, the large -scale motor assembly jig comprises an operation bench, the operation panel both sides hang and are equipped with the tool holder, and the operation panel erects on the support, and the support lower extreme is provided with the gyro wheel, and support one side still is provided with hand push frame, the support is lifting support, and lifting support is last to be provided with spacing locking bolt, be provided with multilayer magnetism baffle in the tool holder, split into a plurality of little check with the tool holder inner chamber, place different instruments, be provided with the brake block on the gyro wheel of the support lower extreme on one side of being close to hand push frame. Through elevating gear on the support and spacing locking bolt, can switch over between different stations frame, adapt to the not operation needs of co -altitude, the tool holder is placed the instrument in unison, and the tool holder is cut apart to the magnetism baffle simultaneously for instrument classification place in the tool holder, and adsorb on the magnetism baffle, be difficult for losing, simple structure, economy is suitable for, makes people when disassembling the operation to the aircraft, and the improvement of the availability factor of instrument is showing.
Description
Technical field:
The utility model relates to technical field of engine overhaul, is specifically related to a kind ofly be applied to the tool car that operation disassembled by aircraft engine.
Background technology:
Disassemble in work at aircraft engine, the conventional tool of use over one hundred kind, and different inter process is frequently changed, operator puts in disorder in the instrument process used, and often mixedly with part puts, and causes the problem generations such as bump injury, affects product quality; Meanwhile, when operating, an operator often travels to and fro between searching instrument between station, causes work discontinuous, affects operating efficiency, increases the physical cost of operation; Knock off check time, spanner occurs sometimes, and to be placed on somewhere covered, finds the situation that just can find half a day.And disassemble in process at aircraft, aircraft build is comparatively large, and operation height is not fixed, and tool car can not meet the requirement of use, in order to address these problems, improves operating efficiency, uses carry out visual and standardized management to the instrument of on-the-spot actual job process.
Utility model content:
The utility model provides a kind of and is applied to the tool car that operation disassembled by aircraft engine, and the operation needs in operation process disassembled by adaptation aircraft.
For achieving the above object, the utility model is by the following technical solutions:
What the utility model provided is a kind ofly applied to the tool car that operation disassembled by aircraft engine, and comprise operating desk, described operating desk both sides are linked with instrument cases, and operating desk is erected on support, and pedestal lower end is provided with roller, and support side is also provided with hand push frame.
Described support is lifting support, lifting support is provided with limiting locking bolt.
Be provided with multi-layered magnetic dividing plate in described instrument cases, be multiple little lattice by instrument cases lumen segmentation, place different instrument.
The roller of the pedestal lower end near hand push frame side is provided with brake block.
The beneficial effects of the utility model: by the lowering or hoisting gear on support and limiting locking bolt, can assemble between station rack in difference and switch, adapt to the operation needs of differing heights, instrument cases are placed unified for instrument, instrument cases are split by magnetic dividing plate simultaneously, tools sort in instrument cases is placed, and be adsorbed on magnetic dividing plate, not easily lose, structure is simple, economic and practical, and makes people when disassembling operation to aircraft, because instrument uses the loaded down with trivial details quality problems of disassembling caused obviously to reduce, the service efficiency of instrument improves significantly.
Accompanying drawing illustrates:
To be that the utility model is a kind of be applied to the structural representation that the tool car of operation disassembled by aircraft engine to Fig. 1;
Fig. 2 is the structural representation of instrument cases;
1-operating desk, 2-instrument cases, 3-support, 4-roller, 5-hand push frame, 6-limiting locking bolt, 7-magnetic dividing plate, 8-brake block.
Detailed description of the invention:
Below in conjunction with embodiment, the utility model is described in further detail.
According to Fig. 1 ~ Fig. 2, be a kind ofly applied to the tool car that operation disassembled by aircraft engine, comprise operating desk 1, described operating desk 1 both sides are linked with instrument cases 2, operating desk 1 is erected on support 3, and support 3 lower end is provided with roller 4, and support 3 side is also provided with hand push frame 5.
Described support 3 is lifting support, lifting support is provided with limiting locking bolt 6.
Be provided with multi-layered magnetic dividing plate 7 in described instrument cases 2, be multiple little lattice by instrument cases lumen segmentation, place different instrument.
The roller 4 of support 3 lower end near hand push frame 5 side is provided with brake block 8.
Finally should be noted that: above embodiment is only in order to illustrate that the technical solution of the utility model is not intended to limit, although be described in detail the utility model with reference to above-described embodiment, those of ordinary skill in the field are to be understood that: still can modify to detailed description of the invention of the present utility model or equivalent replacement, and not departing from any amendment of the utility model spirit and scope or equivalent replacement, it all should be encompassed in the middle of this right.
Claims (4)
1. be applied to the tool car that operation disassembled by aircraft engine, it is characterized in that: comprise operating desk, described operating desk both sides are linked with instrument cases, and operating desk is erected on support, and pedestal lower end is provided with roller, and support side is also provided with hand push frame.
2. be according to claim 1ly a kind ofly applied to the tool car that operation disassembled by aircraft engine, it is characterized in that: described support is lifting support, lifting support is provided with limiting locking bolt.
3. be according to claim 1ly a kind ofly applied to the tool car that operation disassembled by aircraft engine, it is characterized in that: be provided with multi-layered magnetic dividing plate in described instrument cases, is multiple little lattice by instrument cases lumen segmentation.
4. be according to claim 1ly a kind ofly applied to the tool car that operation disassembled by aircraft engine, it is characterized in that: on the roller of the pedestal lower end near hand push frame side, be provided with brake block.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520844445.8U CN205058016U (en) | 2015-10-28 | 2015-10-28 | Be applied to tool bogie that aircraft engine disassembled operation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520844445.8U CN205058016U (en) | 2015-10-28 | 2015-10-28 | Be applied to tool bogie that aircraft engine disassembled operation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205058016U true CN205058016U (en) | 2016-03-02 |
Family
ID=55384617
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520844445.8U Expired - Fee Related CN205058016U (en) | 2015-10-28 | 2015-10-28 | Be applied to tool bogie that aircraft engine disassembled operation |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205058016U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108466245A (en) * | 2018-06-26 | 2018-08-31 | 中电科芜湖钻石飞机制造有限公司 | Instrument cases applied to the manufacture of aircraft avionics and assembling work |
-
2015
- 2015-10-28 CN CN201520844445.8U patent/CN205058016U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108466245A (en) * | 2018-06-26 | 2018-08-31 | 中电科芜湖钻石飞机制造有限公司 | Instrument cases applied to the manufacture of aircraft avionics and assembling work |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6 Patentee after: Chinese Hangfa Shenyang Liming Aero engine limited liability company Address before: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6 Patentee before: Liming Aeroplane Engine (Group) Co., Ltd., Shenyang City |
|
| CP01 | Change in the name or title of a patent holder | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160302 Termination date: 20201028 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |