CN208855887U - A kind of auxiliary device for aircraft maintenance - Google Patents
A kind of auxiliary device for aircraft maintenance Download PDFInfo
- Publication number
- CN208855887U CN208855887U CN201821368712.9U CN201821368712U CN208855887U CN 208855887 U CN208855887 U CN 208855887U CN 201821368712 U CN201821368712 U CN 201821368712U CN 208855887 U CN208855887 U CN 208855887U
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- CN
- China
- Prior art keywords
- side cover
- tool box
- right end
- shape block
- handle
- Prior art date
- 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.)
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- Workshop Equipment, Work Benches, Supports, Or Storage Means (AREA)
- Details Of Spanners, Wrenches, And Screw Drivers And Accessories (AREA)
Abstract
The utility model provides a kind of auxiliary device for aircraft maintenance, including tool box, the tool box right end opens up fluted, the inside grooves are equipped with magnet, the magnet is fixed on side cover left end, the side cover is embedded in tool box right end, the side cover right end installs L shape block, the L shape block right end is equipped with connection bolt, the connection bolt passes through L shape block and is connected with side cover, the L shape block inner end is equipped with handle one, the handle one is mounted on side cover right end, the side cover right end upper position is equipped with flat mouth hasp one, the flat mouth hasp one is mounted on tool box right end, the tool box is connected by flat mouth hasp one with side cover, the design is convenient for the temporarily placement small irony connector such as bolt and nut, the utility model is structurally reasonable, it is easy to use, convenient for being placed to iron piece, it avoids losing.
Description
Technical field
The utility model is a kind of auxiliary device for aircraft maintenance, belongs to aircraft maintenance technical field.
Background technique
Aircraft maintenance is a kind of work, including aircraft body structure and attachment are repaired, assembly and debugging, Aircraft Flight Test and its
The actions such as fault diagnosis and troubleshooting, aircraft repair technical management, aircraft flight-line service.
In the prior art, it is attached due to the part of aircraft by the ironys connector such as bolt and nut,
When repairing, often need to disassemble the ironys connector such as bolt and nut, and the ironys such as bolt and nut connect
The small volume of part, after the ironys connector such as bolt and nut is placed on pallet by staff, bolt and nut etc.
Irony connector is easy to happen movement, falls to generate, and bolt and nut is caused to be lost.
Utility model content
In view of the deficienciess of the prior art, the utility model aim is to provide a kind of auxiliary dress for aircraft maintenance
It sets, to solve the problems mentioned in the above background technology, the utility model is structurally reasonable, and it is easy to use, convenient for small to irony by zero
Part is placed, and avoids losing.
To achieve the goals above, the utility model is achieved through the following technical solutions: a kind of tie up for aircraft
The auxiliary device repaired, including tool box, the tool box right end open up it is fluted, the inside grooves be equipped with magnet, the magnetic
In side cover left end, the side cover is embedded in tool box right end for ferropexy, and the side cover right end installs L shape block, the L shape block right end
Equipped with connection bolt, the connection bolt passes through L shape block and is connected with side cover, and the L shape block inner end is equipped with handle one, and described
Hand one is mounted on side cover right end, and the side cover right end upper position is equipped with flat mouth hasp one, and the flat mouth hasp one is mounted on work
Has case right end, the tool box is connected by flat mouth hasp one with side cover.
Further, there are two the flat mouth hasp one is set, two flat mouth hasps one are symmetrically mounted on the tool box right side
End, two flat mouth hasps one are connected with tool box and side cover by screw respectively.
Further, cover board is installed in the tool box upper end, and cover board lower-end rear portion position passes through hinge and tool box phase
Connection, and cover forward end is connected by two flat mouth hasps two with tool box.
Further, tool box front center position is equipped with handle two by screw, and is enclosed on handle two
Rubber sleeve.
Further, there are two the L shape block and connection bolt are all provided with, two L shape blocks are symmetrically mounted on side cover
Right end, two L shape blocks are symmetrically mounted on one rear and front end of handle, and two L shape blocks pass through shaft and one phase of handle
Connection, two L shape blocks pass through connection bolt is mutually fixed with side cover, the side cover right end symmetrically open up there are two screw thread
Hole, through-hole is offered on the L shape block, and the connection bolt passes through through-hole and is engaged with threaded hole.
Further, the magnet is connected by viscose glue with side cover.
The utility model has the beneficial effects that a kind of auxiliary device for aircraft maintenance of the utility model, this is practical new
Type is opened because increasing side cover, flat mouth hasp one, tool box, handle one, L shape block, connection bolt, magnet and groove, the design
Then the small irony connector such as the bolt disassembled in maintenance work is placed on magnet by side cover, magnet is to these iron
Matter connector is adsorbed and is fixed, so that irony connector be avoided to fall and lose, is solved in the prior art
Due to the small volume of the ironys connector such as bolt and nut, staff places the ironys connector such as bolt and nut
After on pallet, the ironys connector such as bolt and nut is easy to happen movement, falls to generate, leads to bolt and nut
The drawbacks of loss, the utility model is structurally reasonable, easy to use, convenient for placing iron piece, avoids losing.
Detailed description of the invention
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model
Sign, objects and advantages will become more apparent upon:
Fig. 1 is a kind of structural schematic diagram of the auxiliary device for aircraft maintenance of the utility model；
Fig. 2 is the partial enlarged view of A in a kind of auxiliary device for aircraft maintenance of the utility model；
Fig. 3 is side cover, flat mouth hasp one, tool box, magnetic in a kind of auxiliary device for aircraft maintenance of the utility model
The assembling figure of iron and groove；
In figure: 1- side cover, 2- flat mouth hasp one, the tool box 3-, 4- handle one, 5-L shape block, 6- connection bolt, 7- magnet,
8- groove.
Specific embodiment
To be easy to understand the technical means, creative features, achievement of purpose, and effectiveness of the utility model, below
In conjunction with specific embodiment, the utility model is further described.
Fig. 1-Fig. 3 is please referred to, the utility model provides a kind of technical solution: a kind of auxiliary device for aircraft maintenance,
Including tool box 3, the maintenance tools such as screwdriver are mounted with inside tool box 3,3 right end of tool box opens up fluted 8, groove 8
Design is equipped with magnet 7 convenient for accommodating to magnet 7 and side cover 1 inside groove 8, magnet 7 is fixed on 1 left end of side cover, side cover
1 is embedded in 3 right end of tool box, and 1 right end of side cover installs L shape block 5, and 5 right end of L shape block is equipped with connection bolt 6, and connection bolt 6 passes through L
Shape block 5 is connected with side cover 1, and 5 inner end of L shape block is equipped with handle 1, and handle 1 is mounted on 1 right end of side cover, and handle 1 passes through L
Shape block 5 is attached with side cover 1, and L shape block 5 is attached by connecting bolt 6 with side cover 1, and 1 right end upper position of side cover is equipped with
Flat mouth hasp 1, flat mouth hasp 1 are mounted on 3 right end of tool box, and tool box 3 is connected by flat mouth hasp 1 with side cover 1,
Staff opens flat mouth hasp 1, and then the locking of releasing appliance case 3 and side cover 1 holds conservative 1, and the handle that moves right
Hand 1, handle 1, which moves right, drives side cover 1 to be rotated around hinge, and side cover 1 is opened in realization, to keep magnet 7 naked
Dew in air, then staff by aircraft maintenance work in the small irony connector such as the bolt that generates and nut put
It sets in 7 upper end of magnet, magnet 7 is adsorbed and fixed to irony connector, is effectively avoided irony connector and is fallen
It falls and loses.
There are two flat mouth hasp 1 is set, two flat mouth hasps 1 are symmetrically mounted on 3 right end of tool box, two flat mouth hasps
One 2 are connected with tool box 3 and side cover 1 respectively by screw, screw realize flat mouth hasp 1 and tool box 3 and
The connection of side cover 1.
Cover board is installed in 3 upper end of tool box, and cover board lower-end rear portion position is connected by hinge with tool box 3, and cover board
Front end is connected by two flat mouth hasps two with tool box 3, and when repairing, staff opens flat mouth hasp two, then
Around hinge rotating plate, cover board is opened in realization, then takes out the maintenance tool inside tool box 3, and enforcement of going forward side by side is used.
3 front center position of tool box is equipped with handle two by screw, and rubber sleeve is wrapped up on handle two, handle two
Convenient for carrying out lifting carrying to the utility model, the design of rubber sleeve improves the comfort level of lifting.
There are two L shape block 5 and connection bolt 6 are all provided with, two L shape blocks 5 are symmetrically mounted on 1 right end of side cover, two L
Shape block 5 is symmetrically mounted on one 4 rear and front end of handle, and two L shape blocks 5 are connected by shaft with handle 1, two L
Shape block 5 is fixed by connection bolt 6 with 1 phase of side cover, 1 right end of side cover symmetrically open up there are two threaded hole, open up on L shape block 5
There is through-hole, connection bolt 6 passes through through-hole and is engaged with threaded hole, convenient between connection bolt 6 and L shape block 5 and side cover 1
Connection.
Magnet 7 is connected by viscose glue with side cover 1, convenient for the connection of magnet 7 and side cover 1.
The basic principles and main features of the present invention and the advantages of the present invention have been shown and described above, for
For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this
In the case where the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute
Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent elements of the claims
All changes are embraced therein.It should not treat any reference in the claims as limiting related right
It is required that.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiments being understood that.
Claims (6)
1. a kind of auxiliary device for aircraft maintenance, including tool box (3), it is characterised in that: tool box (3) right end is opened
Equipped with groove (8), magnet (7) are equipped with inside the groove (8), the magnet (7) is fixed on side cover (1) left end, the side cover
(1) it is embedded in tool box (3) right end, side cover (1) right end installs L shape block (5), and L shape block (5) right end is equipped with connection spiral shell
Bolt (6), the connection bolt (6) pass through L shape block (5) and are connected with side cover (1), and the L shape block (5) inner end is equipped with handle one
(4), the handle one (4) is mounted on side cover (1) right end, and side cover (1) the right end upper position is equipped with flat mouth hasp one (2),
The flat mouth hasp one (2) is mounted on tool box (3) right end, and the tool box (3) passes through flat mouth hasp one (2) and side cover (1)
It is connected.
2. a kind of auxiliary device for aircraft maintenance according to claim 1, it is characterised in that: the flat mouth hasp one
(2) there are two setting, two flat mouth hasps one (2) are symmetrically mounted on tool box (3) right end, two flat mouth hasps one
(2) it is connected respectively with tool box (3) and side cover (1) by screw.
3. a kind of auxiliary device for aircraft maintenance according to claim 1, it is characterised in that: the tool box (3)
Cover board is installed in upper end, and cover board lower-end rear portion position is connected by hinge with tool box (3), and cover forward end is flat by two
Mouth hasp two is connected with tool box (3).
4. a kind of auxiliary device for aircraft maintenance according to claim 1, it is characterised in that: the tool box (3)
Front center position is equipped with handle two by screw, and wraps up rubber sleeve on handle two.
5. a kind of auxiliary device for aircraft maintenance according to claim 1, it is characterised in that: the L shape block (5) with
And connection bolt (6) be all provided with there are two, two L shape blocks (5) are symmetrically mounted on side cover (1) right end, two L shape blocks
(5) it is symmetrically mounted on handle one (4) rear and front end, two L shape blocks (5) are connected by shaft with handle one (4), and two
A L shape block (5) is mutually fixed by connecting bolt (6) with side cover (1), there are two side cover (1) right end symmetrically opens up
Threaded hole, through-hole is offered on the L shape block (5), and the connection bolt (6) passes through through-hole and is engaged with threaded hole.
6. a kind of auxiliary device for aircraft maintenance according to claim 1, it is characterised in that: the magnet (7) is logical
It crosses viscose glue to be connected with side cover (1), side cover (1) lower end is connected by hinge with tool box (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821368712.9U CN208855887U (en) | 2018-08-22 | 2018-08-22 | A kind of auxiliary device for aircraft maintenance |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821368712.9U CN208855887U (en) | 2018-08-22 | 2018-08-22 | A kind of auxiliary device for aircraft maintenance |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208855887U true CN208855887U (en) | 2019-05-14 |
Family
ID=66415574
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821368712.9U Active CN208855887U (en) | 2018-08-22 | 2018-08-22 | A kind of auxiliary device for aircraft maintenance |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208855887U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113049628A (en) * | 2021-04-09 | 2021-06-29 | 中铁上海设计院集团有限公司 | Swelling soil wet swelling-frost heaving force combined tester |
-
2018
- 2018-08-22 CN CN201821368712.9U patent/CN208855887U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113049628A (en) * | 2021-04-09 | 2021-06-29 | 中铁上海设计院集团有限公司 | Swelling soil wet swelling-frost heaving force combined tester |
| CN113049628B (en) * | 2021-04-09 | 2023-07-25 | 中铁上海设计院集团有限公司 | Swelling soil wet swelling-frost heaving force combined tester |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 300000 19-1-314 Ruihang Plaza, pilot free trade zone (Airport Economic Zone) of Binhai New Area, Tianjin Patentee after: Liangjie Aviation Technical Service (Tianjin) Co.,Ltd. Address before: 300000 19-1-314 Ruihang Plaza, pilot free trade zone (Airport Economic Zone) of Binhai New Area, Tianjin Patentee before: LIGHTJET AVIATION TECHNOLOGY SERVICE Co.,Ltd. |