CN204198231U - Dismountable aircraft dispatch bracket hanging - Google Patents
Dismountable aircraft dispatch bracket hanging Download PDFInfo
- Publication number
- CN204198231U CN204198231U CN201420527809.5U CN201420527809U CN204198231U CN 204198231 U CN204198231 U CN 204198231U CN 201420527809 U CN201420527809 U CN 201420527809U CN 204198231 U CN204198231 U CN 204198231U
- Authority
- CN
- China
- Prior art keywords
- arm
- hanging
- truss
- connecting panel
- dismountable
- 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.)
- Expired - Fee Related
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- Conveying And Assembling Of Building Elements In Situ (AREA)
Abstract
The utility model relates to a kind of dismountable aircraft dispatch bracket hanging, and truss left and right end face is equipped with the arm with hanger, and arm is arranged with truss is vertical and is connected by connecting panel, and arm lower surface is connected with hanging belt, and hanging belt lower surface is provided with shackle.Reassembling type structure is convenient carries out dismounting in transport and use procedure, saves space, is easy to carrying, can Reusability, saving work-hours.
Description
Technical field
The utility model relates to a kind of hanging, and particularly a kind of detachable hanging, belongs to mechanical air transportation field.
Background technology
In air transportation field, bracket hanging is mainly used in transporting together with pallet for transporting, loading and unloading, product is being put into together with bracket in the process on truck, or by product and bracket from truck unload then install in freight container time, or in the process after arrival destination, product and bracket unloaded, all need to use transport hanging, hanging is used for aircraft bucket section and the lifting of bracket in transportation, after aircraft bucket section is put on pallet for transporting, need bucket section to be put into together with bracket on truck to transport, to unload product at harbour simultaneously, then install in freight container and transport.
Hanging used is at present all integral structure, and in transport and use procedure, bring very big inconvenience, existing hanging also exists to take up room and is not easy greatly to deposit, the volume comparatively greatly also not easily shortcoming such as carrying own.
Utility model content
The technical problems to be solved in the utility model is to provide the hanging of a kind of dismountable aircraft dispatch bracket, and reassembling type structure is convenient carries out dismounting in transport and use procedure, saves space, is easy to carrying, can Reusability, saving work-hours.
For overcoming the above problems, concrete technical scheme of the present utility model is as follows: a kind of dismountable aircraft dispatch bracket hanging, truss left and right end face is equipped with the arm with hanger, arm is isosceles trapezoidal structure, arm is arranged with truss is vertical and is connected by connecting panel, and connecting panel is fixedly connected on the end face that arm contacts with truss respectively, and two-layer connecting panel is bolted, arm lower surface is connected with hanging belt, and hanging belt lower surface is provided with shackle.Be connected by connecting panel between arm with truss, being bolted two-layer connecting panel can facilitate device to dismantle, time saving and energy saving, when needing in transportation to dismantle, arm and truss can be split by the anchor fitting unclamped between connecting panel by instrument, reduce the volume of product own, convenient transport and storage.
The beneficial effect that the utility model brings is: hanging the mode adopting flexible connection between each parts conveniently can carry out dismounting to hanging, reduce device to take up room, solving device is difficult to the problem of carrying, if section components damages, a certain parts can be changed separately, effectively cost-saving.
Accompanying drawing explanation
Fig. 1 is the structural representation of dismountable aircraft dispatch bracket hanging.
Fig. 2 is the right elevation of Fig. 1.
Wherein, 1-truss, 2-arm, 3-hanging belt, 4-shackle, 5-connecting panel.
Detailed description of the invention
A kind of dismountable aircraft dispatch bracket hanging, truss about 1 end face is equipped with the arm 2 with hanger, arm is isosceles trapezoidal structure, arm 2 is arranged with truss 1 is vertical and is connected by connecting panel 5, connecting panel 5 is fixedly connected on the end face that arm 2 contacts with truss 1 respectively, and two-layer connecting panel 5 is bolted.Arm 2 lower surface is connected with hanging belt 3, and hanging belt 3 lower surface is provided with shackle 4.Be connected by connecting panel 5 between arm 2 with truss 1, being bolted two-layer connecting panel 5 can facilitate device to dismantle, time saving and energy saving, when needing in transportation to dismantle, unclamped by instruments such as screwdrivers and fix arm 2 and truss 1 can being split of bolt between two connecting panels 5, reduce the volume of product own, convenient transport and storage.
Working process:
During work, first first by bolt, the connecting panel 5 of truss 1 with arm 2 is fixed together, hanging belt 3 is connected in arm 2 lower surface, shackle 4 is connected to the lower surface of hanging belt 3, check that whether two arms 2 are vertical with truss 1 after hanging installs, guarantee that front two arms 2 of construction are vertical with truss 1, then shackle 4 is connected with pallet for transporting and can carries out crane lifting service, by instruments such as screwdrivers, the bolt on connecting panel 5 is dismantled after having worked, i.e. dismantled and assembled hanging.
Claims (1)
1. a dismountable aircraft dispatch bracket hanging, it is characterized in that: truss left and right end face is equipped with the arm with hanger, arm is isosceles trapezoidal structure, arm is arranged with truss is vertical and is connected by connecting panel, connecting panel is fixedly connected on the end face that arm contacts with truss respectively, two-layer connecting panel is bolted, and arm lower surface is connected with hanging belt, and hanging belt lower surface is provided with shackle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420527809.5U CN204198231U (en) | 2014-09-15 | 2014-09-15 | Dismountable aircraft dispatch bracket hanging |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420527809.5U CN204198231U (en) | 2014-09-15 | 2014-09-15 | Dismountable aircraft dispatch bracket hanging |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204198231U true CN204198231U (en) | 2015-03-11 |
Family
ID=52656215
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420527809.5U Expired - Fee Related CN204198231U (en) | 2014-09-15 | 2014-09-15 | Dismountable aircraft dispatch bracket hanging |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204198231U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105060089A (en) * | 2015-07-24 | 2015-11-18 | 中国运载火箭技术研究院 | Lifting appliance structure used for lifting and overturning aircraft |
-
2014
- 2014-09-15 CN CN201420527809.5U patent/CN204198231U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105060089A (en) * | 2015-07-24 | 2015-11-18 | 中国运载火箭技术研究院 | Lifting appliance structure used for lifting and overturning aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150311 Termination date: 20170915 |