CN209176927U - Aircraft tractor detachable balance weight - Google Patents
Aircraft tractor detachable balance weight Download PDFInfo
- Publication number
- CN209176927U CN209176927U CN201822025885.7U CN201822025885U CN209176927U CN 209176927 U CN209176927 U CN 209176927U CN 201822025885 U CN201822025885 U CN 201822025885U CN 209176927 U CN209176927 U CN 209176927U
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- CN
- China
- Prior art keywords
- clump weight
- plane
- hoisting ring
- aircraft tractor
- sides
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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.)
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Abstract
The utility model discloses a kind of aircraft tractor detachable balance weights, equipped with clump weight, it is characterized in that the clump weight is cube, the end face of the configuration block two sides is symmetrically formed slopely inclined-plane to center from the bottom to top respectively, deep gouge is symmetrically arranged on the inclined-plane of two sides, hoisting ring is equipped in the deep gouge, increase hoisting ring without additional when lifting, the hoisting ring upper end is lower than inclined-plane, in favor of being stacked with for clump weight, facilitate placement, the clump weight upper surface is set there are two mounting hole, the utility model is due to using the above structure, it is simple with structure, it is easy to use, the advantages that convenient disassembly.
Description
Technical field
The utility model relates to Ground facility technology field, specifically a kind of aircraft tractor is with detachably matching
Weight.
Background technique
Aircraft tractor is mainly used for leaving aircraft pushing tow into aircraft shutdown shelter bridge, or aircraft is led from the position of fault
Lead to maintenance hangar, in towing aircraft, aircraft tractor in addition to have enough tractive force, also to possess it is enough itself
Weight can have skidded phenomenon by tire during towing aircraft if aircraft tractor own wt is insufficient.So flying
Machine factory when purchasing aircraft tractor by the aircraft tractor self weight also index important as one, the self weight of aircraft tractor oneself
So also become the important configuration parameter of tractor.
Summary of the invention
Present invention aim to address above-mentioned the deficiencies in the prior art, provide that a kind of structure is simple, easy to use, disassembly side
Just aircraft tractor detachable balance weight.
The technical scheme in the invention for solving the above technical problem is:
A kind of aircraft tractor detachable balance weight is equipped with clump weight, it is characterised in that the clump weight is cube, institute
The end face for stating configuration block two sides is symmetrically formed slopely inclined-plane to center from the bottom to top respectively, and it is heavy to be symmetrically arranged on the inclined-plane of two sides
Slot, is equipped with hoisting ring in the deep gouge, increases hoisting ring without additional when lifting, the hoisting ring upper end is lower than inclined-plane, with benefit
In being stacked with for clump weight, facilitate placement, the clump weight upper surface is set there are two mounting hole, in favor of passing through two installations
Hole is connected together with the cover board handle on aircraft tractor.
The utility model is due to using the above structure, having many advantages, such as that structure is simple, easy to use, convenient disassembly.
Detailed description of the invention
Fig. 1 is structural schematic diagram of the invention.
Fig. 2 is the top view of Fig. 1.
Fig. 3 is the left view of Fig. 1.
Appended drawing reference: hoisting ring 1, mounting hole 2, configuration block 3.
Specific embodiment
The following further describes the present invention with reference to the drawings:
As shown in the picture, a kind of aircraft tractor detachable balance weight is equipped with clump weight 3, it is characterised in that the counterweight
Block 3 is cube, and the end face of 3 two sides of configuration block is symmetrically formed slopely inclined-plane to center from the bottom to top respectively, two sides it is oblique
It is symmetrically arranged with deep gouge on face, is equipped with hoisting ring 1 in the deep gouge, increase hoisting ring 1, the hoisting ring 1 without additional when lifting
Upper end is lower than inclined-plane, in favor of being stacked with for clump weight, facilitates placement, and the clump weight upper surface is set there are two mounting hole 2,
In favor of being connected together by two mounting holes and the cover board handle on aircraft tractor.
Embodiment: from figure 2 it can be seen that clump weight is set there are two hoisting ring 1, hoisting ring is located at counterweight two sides deep gouge
In, it does not affect the appearance usually, increases hoisting ring without additional when needing to lift by crane.In addition, setting among counterweight, there are two mounting holes, can
By counterweight with cover board being connected together, counterweight can be removed by only needing connecting bolt will be laid down when needing to dismantle counterweight.
As can be seen that counterweight is installed on the outside of car body from 3, and vehicle shape one integrated mass, increased counterweight is not only not
Beauty is influenced, increases strength sense to vehicle instead.It, can be by adjusting matching when the complete vehicle weight difference that different clients need
The weight of pouring weight is realized, rather than is realized by making different vehicle frames.Product not only may be implemented in being adjusted flexibly for counterweight
Diversification, and the versatility for the big part such as vehicle frame can be improved, to reduce the cost of production and management.
The utility model is due to using the above structure, having many advantages, such as that structure is simple, easy to use, convenient disassembly.
Claims (1)
1. a kind of aircraft tractor detachable balance weight is equipped with clump weight, it is characterised in that the clump weight is cube, described
The end face of clump weight two sides is symmetrically formed slopely inclined-plane to center from the bottom to top respectively, is symmetrically arranged with deep gouge on the inclined-plane of two sides,
It is equipped with hoisting ring in the deep gouge, the hoisting ring upper end is lower than inclined-plane, and the clump weight upper surface sets that there are two mounting holes.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822025885.7U CN209176927U (en) | 2018-12-04 | 2018-12-04 | Aircraft tractor detachable balance weight |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822025885.7U CN209176927U (en) | 2018-12-04 | 2018-12-04 | Aircraft tractor detachable balance weight |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209176927U true CN209176927U (en) | 2019-07-30 |
Family
ID=67375567
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822025885.7U Active CN209176927U (en) | 2018-12-04 | 2018-12-04 | Aircraft tractor detachable balance weight |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209176927U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115163746A (en) * | 2022-06-17 | 2022-10-11 | 中航西安飞机工业集团股份有限公司 | Counterweight balancing device and counterweight balancing method in aircraft assembly process |
-
2018
- 2018-12-04 CN CN201822025885.7U patent/CN209176927U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115163746A (en) * | 2022-06-17 | 2022-10-11 | 中航西安飞机工业集团股份有限公司 | Counterweight balancing device and counterweight balancing method in aircraft assembly process |
| CN115163746B (en) * | 2022-06-17 | 2023-07-21 | 中航西安飞机工业集团股份有限公司 | Counterweight balancing device and counterweight balancing method in aircraft assembly process |
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Legal Events
| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant |