CN206069285U - A kind of mechanical balance counter weight type aircraft service ensures hoistable platform balance weight assembly - Google Patents
A kind of mechanical balance counter weight type aircraft service ensures hoistable platform balance weight assembly Download PDFInfo
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- CN206069285U CN206069285U CN201620947672.8U CN201620947672U CN206069285U CN 206069285 U CN206069285 U CN 206069285U CN 201620947672 U CN201620947672 U CN 201620947672U CN 206069285 U CN206069285 U CN 206069285U
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Abstract
This utility model is related to balance weight assembly technical field, specifically discloses a kind of mechanical balance counter weight type aircraft service and ensures hoistable platform balance weight assembly, including base, some pieces of balancing weights, some pieces of top boards；Two symmetrical small sircle holes are provided with the centrage of the balancing weight and top board, the irregularly-shaped hole of a big hole and rectangular opening composition on another centrage, is provided with；The balancing weight side is also provided with a gap；Install in locating shaft, rectangular opening to install in the big hole and install in location-plate, the small sircle hole holding screw；, through top board, balancing weight, the other end is respectively positioned in base for the locating shaft, location-plate, holding screw.The utility model has the advantages that, it is per two pieces of balancing weight gap dislocation arrangements, convenient to dismantle；Location-plate, locating shaft and holding screw three coordinate, and can firmly fasten balance weight assembly, to avoid and drop.
Description
Technical field
This utility model is related to balance weight assembly technical field, particularly relates to a kind of mechanical balance counter weight type aircraft service and ensures
Hoistable platform balance weight assembly.
Background technology
Mechanical balance type lifts comprehensive coverage platform in use or operating process, and balance weight assembly moves up and down, and easily drops,
Generation contingency, and balancing weight is heavier, during dismounting, labor strength is big, and removal efficiency is low.
Utility model content
The purpose of this utility model is to provide a kind of mechanical balance counter weight type aircraft service and ensures hoistable platform weight set
Part, easy installation and removal, connection fastening, accurate positioning between balance weight assembly.
To achieve these goals, this utility model employs following technical scheme：A kind of mechanical balance counter weight type flies
Machine duty assurance hoistable platform balance weight assembly, including base, some pieces of balancing weights, some pieces of top boards；
Two symmetrical small sircle holes are provided with the centrage of the balancing weight and top board, one on another centrage, is provided with
The irregularly-shaped hole of big hole and rectangular opening composition；
The balancing weight side is also provided with a gap；
Install in locating shaft, rectangular opening to install in the big hole and install in location-plate, the small sircle hole holding screw；
, through top board, balancing weight, the other end is respectively positioned in base for the locating shaft, location-plate, holding screw.
Wherein, the gap Heterogeneous Permutation of the balancing weight.
Wherein, blob of viscose is provided with below the base, and blob of viscose length and width is all higher than base length and width.
The beneficial effects of the utility model are：It is per two pieces of balancing weight gap dislocation arrangements, convenient to dismantle；It is location-plate, fixed
Position axle and holding screw three coordinate, and can firmly fasten balance weight assembly, to avoid and drop.
Description of the drawings
In order to be illustrated more clearly that this utility model embodiment technical scheme, below will be to making needed for embodiment description
Accompanying drawing is briefly described, it should be apparent that, drawings in the following description are only this utility model in order to more clearly
This utility model embodiment or technical scheme of the prior art are illustrated, below by institute in p- embodiment or description of the prior art
The accompanying drawing that needs are used is briefly described, for those of ordinary skill in the art, before creative work is not paid
Put, can be with according to these other accompanying drawings of accompanying drawings acquisition.
Fig. 1 is structural representation of the present utility model；
Structural representations of the Fig. 2 for top board；
Structural representations of the Fig. 3 for balancing weight.
Specific embodiment
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only this utility model a part of embodiment, rather than whole
Embodiment.Based on the embodiment in this utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment for being obtained, belongs to the scope of this utility model protection.
A kind of mechanical balance counter weight type aircraft service as shown in Figures 1 to 3 ensures hoistable platform balance weight assembly, including bottom
Seat 6, some pieces of balancing weights 1, some pieces of top boards 2；Be provided with the centrage of the balancing weight 1 and top board 2 two it is symmetrical little
Circular hole, is provided with the irregularly-shaped hole 7 of a big hole and rectangular opening composition on another centrage, locating shaft is installed in the big hole
3, install in rectangular opening in location-plate 5, the small sircle hole and holding screw 4 is installed；The locating shaft 3, location-plate 5, holding screw 4
Through top board 3, balancing weight 1, the other end is respectively positioned in base 6, by top board 3, balancing weight 1,6 accurate positioning of base, firmly
Connection.
1 side of the balancing weight is also provided with a gap, and the gap Heterogeneous Permutation of balancing weight 1 as shown in Figure 2, due to counterweight
The weight of block is not light, and gap mistake is put, and during dismounting, workman just can take off handss in gap position, by balancing weight 1 one by one
Remove, it is convenient to dismantle.
As can be seen from Figure 3 the rectangular opening on balancing weight 1 is driveed to edge, is to insert balancing weight for the ease of location-plate 5,
And the rectangular opening on top board 2 is not driveed to edge, top board 2 is above, is positioned such that plate 5 just can will be locating shaft 3 stuck.
Preferred embodiment of the present utility model is the foregoing is only, it is not to limit this utility model, all at this
Within the spirit and principle of utility model, any modification, equivalent substitution and improvements made etc. should be included in this utility model
Protection domain within.
Claims (2)
1. a kind of mechanical balance counter weight type aircraft service ensures hoistable platform balance weight assembly, it is characterised in that：Including base
(6), some pieces of balancing weights (1), some pieces of top boards (2)；
Two symmetrical small sircle holes are provided with the centrage of the balancing weight (1) and top board (2), are provided with another centrage
The irregularly-shaped hole (7) of one big hole and rectangular opening composition；
Balancing weight (1) side is also provided with a gap；
Install in locating shaft (3), rectangular opening to install in the big hole and install in location-plate (5), the small sircle hole holding screw
(4)；
, through top board (2), balancing weight (1), the other end is respectively positioned on for the locating shaft (3), location-plate (5), holding screw (4)
In base (6).
2. a kind of mechanical balance counter weight type aircraft service according to claim 1 ensures hoistable platform balance weight assembly, its
It is characterised by：The gap Heterogeneous Permutation of the balancing weight (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620947672.8U CN206069285U (en) | 2016-08-25 | 2016-08-25 | A kind of mechanical balance counter weight type aircraft service ensures hoistable platform balance weight assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620947672.8U CN206069285U (en) | 2016-08-25 | 2016-08-25 | A kind of mechanical balance counter weight type aircraft service ensures hoistable platform balance weight assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206069285U true CN206069285U (en) | 2017-04-05 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201620947672.8U Active CN206069285U (en) | 2016-08-25 | 2016-08-25 | A kind of mechanical balance counter weight type aircraft service ensures hoistable platform balance weight assembly |
Country Status (1)
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| CN (1) | CN206069285U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109229401A (en) * | 2018-08-02 | 2019-01-18 | 哈尔滨飞机工业集团有限责任公司 | Center of gravity counter weight device before a kind of adjustable helicopter |
| CN110828724A (en) * | 2018-08-10 | 2020-02-21 | 车王电子股份有限公司 | Battery pack and electric stacking carrier |
| 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 |
-
2016
- 2016-08-25 CN CN201620947672.8U patent/CN206069285U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109229401A (en) * | 2018-08-02 | 2019-01-18 | 哈尔滨飞机工业集团有限责任公司 | Center of gravity counter weight device before a kind of adjustable helicopter |
| CN110828724A (en) * | 2018-08-10 | 2020-02-21 | 车王电子股份有限公司 | Battery pack and electric stacking carrier |
| 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 |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: Building B6, military civilian integration industrial park, 176 Biyuan 2nd Road, Zhangba street, hi tech Zone, Xi'an City, Shaanxi Province Patentee after: Xi'an Ruinuo Aviation Equipment Co., Ltd Address before: 710000, 1 floor, Xin Tong Technology Industrial Park, No. two, 9, No. 1 road, Xi'an high tech Zone, Shaanxi, China. 1 floors Patentee before: XI'AN RUINUO TO NOVEL ENERGY Co.,Ltd. |
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| CP03 | Change of name, title or address |