CN105216543A - A kind of aircraft balance block - Google Patents
A kind of aircraft balance block Download PDFInfo
- Publication number
- CN105216543A CN105216543A CN201510583198.5A CN201510583198A CN105216543A CN 105216543 A CN105216543 A CN 105216543A CN 201510583198 A CN201510583198 A CN 201510583198A CN 105216543 A CN105216543 A CN 105216543A
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- CN
- China
- Prior art keywords
- balance block
- grab
- aircraft
- covered
- pedestal
- Prior art date
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Abstract
The invention discloses a kind of aircraft balance block, described grab is made up of aluminum alloy materials, there is good elasticity, thus convenient operation personnel to balance block carry out installation fix, the outside face of described balance block and grab is covered with one deck zinc coating, zinc coating is also covered with epoxy resin layer outward, not only withstanding corrosion, long service life, and environmental protection, balance block pedestal is identical with the radian at aircraft wheel edge, thus be convenient to edge balance block being fastened on aircraft wheel, prevent other structure on balance block pedestal and tire from scratching, described grab internal layer is covered with adhesive layer, grab can be made to be combined with aircraft wheel edges close, difficult drop-off, it is good that this aircraft balance block has safety performance, environmental protection, the advantage of long service life, there are wide market outlook.
Description
Technical field
The present invention relates to aircraft circles, particularly a kind of aircraft balance block.
Background technology
Traditional balance block is fixed on aircraft wheel edge often through the hook be arranged on balance block, and described hook provides thrust by elastic deformation, to ensure being fixedly connected with of balance block and aircraft wheel.But, when corrosion and ageing appears in hook, or pavement conditions is harsh, when wheel is clashed into, hook cannot provide enough thrusts, thus causes coming off of balance block, the aircraft wheel of lack of equilibrium block, the correction of disappearance to amount of unbalance, causes aircraft wheel mass distribution overbalance, thus affects the drive safety of aircraft.
Summary of the invention
Technical matters to be solved by this invention is to provide a kind of aircraft balance block, to solve the above-mentioned multinomial defect caused in prior art.
6. for achieving the above object, the invention provides following technical scheme: a kind of aircraft balance block, be made up of balance block pedestal and grab, described balance block pedestal is provided with left plane groove and right plane groove, described grab comprises left grab and right grab, the lower platform a of left grab is by rivet in the left plane groove of balance block pedestal, and the lower platform b of right grab is riveted in the right plane groove of balance block pedestal, and the upper mounting plate of grab is not higher than balance block seat surface.
Preferably, described grab is made up of aluminum alloy materials.
Preferably, the outside face of described aircraft balance block and grab is covered with one deck zinc coating, and zinc coating is also covered with epoxy resin layer outward.
Preferably, described balance block pedestal is identical with the radian at aircraft wheel edge.
Preferably, described grab internal layer is covered with adhesive layer.
The beneficial effect of above technical scheme is adopted to be: to the invention discloses a kind of aircraft balance block, described grab is made up of aluminum alloy materials, there is good elasticity, thus convenient operation personnel to balance block carry out installation fix, the outside face of described balance block and grab is covered with one deck zinc coating, zinc coating is also covered with epoxy resin layer outward, not only withstanding corrosion, long service life, and environmental protection, balance block pedestal is identical with the radian at aircraft wheel edge, thus be convenient to edge balance block being fastened on aircraft wheel, prevent other structure on balance block pedestal and tire from scratching, described grab internal layer is covered with adhesive layer, grab can be made to be combined with aircraft wheel edges close, difficult drop-off, it is good that this aircraft balance block has safety performance, environmental protection, the advantage of long service life, there are wide market outlook.
Accompanying drawing explanation
Fig. 1 is the structural representation of aircraft balance block of the present invention:
Fig. 2 is the structural representation of the left view of aircraft balance block.
Wherein, 1-balance block pedestal, 2-grab, the left plane groove of 3-, the right plane groove of 4-, the left grab of 5-, the right grab of 6-, 7-lower platform a, 8-rivet, 9-lower platform b, 10-upper mounting plate, 11-zinc coating, 12-epoxy resin layer, 13-adhesive layer.
Detailed description of the invention
The preferred embodiment of the present invention is described in detail below in conjunction with accompanying drawing.
7. Fig. 1 shows the specific embodiment of the present invention: a kind of aircraft balance block, be made up of balance block pedestal 1 and grab 2, described balance block pedestal 1 is provided with left plane groove 3 and right plane groove 4, described grab 2 comprises left grab 5 and right grab 6, the lower platform a7 of left grab 5 is riveted in the left plane groove 3 of balance block pedestal 1 by rivet 8, the lower platform b9 of right grab 6 is riveted in the right plane groove 4 of balance block pedestal 1 by rivet 8, and the upper mounting plate 10 of grab 2 is not higher than balance block pedestal 1.
In addition, Fig. 2 shows the detailed description of the invention of left view of the present invention: described aircraft balance block pedestal 1 is covered with one deck zinc coating 11 with the outside face of grab 2, and zinc coating 11 is outer is also covered with epoxy resin layer 12, and described grab 2 internal layer is covered with adhesive layer 13.
Above-described is only the preferred embodiment of the present invention, it should be pointed out that for the person of ordinary skill of the art, and without departing from the concept of the premise of the invention, can also make some distortion and improvement, these all belong to protection scope of the present invention.
Claims (5)
1. an aircraft balance block, it is characterized in that, be made up of balance block pedestal and grab, described balance block pedestal is provided with left plane groove and right plane groove, described grab comprises left grab and right grab, the side platform of left grab is riveted in the left plane groove of balance block pedestal, and the side platform of right grab is by rivet in the right plane groove of balance block pedestal, and the upper mounting plate of grab is not higher than balance block seat surface.
2. aircraft balance block according to claim 1, is characterized in that, described grab is made up of aluminum alloy materials.
3. aircraft balance block according to claim 1, is characterized in that, the outside face of described balance block pedestal and grab is covered with one deck zinc coating, and zinc coating is also covered with epoxy resin layer outward.
4. aircraft balance block according to claim 1, is characterized in that, described balance block pedestal is identical with the radian at aircraft wheel edge.
5. aircraft balance block according to claim 1, is characterized in that, described grab internal layer is covered with adhesive layer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510583198.5A CN105216543A (en) | 2015-09-14 | 2015-09-14 | A kind of aircraft balance block |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510583198.5A CN105216543A (en) | 2015-09-14 | 2015-09-14 | A kind of aircraft balance block |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105216543A true CN105216543A (en) | 2016-01-06 |
Family
ID=54985966
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510583198.5A Pending CN105216543A (en) | 2015-09-14 | 2015-09-14 | A kind of aircraft balance block |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105216543A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH11201235A (en) * | 1998-01-08 | 1999-07-27 | Topy Ind Ltd | Wheel balancing weight and manufacture thereof |
| CN201179815Y (en) * | 2008-02-15 | 2009-01-14 | 杨颖� | Vehicle wheel balance weight |
| CN201231647Y (en) * | 2008-06-03 | 2009-05-06 | 上海工程技术大学 | Large gram automobile wheel balance block prepared by chongqing steel |
| KR20100054774A (en) * | 2010-05-04 | 2010-05-25 | 강명자 | Blance weight |
| CN203511149U (en) * | 2013-09-04 | 2014-04-02 | 上海通用汽车有限公司 | Counterweight for wheel |
| CN103832207A (en) * | 2012-11-23 | 2014-06-04 | 威格曼汽车有限两合公司 | Balancing weights |
-
2015
- 2015-09-14 CN CN201510583198.5A patent/CN105216543A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH11201235A (en) * | 1998-01-08 | 1999-07-27 | Topy Ind Ltd | Wheel balancing weight and manufacture thereof |
| CN201179815Y (en) * | 2008-02-15 | 2009-01-14 | 杨颖� | Vehicle wheel balance weight |
| CN201231647Y (en) * | 2008-06-03 | 2009-05-06 | 上海工程技术大学 | Large gram automobile wheel balance block prepared by chongqing steel |
| KR20100054774A (en) * | 2010-05-04 | 2010-05-25 | 강명자 | Blance weight |
| CN103832207A (en) * | 2012-11-23 | 2014-06-04 | 威格曼汽车有限两合公司 | Balancing weights |
| CN203511149U (en) * | 2013-09-04 | 2014-04-02 | 上海通用汽车有限公司 | Counterweight for wheel |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160106 |