CN104196847B - A kind of spacecraft controllable inflation launches support arm inner bag end face adhesive mould - Google Patents
A kind of spacecraft controllable inflation launches support arm inner bag end face adhesive mould Download PDFInfo
- Publication number
- CN104196847B CN104196847B CN201410382538.3A CN201410382538A CN104196847B CN 104196847 B CN104196847 B CN 104196847B CN 201410382538 A CN201410382538 A CN 201410382538A CN 104196847 B CN104196847 B CN 104196847B
- Authority
- CN
- China
- Prior art keywords
- sleeve pipe
- support arm
- inner bag
- screw rod
- spacecraft
- 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
Links
- 239000000853 adhesive Substances 0.000 title claims abstract description 9
- 230000001070 adhesive effect Effects 0.000 title claims abstract description 9
- 239000000463 material Substances 0.000 claims description 2
- 239000010409 thin film Substances 0.000 abstract description 9
- 239000010408 film Substances 0.000 abstract description 4
- 238000000034 method Methods 0.000 description 3
- 238000004026 adhesive bonding Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
Landscapes
- Lining Or Joining Of Plastics Or The Like (AREA)
Abstract
A kind of spacecraft controllable inflation launches support arm inner bag end face adhesive mould, belong to developing space inflation support arm technical field, solve the problem of the mould of the adhering film inner bag end face be not applicable at present, it comprises sleeve pipe, slide block, pressing plate and screw rod, described sleeve pipe has two, two slide blocks are provided with in each sleeve pipe, two slide blocks being positioned at two sleeve pipe the same sides are respectively connected by a block pressur plate, the breach that pressing plate enters is provided with at the two ends of two sleeve pipe opposing sides, on sleeve pipe, the distance of two breach is less than the total length of two slide blocks in sleeve pipe, the center of two pressing plates is connected by screw rod, the two ends of screw rod are provided with nut.The present invention is used for bonding for the end face alignment of two joint thin film inner containers.
Description
Technical field
The invention belongs to developing space inflation support arm technical field, be specifically related to a kind of spacecraft controllable inflation and launch support arm inner bag end face adhesive mould.
Background technique
A kind of spacecraft controllable inflation launches support arm inner bag, it comprises more piece thin film inner container, more piece thin film inner container successively head and the tail is bonding, in the bonding process of more piece thin film inner container, will by bonding for the end face alignment of adjacent two joint thin film inner containers, the mould of the adhering film inner bag end face be not applicable at present, make bonding end face be difficult to alignment, bonding quality is bad.
Summary of the invention
The object of the invention is the problem of the mould in order to solve the adhering film inner bag end face be not applicable at present, provide a kind of spacecraft controllable inflation and launch support arm inner bag end face adhesive mould, its technological scheme is as follows:
A kind of spacecraft controllable inflation launches support arm inner bag end face adhesive mould, it comprises sleeve pipe, slide block, pressing plate and screw rod, described sleeve pipe has two, two slide blocks are provided with in each sleeve pipe, two slide blocks being positioned at two sleeve pipe the same sides are respectively connected by a block pressur plate, the breach that pressing plate enters is provided with at the two ends of two sleeve pipe opposing sides, on sleeve pipe, the distance of two breach is less than the total length of two slide blocks in sleeve pipe, the center of two pressing plates is connected by screw rod, and the two ends of screw rod are provided with nut.
Beneficial effect of the present invention is: the end face of adjacent two joint thin film inner containers can be alignd bonding and can apply pressure, ensure bonding quality.
accompanying drawing illustrates:
Fig. 1 is structural representation of the present invention;
Fig. 2 is the decomposing schematic representation of Fig. 1.
embodiment:
See figures.1.and.2, a kind of spacecraft controllable inflation launches support arm inner bag end face adhesive mould, it comprises sleeve pipe 1, slide block 2, pressing plate 3 and screw rod 4, described sleeve pipe 1 has two, two slide blocks 2 are provided with in each sleeve pipe 1, two slide blocks 2 being positioned at two sleeve pipe 1 the same sides are respectively connected by a block pressur plate 3, the breach 3-1 that pressing plate 3 enters is provided with at the two ends of two sleeve pipe 1 opposing sides, on sleeve pipe 1, the distance of two breach 3-1 is less than the total length of interior two slide blocks 2 of sleeve pipe 1, the center of two pressing plates 3 is connected by screw rod 4, the two ends of screw rod 4 are provided with nut.
Described slide block 2 adopts quality of rubber materials, or arranges rubber pad in the front end of slide block 2.
Using method: current thin film inner bag is after being surrounded sticked into cylinder by rectangular shaped sheet, again two ends shutoff is formed thin film inner container, use this mould by two joint thin film inner containers end face bonding before, first one end of two rectangular shaped sheet is surrounded and stick into length and be less than the tubular of slide block 2 length and shutoff, then tubular one end of two rectangular shaped sheet is enclosed within a slide block 2 respectively, again after end face gluing, be inserted into from the two ends of a sleeve pipe 1 in sleeve pipe 1, finally load onto screw rod 4 and pressurize with nut.Owing to there being two sleeve pipes 1, so can two group leader's film square carry out simultaneously.
Claims (2)
1. a spacecraft controllable inflation launches support arm inner bag end face adhesive mould, it is characterized in that it comprises sleeve pipe (1), slide block (2), pressing plate (3) and screw rod (4), described sleeve pipe (1) has two, two slide blocks (2) are provided with in each sleeve pipe (1), two slide blocks (2) being positioned at two sleeve pipe (1) the same sides are respectively connected by a block pressur plate (3), the breach (3-1) that pressing plate (3) enters is provided with at the two ends of two sleeve pipe (1) opposing sides, the distance of upper two breach (3-1) of sleeve pipe (1) is less than the total length of interior two slide blocks (2) of sleeve pipe (1), the center of two pressing plates (3) is connected by screw rod (4), the two ends of screw rod (4) are provided with nut.
2. a kind of spacecraft controllable inflation launches support arm inner bag end face adhesive mould as claimed in claim 1, it is characterized in that described slide block (2) adopts quality of rubber materials, or arranges rubber pad in the front end of slide block (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410382538.3A CN104196847B (en) | 2014-08-06 | 2014-08-06 | A kind of spacecraft controllable inflation launches support arm inner bag end face adhesive mould |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410382538.3A CN104196847B (en) | 2014-08-06 | 2014-08-06 | A kind of spacecraft controllable inflation launches support arm inner bag end face adhesive mould |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104196847A CN104196847A (en) | 2014-12-10 |
| CN104196847B true CN104196847B (en) | 2016-02-24 |
Family
ID=52082189
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410382538.3A Expired - Fee Related CN104196847B (en) | 2014-08-06 | 2014-08-06 | A kind of spacecraft controllable inflation launches support arm inner bag end face adhesive mould |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104196847B (en) |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4202351C2 (en) * | 1992-01-29 | 1995-01-19 | Fickenscher & Co Gmbh Werkzeug | Process for injection molding objects from at least two parts |
| US5664373A (en) * | 1992-08-20 | 1997-09-09 | Downing; Brian B. | Inflatable mold for use in space |
| JP2000103692A (en) * | 1998-09-30 | 2000-04-11 | Daicel Chem Ind Ltd | Gas generator composition molding product for air bag |
| JP5489741B2 (en) * | 2010-01-21 | 2014-05-14 | 新電元工業株式会社 | Resin sealing mold, resin sealing package manufacturing method, and resin sealing package |
| CN202811715U (en) * | 2012-09-25 | 2013-03-20 | 安徽大地熊新材料股份有限公司 | Auxiliary device for bonding magnetic products |
| CN103817237B (en) * | 2014-02-18 | 2015-08-05 | 哈尔滨工业大学 | Inflated spatial controls to launch the curling folding die of support arm |
-
2014
- 2014-08-06 CN CN201410382538.3A patent/CN104196847B/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CN104196847A (en) | 2014-12-10 |
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|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160224 |
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| CF01 | Termination of patent right due to non-payment of annual fee |