CN205221139U - A gradual change inflatable interfacing apparatus that contracts in for space - Google Patents
A gradual change inflatable interfacing apparatus that contracts in for space Download PDFInfo
- Publication number
- CN205221139U CN205221139U CN201520928308.2U CN201520928308U CN205221139U CN 205221139 U CN205221139 U CN 205221139U CN 201520928308 U CN201520928308 U CN 201520928308U CN 205221139 U CN205221139 U CN 205221139U
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- space
- interior pipe
- elastic body
- collar stop
- docking
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Abstract
The utility model discloses a (B, ) the space gradual change inflatable interfacing apparatus (b) that contracts in, including the butt joint pipeline, the butt joint pipeline includes outer tube and inner tube, be the intermediate layer space between outer tube and the inner tube, the first end of butt joint pipeline is connected with flange, seal between the second end of outer tube and inner tube and connect, begin to be equipped with multiunit collar stop and interval gradual change in proper order to the direction of first end from the second end on the inner wall of inner tube, every group collar stop is close to the collar stop of arranging by two and constitutes, between adjacent two sets of collar stop respectively seal installation have pipy elastomer, the elasticity of a plurality of elastomers is the same or the same basically, be located head, be equipped with communicating through -hole inside and outside a plurality of on the pipe wall of the inner tube between the two sets of collar stops of tail. The utility model discloses an install the mode on the inner tube of butt joint pipeline with elastomeric seal to it to the stability of carried forward, is favorable to carrying out the reliable operation to controlled object, and has enlarged this interfacing apparatus's application scope to have strengthened whole interfacing apparatus.
Description
Technical field
The utility model relates to a kind of docking facilities of space flight, particularly relates to inside contract gradual change inflatable docking facilities for space.
Background technology
Along with the development of aerospace industry, various space equipment gets more and more, such as various space satellite, space station, space shuttle etc.These space equipments run on high and need to carry out in some cases various change and run, and such as dock in-orbit satellite, with operations such as the catching of implementation space target, posture adjustment, change rail and transfers.
Existing docking mechanism generally adopts mechanical type docking mechanism, there is complex structure, launches the shortcomings such as size is large, control overflow is high, control difficulty is large, easy damaged docking target.
In order to solve the problem, patent documentation is had to propose inflatable docking mechanism, such as number of patent application is the utility application of " 201510139308.9 ", disclose a kind of front end expand formula inflation docking mechanism, comprise support tube and expansion termination, expansion termination is arranged on the front end of support tube, align with support tube center and arrange in expansion termination, expansion termination is fixedly connected with support tube, support tube and expansion termination are all flexible gas-filled structures, the external diameter of support tube is less than the length of the longest straight line distance on the cross section parallel with the cross-sectional plane of support tube, expansion termination, the side of support tube is provided with longitudinal wind spring.This structure adopts inflatable structure, have structure simple, be easy to docking, docking operation control overflow is low, mode simple, launch that volume is little, lightweight, low cost and other advantages, but, expansion termination is arranged on the front end of support tube, support tube is to the underbraced of expansion termination, make expansion termination stable not after inflation docking, and due to expansion termination be one, corresponding one of its optimum degree of tension, so the diameter of the docking object adapted to most can only be one, which limit the Applicable scope of this docking mechanism; In addition, this docking mechanism can not be used for docking the situation that object is solid pillar.
Summary of the invention
The purpose of this utility model is just to provide to solve the problem a kind of docking stable, applied widely to inside contract gradual change inflatable docking facilities for space.
The utility model is achieved through the following technical solutions above-mentioned purpose:
A kind ofly inside contract gradual change inflatable docking facilities for space, comprise docking pipeline, the first end of described docking pipeline is provided with butt flange, described docking pipeline comprises coaxial outer tube and interior pipe, be mezzanine space between described outer tube and described interior pipe, the first end of described outer tube and the first end of described interior pipe are all connected with described butt flange and described butt flange is provided with the annular through-hole communicated with described mezzanine space, close between second end of described outer tube and the second end of described interior pipe and connect, the inwall of described interior pipe is provided with many group collar stops successively to the direction of first end from the second end and spacing between the described collar stop of many groups is increasing or more and more less, often organize described collar stop to form near the described collar stop arranged by two, the elastic body of tubulose is separately installed with between collar stop described in two adjacent groups, described elastomeric two ends are tightly connected with collar stop described in corresponding two groups respectively, described elastomeric termination to be placed between two described collar stops and to be sealed, multiple described elastomeric elasticity is identical or substantially identical, be positioned at head, the tube wall of the described interior pipe described in two groups, tail between collar stop be provided with multiple in the through hole that is interlinked to the outside.
In said structure, collar stop is for installing elastic body, and multiple elastic body forms utricule jointly with inner core inwall after mounting, air bag is formed after inflation, its enlarged-diameter, realizes the compact siro spinning technology between the outer wall of the docking post or butt tube that dock object, thus realizes rapid abutting joint; Multiple elastomeric structure can dock post when each elastic body is in optimum degree of tension with other of corresponding diameter or butt tube realizes compact siro spinning technology.
Particularly, described collar stop is altogether five groups, and described elastic body is altogether four, and four described elastomeric length is reduced to the direction of first end successively by the second end of described interior pipe.
As preferably, described elastic body is followed successively by air-retaining liner, bearing layer and elastic layer from inside to outside.
More preferably, described air-retaining liner is butyl rubber film, and described bearing layer is aramid fiber, and described elastic layer is rubber film.
The beneficial effects of the utility model are:
The utility model adopts the mode being installed on by elastomeric seal and docking in pipeline on pipe, also can be connected with interior pipe is stable, thus enhance the stability after the docking of whole docking facilities, be conducive to carrying out reliable operation to control object after elastic body is inflated; Adopt multiple increasing lengths or successively decrease and the consistent elastic body of elasticity, make this docking facilities can adapt to the different docking object of multiple diameter, thus expand the Applicable scope of this docking facilities, and when the docking object larger for diameter, the air bag formed after inflating owing to there being more than one elastic body all with the wall contacts docking object, can improve so it docks stability further; This docking facilities is applicable to dock with the object-based device that docks had compared with pipe with small pipe diameter hollow tubular or solid pillar.
Accompanying drawing explanation
Fig. 1 be described in the utility model for space inside contract the docking facilities unaerated of gradual change inflatable time main TV structure schematic diagram, there is shown the structure in docking pipeline;
Fig. 2 is one of main TV structure schematic diagram inside contracted after the inflation of gradual change inflatable docking facilities for space described in the utility model, there is shown the structure in docking pipeline;
Fig. 3 is the main TV structure schematic diagram two inside contracted after the inflation of gradual change inflatable docking facilities for space described in the utility model, there is shown the structure in docking pipeline;
Fig. 4 is the main TV structure schematic diagram three inside contracted after the inflation of gradual change inflatable docking facilities for space described in the utility model, there is shown the structure in docking pipeline;
Fig. 5 is the main TV structure schematic diagram four inside contracted after the inflation of gradual change inflatable docking facilities for space described in the utility model, there is shown the structure in docking pipeline.
Detailed description of the invention
Below in conjunction with accompanying drawing, the utility model is described in further detail:
As shown in Figure 1, the gradual change inflatable docking facilities that inside contracts for space described in the utility model comprises docking pipeline, the first end (in figure right-hand member) of described docking pipeline is provided with butt flange 10, described docking pipeline comprises coaxial outer tube 7 and interior pipe 8, it is mezzanine space 9 between outer tube 7 and interior pipe 8, the first end (in figure right-hand member) of outer tube 7 and the first end (in figure right-hand member) of interior pipe 8 are all connected with butt flange 10 and butt flange 10 is provided with the annular through-hole (not shown) communicated with mezzanine space 9, close between second end (in figure left end) of outer tube 7 and second end (in figure left end) of interior pipe 8 and connect, the inwall of interior pipe 8 is provided with five groups of collar stops 1 successively to the direction of first end from the second end and spacing between five groups of collar stops 1 is more and more less, also can be increasing, often organize collar stop 1 to form near the collar stop 1 arranged by two, the elastic body of tubulose is separately installed with between two adjacent groups collar stop 1, comprise the first elastic body 2, second elastic body 3, 3rd elastic body 5 and the 4th elastic body 6, each elastomeric two ends are tightly connected with corresponding two groups of collar stops 1 respectively, each elastomeric termination to be placed between two collar stops 1 and to be sealed, first elastic body 2, second elastic body 3, 3rd elastic body 5 is identical with the elasticity of the 4th elastic body 6 or substantially identical, be positioned at head, the tube wall of the interior pipe 8 between tail two groups of collar stops 1 be provided with multiple in the through hole 4 that is interlinked to the outside, first elastic body 2, second elastic body 3, the length of the 3rd elastic body 5 and the 4th elastic body 6 reduces successively, each elastic body is followed successively by air-retaining liner, bearing layer and elastic layer from inside to outside, and air-retaining liner is butyl rubber film, and bearing layer is aramid fiber, and elastic layer is rubber film.
As Figure 1-Figure 5, during use, this docking facilities is connected on the control device by butt flange 10, and the docking mezzanine space 9 of pipeline is connected with the high-pressure air feed seal of tube of control convenience, do not inflate before docking, each elastic body invests the inwall of interior pipe 8, and its overall internal diameter is comparatively large, is easy to be inserted on the docking post of docking object and controlled device; After on the docking post interior pipe 8 being inserted in controlled device, start to inflate in mezzanine space 9, the air pressure of inflation is determined according to the external diameter of the docking post of controlled device, specific as follows:
As shown in Figure 2, when the external diameter of the docking post of controlled device is less, inner gas pressure is relatively large, because the length of the first elastic body 2 is the longest, so expansion is maximum after its inflation, the internal diameter of the air bag jointly formed with the inwall of interior pipe 8 after inflation is minimum, namely the central through hole diameter that surrounds of air bag is minimum, second elastic body 3, the internal diameter that 3rd elastic body 5 and the 4th elastic body 6 inflate the air bag that inwall that is rear and interior pipe 8 is formed jointly increases successively, namely the diameter of central through hole that each air bag surrounds increases successively, now the first elastic body 2 inflates the inwall of air bag and the wall contacts docking post of controlled device that are jointly formed with the inwall of interior pipe 8 afterwards.
As shown in Figure 3, when the external diameter of the docking post of controlled device is a bit greatly, inner gas pressure is a little bit smaller, first elastic body 2 and the second elastic body 3 inflate that rear expansion is comparatively large and internal diameter is basically identical, the internal diameter of the air bag that the 3rd elastic body 5 and the 4th elastic body 6 are formed jointly with the inwall of interior pipe 8 after inflating reduces successively, now the inwall of air bag that jointly formed with the inwall of interior pipe 8 after inflating of the first elastic body 2 and the second elastic body 3 all with the wall contacts docking post of controlled device.
As shown in Figure 4, the docking post of controlled device internal diameter larger some time, inner gas pressure is a little bit smaller again, first elastic body 2, second elastic body 3 and the 3rd elastic body 5 inflate that rear expansion is comparatively large and internal diameter is basically identical, the internal diameter of the air bag that the 4th elastic body 6 is formed jointly with the inwall of interior pipe 8 after inflating is minimum, now the inwall of air bag that jointly formed with the inwall of interior pipe 8 after inflating of the first elastic body 2, second elastic body 3 and the 3rd elastic body 5 all with the wall contacts docking post of controlled device.
As shown in Figure 5, when the external diameter of the docking post of controlled device is maximum, inner gas pressure is minimum, it is basically identical that first elastic body 2, second elastic body 3, the 3rd elastic body 5 and the 4th elastic body 6 inflate rear internal diameter, now the inwall of air bag that jointly formed with the inwall of interior pipe 8 after inflating of the first elastic body 2, second elastic body 3, the 3rd elastic body 5 and the 4th elastic body 6 all with the wall contacts docking post of controlled device.
Above-described embodiment is preferred embodiment of the present utility model; it is not the restriction to technical solutions of the utility model; as long as without the technical scheme that creative work can realize on the basis of above-described embodiment, all should be considered as falling within the scope of the rights protection of the utility model patent.
Claims (4)
1. one kind inside contracts gradual change inflatable docking facilities for space, comprise docking pipeline, the first end of described docking pipeline is provided with butt flange, it is characterized in that: described docking pipeline comprises coaxial outer tube and interior pipe, be mezzanine space between described outer tube and described interior pipe, the first end of described outer tube and the first end of described interior pipe are all connected with described butt flange and described butt flange is provided with the annular through-hole communicated with described mezzanine space, close between second end of described outer tube and the second end of described interior pipe and connect, the inwall of described interior pipe is provided with many group collar stops successively to the direction of first end from the second end and spacing between the described collar stop of many groups is increasing or more and more less, often organize described collar stop to form near the described collar stop arranged by two, the elastic body of tubulose is separately installed with between collar stop described in two adjacent groups, described elastomeric two ends are tightly connected with collar stop described in corresponding two groups respectively, described elastomeric termination to be placed between two described collar stops and to be sealed, multiple described elastomeric elasticity is identical or substantially identical, be positioned at head, the tube wall of the described interior pipe described in two groups, tail between collar stop be provided with multiple in the through hole that is interlinked to the outside.
2. according to claim 1ly inside contract gradual change inflatable docking facilities for space, it is characterized in that: described collar stop is altogether five groups, described elastic body is altogether four, and four described elastomeric length is reduced to the direction of first end successively by the second end of described interior pipe.
3. according to claim 1 and 2ly inside contract gradual change inflatable docking facilities for space, it is characterized in that: described elastic body is followed successively by air-retaining liner, bearing layer and elastic layer from inside to outside.
4. according to claim 3ly inside contract gradual change inflatable docking facilities for space, it is characterized in that: described air-retaining liner is butyl rubber film, described bearing layer is aramid fiber, and described elastic layer is rubber film.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201520928308.2U CN205221139U (en) | 2015-11-20 | 2015-11-20 | A gradual change inflatable interfacing apparatus that contracts in for space |
Applications Claiming Priority (1)
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CN201520928308.2U CN205221139U (en) | 2015-11-20 | 2015-11-20 | A gradual change inflatable interfacing apparatus that contracts in for space |
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CN205221139U true CN205221139U (en) | 2016-05-11 |
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CN201520928308.2U Withdrawn - After Issue CN205221139U (en) | 2015-11-20 | 2015-11-20 | A gradual change inflatable interfacing apparatus that contracts in for space |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105270651A (en) * | 2015-11-20 | 2016-01-27 | 成都尔珏科技有限公司 | Internal shrink gradual change inflatable docking apparatus for space |
CN106965134A (en) * | 2017-05-16 | 2017-07-21 | 四川钰萌光电科技有限公司 | Workbench and assembly method for assembling street lamp post flange chassis and pedestal |
-
2015
- 2015-11-20 CN CN201520928308.2U patent/CN205221139U/en not_active Withdrawn - After Issue
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105270651A (en) * | 2015-11-20 | 2016-01-27 | 成都尔珏科技有限公司 | Internal shrink gradual change inflatable docking apparatus for space |
CN105270651B (en) * | 2015-11-20 | 2017-04-19 | 成都尔珏科技有限公司 | Internal shrink gradual change inflatable docking apparatus for space |
CN106965134A (en) * | 2017-05-16 | 2017-07-21 | 四川钰萌光电科技有限公司 | Workbench and assembly method for assembling street lamp post flange chassis and pedestal |
CN106965134B (en) * | 2017-05-16 | 2023-08-18 | 四川钰萌光电科技有限公司 | Working platform for assembling flange chassis and base of street lamp post and assembling method |
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Legal Events
Date | Code | Title | Description |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
AV01 | Patent right actively abandoned | ||
AV01 | Patent right actively abandoned |
Granted publication date: 20160511 Effective date of abandoning: 20170419 |