CN105292524B - Gradual change inflatable docking facilities are extended out for space - Google Patents

Gradual change inflatable docking facilities are extended out for space Download PDF

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Publication number
CN105292524B
CN105292524B CN201510804902.5A CN201510804902A CN105292524B CN 105292524 B CN105292524 B CN 105292524B CN 201510804902 A CN201510804902 A CN 201510804902A CN 105292524 B CN105292524 B CN 105292524B
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docking
elastomer
pipeline
block
gradual change
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CN105292524A (en
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刘岗
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Ding Wenling
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Abstract

The invention discloses a kind of gradual change inflatable docking facilities are extended out for space, including docking pipeline, the first end of docking pipeline is provided with connecting flange, dock the multigroup block for being equipped with spacing gradual change on pipeline successively to the direction of first end since second end, every group of block is made of two blocks close to arrangement, the elastomer of tubulose is sealed and installed between two adjacent groups block respectively, the elasticity of multiple elastomers is identical or essentially identical, and the tube wall of the docking pipeline between two groups of blocks of initial and end is equipped with the through hole being interlinked to the outside in multiple.The present invention enhances the stability after whole docking facilities docking, is conducive to carry out reliable operation to control object by the way of elastomeric seal is installed on docking pipeline;Using multiple increasing lengths or successively decrease and elastomer that elasticity is consistent, this docking facilities is adapted to the different docking object of multiple diameter, so as to expand the scope of application of this docking facilities.

Description

Gradual change inflatable docking facilities are extended out for space
Technical field
The present invention relates to a kind of docking facilities of space flight, more particularly to a kind of extend out gradual change inflatable pair for space Connection device.
Background technology
With the development of aerospace industry, various space equipments are more and more, such as various space satellites, space station, space flight Aircraft etc..These space equipments are run on high to be needed to carry out various change operation in some cases, for example satellite is carried out In-orbit docking, to realize the capture of extraterrestrial target, posture adjustment, become the operation such as rail and transfer.
Existing docking mechanism generally uses mechanical docking mechanism, there are it is complicated, transmitting size is big, control requires The shortcomings of height, control difficulty are big, easy damaged docking target.
To solve the above-mentioned problems, patent document proposes that inflatable docking mechanism, such as number of patent application are The application for a patent for invention of " 201510139308.9 ", discloses a kind of front end and expands formula inflation docking mechanism, comprising support tube and Termination is expanded, expansion termination is arranged on the front end of support tube, and expansion termination is set with support tube center alignment, expansion termination and branch Stay tube is fixedly connected, and support tube and expansion termination are all flexible gas-filled structures, and the outside diameter of support tube is less than expansion termination and support The length of most long straight line distance on the parallel section in the cross section of pipe;Longitudinal volume is provided with the side of support tube Spring.This structure uses inflatable structure, have it is simple in structure, be easy to docking, docking operation control requires that low, control mode is simple The advantages such as singly, transmitting is small, light-weight, cost is low, still, expansion termination are arranged on the front end of support tube, and support tube is to swollen The underbraced of swollen termination, makes expansion termination be not sufficiently stable after inflation is docked, and since expansion termination is one, it is most suitable Suitable rate of tension corresponds to one, so the diameter of the docking object most adapted to can only be one, which limit the docking mechanism The scope of application.
The content of the invention
The purpose of the present invention is that to solve the above-mentioned problems and provides a kind of docking and stablize, applied widely be used for Space extends out gradual change inflatable docking facilities.
The present invention is achieved through the following technical solutions above-mentioned purpose:
It is a kind of to extend out gradual change inflatable docking facilities for space, including pipeline is docked, the first of the docking pipeline End is provided with connecting flange, is equipped with to the direction of first end since second end multigroup block and more on the docking pipeline successively Spacing between the group block is increasing or less and less, and block described in every group is by two block groups close to arrangement Into being separately installed with the elastomer of tubulose between block described in two adjacent groups, the both ends of the elastomer are respectively with corresponding two The group block is tightly connected, and the termination of the elastomer is placed between two blocks and is sealed, multiple elasticity The elasticity of body is identical or essentially identical, and the tube wall of the docking pipeline between block described in two groups of initial and end is equipped with The through hole being interlinked to the outside in multiple.
In said structure, block is used to install elastomer, and multiple elastomers form utricule, gas is formed after inflation after mounting Capsule, its enlarged-diameter, realizes the close connection between the inner wall of other butt tube, so as to fulfill rapid abutting joint;Multiple bullets Property body structure can be real with other butt tubes of corresponding diameter in the case where each elastomer is in optimum rate of tension Now close connection.
Specifically, the block is five groups altogether, and the elastomer is four altogether, the length of four elastomers by The second end of the docking pipeline is sequentially reduced to the direction of first end.
Preferably, the elastomer is followed successively by inner liner, bearing layer and elastic layer from inside to outside.
It is highly preferred that the inner liner is butyl rubber film, the bearing layer is aramid fiber, and the elastic layer is rubber Glue film.
The beneficial effects of the present invention are:
The present invention makes elastomer also can be with docking after inflating by the way of elastomeric seal is installed on docking pipeline Pipeline stabilization connects, so as to enhance the stability after whole docking facilities docking, is conducive to reliably grasp control object Make;Using multiple increasing lengths or successively decrease and elastomer that elasticity is consistent, this docking facilities is adapted to multiple diameter not Same docking object, so that the scope of application of this docking facilities is expanded, and in docking object less for diameter, by The air bag formed after having more than one elastomer to inflate can be contacted with docking the inner wall of object, so it docks stability It can further improve;This docking facilities is suitable for docking with the object-based device that docks compared with Large Diameter Pipeline hollow pipe.
Brief description of the drawings
Fig. 1 is that front view structure when extending out gradual change inflatable docking facilities unaerated of the present invention for space is illustrated Scheme, the structure in elastomer is shown in figure;
Fig. 2 is the main structure diagram of the present invention that extend out after the inflation of gradual change inflatable docking facilities for being used for space One of, the structure in elastomer is shown in figure;
Fig. 3 is the main structure diagram of the present invention that extend out after the inflation of gradual change inflatable docking facilities for being used for space Two, the structure in elastomer is shown in figure;
Fig. 4 is the main structure diagram of the present invention that extend out after the inflation of gradual change inflatable docking facilities for being used for space Three, the structure in elastomer is shown in figure;
Fig. 5 is the main structure diagram of the present invention that extend out after the inflation of gradual change inflatable docking facilities for being used for space Four, the structure in elastomer is shown in figure.
Embodiment
The invention will be further described below in conjunction with the accompanying drawings:
As shown in Figure 1, the gradual change inflatable docking facilities that extend out of the present invention for space include docking pipeline 8, it is right The first end in adapter road 8(Right end in figure)Connecting flange 9 is installed, is docked on pipeline 8 from second end(Left end in figure)Start to The spacing that the direction of first end is equipped between five groups of blocks 1 and five groups of blocks 1 successively is less and less, can also be increasing, often Group block 1 is made of two blocks 1 close to arrangement, and the elastomer of tubulose is separately installed between two adjacent groups block 1, elasticity Body includes the first elastomer 2, the second elastomer 3, the 3rd elastomer 5, the 4th elastomer 6, the both ends of each elastomer respectively with it is right The two groups of blocks 1 answered are tightly connected, and the termination of each elastomer is placed between two blocks 1 and is sealed, the first elastomer 2, The elasticity of two elastomers 3, the 3rd elastomer 5 and the 4th elastomer 6 is identical or essentially identical, positioned at two groups of blocks 1 of initial and end it Between the tube wall of docking pipeline 8 be equipped with the through holes 7 that are interlinked to the outside in multiple, the first elastomer 2, the elasticity of the second elastomer the 3, the 3rd The length of 5 and the 4th elastomer 6 of body is sequentially reduced;Each elastomer is followed successively by inner liner, bearing layer and elastic layer, gas from inside to outside Close layer is butyl rubber film, and bearing layer is aramid fiber, and elastic layer is rubber film.Above-mentioned block 1 is collar stop, fixed It is installed on the outer wall of docking pipeline 8.
As Figure 1-Figure 5, in use, this docking facilities is connected on the control device by connecting flange 9, and will be right Adapter road 8 is connected with the high-pressure air feed seal of tube of control device, non-aerating before docking, and each elastomer invests docking pipeline 8, its is whole External footpath is smaller, is easy to stretch into the docking object i.e. butt tube of controlled device;Docking pipeline 8 is being stretched into pair of controlled device After in adapter, start to inflate into docking pipeline 8, the air pressure of inflation is determined according to the internal diameter of the butt tube of controlled device, tool Body is as follows:
As shown in Fig. 2, when the internal diameter of the butt tube of controlled device is larger, inner gas pressure is relatively large, due to the first bullet Property body 2 length it is most long, so expand maximum, the largest outside diameter of the air bag formed after inflation after its inflation, the second elastomer 3, The outside diameter of the air bag formed after 3rd elastomer 5 and the inflation of the 4th elastomer 6 is sequentially reduced, after the first elastomer 2 inflation at this time The outer wall of the air bag of formation is contacted with the inner wall of the butt tube of controlled device.
As shown in figure 3, when the internal diameter of the butt tube of controlled device is a little bit smaller, inner gas pressure is also a little bit smaller, the first elasticity It is basically identical that larger and outside diameter is expanded after the inflation of 2 and second elastomer 3 of body, shape after the 3rd elastomer 5 and the inflation of the 4th elastomer 6 Into the outside diameter of air bag be sequentially reduced, the outer wall of the air bag formed at this time after the first elastomer 2 and the inflation of the second elastomer 3 with The inner wall contact of the butt tube of controlled device.
As shown in figure 4, when the internal diameter of the butt tube of controlled device is a little bit smaller again, inner gas pressure is also a little bit smaller again, first Expand that larger and outside diameter is basically identical, and the 4th elastomer 6 is inflated after elastomer 2, the second elastomer 3 and the inflation of the 3rd elastomer 5 The minimum outer diameter of the air bag formed afterwards, the gas formed at this time after the first elastomer 2, the second elastomer 3 and the inflation of the 3rd elastomer 5 Inner wall of the outer wall of capsule with the butt tube of controlled device contacts.
As shown in figure 5, when the internal diameter of the butt tube of controlled device is minimum, inner gas pressure is also minimum, the first elastomer 2, Outside diameter is basically identical after second elastomer 3, the 3rd elastomer 5 and the inflation of the 4th elastomer 6, at this time the first elastomer 2, the second bullet Property body 3, the 3rd elastomer 5 and the inflation of the 4th elastomer 6 after the outer wall of air bag that is formed it is interior with the butt tube of controlled device Wall contacts.
Above-described embodiment is presently preferred embodiments of the present invention, is not the limitation to technical solution of the present invention, as long as The technical solution that can be realized without creative work on the basis of above-described embodiment, is regarded as falling into patent of the present invention Rights protection scope in.

Claims (4)

1. a kind of extend out gradual change inflatable docking facilities, including docking pipeline, the first end of the docking pipeline for space Connecting flange is installed, it is characterised in that:On the docking pipeline since second end to the direction of first end successively be equipped with it is more Spacing between group block and multigroup block is increasing or less and less, and block described in every group is by two close to arrangement The block forms, and the elastomer of tubulose, the both ends difference of the elastomer are separately installed between block described in two adjacent groups It is tightly connected with block described in corresponding two groups, the termination of the elastomer is placed between two blocks and is sealed, more The elasticity of a elastomer is identical or essentially identical, the docking pipeline between block described in two groups of initial and end Tube wall is equipped with the through hole being interlinked to the outside in multiple.
2. according to claim 1 extend out gradual change inflatable docking facilities for space, it is characterised in that:The block Be five groups altogether, the elastomer is four altogether, the length of four elastomers from the docking pipeline second end to The direction of first end is sequentially reduced.
3. according to claim 1 or 2 extend out gradual change inflatable docking facilities for space, it is characterised in that:It is described Elastomer is followed successively by inner liner, bearing layer and elastic layer from inside to outside.
4. according to claim 3 extend out gradual change inflatable docking facilities for space, it is characterised in that:It is described airtight Layer is butyl rubber film, and the bearing layer is aramid fiber, and the elastic layer is rubber film.
CN201510804902.5A 2015-11-20 2015-11-20 Gradual change inflatable docking facilities are extended out for space Active CN105292524B (en)

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CN109131952B (en) * 2018-09-07 2022-03-04 哈尔滨工业大学 Spacecraft capturing system capturing method based on nozzle capturing and satellite-rocket docking ring locking

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US4273505A (en) * 1978-09-22 1981-06-16 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Pneumatic inflatable end effector
DE102004007023A1 (en) * 2004-02-12 2005-09-08 Kastriot Merlaku Space rope for transporting objects from Earth's surface into the space and vice versa is provided with gas balloons fixed along its length to provide a lift
CN201287820Y (en) * 2008-09-11 2009-08-12 王晓勇 Tool for stopping leak and supporting with air chamber
CN102887234B (en) * 2012-10-26 2014-08-13 哈尔滨工业大学 Rapidly-inflatable-deployment thin-film support tube for space craft
CN104149991B (en) * 2014-08-06 2016-02-24 哈尔滨工业大学 A kind of space vehicle controllable inflation launches hold-down arm inner bag
CN104691789B (en) * 2015-03-28 2016-08-24 哈尔滨工业大学 Formula inflation docking mechanism is expanded in a kind of front end
CN105000200B (en) * 2015-07-24 2016-09-21 北京空间飞行器总体设计部 A kind of flexible docking bar of anti-erroneous judgement band signal feedback
CN205221140U (en) * 2015-11-20 2016-05-11 成都尔珏科技有限公司 A expand gradual change inflatable interfacing apparatus outward for space

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Effective date of registration: 20180213

Address after: 325615 Wenzhou City, Yueqing Province, the town of fog lake town, Ling Ling Village Lane No. 3, Lane 103, No.

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Effective date of registration: 20191107

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Address before: 325615, No. 3, Lane 103, tou Ling village, lake mist Town, Wenzhou City, Zhejiang Province, Yueqing

Patentee before: Zhu Zhengzhi