CN100453404C - Extra long aerated expansion supporting rod for outer space - Google Patents
Extra long aerated expansion supporting rod for outer space Download PDFInfo
- Publication number
- CN100453404C CN100453404C CNB2006100098823A CN200610009882A CN100453404C CN 100453404 C CN100453404 C CN 100453404C CN B2006100098823 A CNB2006100098823 A CN B2006100098823A CN 200610009882 A CN200610009882 A CN 200610009882A CN 100453404 C CN100453404 C CN 100453404C
- Authority
- CN
- China
- Prior art keywords
- outer tube
- inner layer
- present
- supporting rod
- specific embodiment
- 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
Images
Landscapes
- Road Signs Or Road Markings (AREA)
- Laminated Bodies (AREA)
Abstract
The present invention relates to an ultralong aerated expansion supporting rod for outer space, which relates to an expansion structural member applied to the outer space. In order to solve the problems of high weight, low folding efficiency, incapability of building large-scale space structures, etc. existing in the present mechanical development structure, an inner layer tube (1) of the present invention is arranged in an outer layer tube (2); an inflating holes (3-1) are arranged at the centers of end covers (3); two end covers (3) are respectively connected with both ends of the inner layer tube (1) and the outer layer tube (2) in a sealing mode; the length L of the supporting rod is from 10 to 100 m; the inner layer tube (1) and the outer layer tube (2) are thin film material. The present invention is stored under a folded state and has the advantages of light weight and high folding efficiency; the tubes can not be limited by dimensions, so the manufacture of exceeding dimensions is realized. In the outer space, the present invention provides an effective solving way for building the large-scale structure members; the present invention can be used for unfolding drive mechanisms and supporting structures of the large-scale space structures; on ground, the present invention can be used in the aspects of supporting temporary advertisement lamp boxes, supporting extending antennas for temporary communication in areas with complicated terrain.
Description
Technical field
The present invention relates to a kind of deployed configuration spare that is applied to space.
Background technology
Owing to be subjected to the restriction of the effective launch load and the emission volume of carrier rocket, be to have very little weight and very little emission volume for the requirement of the capacity weight that carries.Large-scale space structure all is in folded state when emission, form the state of its designing requirement after emission is entered the orbit by the mode of launching, and realizes its design function.The mode that existing deployed configuration mostly launches by machinery, this deployed configuration is the weight height not only, and folding efficiency is also less.In addition, in order to satisfy the requirement of survey of deep space, for the survey of deep space structure member of overlength, traditional frame mode is powerless especially.
Summary of the invention
Be the problem that solves the existing weight height of existing machinery deployed configuration, folding efficiency is less and can't makes up large space structure, the invention provides a kind of extra long aerated expansion supporting rod for outer space, it is mainly made up by membraneous material and forms, the present invention includes the termination lid of inner layer pipe, outer tube and two tubulars, inner layer pipe is put in outer tube, the center of each termination lid has air-filled pore, two terminations lid is connected by sealing with the two ends of inner layer pipe and outer tube respectively, and inner layer pipe and outer tube are membraneous material; It also comprises firm bar, stick, and described firm bar is fixed on the inside face of outer tube, and described stick is fixed on the outside face of outer tube, and the length L of strut bar is 10～100m.Inner layer pipe of the present invention and outer tube adopt membraneous material, adopt the mode of curling to fold, and are in folded state when putting into the rocket load compartment, after emission enters space, the air-filled pore that covers by the termination charges into gas to tube interior, and strut bar fully launches, and reaches mode of operation.The present invention can be used for the isostructural expansion driver train of sun shade of large aperture antenna, solar sail, solar energy sailboard, super long type one pole and dipole antenna, satellite truss structure, large-scale high-precision optical mirror; Also can be used as structure member and use, be used for support cameras and other load; On ground, the present invention can be used for the support of interim advertising lamp box and at the aspects such as support of the protruding antenna of the landform of complexity zone provisional communication.
Outstanding advantage of the present invention is: one, it is mainly made up by membraneous material and forms, and in light weight, simple in structure, it is convenient to connect with other structure.After vacuumizing, adopt efficient folding mode can occupy very little storage volume, the inflation back is deployable, has in light weight and the high advantage of folding efficiency.Two, because single, the no joint of tubing so just can realize that failure-free launches, expansion process is easy to control simultaneously.Three, can carry out corresponding structure design according to the requirement of different expansion propulsive effort, duration of run, mechanical property and version, satisfy different operatings needs, have stronger designability, Applicable scope is very wide.Four, can realize the making of overlength, reach up to a hundred meters length, thereby satisfy the requirement of survey of deep space.
Performance figure of the present invention are as shown in the table:
| Strut bar length | 10～100m |
| Strut bar weight | ≤250g |
| Folding ratio | ≥30 |
| The compression buckling load | ≥50N |
| Fundamental frequency | ≥0.6Hz |
| Bending stiffness | ≥1N-m 2 |
Description of drawings
Fig. 1 is an integral structure scheme drawing of the present invention, and Fig. 2 is the A-A cutaway view of Fig. 1, and Fig. 3 is that the B-B of Fig. 1 analyses and observe enlarged view, and Fig. 4 is a folding scheme drawing of the present invention, and Fig. 5 is the structural representation of the specific embodiment 19.
The specific embodiment
The specific embodiment one: (referring to Fig. 1-Fig. 4) present embodiment is made up of the termination lid 3 of inner layer pipe 1, outer tube 2 and two tubulars, inner layer pipe 1 is put in outer tube 2, the center of each termination lid 3 has air-filled pore 3-1, and two termination lids 3 are connected by sealing with the two ends of inner layer pipe 1 and outer tube 2 respectively; The length L of strut bar is 10～100m; Inner layer pipe 1 and outer tube 2 are membraneous material.
The specific embodiment two: (difference referring to the present embodiment of Fig. 1-Fig. 4) and the specific embodiment one is that the length L of strut bar is 10～39m.Other composition is identical with the specific embodiment one with annexation.
The specific embodiment three: (difference referring to the present embodiment of Fig. 1-Fig. 4) and the specific embodiment one is that the length L of strut bar is 10m.Other composition is identical with the specific embodiment one with annexation.
The specific embodiment four: (difference referring to the present embodiment of Fig. 1-Fig. 4) and the specific embodiment one is that the length L of strut bar is 25m.Other composition is identical with the specific embodiment one with annexation.
The specific embodiment five: (difference referring to the present embodiment of Fig. 1-Fig. 4) and the specific embodiment one is that the length L of strut bar is 39m.Other composition is identical with the specific embodiment one with annexation.
The specific embodiment six: (difference referring to the present embodiment of Fig. 1-Fig. 4) and the specific embodiment one is that the length L of strut bar is 40～69m.Other composition is identical with the specific embodiment one with annexation.
The specific embodiment seven: (difference referring to the present embodiment of Fig. 1-Fig. 4) and the specific embodiment one is that the length L of strut bar is 40m.Other composition is identical with the specific embodiment one with annexation.
The specific embodiment eight: (difference referring to the present embodiment of Fig. 1-Fig. 4) and the specific embodiment one is that the length L of strut bar is 55m.Other composition is identical with the specific embodiment one with annexation.
The specific embodiment nine: (difference referring to the present embodiment of Fig. 1-Fig. 4) and the specific embodiment one is that the length L of strut bar is 69m.Other composition is identical with the specific embodiment one with annexation.
The specific embodiment ten: (difference referring to the present embodiment of Fig. 1-Fig. 4) and the specific embodiment one is that the length L of strut bar is 70～100m.Other composition is identical with the specific embodiment one with annexation.
The specific embodiment 11: (difference referring to the present embodiment of Fig. 1-Fig. 4) and the specific embodiment one is that the length L of strut bar is 70m.Other composition is identical with the specific embodiment one with annexation.
The specific embodiment 12: (difference referring to the present embodiment of Fig. 1-Fig. 4) and the specific embodiment one is that the length L of strut bar is 85m.Other composition is identical with the specific embodiment one with annexation.
The specific embodiment 13: (difference referring to the present embodiment of Fig. 1-Fig. 4) and the specific embodiment one is that the length L of strut bar is 100m.Other composition is identical with the specific embodiment one with annexation.
The specific embodiment 14: (be that referring to the present embodiment of Fig. 1-Fig. 4) and the specific embodiment one to the difference of the specific embodiment 13 it has increased by two cassette tapes 4, the outside face upper edge circumference of the barrel of described termination lid 3 has ring-type cassette tape groove 3-2, two terminations lid 3 places respectively in the termination at inner layer pipe 1 two ends, two cassette tapes 4 be anchored on respectively two terminations cover 3 outsides outer tube 2 outside face and be installed on respectively on two terminations lids 3 in the cassette tape groove 3-2.Other composition is identical to the specific embodiment 13 with the specific embodiment one with annexation.Present embodiment is fastenedly connected by the outside face of cassette tape 4 with the termination lid 3 of inner layer pipe 1 and outer tube 2 and two tubulars, and technology is simple, reliable.
The specific embodiment 15: (be that referring to the present embodiment of Fig. 1-Fig. 4) and the specific embodiment one to the difference of the specific embodiment 14 it has increased firm bar 5, just bar 5 is fixed on the inside face of outer tube 2.Other composition is identical to the specific embodiment 14 with the specific embodiment one with annexation.The material of the firm bar 5 that present embodiment increased adopts high resiliency steel 65Mn, and its effect is to improve the bending stiffness of pipe; Can adjust the quantity of firm bar, parameters such as width according to different rigidity requirements.
The specific embodiment 16: (be that referring to the present embodiment of Fig. 1-Fig. 4) and the specific embodiment one to the difference of the specific embodiment 15 it has increased stick 6, stick 6 is fixed on the outside face of outer tube 2.Other composition is identical to the specific embodiment 15 with the specific embodiment one with annexation.The effect of the stick 6 that present embodiment increased is that the bonding force of stick 6 can make pipe be crimped onto together closely.
The specific embodiment 17: (be that referring to the present embodiment of Fig. 1-Fig. 4) and the specific embodiment one to the difference of the specific embodiment 16 material of described stick 6 is a velcro, the quantity of stick 6 is even number and is symmetrical arranged along the radial centre lines of outer tube 2.Other composition is identical to the specific embodiment 16 with the specific embodiment one with annexation.Present embodiment is after vacuumizing, and the stick 6 on the outer tube surface of assurance flat form is in upper and lower cooresponding position, when curling, guarantees stick alignment (as shown in Figure 4).Like this, in the expansion process of pipe,, realize the controlled expansion of pipe by the dumping force that stick provides; Can reasonably select the quantity and the width of stick for use according to the requirement of different propulsive effort and deployment rate.
The specific embodiment 18: (be that referring to the present embodiment of Fig. 1-Fig. 4) and the specific embodiment one to the difference of the specific embodiment 17 described inner layer pipe 1 and outer tube 2 are prismatic cylinder.Other composition is identical to the specific embodiment 17 with the specific embodiment one with annexation.
The specific embodiment 19: (referring to Fig. 5) present embodiment and the specific embodiment one to the difference of the specific embodiment 17 is that described inner layer pipe 1 and outer tube 2 are the circular cone stage body of variable section.Other composition is identical to the specific embodiment 17 with the specific embodiment one with annexation.
Claims (6)
1, extra long aerated expansion supporting rod for outer space, it comprises the termination lid (3) of inner layer pipe (1), outer tube (2) and two tubulars, inner layer pipe (1) is put in outer tube (2), the center of each termination lid (3) has air-filled pore (3-1), two terminations lid (3) is connected by sealing with the two ends of inner layer pipe (1) and outer tube (2) respectively, and inner layer pipe (1) and outer tube (2) are membraneous material; It is characterized in that it also comprises firm bar (5), stick (6), described firm bar (5) is fixed on the inside face of outer tube (2), and described stick (6) is fixed on the outside face of outer tube (2), and the length L of strut bar is 10～100m.
2, extra long aerated expansion supporting rod for outer space according to claim 1, it is characterized in that it has increased by two cassette tapes (4), the outside face upper edge circumference of the barrel of described termination lid (3) has ring-type cassette tape groove (3-2), two termination lids (3) place respectively in the termination at inner layer pipe (1) two ends, and two cassette tapes (4) are anchored on the outside face of the outer tube (2) outside two termination lids (3) respectively and are installed on two terminations lids (3) respectively and go up in the cassette tape groove (3-2).
3, extra long aerated expansion supporting rod for outer space according to claim 1 is characterized in that the material of described firm bar (5) adopts high resiliency steel 65Mn.
4, extra long aerated expansion supporting rod for outer space according to claim 1, the material that it is characterized in that described stick (6) is a velcro, the quantity of stick (6) is even number and is symmetrical arranged along the radial centre lines of outer tube (2).
5, extra long aerated expansion supporting rod for outer space according to claim 1 and 2 is characterized in that described inner layer pipe (1) and outer tube (2) are prismatic cylinder.
6, extra long aerated expansion supporting rod for outer space according to claim 1 and 2 is characterized in that described inner layer pipe (1) and outer tube (2) are the circular cone stage body of variable section.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2006100098823A CN100453404C (en) | 2006-03-31 | 2006-03-31 | Extra long aerated expansion supporting rod for outer space |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2006100098823A CN100453404C (en) | 2006-03-31 | 2006-03-31 | Extra long aerated expansion supporting rod for outer space |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1824578A CN1824578A (en) | 2006-08-30 |
| CN100453404C true CN100453404C (en) | 2009-01-21 |
Family
ID=36935454
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB2006100098823A Expired - Fee Related CN100453404C (en) | 2006-03-31 | 2006-03-31 | Extra long aerated expansion supporting rod for outer space |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN100453404C (en) |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101295810B (en) * | 2008-06-25 | 2012-02-22 | 哈尔滨工业大学 | Single motor-driving thin film antenna bean-pod shaped bracing stick two-side expansion mechanism |
| CN101913270B (en) * | 2010-07-23 | 2012-11-21 | 哈尔滨工业大学 | Foldable-expandable shape memory supporting pipe and preparation method thereof |
| CN102320384B (en) * | 2011-06-23 | 2014-12-10 | 哈尔滨工业大学 | Dual-omega-shaped carbon fiber composite air-filled extension arm |
| CN102381491A (en) * | 2011-08-18 | 2012-03-21 | 哈尔滨工业大学 | Unfolding control device for three-dimensional inflatable unfolding truss structure |
| CN104627387B (en) * | 2013-11-11 | 2017-01-18 | 北京航天长征飞行器研究所 | Space inflatable structure capable of being unfolded and formed in reverse direction and cladding |
| CN103872423B (en) * | 2014-03-28 | 2016-01-06 | 哈尔滨工业大学 | A kind of curling folding and inflatable deployment structure of inflating expanded parabolic-cylinder antenna |
| 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 |
| CN106384867A (en) * | 2016-11-23 | 2017-02-08 | 上海卫星工程研究所 | Inflation moulded parabola type supporting structure |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020116877A1 (en) * | 2001-02-28 | 2002-08-29 | Elmar Breitbach | Apparatus including a boom to be compressed and rolled up |
| US6568640B1 (en) * | 1999-07-22 | 2003-05-27 | Lockheed Martin Corporation | Inflatable satellite design |
| US20030183726A1 (en) * | 2002-03-27 | 2003-10-02 | Lounge John M. | Space cargo delivery apparatus |
| US20030182878A1 (en) * | 2002-04-02 | 2003-10-02 | Warren Peter A. | Flat folding tube |
| US20040046085A1 (en) * | 2002-08-29 | 2004-03-11 | L'garde, Inc. | Deployable inflatable boom and methods for packaging and deploying a deployable inflatable boom |
| JP2005119541A (en) * | 2003-10-17 | 2005-05-12 | Japan Aerospace Exploration Agency | Inflatable tube |
| US6910308B2 (en) * | 2003-02-04 | 2005-06-28 | Ilc Dover Lp | Inflatable rigidizable boom |
-
2006
- 2006-03-31 CN CNB2006100098823A patent/CN100453404C/en not_active Expired - Fee Related
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6568640B1 (en) * | 1999-07-22 | 2003-05-27 | Lockheed Martin Corporation | Inflatable satellite design |
| US20020116877A1 (en) * | 2001-02-28 | 2002-08-29 | Elmar Breitbach | Apparatus including a boom to be compressed and rolled up |
| US20030183726A1 (en) * | 2002-03-27 | 2003-10-02 | Lounge John M. | Space cargo delivery apparatus |
| US20030182878A1 (en) * | 2002-04-02 | 2003-10-02 | Warren Peter A. | Flat folding tube |
| US20040046085A1 (en) * | 2002-08-29 | 2004-03-11 | L'garde, Inc. | Deployable inflatable boom and methods for packaging and deploying a deployable inflatable boom |
| US6910308B2 (en) * | 2003-02-04 | 2005-06-28 | Ilc Dover Lp | Inflatable rigidizable boom |
| JP2005119541A (en) * | 2003-10-17 | 2005-05-12 | Japan Aerospace Exploration Agency | Inflatable tube |
Also Published As
| Publication number | Publication date |
|---|---|
| CN1824578A (en) | 2006-08-30 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN100453404C (en) | Extra long aerated expansion supporting rod for outer space | |
| RU2748242C2 (en) | Folding radio frequency membrane antenna | |
| CN104260900B (en) | Truss-like telescopic unit and telescopic support arm that elastic hinge drives | |
| CN101224793B (en) | Space extensible catopter device | |
| CN102011922B (en) | Deployable surface device with fixed truss structure | |
| US5104211A (en) | Splined radial panel solar concentrator | |
| CN101276961B (en) | Rigidizable inflating-expansion radial direction rib support type offset-feed paraboloidal antenna | |
| CN101314411B (en) | Shielding surface apparatus with space capable of being expanded | |
| US20080111031A1 (en) | Deployable flat membrane structure | |
| US6624796B1 (en) | Semi-rigid bendable reflecting structure | |
| CN102437404A (en) | Integrated structure of rigidized inflatable deployable truss type planar antenna and solar array | |
| CN102320384B (en) | Dual-omega-shaped carbon fiber composite air-filled extension arm | |
| CN103786906A (en) | Space deployable mechanism | |
| US8384613B1 (en) | Deployable structures with quadrilateral reticulations | |
| US20070145195A1 (en) | Deployable array support structure | |
| WO2011006506A1 (en) | Foldable frame supporting electromagnetic radiation collectors | |
| JP2003531544A (en) | An antenna based on a compact, stowable, thin, continuous surface with radial and circumferential stiffness that deploys and maintains the antenna surface in a predetermined surface geometry | |
| CN108598662B (en) | Double-layer parallelogram annular expandable truss | |
| ES2848727T3 (en) | Deployable mast structure | |
| US20220297855A1 (en) | Large space self-deployable boom | |
| CN207550546U (en) | A kind of deployable space support structure of gapless of elastic hinge driving | |
| GB2555656A (en) | Deployable wrapped rib assembly | |
| CN103863580A (en) | Folding method applicable to sail surfaces of blocked square support rod type solar sails | |
| US11183768B1 (en) | Dual boom deployable parabolic trough reflector | |
| CN110661075B (en) | Telescopic modular cylindrical antenna for ultra-long caliber |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 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 | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20090121 |