CN103682668B - Bending-forming-based parabolic cylinder antenna reflector and method for reflector to achieve parabolic cylinder - Google Patents
Bending-forming-based parabolic cylinder antenna reflector and method for reflector to achieve parabolic cylinder Download PDFInfo
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- CN103682668B CN103682668B CN201310696325.3A CN201310696325A CN103682668B CN 103682668 B CN103682668 B CN 103682668B CN 201310696325 A CN201310696325 A CN 201310696325A CN 103682668 B CN103682668 B CN 103682668B
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Abstract
The invention discloses a bending-forming-based parabolic cylinder antenna reflector and a method for the reflector to achieve a parabolic cylinder, and belongs to the technical field of satellite-borne antennae. The problems that satellite-borne parabolic cylinder antennae are heavy, large in size after being curved, small in rigidity and low in face forming accuracy are solved. The bending-forming-based parabolic cylinder antenna reflector comprises a mandrel, a supporting plate, a film reflector, a film inflating tube, elastic buckles and a hauling cable. The method for the bending-forming-based parabolic cylinder antenna reflector to achieve the parabolic cylinder includes the steps that first, an air tank and other inflating devices are used for inflating the film inflating tube through an inflating opening, then, the hauling cable is rolled and shrunken through a motor and the like to combine the elastic buckles, the supporting plate and the film reflector bend along with combining of the elastic buckles so that the parabolic cylinder can be formed, and finally, the supporting plate and the film inflating tube are toughened through ultraviolet irradiation. The bending-forming-based parabolic cylinder antenna reflector is used as a satellite-borne antenna reflector.
Description
Technical field
The invention belongs to satellite antenna technical field, be specifically related to a kind of parabolic-cylinder antenna reflecting surface based on bent into shape and realize the method for parabolic cylinder.
Background technology
Spaceborne parabolic-cylinder antenna is in the parabolic cylinder surface accuracy situation that maintenance is higher, and need to reach overall weight little, structural reliability is high, rollable folding and controlled expansion.Following problem is there is in current spaceborne parabolic-cylinder antenna:
1. it is comparatively large that the reflecting surface of the parabolic-cylinder antenna launched by hinging manner need introduce construction weight, and curling rear volume is comparatively large, and surface accuracy not easily keeps;
2. it is little to there is integral rigidity in the reflecting surface of the parabolic-cylinder antenna launched by high accuracy guidance tape, and the shortcoming such as surface accuracy is low.
Summary of the invention
The object of the invention is the problem that large, the curling rear volume of weight is large and rigidity is little, surface accuracy is low existed to solve above-mentioned spaceborne parabolic-cylinder antenna, provide a kind of parabolic-cylinder antenna reflecting surface based on bent into shape and realize the method for parabolic cylinder, its technical scheme is as follows:
Based on a parabolic-cylinder antenna reflecting surface for bent into shape, it comprises mandrel, supporting bracket, film reflector face, membrane inflatable tube, Elastic buckle and pull rope; Described mandrel has two, and two mandrels adopt semi-circular carbon fiber pipe; Described supporting bracket has two pieces, two pieces of supporting brackets adopt fibre reinforced can rigidifying epoxide resin material, one end of two pieces of supporting brackets is gradually wide to the other end, two pieces of supporting brackets are fixedly connected between two mandrels, be provided with match block in the junction of supporting bracket and mandrel, described film reflector face is adhered to the surface of supporting bracket; Described membrane inflatable tube adopts aramid fiber to strengthen can rigidifying epoxide resin material, membrane inflatable tube has two, the two ends of two membrane inflatable tube are all closed, two membrane inflatable tube are separately positioned on the both sides in film reflector face, the two ends of the left end of two membrane inflatable tube and a mandrel are rotationally connected, and the left end of two membrane inflatable tube is provided with inflation inlet; Described elastic card is buckled with two, Elastic buckle comprises socket and elastic plug, the socket of two Elastic buckles is fixedly connected with the right-hand member of two membrane inflatable tube respectively, the elastic plug of two Elastic buckles is rotationally connected with the two ends of another root mandrel respectively, and two elastic plugs are provided with guide pipe; The two ends of described pull rope are passed from the guide pipe of two elastic plugs respectively and are connected with socket.
A kind of parabolic-cylinder antenna reflecting surface based on bent into shape realizes the method for parabolic cylinder, the aerating devices such as gas tank are first used to be inflated in membrane inflatable tube by inflation inlet, then the scrollings such as motor are used to shrink pull rope, Elastic buckle is combined, supporting bracket and film reflector face are bent to form parabolic cylinder thereupon, make supporting bracket and membrane inflatable tube rigidifying finally by Ultraviolet radiation.
Beneficial effect of the present invention is: structure is reliable, and it is little that overall structure introduces weight, and curling rear volume is little, and bent into shape back reflection surface accuracy is high, and has higher rigidity and stability.
accompanying drawing illustrates:
Fig. 1 is structural representation of the present invention;
Fig. 2 is mandrel in the present invention and match block schematic diagram;
Fig. 3 is the shaping rear schematic diagram of the present invention.
embodiment:
With reference to Fig. 1, Fig. 2 and Fig. 3, a kind of parabolic-cylinder antenna reflecting surface based on bent into shape, it comprises mandrel 1, supporting bracket 2, film reflector face 3, membrane inflatable tube 4, Elastic buckle 5 and pull rope 6; Described mandrel 1 has two, and two mandrels 1 adopt semi-circular carbon fiber pipe; Described supporting bracket 2 has two pieces, two pieces of supporting brackets 2 adopt fibre reinforced can rigidifying epoxide resin material, one end of two pieces of supporting brackets 2 is gradually wide to the other end, two pieces of supporting brackets 2 are fixedly connected between two mandrels 1, be provided with match block 1-1 in supporting bracket 2 and the junction of mandrel 1, described film reflector face 3 is adhered to the surface of supporting bracket 2; Described membrane inflatable tube 4 adopts aramid fiber to strengthen can rigidifying epoxide resin material, membrane inflatable tube 4 has two, the two ends of two membrane inflatable tube 4 are all closed, two membrane inflatable tube 4 are separately positioned on the both sides in film reflector face 3, the two ends of the left end of two membrane inflatable tube 4 and a mandrel 1 are rotationally connected, and the left end of two membrane inflatable tube 4 is provided with inflation inlet 4-1; Described Elastic buckle 5 has two, Elastic buckle 5 comprises socket 5-1 and elastic plug 5-2, the socket 5-1 of two Elastic buckles 5 is fixedly connected with the right-hand member of two membrane inflatable tube 4 respectively, the elastic plug 5-2 of two Elastic buckles 5 is rotationally connected with the two ends of another root mandrel 1 respectively, and two elastic plug 5-2 are provided with guide pipe 5-2-1; The two ends of described pull rope 6 are passed from the guide pipe 5-2-1 of two elastic plug 5-2 respectively and are connected with socket 5-1.
A kind of parabolic-cylinder antenna reflecting surface based on bent into shape realizes the method for parabolic cylinder, the aerating devices such as gas tank are first used to be inflated in membrane inflatable tube 4 by inflation inlet 4-1, then the scrollings such as motor are used to shrink pull rope 6, Elastic buckle 5 is combined, supporting bracket 2 and film reflector face 3 are bent to form parabolic cylinder thereupon, make supporting bracket 2 and membrane inflatable tube 4 rigidifying finally by Ultraviolet radiation.
Inventive principle: supporting bracket 2 of the present invention and membrane inflatable tube 4 adopt can rigidifying material, rollable, is easy to carry, launching to be formed can rigidifying through irradiation ultraviolet radiation after parabolic cylinder, increases stability.Mandrel 1 adopts return bend, and is connected and fixed by match block 1-1 and supporting bracket 2, the advantages such as have firmly easy to connect, construction weight is little, and rolled efficiency is good.
Claims (2)
1., based on a parabolic-cylinder antenna reflecting surface for bent into shape, it is characterized in that it comprises mandrel (1), supporting bracket (2), film reflector face (3), membrane inflatable tube (4), Elastic buckle (5) and pull rope (6); Described mandrel (1) has two, and two mandrels (1) adopt semi-circular carbon fiber pipe; Described supporting bracket (2) has two pieces, two pieces of supporting brackets (2) adopt fibre reinforced can rigidifying epoxide resin material, one end of two pieces of supporting brackets (2) is gradually wide to the other end, two pieces of supporting brackets (2) are fixedly connected between two mandrels (1), be provided with match block (1-1) in supporting bracket (2) and the junction of mandrel (1), described film reflector face (3) is adhered to the surface of supporting bracket (2); Described membrane inflatable tube (4) adopts aramid fiber to strengthen can rigidifying epoxide resin material, membrane inflatable tube (4) has two, the two ends of two membrane inflatable tube (4) are all closed, two membrane inflatable tube (4) are separately positioned on the both sides of film reflector face (3), the left end of two membrane inflatable tube (4) and the two ends of a mandrel (1) are rotationally connected, and the left end of two membrane inflatable tube (4) is provided with inflation inlet (4-1); Described Elastic buckle (5) has two, Elastic buckle (5) comprises socket (5-1) and elastic plug (5-2), the socket (5-1) of two Elastic buckles (5) is fixedly connected with the right-hand member of two membrane inflatable tube (4) respectively, the elastic plug (5-2) of two Elastic buckles (5) is rotationally connected with the two ends of another root mandrel (1) respectively, and two elastic plugs (5-2) are provided with guide pipe (5-2-1); The two ends of described pull rope (6) are passed from the guide pipe (5-2-1) of two elastic plugs (5-2) respectively and are connected with socket (5-1).
2. the parabolic-cylinder antenna reflecting surface based on bent into shape realizes the method for parabolic cylinder, it is characterized in that first using gas tank aerating device by inflation inlet (4-1) inflation in membrane inflatable tube (4), then motor scrolling is used to shrink pull rope (6), Elastic buckle (5) is combined, supporting bracket (2) and film reflector face (3) are bent to form parabolic cylinder thereupon, make supporting bracket (2) and membrane inflatable tube (4) rigidifying finally by Ultraviolet radiation.
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CN201310696325.3A CN103682668B (en) | 2013-12-18 | 2013-12-18 | Bending-forming-based parabolic cylinder antenna reflector and method for reflector to achieve parabolic cylinder |
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CN103682668B true CN103682668B (en) | 2015-06-17 |
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CN103943966B (en) * | 2014-04-28 | 2016-02-24 | 哈尔滨工业大学 | Inflated supporting pipe mixes with hinge to support and launches spaceborne parabolic-cylinder antenna |
CN106450791A (en) * | 2016-11-23 | 2017-02-22 | 上海卫星工程研究所 | Large-size spatial parabolic cylinder-shaped reelable metal surface antenna reflection surface structure |
CN113381160B (en) * | 2021-06-18 | 2022-07-01 | 上海航天测控通信研究所 | Film antenna tensile force active adjusting mechanism |
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US4527166A (en) * | 1981-03-26 | 1985-07-02 | Luly Robert A | Lightweight folding parabolic reflector and antenna system |
CN100348408C (en) * | 2005-04-08 | 2007-11-14 | 哈尔滨工业大学 | Composite thermosetting film for inflated spatial expanded structure and its making and rigidizing process |
CN100362693C (en) * | 2005-09-26 | 2008-01-16 | 哈尔滨工业大学 | Plane framework supporting structure capable of steel charge expansion |
CN1751965A (en) * | 2005-10-31 | 2006-03-29 | 哈尔滨工业大学 | Ultraviolet light rigidization composite film capable of aeration expanding outer space structure |
CN101369686B (en) * | 2008-02-01 | 2012-07-04 | 西安电子科技大学 | Reflection surface system capable of spacing expansion |
CN101276961B (en) * | 2008-05-16 | 2012-08-15 | 哈尔滨工业大学 | Rigidizable inflating-expansion radial direction rib support type offset-feed paraboloidal antenna |
CN102267573A (en) * | 2011-05-11 | 2011-12-07 | 哈尔滨工业大学 | On-track inflatable rigidizable aerated satellite |
CN102270681B (en) * | 2011-05-11 | 2015-04-15 | 东北农业大学 | Solar cell sailboard matched with shape of rigid inflatable and deployable satellite |
CN102280716B (en) * | 2011-05-11 | 2013-10-16 | 哈尔滨工业大学 | Body-mounted parabolic antenna for gas-filled satellite |
CN102358435B (en) * | 2011-08-18 | 2013-11-27 | 哈尔滨工业大学 | Truss unit capable of being foldable to launch and simultaneously extensional in Z axial direction and X direction |
CN102437404B (en) * | 2011-08-18 | 2014-02-12 | 哈尔滨工业大学 | Integrated structure of rigidized inflatable deployable truss type planar antenna and solar array |
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