CN102324438A - Inflation expansion truss solar panel array capable of on-orbit assembly - Google Patents
Inflation expansion truss solar panel array capable of on-orbit assembly Download PDFInfo
- Publication number
- CN102324438A CN102324438A CN201110237799A CN201110237799A CN102324438A CN 102324438 A CN102324438 A CN 102324438A CN 201110237799 A CN201110237799 A CN 201110237799A CN 201110237799 A CN201110237799 A CN 201110237799A CN 102324438 A CN102324438 A CN 102324438A
- Authority
- CN
- China
- Prior art keywords
- truss
- assembly type
- unit
- inflating expanded
- solar
- 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.)
- Granted
Links
Images
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
Landscapes
- Photovoltaic Devices (AREA)
Abstract
The invention provides an inflation expansion truss solar panel array capable of on-orbit assembly. The invention relates to an inflation expansion truss solar panel array to solve a problem that a present solar panel can not satisfy a large area solar panel requirement of spacecrafts such as a satellite, a space station and the like. Technical schemes of the invention are as follows: firstly, along a vertical equal interval, an assembly inflation expansion vertical truss is provided with a plurality of assembly inflation expansion solar panel units which are in mortise-tenon connection with truss unit connection columns of an assembly inflation expansion truss unit through framework unit connection columns; secondly, along a vertical direction, the assembly inflation expansion vertical truss is provided with a plurality of the assembly inflation expansion solar panel units; thirdly, one end of an assembly inflation expansion transverse truss is aligned with one end of the assembly inflation expansion vertical truss, and is in mortise-tenon connection with the truss unit connection columns through the framework unit connection columns. The inflation expansion truss solar panel array is applied to an astronaut on-orbit assembly inflation expansion truss solar panel array.
Description
Technical field
The present invention relates to a kind of inflating expanded truss formula solar array array.
Background technology
Along with the development of space station technology, spacecrafts such as satellite, space station need more powerful supply of electric power, and this has just required more large-area solar array.
Existing solar array mainly is to adopt mechanical type deploying solar windsurfing version.It is to be formed by connecting through bindiny mechanism, control development mechanism and retaining mechanism a lot of rigid members that mechanical type launches supporting construction, in use has problems such as complex structure, easy break-down, expansion poor reliability, overall weight weigh, folding efficiency is low, the emission volume is big; Because the windsurfing physical dimension increases, its emission volume significantly increases, and causes spacecraft emission difficulties such as satellite or space station, even can't launch; Because physical dimension and quality are big, installing at rail of solar array is very difficult; The solar array size can have a strong impact on the configuration out of my cabin of spacecrafts such as space station, even cause and other mutual interference between parts out of my cabin after increasing; Problems such as the rigidity of structure that also exists the spacecrafts such as satellite, space station that the large scale solar array is installed significantly reduces, flexiblely enlarge markedly, fundamental vibration frequency reduces greatly cause attitude of flight vehicle control difficult.
In a word, existing solar array can not satisfy the active demand of spacecrafts such as satellite, space station to the large tracts of land solar array.
Summary of the invention
The objective of the invention is that mechanical type deploying solar windsurfing in use exists complex structure, easy break-down, expansion poor reliability, overall weight is heavy, folding efficiency is low, the emission volume is big in order to solve, emission and in problems such as rail difficult installation; Solve simultaneously because of adopting the large tracts of land solar array to exist the rigidity of structure and fundamental frequency to increase and reduce with physical dimension; Be prone to cause with aircraft body resonance and cause the problem difficult attitude of flight vehicle control, so provide a kind of can be at the inflating expanded truss formula solar array array of rail assembling.
The objective of the invention is to realize, totally three technical schemes through following technical scheme:
First technical scheme:
Of the present inventionly a kind ofly can comprise a plurality of assembly type inflatable deploying solars windsurfing unit and a plurality of assembly type inflating expanded truss unit at the inflating expanded truss formula solar array array of rail assembling; Each assembly type inflatable deploying solar windsurfing unit is made up of an inflating expanded frame unit of assembly type, two solar cell substrates and multi-disc solar cell piece at least; Described at least two solar cell substrates are installed on the inflating expanded frame unit of assembly type, are pasted with the multi-disc solar cell piece on the every solar cell substrate; The inflating expanded frame unit of each assembly type is connected column with two frame units and is constituted by two inflating expanded frame unit stay pipes, two transverse slats; Two inflating expanded frame unit stay pipes and two transverse slats are formed the quadrilateral frame shelf structure, and any transverse slat two ends in described two transverse slats respectively are equipped with a frame unit and connect column; Each assembly type inflating expanded truss unit is connected the cross section that column forms by at least eight inflating expanded truss unit supports pipes with four truss elements be rectangular truss structure; Adjacent two assembly type inflating expanded truss unit connect and compose the inflating expanded longitudiual truss of assembly type through four truss elements connection column tenon fourths of the twelve Earthly Branches that are positioned on the Width; The inflating expanded longitudiual truss of described assembly type has a plurality of assembly type inflatable deploying solar windsurfings unit along its vertical spaced set, and each assembly type inflatable deploying solar windsurfing unit connects through two frame units and is positioned at longitudinally two truss elements on columns and the corresponding assembly type inflating expanded truss unit and is connected the column tenon fourth of the twelve Earthly Branches and is connected to form inflating expanded truss formula solar array array.
Of the present invention a kind of can be at the inflating expanded truss formula solar array array of rail assembling, the quantity of solar cell substrate is five.
Of the present invention a kind of can be at the inflating expanded truss formula solar array array of rail assembling, the quantity of assembly type inflatable deploying solar windsurfing unit is three, the quantity of assembly type inflating expanded truss unit is five.
Of the present invention a kind of can be at the inflating expanded truss formula solar array array of rail assembling, every inflating expanded truss unit supports pipe and every inflating expanded frame unit stay pipe all adopt flexible composite to process.
Second technical scheme:
Of the present inventionly a kind ofly can comprise a plurality of assembly type inflatable deploying solars windsurfing unit and a plurality of assembly type inflating expanded truss unit at the inflating expanded truss formula solar array array of rail assembling; Each assembly type inflatable deploying solar windsurfing unit is made up of an inflating expanded frame unit of assembly type, two solar cell substrates and multi-disc solar cell piece at least; Described at least two solar cell substrates are installed on the inflating expanded frame unit of assembly type, are pasted with the multi-disc solar cell piece on the every solar cell substrate; The inflating expanded frame unit of each assembly type is connected column with two frame units and is constituted by two inflating expanded frame unit stay pipes, two transverse slats; Two inflating expanded frame unit stay pipes and two transverse slats are formed the quadrilateral frame shelf structure, and any transverse slat two ends in described two transverse slats respectively are equipped with a frame unit and connect column; Each assembly type inflating expanded truss unit is connected the cross section that column forms by at least eight inflating expanded truss unit supports pipes with four truss elements be rectangular truss structure; Adjacent two assembly type inflating expanded truss unit connect and compose the inflating expanded longitudiual truss of assembly type through four truss elements connection column tenon fourths of the twelve Earthly Branches that are positioned on the Width; Described a plurality of assembly type inflating expanded truss unit and the corresponding one by one setting in a plurality of assembly type inflatable deploying solar windsurfings unit, each assembly type inflatable deploying solar windsurfing unit connects two truss elements that are positioned at vertical setting on columns and the corresponding assembly type inflating expanded truss unit through two frame units and is connected the column tenon fourth of the twelve Earthly Branches and is connected to form inflating expanded truss formula solar array array.
Of the present invention a kind of can be at the inflating expanded truss formula solar array array of rail assembling, the quantity of assembly type inflatable deploying solar windsurfing unit and the quantity of assembly type inflating expanded truss unit respectively are five.
Of the present invention a kind of can be at the inflating expanded truss formula solar array array of rail assembling, every inflating expanded truss unit supports pipe and every inflating expanded frame unit stay pipe all adopt flexible composite to process.
The 3rd technical scheme:
Of the present inventionly a kind ofly can comprise a plurality of assembly type inflatable deploying solars windsurfing unit and a plurality of assembly type inflating expanded truss unit at the inflating expanded truss formula solar array array of rail assembling; A plurality of assembly type inflatable deploying solar windsurfings unit comprises a plurality of first assembly type inflatable deploying solar windsurfing unit and a plurality of second assembly type inflatable deploying solar windsurfing unit; A plurality of assembly type inflating expanded truss unit comprises a plurality of first assembly type inflating expanded truss unit and a plurality of second assembly type inflating expanded truss unit; Each first assembly type inflatable deploying solar windsurfing unit and each second assembly type inflatable deploying solar windsurfing unit constitute by an inflating expanded frame unit of assembly type, two solar cell substrates and multi-disc solar cell piece at least; Described at least two solar cell substrates are installed on the inflating expanded frame unit of assembly type, are pasted with the multi-disc solar cell piece on the every solar cell substrate; The inflating expanded frame unit of each assembly type is connected column with two frame units and is constituted by two inflating expanded frame unit stay pipes, two transverse slats; Two inflating expanded frame unit stay pipes and two transverse slats are formed the quadrilateral frame shelf structure, and any transverse slat two ends in described two transverse slats respectively are equipped with a frame unit and connect column; Each first assembly type inflating expanded truss unit and each second assembly type inflating expanded truss unit all are connected the cross section that column forms by at least eight inflating expanded truss unit supports pipes with four truss elements be rectangular truss structure; Adjacent two first assembly type inflating expanded truss unit connect and compose the inflating expanded longitudiual truss of assembly type through four truss elements connection column tenon fourths of the twelve Earthly Branches that are positioned on the Width; The inflating expanded longitudiual truss of described assembly type has a plurality of first assembly type inflatable deploying solar windsurfing unit along its vertical spaced set, and each first assembly type inflatable deploying solar windsurfing unit connects through two frame units on it and is positioned at longitudinally on column and the corresponding first assembly type inflating expanded truss unit that two truss elements are connected the connection of the column tenon fourth of the twelve Earthly Branches; Adjacent two second assembly type inflating expanded truss unit connect and compose the inflating expanded transverse truss of assembly type through four truss elements connection column tenon fourths of the twelve Earthly Branches that are positioned on the length direction; The inflating expanded transverse truss of described assembly type has a plurality of second assembly type inflatable deploying solar windsurfing unit along its horizontal spaced set, and each second assembly type inflatable deploying solar windsurfing unit connects through two frame units on it and is positioned at two horizontal truss elements on column and the corresponding second assembly type inflating expanded truss unit and is connected the connection of the column tenon fourth of the twelve Earthly Branches; One end of the inflating expanded transverse truss of described assembly type aligns with an end of the inflating expanded longitudiual truss of assembly type and meets at right angles setting; The inflating expanded longitudiual truss of described assembly type is connected column with the inflating expanded transverse truss of assembly type through corresponding frame unit and is connected the connection of the column tenon fourth of the twelve Earthly Branches with truss element, forms the combined truss that has transverse branch.
Of the present invention a kind of can be at the inflating expanded truss formula solar array array of rail assembling; The quantity of the first assembly type inflating expanded truss unit is four; The quantity of the second assembly type inflating expanded truss unit is four; The quantity of the first assembly type inflatable deploying solar windsurfing unit is two, and the quantity of the second assembly type inflatable deploying solar windsurfing unit is two.
Of the present invention a kind of can be at the inflating expanded truss formula solar array array of rail assembling, every inflating expanded truss unit supports pipe and every inflating expanded frame unit stay pipe all adopt flexible composite to process.
The invention has the beneficial effects as follows: the present invention provides good solution route to the large tracts of land solar array problem that solves spacecraft demands such as satellite, space station; But adopt the gas-filled unfolded structure of flexible folding emission, solved because the problem that spacecrafts such as the satellite that large tracts of land solar array and large scale truss structure bring, space station are difficult to launch; Adopt truss-like solar array array; Solved the problem that the large tracts of land solar array can cause the reduction of spacecraft structure rigidity, flexible increase, fundamental vibration frequency to reduce; Assembly type inflatable deploying solar windsurfing unit and assembly type truss structure unit have little, the lightweight advantage of folding volume; Be convenient to the astronaut and install, can carry out space assembling and expansion very easily, for good basis is established in further expanding of space station structure and space station solar array array and the overall development in space station at rail.
Description of drawings
Fig. 1 is the overall structure sketch map of scheme one of the present invention;
Fig. 2 is an assembly type inflating expanded truss cellular construction sketch map;
Fig. 3 is an assembly type inflatable deploying solar windsurfing cellular construction sketch map;
Fig. 4 is the overall structure sketch map of scheme two of the present invention;
Fig. 5 is the overall structure sketch map of scheme three of the present invention.
Annotate: consider the definition of drawing, the frame unit connection column 6 among the above-mentioned figure is connected the tenon fourth of the twelve Earthly Branches of matching on the column 11 and does not draw with truss element.
Embodiment
Embodiment one: see Fig. 1-Fig. 3, a kind of of this execution mode can comprise a plurality of assembly type inflatable deploying solar windsurfings unit 1 and a plurality of assembly type inflating expanded truss unit 7 at the inflating expanded truss formula solar array array of rail assembling; Each assembly type inflatable deploying solar windsurfing unit 1 is made up of the inflating expanded frame unit of assembly type 4, two solar cell substrates 2 and multi-disc solar cell piece 3 at least; Described at least two solar cell substrates 2 are installed on the inflating expanded frame unit 4 of assembly type, are pasted with multi-disc solar cell piece 3 on the every solar cell substrate 2; The inflating expanded frame unit 4 of each assembly type is connected column 6 with two frame units and is constituted by two inflating expanded frame unit stay pipes 10, two transverse slats 5; Two inflating expanded frame unit stay pipes 10 and two transverse slats 5 are formed the quadrilateral frame shelf structure, and the two ends of any transverse slat 5 in described two transverse slats 5 respectively are equipped with a frame unit and connect column 6; Each assembly type inflating expanded truss unit 7 is connected the cross section that column 11 forms by at least eight inflating expanded truss unit supports pipes 8 with four truss elements be rectangular truss structure; Adjacent two assembly type inflating expanded truss unit 7 connect and compose the inflating expanded longitudiual truss of assembly type through four truss elements connection column 11 tenon fourths of the twelve Earthly Branches that are positioned on the Width; The inflating expanded longitudiual truss of described assembly type has a plurality of assembly type inflatable deploying solar windsurfings unit 1 along its vertical spaced set, and each assembly type inflatable deploying solar windsurfing unit 1 connects through two frame units and is positioned at longitudinally two truss elements on columns 6 and the corresponding assembly type inflating expanded truss unit 7 and is connected the column 11 tenon fourths of the twelve Earthly Branches and is connected to form inflating expanded truss formula solar array array.
Two corresponding truss elements connect column 11 and truss element and connect column 11 and be connected column 6 with frame unit and adopt the connection of the tenon fourth of the twelve Earthly Branches respectively, can make things convenient for the astronaut to install at rail.
Embodiment two: see Fig. 3, embodiment one described a kind of can be at the inflating expanded truss formula solar array array of rail assembling, the quantity of solar cell substrate 2 is five.
Embodiment three: see Fig. 1; Embodiment one described a kind of can be at the inflating expanded truss formula solar array array of rail assembling; The quantity of assembly type inflatable deploying solar windsurfing unit 1 is three, and the quantity of assembly type inflating expanded truss unit 7 is five.
Embodiment four: see Fig. 1-Fig. 3; Embodiment one, two or three described a kind of can be at the inflating expanded truss formula solar array array of rail assembling, every inflating expanded truss unit supports pipe 8 all adopts flexible composite to process with every inflating expanded frame unit stay pipe 10.
Can fold, inflating expanded and firmization.Assembly type inflatable deploying solar windsurfing unit 1 can fold along the length direction of inflating expanded frame unit stay pipe 10, and assembly type inflating expanded truss unit 7 can fold along inflating expanded truss unit supports pipe 8 horizontal, longitudinal direction.
Embodiment five: see Fig. 2-Fig. 4, a kind of of this execution mode can comprise a plurality of assembly type inflatable deploying solar windsurfings unit 1 and a plurality of assembly type inflating expanded truss unit 7 at the inflating expanded truss formula solar array array of rail assembling; Each assembly type inflatable deploying solar windsurfing unit 1 is made up of the inflating expanded frame unit of assembly type 4, two solar cell substrates 2 and multi-disc solar cell piece 3 at least; Described at least two solar cell substrates 2 are installed on the inflating expanded frame unit 4 of assembly type, are pasted with multi-disc solar cell piece 3 on the every solar cell substrate 2; The inflating expanded frame unit 4 of each assembly type is connected column 6 with two frame units and is constituted by two inflating expanded frame unit stay pipes 10, two transverse slats 5; Two inflating expanded frame unit stay pipes 10 and two transverse slats 5 are formed the quadrilateral frame shelf structure, and the two ends of any transverse slat 5 in described two transverse slats 5 respectively are equipped with a frame unit and connect column 6; Each assembly type inflating expanded truss unit 7 is connected the cross section that column 11 forms by at least eight inflating expanded truss unit supports pipes 8 with four truss elements be rectangular truss structure; Adjacent two assembly type inflating expanded truss unit 7 connect and compose the inflating expanded longitudiual truss of assembly type through four truss elements connection column 11 tenon fourths of the twelve Earthly Branches that are positioned on the Width; Described a plurality of assembly type inflating expanded truss unit 7 and the 1 corresponding one by one setting of a plurality of assembly type inflatable deploying solar windsurfings unit, each assembly type inflatable deploying solar windsurfing unit 1 connects two truss elements that are positioned at vertical setting on columns 6 and the corresponding assembly type inflating expanded truss unit 7 through two frame units and is connected the column 11 tenon fourths of the twelve Earthly Branches and is connected to form inflating expanded truss formula solar array array.
Two corresponding truss elements connect column 11 and truss element and connect column 11 and be connected column 6 with frame unit and adopt the connection of the tenon fourth of the twelve Earthly Branches respectively, can make things convenient for the astronaut to install at rail.
Embodiment six: see Fig. 4, embodiment five described a kind of can be at the inflating expanded truss formula solar array array of rail assembling, the quantity of assembly type inflatable deploying solar windsurfing unit 1 and the quantity of assembly type inflating expanded truss unit 7 respectively are five.
Embodiment seven: see Fig. 2-Fig. 4; Embodiment five or six described a kind of can be at the inflating expanded truss formula solar array array of rail assembling, every inflating expanded truss unit supports pipe 8 all adopts flexible composite to process with every inflating expanded frame unit stay pipe 10.
Can fold, inflating expanded and firmization.Assembly type inflatable deploying solar windsurfing unit 1 can fold along the length direction of inflating expanded frame unit stay pipe 10, and assembly type inflating expanded truss unit 7 can fold along inflating expanded truss unit supports pipe 8 horizontal, longitudinal direction.
Embodiment eight: see Fig. 2, Fig. 3 and Fig. 5, a kind of of this embodiment can comprise a plurality of assembly type inflatable deploying solars windsurfing unit and a plurality of assembly type inflating expanded truss unit at the inflating expanded truss formula solar array array of rail assembling; A plurality of assembly type inflatable deploying solar windsurfings unit comprises a plurality of first assembly type inflatable deploying solar windsurfing unit 12 and a plurality of second assembly type inflatable deploying solar windsurfing unit 13; A plurality of assembly type inflating expanded truss unit comprises a plurality of first assembly type inflating expanded truss unit 14 and a plurality of second assembly type inflating expanded truss unit 15; Each first assembly type inflatable deploying solar windsurfing unit 12 and each second assembly type inflatable deploying solar windsurfing unit 13 constitute by the inflating expanded frame unit of assembly type 4, two solar cell substrates 2 and multi-disc solar cell piece 3 at least; Described at least two solar cell substrates 2 are installed on the inflating expanded frame unit 4 of assembly type, are pasted with multi-disc solar cell piece 3 on the every solar cell substrate 2; The inflating expanded frame unit 4 of each assembly type is connected column 6 with two frame units and is constituted by two inflating expanded frame unit stay pipes 10, two transverse slats 5; Two inflating expanded frame unit stay pipes 10 and two transverse slats 5 are formed the quadrilateral frame shelf structure, and the two ends of any transverse slat 5 in described two transverse slats 5 respectively are equipped with a frame unit and connect column 6; Each first assembly type inflating expanded truss unit 14 and each second assembly type inflating expanded truss unit 15 all are connected the cross section that column 6 forms by at least eight inflating expanded truss unit supports pipes 8 with four truss elements be rectangular truss structure; Adjacent two first assembly type inflating expanded truss unit 14 connect and compose the inflating expanded longitudiual truss of assembly type through four truss elements connection column 11 tenon fourths of the twelve Earthly Branches that are positioned on the Width; The inflating expanded longitudiual truss of described assembly type has a plurality of first assembly type inflatable deploying solar windsurfing unit 12 along its vertical spaced set, and each first assembly type inflatable deploying solar windsurfing unit 12 connects through two frame units on it and is positioned at longitudinally on column 6 and the corresponding first assembly type inflating expanded truss unit 14 that two truss elements are connected the connection of the column 11 tenon fourths of the twelve Earthly Branches; Adjacent two second assembly type inflating expanded truss unit 15 connect and compose the inflating expanded transverse truss of assembly type through four truss elements connection column 11 tenon fourths of the twelve Earthly Branches that are positioned on the length direction; The inflating expanded transverse truss of described assembly type has a plurality of second assembly type inflatable deploying solar windsurfing unit 13 along its horizontal spaced set, and each second assembly type inflatable deploying solar windsurfing unit 13 connects through two frame units on it and is positioned at two horizontal truss elements on column 6 and the corresponding second assembly type inflating expanded truss unit 15 and is connected the connection of the column 11 tenon fourths of the twelve Earthly Branches; One end of the inflating expanded transverse truss of described assembly type aligns with an end of the inflating expanded longitudiual truss of assembly type and meets at right angles setting; The inflating expanded longitudiual truss of described assembly type is connected column 6 with the inflating expanded transverse truss of assembly type through corresponding frame unit and is connected the connection of the column 11 tenon fourths of the twelve Earthly Branches with truss element, forms the combined truss that has transverse branch.
Two corresponding truss elements connect column 11 and truss element and connect column 11 and be connected column 6 with frame unit and adopt the connection of the tenon fourth of the twelve Earthly Branches respectively, can make things convenient for the astronaut to install at rail.
Embodiment nine: see Fig. 5; Embodiment eight described a kind of can be at the inflating expanded truss formula solar array array of rail assembling; The quantity of the first assembly type inflating expanded truss unit 14 is four; The quantity of the second assembly type inflating expanded truss unit 15 is four, and the quantity of the first assembly type inflatable deploying solar windsurfing unit 12 is two, and the quantity of the second assembly type inflatable deploying solar windsurfing unit 13 is two.
Embodiment ten: see Fig. 2, Fig. 3 and Fig. 5; Embodiment eight or nine described a kind of can be at the inflating expanded truss formula solar array array of rail assembling, every inflating expanded truss unit supports pipe 8 all adopts flexible composite to process with every inflating expanded frame unit stay pipe 10.
Can fold, inflating expanded and firmization.Assembly type inflatable deploying solar windsurfing unit 1 can fold along the length direction of inflating expanded frame unit stay pipe 10, and assembly type inflating expanded truss unit 7 can fold along inflating expanded truss unit supports pipe 8 horizontal, longitudinal direction.
Each assembly type inflatable deploying solar windsurfing unit after folding and assembly type inflating expanded truss unit 7 folding volumes are little, in light weight, are convenient to emission.After emission is entered the orbit, be convenient to the astronaut and carry deliver from vault, carry out reaching desired structure rigidity in rail assembling, inflating expanded and firmization.
Claims (10)
1. one kind can is characterized in that at the inflating expanded truss formula solar array array of rail assembling, comprises a plurality of assembly type inflatable deploying solar windsurfing unit (1) and a plurality of assembly type inflating expanded truss unit (7); Each assembly type inflatable deploying solar windsurfing unit (1) is made up of an inflating expanded frame unit of assembly type (4), two solar cell substrates (2) and multi-disc solar cell piece (3) at least; Described at least two solar cell substrates (2) are installed on the inflating expanded frame unit of assembly type (4), are pasted with multi-disc solar cell piece (3) on the every solar cell substrate (2); The inflating expanded frame unit of each assembly type (4) is connected column (6) by two inflating expanded frame unit stay pipes (10), two transverse slats (5) and two frame units and constitutes; Two inflating expanded frame unit stay pipes (10) are formed the quadrilateral frame shelf structure with two transverse slats (5), and the two ends of any transverse slat (5) in described two transverse slats (5) respectively are equipped with a frame unit and connect column (6); Each assembly type inflating expanded truss unit (7) is connected the cross section that column (11) forms by at least eight inflating expanded truss unit supports pipes (8) with four truss elements be rectangular truss structure; Adjacent two assembly type inflating expanded truss unit (7) connect and compose the inflating expanded longitudiual truss of assembly type through four truss elements connection column (11) tenon fourths of the twelve Earthly Branches that are positioned on the Width; The inflating expanded longitudiual truss of described assembly type has a plurality of assembly type inflatable deploying solar windsurfing unit (1) along its vertical spaced set, and each assembly type inflatable deploying solar windsurfing unit (1) connects through two frame units and is positioned at longitudinally two truss elements on columns (6) and the corresponding assembly type inflating expanded truss unit (7) and is connected column (11) the tenon fourth of the twelve Earthly Branches and is connected to form inflating expanded truss formula solar array array.
2. according to claim 1ly a kind ofly can it is characterized in that the quantity of solar cell substrate (2) is five at the inflating expanded truss formula solar array array of rail assembling.
3. according to claim 1ly a kind ofly can it is characterized in that the quantity of assembly type inflatable deploying solar windsurfing unit (1) is three at the inflating expanded truss formula solar array array of rail assembling, the quantity of assembly type inflating expanded truss unit (7) is five.
According to claim 1,2 or 3 described a kind of can be at the inflating expanded truss formula solar array array of rail assembling; It is characterized in that every inflating expanded truss unit supports pipe (8) and every inflating expanded frame unit stay pipe (10) all adopt flexible composite to process.
5. one kind can is characterized in that at the inflating expanded truss formula solar array array of rail assembling, comprises a plurality of assembly type inflatable deploying solar windsurfing unit (1) and a plurality of assembly type inflating expanded truss unit (7); Each assembly type inflatable deploying solar windsurfing unit (1) is made up of an inflating expanded frame unit of assembly type (4), two solar cell substrates (2) and multi-disc solar cell piece (3) at least; Described at least two solar cell substrates (2) are installed on the inflating expanded frame unit of assembly type (4), are pasted with multi-disc solar cell piece (3) on the every solar cell substrate (2); The inflating expanded frame unit of each assembly type (4) is connected column (6) by two inflating expanded frame unit stay pipes (10), two transverse slats (5) and two frame units and constitutes; Two inflating expanded frame unit stay pipes (10) are formed the quadrilateral frame shelf structure with two transverse slats (5), and the two ends of any transverse slat (5) in described two transverse slats (5) respectively are equipped with a frame unit and connect column (6); Each assembly type inflating expanded truss unit (7) is connected the cross section that column (11) forms by at least eight inflating expanded truss unit supports pipes (8) with four truss elements be rectangular truss structure; Adjacent two assembly type inflating expanded truss unit (7) connect and compose the inflating expanded longitudiual truss of assembly type through four truss elements connection column (11) tenon fourths of the twelve Earthly Branches that are positioned on the Width; Described a plurality of assembly type inflating expanded truss unit (7) and the corresponding one by one setting in a plurality of assembly type inflatable deploying solar windsurfing unit (1), each assembly type inflatable deploying solar windsurfing unit (1) connects two truss elements that are positioned at vertical setting on columns (6) and the corresponding assembly type inflating expanded truss unit (7) through two frame units and is connected column (11) the tenon fourth of the twelve Earthly Branches and is connected to form inflating expanded truss formula solar array array.
6. according to claim 5ly a kind ofly can it is characterized in that the quantity of the quantity of assembly type inflatable deploying solar windsurfing unit (1) and assembly type inflating expanded truss unit (7) respectively is five at the inflating expanded truss formula solar array array of rail assembling.
According to claim 5 or 6 described a kind of can be at the inflating expanded truss formula solar array array of rail assembling; It is characterized in that every inflating expanded truss unit supports pipe (8) and every inflating expanded frame unit stay pipe (10) all adopt flexible composite to process.
8. one kind can is characterized in that at the inflating expanded truss formula solar array array of rail assembling, comprises a plurality of assembly type inflatable deploying solars windsurfing unit and a plurality of assembly type inflating expanded truss unit; A plurality of assembly type inflatable deploying solar windsurfings unit comprises a plurality of first assembly type inflatable deploying solar windsurfing unit (12) and a plurality of second assembly type inflatable deploying solar windsurfing unit (13); A plurality of assembly type inflating expanded truss unit comprises a plurality of first assembly type inflating expanded truss unit (14) and a plurality of second assembly type inflating expanded truss unit (15); Each first assembly type inflatable deploying solar windsurfing unit (12) and each second assembly type inflatable deploying solar windsurfing unit (13) constitute by an inflating expanded frame unit of assembly type (4), two solar cell substrates (2) and multi-disc solar cell piece (3) at least; Described at least two solar cell substrates (2) are installed on the inflating expanded frame unit of assembly type (4), are pasted with multi-disc solar cell piece (3) on the every solar cell substrate (2); The inflating expanded frame unit of each assembly type (4) is connected column (6) by two inflating expanded frame unit stay pipes (10), two transverse slats (5) and two frame units and constitutes; Two inflating expanded frame unit stay pipes (10) are formed the quadrilateral frame shelf structure with two transverse slats (5), and the two ends of any transverse slat (5) in described two transverse slats (5) respectively are equipped with a frame unit and connect column (6); Each first assembly type inflating expanded truss unit (14) and each second assembly type inflating expanded truss unit (15) all are connected the cross section that column (6) forms by at least eight inflating expanded truss unit supports pipes (8) with four truss elements be rectangular truss structure; Adjacent two first assembly type inflating expanded truss unit (14) connect and compose the inflating expanded longitudiual truss of assembly type through four truss elements connection column (11) tenon fourths of the twelve Earthly Branches that are positioned on the Width; The inflating expanded longitudiual truss of described assembly type has a plurality of first assembly type inflatable deploying solar windsurfing unit (12) along its vertical spaced set, and each first assembly type inflatable deploying solar windsurfing unit (12) connects through two frame units on it and is positioned at longitudinally on columns (6) and the corresponding first assembly type inflating expanded truss unit (14) that two truss elements are connected the connection of column (11) the tenon fourth of the twelve Earthly Branches; Adjacent two second assembly type inflating expanded truss unit (15) connect and compose the inflating expanded transverse truss of assembly type through four truss elements connection column (11) tenon fourths of the twelve Earthly Branches that are positioned on the length direction; The inflating expanded transverse truss of described assembly type has a plurality of second assembly type inflatable deploying solar windsurfing unit (13) along its horizontal spaced set, and each second assembly type inflatable deploying solar windsurfing unit (13) connects through two frame units on it and is positioned at two horizontal truss elements on columns (6) and the corresponding second assembly type inflating expanded truss unit (15) and is connected the connection of column (11) the tenon fourth of the twelve Earthly Branches; One end of the inflating expanded transverse truss of described assembly type aligns with an end of the inflating expanded longitudiual truss of assembly type and meets at right angles setting; The inflating expanded longitudiual truss of described assembly type is connected column (6) with the inflating expanded transverse truss of assembly type through corresponding frame unit and is connected the connection of column (11) the tenon fourth of the twelve Earthly Branches with truss element, forms the combined truss that has transverse branch.
9. according to claim 8 a kind of can be at the inflating expanded truss formula solar array array of rail assembling; It is characterized in that; The quantity of the first assembly type inflating expanded truss unit (14) is four; The quantity of the second assembly type inflating expanded truss unit (15) is four, and the quantity of the first assembly type inflatable deploying solar windsurfing unit (12) is two, and the quantity of the second assembly type inflatable deploying solar windsurfing unit (13) is two.
According to Claim 8 or 9 described a kind of can be at the inflating expanded truss formula solar array array of rail assembling; It is characterized in that every inflating expanded truss unit supports pipe (8) and every inflating expanded frame unit stay pipe (10) all adopt flexible composite to process.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011102377992A CN102324438B (en) | 2011-08-18 | 2011-08-18 | Inflation expansion truss solar panel array capable of on-orbit assembling |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011102377992A CN102324438B (en) | 2011-08-18 | 2011-08-18 | Inflation expansion truss solar panel array capable of on-orbit assembling |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102324438A true CN102324438A (en) | 2012-01-18 |
| CN102324438B CN102324438B (en) | 2013-01-23 |
Family
ID=45452144
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011102377992A Expired - Fee Related CN102324438B (en) | 2011-08-18 | 2011-08-18 | Inflation expansion truss solar panel array capable of on-orbit assembling |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102324438B (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105197259A (en) * | 2015-10-23 | 2015-12-30 | 中北大学 | Turnover type solar panel capable of unfolding towards light directionally |
| CN109818130A (en) * | 2019-02-14 | 2019-05-28 | 上海卫星工程研究所 | The limit-type pressing system of antenna plate and its method |
| CN112977892A (en) * | 2021-03-18 | 2021-06-18 | 航天科工空间工程发展有限公司 | Method for determining unfolding posture of inflatable solar wing in place on track |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1772562A (en) * | 2005-11-11 | 2006-05-17 | 哈尔滨工业大学 | Inflating expanded truss for outer space use |
| US20070215199A1 (en) * | 2006-03-16 | 2007-09-20 | United Technologies Corporation | Solar tracker |
| KR100881282B1 (en) * | 2008-07-04 | 2009-02-03 | 주식회사 에스엔케이솔라시스템즈 | Support panel for solar energy system |
| US20090032084A1 (en) * | 2007-07-30 | 2009-02-05 | Emcore Corporation | Optimization of ground coverage of terrestrial solar array system |
| CN101640502A (en) * | 2008-07-31 | 2010-02-03 | 昂科公司 | Method for assembling optical collector photoelectrical solar cell array |
| CN101913434A (en) * | 2010-08-23 | 2010-12-15 | 哈尔滨工业大学 | Inflatable and expandable three-dimensional truss on-track maintainable solar panel |
-
2011
- 2011-08-18 CN CN2011102377992A patent/CN102324438B/en not_active Expired - Fee Related
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1772562A (en) * | 2005-11-11 | 2006-05-17 | 哈尔滨工业大学 | Inflating expanded truss for outer space use |
| US20070215199A1 (en) * | 2006-03-16 | 2007-09-20 | United Technologies Corporation | Solar tracker |
| US20090032084A1 (en) * | 2007-07-30 | 2009-02-05 | Emcore Corporation | Optimization of ground coverage of terrestrial solar array system |
| KR100881282B1 (en) * | 2008-07-04 | 2009-02-03 | 주식회사 에스엔케이솔라시스템즈 | Support panel for solar energy system |
| CN101640502A (en) * | 2008-07-31 | 2010-02-03 | 昂科公司 | Method for assembling optical collector photoelectrical solar cell array |
| CN101913434A (en) * | 2010-08-23 | 2010-12-15 | 哈尔滨工业大学 | Inflatable and expandable three-dimensional truss on-track maintainable solar panel |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105197259A (en) * | 2015-10-23 | 2015-12-30 | 中北大学 | Turnover type solar panel capable of unfolding towards light directionally |
| CN109818130A (en) * | 2019-02-14 | 2019-05-28 | 上海卫星工程研究所 | The limit-type pressing system of antenna plate and its method |
| CN109818130B (en) * | 2019-02-14 | 2020-12-08 | 上海卫星工程研究所 | Antenna plate limiting type pressing system and method thereof |
| CN112977892A (en) * | 2021-03-18 | 2021-06-18 | 航天科工空间工程发展有限公司 | Method for determining unfolding posture of inflatable solar wing in place on track |
| CN112977892B (en) * | 2021-03-18 | 2022-09-23 | 航天科工空间工程发展有限公司 | Method for determining in-place unfolding posture of inflatable solar wing on orbit |
Also Published As
| Publication number | Publication date |
|---|---|
| CN102324438B (en) | 2013-01-23 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102437404B (en) | Integrated structure of rigidized inflatable deployable truss type planar antenna and solar array | |
| CN102358435B (en) | Truss unit capable of being foldable to launch and simultaneously extensional in Z axial direction and X direction | |
| CN105501471B (en) | Configuration of satellite loaded with large deployable antenna with double reflecting surfaces | |
| CN103482084B (en) | A kind of novel Stretching of solar wings based on banded spring and supporting mechanism | |
| CN104009278A (en) | Modularized space parabolic cylinder antenna folding and unfolding mechanism | |
| CN109850186B (en) | Plate frame type satellite structure for one-rocket multi-satellite parallel transmission and assembly method | |
| CN102324438B (en) | Inflation expansion truss solar panel array capable of on-orbit assembling | |
| CN101428690A (en) | Swirl type triangle crossarm hinge space extending arm | |
| EA025867B1 (en) | Multiple space vehicle launch system | |
| CN112977882A (en) | High orbit satellite platform structure with central force bearing cylinder type storage boxes tiled in parallel | |
| CN110504522B (en) | Flat plate folding and unfolding unit and flat plate folding and unfolding antenna mechanism | |
| US20190071191A1 (en) | Extendible membrane systems, devices, and methods | |
| CN104554822A (en) | Multilayer hollow interlayer inflated cabin | |
| CN106450649A (en) | H-structure spaceborne-antenna unfoldable mechanism | |
| CN202454720U (en) | Thermal-stabilizing framework of thin film antenna | |
| CN111703592A (en) | Large commercial remote sensing satellite platform configuration and assembly method | |
| CN109672401A (en) | A kind of large area braced frame of Modular Flexible connection | |
| CN111409871B (en) | Satellite platform configuration with extendable truss node pods | |
| CN105775166A (en) | I-shaped satellite platform | |
| CN103863580B (en) | A kind of method for folding being suitable to piecemeal quadrate support rod-type solar sail sail face | |
| CN110217408B (en) | Novel plane expandable structure | |
| CN112736403B (en) | Deployable double-layer hybrid spatial planar antenna | |
| CN111572814A (en) | Configuration and assembly method of ultra-large type assembled satellite platform of static orbit | |
| CN106025488B (en) | A kind of two-dimensional flat plate antenna expanding unit | |
| CN207550546U (en) | A kind of deployable space support structure of gapless of elastic hinge driving |
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: 20130123 Termination date: 20130818 |