CN209183705U - Annular truss formula deployable antenna mechanism based on 3R-RRP mechanism unit - Google Patents
Annular truss formula deployable antenna mechanism based on 3R-RRP mechanism unit Download PDFInfo
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- CN209183705U CN209183705U CN201920084084.XU CN201920084084U CN209183705U CN 209183705 U CN209183705 U CN 209183705U CN 201920084084 U CN201920084084 U CN 201920084084U CN 209183705 U CN209183705 U CN 209183705U
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Abstract
The utility model discloses a kind of annular truss formula deployable antenna mechanism based on 3R-RRP mechanism unit, include 2N 3R-RRP mechanism unit, 2N 3R-RRP mechanism unit is in pairs, by sharing a support rod, a stationary nodes connector and a movement node connector connection, N number of combined mechanism unit is formed；N number of combined mechanism cellular construction is identical, by sharing a support rod and two stationary nodes connector connections between adjacent combination mechanism unit, collectively constitutes multi-panel formula annular truss mechanism；3R-RRP mechanism unit mainly includes two support rods, a root long connecting rod, two short connecting rods, three stationary nodes connectors and a movement node connector；Wherein short connecting rod length is the half of long connecting rod length, and support pole length is greater than three times of short connecting rod length.The overall mechanism structure of the utility model is simple, and flexibly, cost is relatively low for processing and manufacturing for movement, can be used as supporting mechanism and is preferably applied to heavy caliber satellite antenna field.
Description
Technical field
The utility model belongs to aerial mechanical field, and in particular to a kind of annular truss formula based on 3R-RRP mechanism unit
Deployable antenna mechanism.
Background technique
With satellite communication, earth observation and the fast development of other space science causes, the demand of space mechanism is cured
Add urgent.Due to the limitation in carrier rocket space, it is desirable that space mechanism folds up in launching phase, requires after stepping into track
Space mechanism can be deployed into working condition again, and keep certain rigidity and precision.Therefore, aerospace mechanism is mostly deployable
Mechanism, space deployable mechanism has been widely used for the unfolding mechanism, Space Docking Mechanism, space station bone of solar wing at present
The fields such as frame, moon suspension and heavy caliber space deployable antenna, as the U.S. is used for 60 meter Ke Zhan that dimensional topography is observed
Opening radar support arm, international space station owner's solar wing support keel, the tetrahedral framework formula in Russian SOYUZ spacecraft can
The architecture type expandable antenna etc. of deployable antenna and 13 meters of bores on Japan's ETS-8 satellite.
The application of space large caliber antenna can greatly improve earth observation level of resolution, space investigation and accurately beat
Ability etc. is hit, it mainly includes framework type that heavy caliber space deployable antenna, which is a key areas of deployable mechanism application,
Deployable antenna, folding ribbed deployable antenna, ring-cylindricality deployable antenna and annular truss formula deployable antenna etc..?
In the space deployable antenna of numerous types, the large-sized annular truss-like deployable antenna of the net containing flexible cable is a kind of comparative maturity
The netted deployable antenna of large size, for expansion bore up to hundred meters, area coverage will not be unfolded with antenna in the quality of simultaneity factor
Increase and proportional increase, so its attention increasingly by related scientific research personnel.Annular truss formula deployable antenna one
As be made of the deployable sub-truss of annular and rope net system, annular truss supporting mechanism is by single polygon or multiple more
Shape combination in side contacts rope by tensioning and applies pretension, so that needed for the reflecting surface rope net for being arranged in annular truss two sides is formed
Paraboloid.
TRW Astro Aerospace company, the U.S. develops one kind according to the diagonal telescopic feature of parallelogram
Annular truss formula deployable antenna mechanism based on parallelogram element, has been successfully applied to deep space communication task now.It should
Scheme expansion process is simple, and driving source is single, but due to leading to overall mechanism process and assemble there are the engagement of multiple groups conical gear
Cost it is relatively high, while the folding ratio of the program is also to be improved.Related scientific research mechanism, China can to annular truss formula space
Deployable antenna institutions conduct a lot of research work achieves more significant achievement, but annular purlin in orbit at present
Posture deployable antenna is still less, and configuration is also more single, it is, therefore, desirable to provide some structures are simple, it is bigger to fold
And the annular truss formula deployable antenna mechanism of the higher equal high comprehensive performances of rigidity, to meet the need of different space missions
It asks.
Utility model content
For above situation, the utility model provides a kind of deployable day of annular truss formula based on 3R-RRP mechanism unit
Line mechanism, overcome the deficiencies in the prior art are not only simple in structure, and cost is relatively low for overall mechanism process and assemble, and deployable
The folding of antenna mechanism is relatively high.
Technical solution used by the utility model is to provide a kind of annular truss formula based on 3R-RRP mechanism unit can
Deployable antenna mechanism, including 2N 3R-RRP mechanism unit (R represents revolute pair, and P represents prismatic pair), wherein N be more than or equal to
2 integer, 2N 3R-RRP mechanism unit in pairs, pass through shared a support rod, a stationary nodes connector and one
A movement node connector connection, forms N number of combined mechanism unit；Identical, the adjacent group of N number of combined mechanism cellular construction
By sharing a support rod and two stationary nodes connectors connections between conjunction mechanism unit, multi-panel formula annular truss is collectively constituted
Mechanism；The 3R-RRP mechanism unit includes two support rods, a root long connecting rod, two short connecting rods, three stationary nodes connections
Part and a movement node connector, two supporting bar structures are identical, are symmetrically arranged in 3R-RRP mechanism unit
Two side positions；The structure of three stationary nodes connectors is identical, and is set as crank shape, and crank throw two sides respectively set one
A open slot, the open end of the open slot are located at two free ends of crank throw, and crank throw two sides were symmetrical with the plane of bending part, and
Angle between the central plane of both-side opening slot is (180-180/N) °, and stationary nodes connector center position is provided with hole
Hole, described hole are set on the both ends of support rod and are fixed together with support rod, two to be connected on the same support rod
It mutually coincides between the median plane of the open slot of the stationary nodes connector；The movement node connector is set in the branch
On strut, in-between hole forms prismatic pair with support rod and connect, and allows to slide on support rod, the same support
On bar be connected stationary nodes connector and by prismatic pair connect movement node connector open slot central plane between
Mutually coincide；And one end insertion of the long connecting rod is fixed on the opening of the side of the stationary nodes connector of support rod one end
It is connected in slot and by revolute pair, the opening for the movement node connector side that other end insertion is connected in another side support bar
It is connected in slot and by revolute pair；One end of two short connecting rods is interconnected by revolute pair, and in addition both ends are inserted into respectively
It is consolidated in the open slot of the stationary nodes connector side on bar supported on both sides and is connected by revolute pair.
Preferably, all turns auxiliary shafts connected on the long connecting rod and short connecting rod in the same 3R-RRP mechanism unit
Line is parallel to each other.
Preferably, the length of the short connecting rod is the half of long connecting rod length, and the length of the support rod is greater than short connecting rod
Three times of length.
Further, the movement node connector is identical as the structure of the stationary nodes connector.
Preferably, the structure of the short connecting rod is all the same, and the structure of the long connecting rod is also all the same.
Compared with the prior art, the utility model has the following advantages:
1, the utility model structure is simple, and contained kinematic pair only has revolute pair and prismatic pair, no conical gear or other classes
The synchronising hinge device of type, cost is relatively low for processing and manufacturing；
2, the utility model has the characteristics that movement is flexible, it is bigger to fold, and overall structure rigidity is higher；
3, the utility model has the structural symmetry of height, by the quantity and wherein for changing 3R-RRP mechanism unit
The length of rod piece can form the annular truss formula deployable antenna mechanism of different scale, can be used as supporting mechanism preferably
Applied to heavy caliber satellite antenna field.
Detailed description of the invention
Fig. 1 is fully deployed schematic perspective view for the utility model；
Fig. 2 is the half expansion schematic perspective view of the utility model；
Fig. 3 is the complete gathering schematic perspective view of the utility model；
Fig. 4 is that the combined mechanism unit of the utility model is fully deployed schematic perspective view；
Fig. 5 is that schematic perspective view is partly unfolded in the combined mechanism unit of the utility model；
Fig. 6 is that the combined mechanism unit of the utility model collapses schematic perspective view completely；And
Fig. 7 is the stationary nodes connector schematic perspective view of the utility model.
Main appended drawing reference is as follows:
3R-RRP mechanism unit 10, combined mechanism unit 100, stationary nodes connector 1, short connecting rod 2, long connecting rod 3, support
Bar 4, movement node connector 5, open slot 11, hole 12, the first turn hole 13, the second turn hole 14.
Specific embodiment
By the technology contents of detailed the utility model, structure feature, reach purpose and efficacy, below with reference to specification
Attached drawing is described in detail.
The utility model provides a kind of annular truss formula deployable antenna mechanism based on 3R-RRP mechanism unit, such as Fig. 1
Shown in~7, including 2N 3R-RRP mechanism unit 10 (R represents revolute pair, and P represents prismatic pair), wherein N is more than or equal to 2
Integer, 2N 3R-RRP mechanism unit 10 in pairs, pass through shared 4, stationary nodes connectors 1 and one of a support rod
A movement node connector 5 connects, and forms N number of combined mechanism unit 100；N number of 100 structure of combined mechanism unit is identical,
It is connected, is collectively constituted by sharing a support rod 4 and two stationary nodes connectors 1 between adjacent combined mechanism unit 100
Multi-panel formula annular truss mechanism；3R-RRP mechanism unit 10 includes 3, two two support rods 4, root long connecting rod short connecting rods 2, three
A stationary nodes connector 1 and a movement node connector 5, two 4 structures of support rod are identical, are symmetrically arranged in 3R-
Two side positions of RRP mechanism unit 10；The structure of three stationary nodes connectors 1 is identical, and is set as crank shape, bent
It turns two sides and respectively sets an open slot 11, the open end of open slot 11 is located at two free ends of crank throw, and crank throw two sides were symmetrical with folding
The plane of crook, and the angle between the central plane of both-side opening slot 11 is (180-180/N) °, in stationary nodes connector 1
Hole 12 is provided at heart position, hole 12 is set on the both ends of support rod 4 and is fixed together with support rod 4, same support rod 4
It mutually coincides between the median plane of the open slot 11 of upper two connected stationary nodes connectors 1；Movement node connector 5 is worn
On support rod 4, in-between hole 12 forms prismatic pair with support rod 4 and connect, and allows to slide on support rod 4, together
The open slot 11 for the movement node connector 5 that the stationary nodes connector 1 being connected on one support rod 4 is connect with by prismatic pair
It mutually coincides between central plane；The first end insertion of long connecting rod 3 is fixed on the stationary nodes connector 1 of 4 first end of support rod
It is connected to the first turn hole 13 in the open slot 11 of side and by revolute pair, second end insertion is connected in another side support bar 4
5 other side of movement node connector open slot 11 in and the second turn hole 14 is connected to by revolute pair；Two short connecting rods 2
One end is interconnected by revolute pair, and in addition the stationary nodes connector 1 one being consolidated on bar 4 supported on both sides is inserted at both ends respectively
It is connected in the open slot 11 of side and by revolute pair.
All revolute pair axis connected on long connecting rod 3 and short connecting rod 2 in same 3R-RRP mechanism unit 10 are mutual
In parallel；The length of short connecting rod 2 is the half of 3 length of long connecting rod, and the length of support rod 4 is greater than three times of 2 length of short connecting rod；Movement
Node connector 5 is identical as the structure of stationary nodes connector 1；The structure of all short connecting rods 2 is identical；All long connecting rods
3 structure is also identical.
Embodiment 1, the behaviour of the annular truss formula deployable antenna mechanism based on 3R-RRP mechanism unit of the utility model
The process of work can be as follows, takes 12 3R-RRP mechanism units 10, and 12 3R-RRP mechanism units 10 are in pairs, by sharing one
4, stationary nodes connectors 1 of root support rod and a movement node connector 5 connect, and form 6 combined mechanism units
100；The structure of 6 combined mechanism units 100 is identical, by sharing a support between adjacent combination mechanism unit 100
Bar 4 and two stationary nodes connectors 1 connect, and collectively constitute multi-panel formula annular truss mechanism.
3R-RRP mechanism unit 10 mainly includes two support rods 4, the fixation of short connecting rod 2, three of 3, two, a root long connecting rod
Node connector 1 and a movement node connector 5.Two 4 structures of support rod are identical, are arranged symmetrically on 3R-RRP machine
Two side positions of structure unit 10；Three 1 structures of stationary nodes connector are identical, for the crank throw for being up and down in plane, crank throw
Two sides respectively set an open slot 11, and the open end of open slot 11 is located at two free ends of crank throw, and crank throw two sides are to cross bending part
Plane be it is symmetrical, the angle between 11 median plane of both-side opening slot is 150 °, and 1 center of stationary nodes connector is provided with hole
12, it is set on the both ends of support rod 4 and is consolidated with support rod 4, two stationary nodes consolidated on same support rod 4 connect
The median plane of the open slot 11 of fitting 1 is overlapped；The structure of movement node connector 5 is identical as 1 structure of stationary nodes connector,
Difference is after being set on support rod 4 not consolidate with support rod 4, but utilizes in-between hole 12 and the formation of support rod 4
Prismatic pair connection, allows to slide on support rod 4, the stationary nodes connector 1 consolidated on same support rod 4 and passes through shifting
The median plane of the open slot 11 of the movement node connector 5 of dynamic secondary connection is overlapped；The insertion of 3 one end of long connecting rod is consolidated in support rod 4
It is connected in the open slot 11 of the side of the stationary nodes connector 1 of one end and by revolute pair, other end insertion is connected to another
It is connected in the open slot 11 of 5 side of movement node connector in side support bar 4 and by revolute pair；Two 2 structures of short connecting rod
Identical, two 2 one end of short connecting rod are connected by revolute pair, and in addition both ends are inserted into respectively is consolidated on bar 4 supported on both sides
It is connected in the open slot 11 of the side of stationary nodes connector 1 and by revolute pair.
Further, guarantee during the installation process on the long connecting rod 3 and short connecting rod 2 in same 3R-RRP mechanism unit 10
All revolute pair axis connected are parallel；The length of short connecting rod 2 is the half of 3 length of long connecting rod, and the length of support rod 4 is big
In three times of 2 length of short connecting rod；When two short connecting rods 2 interconnected are conllinear, 3R-RRP mechanism unit 10 reaches complete exhibition
Open position, it is in Singular position shape state at this time, and mechanism degeneration is the structure that freedom degree is zero, can be by the bar in structure
Part cancels themselves out the effect of external force, whole to have the preferable rigidity of structure and mechanics without providing additional driving moment
Performance.
In actual use, by 2 every two of short connecting rod one group connected by revolute pair；A support rod 4 is taken,
The first end and second end in support rod 4 is respectively fixedly connected in two stationary nodes connectors 1 by two stationary nodes connectors 1, and
And guarantee that the Center Symmetry Plane of the open slot 11 of two stationary nodes connectors 1 mutually coincides；Take a support rod 4, one
Stationary nodes connector 1, is fixed on the first end of support rod 4 by stationary nodes connector 1 and a movement node connector 5,
Movement node connector 5 is worn thereon from the second end of support rod 4, and a prismatic pair connection is consequently formed.
Take as needed above-mentioned mounted unit piece several, by revolute pair by the fixed knot of 4 first end of support rod
The short connecting rod 2 that point connector 1 is connected with two one group is sequentially connected with, and there are two stationary nodes connectors 1 for installation
Support rod 4 be spaced from each other with the support rod 4 for being equipped with a stationary nodes connector 1 and a movement node connector 5.According to
So as needed, take long connecting rod 3 several, the first end of long connecting rod 3 is connected to by revolute pair and is installed on support rod 4 second
In the open slot 11 of 1 side of stationary nodes connector at end, then the second end of long connecting rod 3 is connected to by revolute pair and is installed on
In the open slot 11 of 5 side of movement node connector of 4 second end of support rod, in short, one end of long connecting rod 3 by revolute pair with
The open slot 11 of stationary nodes connector 1 connects, and the other end is connected by the open slot 11 of revolute pair and movement node connector 5
It connects.
As described above, 2N 3R-RRP mechanism unit 10,2N 3R- can be obtained by this connection mounting means
RRP mechanism unit 10, in pairs, by sharing 4, stationary nodes connectors 1 of a support rod and a movement node
Connector 5 connects, and forms N number of combined mechanism unit 100；Identical, the adjacent combination of N number of 100 structure of combined mechanism unit
It is connected between mechanism unit 100 by sharing a support rod 4 and two stationary nodes connectors 1, collectively constitutes multi-panel formula annular
Truss mechanism.
The above is the preferred embodiment of the application, does not limit the protection scope of the utility model with this, should be referred to
Out, for those skilled in the art, under the premise of not departing from this technology principle, several change can also be made
Into and retouching, these improvements and modifications also should be regarded as the protection scope of the application.
Claims (5)
1. a kind of annular truss formula deployable antenna mechanism based on 3R-RRP mechanism unit, which is characterized in that including 2N 3R-
RRP mechanism unit, wherein N is the integer more than or equal to 2,
2N 3R-RRP mechanism unit in pairs, passes through a shared support rod, a stationary nodes connector and a fortune
Dynamic node connector connection, forms N number of combined mechanism unit；Identical, the adjacent combination machine of N number of combined mechanism cellular construction
By sharing a support rod and two stationary nodes connector connections between structure unit, multi-panel formula annular truss machine is collectively constituted
Structure；
The 3R-RRP mechanism unit includes two support rods, a root long connecting rod, two short connecting rods, three stationary nodes connectors
With a movement node connector, two supporting bar structures are identical, are symmetrically arranged in the two of 3R-RRP mechanism unit
Side position；The structure of three stationary nodes connectors is identical, and is set as crank shape, and crank throw two sides respectively set one
Open slot, the open end of the open slot are located at two free ends of crank throw, and crank throw two sides were symmetrical with the plane of bending part, and two
Angle between the central plane of side open groove is (180-180/N) °, and stationary nodes connector center position is provided with hole,
Described hole is set on the both ends of support rod and is fixed together with support rod, described in two to be connected on the same support rod
It mutually coincides between the median plane of the open slot of stationary nodes connector；The movement node connector is set in the support rod
On, in-between hole forms prismatic pair with support rod and connect, and allows to slide on support rod, on the same support rod
Between the central plane of the open slot of connected stationary nodes connector and the movement node connector connected by prismatic pair mutually
It is overlapped；And
In the open slot for the stationary nodes connector side that one end insertion of the long connecting rod is fixed on support rod one end and pass through
Revolute pair connection, the other end are inserted into the open slot for the movement node connector side being connected in another side support bar and pass through
Revolute pair connection；One end of two short connecting rods is interconnected by revolute pair, and in addition both ends are inserted into are consolidated in two sides respectively
It is connected in the open slot of stationary nodes connector side on support rod and by revolute pair.
2. the annular truss formula deployable antenna mechanism according to claim 1 based on 3R-RRP mechanism unit, feature
It is, all revolute pair axis connected on the long connecting rod and short connecting rod in the same 3R-RRP mechanism unit are put down mutually
Row.
3. the annular truss formula deployable antenna mechanism according to claim 1 based on 3R-RRP mechanism unit, feature
It is, the length of the short connecting rod is the half of long connecting rod length, and the length of the support rod is greater than three times of short connecting rod length.
4. the annular truss formula deployable antenna mechanism according to claim 1 based on 3R-RRP mechanism unit, feature
It is, the movement node connector is identical as the structure of the stationary nodes connector.
5. the annular truss formula deployable antenna mechanism according to claim 1 based on 3R-RRP mechanism unit, feature
It is, the structure of the short connecting rod is all the same, and the structure of the long connecting rod is also all the same.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201920084084.XU CN209183705U (en) | 2019-01-18 | 2019-01-18 | Annular truss formula deployable antenna mechanism based on 3R-RRP mechanism unit |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201920084084.XU CN209183705U (en) | 2019-01-18 | 2019-01-18 | Annular truss formula deployable antenna mechanism based on 3R-RRP mechanism unit |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109659659A (en) * | 2019-01-18 | 2019-04-19 | 燕山大学 | Annular truss formula deployable antenna mechanism based on 3R-RRP mechanism unit |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109659659A (en) * | 2019-01-18 | 2019-04-19 | 燕山大学 | Annular truss formula deployable antenna mechanism based on 3R-RRP mechanism unit |
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