A novel modular deployable mechanism for the truss antenna: Assembly principle and performance analysis

Abstract The truss antenna based on the tetrahedral deployable mechanism has the advantages of good deployment stability, high stiffness, large folding rate and high profile accuracy. A new modular deployable antenna mechanism based on the 3RR-3URU tetrahedral symmetrical combination unit is proposed in the present study. It should be indicated that the construction method of the modular mechanism is proposed initially based on the 3RR-3URU tetrahedral symmetrical combination unit as a basic module. The assembly method of modular mechanism and the arrangement of the joints connecting different modules are introduced in detail. Moreover, the large aperture antenna mechanism composed of more modules is described. The basic module and the modular mechanism composed of multiple modules belong to the spatial multi-closed-loop mechanism, so the degree of freedom (DOF) of the one-circle modular mechanism is analyzed by using the idea of ‘equivalent mechanism’ and screw theory. Moreover, the law of DOF of the multi-circle modular mechanism is further explored. The screw topological graph and screw coefficient matrix are applied for this kind of multi-closed-loop mechanism to obtain the results of the reasonable choice of actuation. Then, kinematics analysis of the modular mechanism is completed by the coordinate transformation and vector method. The folding rate is discussed and compared with other mechanisms for the truss antenna based on the kinematics. Finally, the simulation analysis model is established by using Solidworks and Adams modeling and simulation software. The correctness of the DOF and kinematics theory analysis is verified by the simulation analysis. Furthermore, the proposed mechanism is compared with the existing mechanisms. The proposed modular deployable antenna mechanism has the advantages of large folding rate and high reconfigurability. Therefore, it obtains great application prospects in the fields of the aerospace deployable antennas.

[1]  Bo Han,et al.  Design and analysis of a scissors double-ring truss deployable mechanism for space antennas , 2019, Aerospace Science and Technology.

[2]  Tuanjie Li,et al.  Deployment Analysis and Control of Deployable Space Antenna , 2012, AISM 2010.

[3]  Douglas C. Hofmann,et al.  Investigating bulk metallic glasses as ball-and-cone locators for spacecraft deployable structures , 2018, Aerospace Science and Technology.

[4]  Xianwen Kong,et al.  Deployable mechanisms constructed by connecting orthogonal Bricard linkages, 8R or 10R single-loop linkages using S joints , 2018 .

[5]  Baiyan He,et al.  Optimization design method for the cable network of mesh reflector antennas considering space thermal effects , 2019, Aerospace Science and Technology.

[6]  Yan Xu,et al.  Structure–electronic synthesis design of deployable truss antenna , 2013 .

[7]  Jian S. Dai,et al.  Design and kinematic analysis of a novel prism deployable mechanism , 2013 .

[8]  Qiangqiang Zhao,et al.  Analysis of angular errors of the planar multi-closed-loop deployable mechanism with link deviations and revolute joint clearances , 2019, Aerospace Science and Technology.

[9]  S. R. Mahmoud,et al.  Buckling and dynamic behavior of the simply supported CNT-RC beams using an integral-first shear deformation theory , 2020 .

[10]  Tzong-Shi Liu,et al.  A graph-theory approach to designing deployable mechanism of reflector antenna , 2013 .

[11]  J. Hedgepeth Accuracy potentials for large space antenna reflectors with passive structure , 1982 .

[12]  Jian S. Dai,et al.  Mobility and Geometric Analysis of the Hoberman Switch-Pitch Ball and Its Variant , 2010 .

[13]  Huifang Gao Design of a 1-DOF Symmetrical Deployable Coupled Mechanism , 2018 .

[14]  Cheng Wei,et al.  Analytical kinematics and trajectory planning of large scale hexagonal modular mesh deployable antenna , 2016 .

[15]  Abdelouahed Tounsi,et al.  Bending analysis of anti-symmetric cross-ply laminated plates under nonlinear thermal and mechanical loadings , 2019 .

[16]  A. Barton,et al.  A review on large deployable structures for astrophysics missions , 2010 .

[17]  Hang Shi,et al.  New Methodology of Surface Mesh Geometry Design for Deployable Mesh Reflectors , 2017 .

[18]  S. R. Mahmoud,et al.  Static analysis of laminated reinforced composite platesusing a simple first-order shear deformation theory , 2019 .

[19]  Bing Li,et al.  A large ring deployable mechanism for space satellite antenna , 2016 .

[20]  Abdelouahed Tounsi,et al.  Thermomechanical analysis of antisymmetric laminated reinforced composite plates using a new four variable trigonometric refined plate theory , 2019 .

[21]  Zongquan Deng,et al.  A Novel Surface Deployable Antenna Structure Based on Special Form of Bricard Linkages , 2012 .

[22]  Charis J. Gantes,et al.  Deployable Structures : Analysis and Design , 2001 .

[23]  Jinwei Guo,et al.  Design and analysis of a truss deployable antenna mechanism based on a 3UU-3URU unit , 2019 .

[24]  Robert Levy,et al.  Evaluation of Deployable Structures for Space Enclosures , 2001 .

[25]  A. Tounsi,et al.  A simple nth-order shear deformation theory for thermomechanical bending analysis of different configurations of FG sandwich plates , 2020 .

[26]  Zongquan Deng,et al.  Structural design and optimization of large cable–rib tension deployable antenna structure with dynamic constraint , 2018, Acta Astronautica.

[27]  Xianwen Kong,et al.  Deployable polyhedron mechanisms constructed by connecting spatial single-loop linkages of different types and/or in different sizes using S joints , 2018 .

[28]  Yanju Liu,et al.  Theoretical analysis and experiments of a space deployable truss structure , 2014 .

[29]  Xianwen Kong,et al.  A variable-DOF single-loop 7R spatial mechanism with five motion modes , 2018 .

[30]  A. Tounsi,et al.  A four variable trigonometric integral plate theory for hygro-thermo-mechanical bending analysis of AFG ceramic-metal plates resting on a two-parameter elastic foundation , 2020 .

[31]  Xilun Ding,et al.  A new family of deployable mechanisms based on the Hoekens linkage , 2014 .

[32]  Yongsheng Zhao,et al.  Type Synthesis of the Deployable Mechanisms for the Truss Antenna Using the Method of Adding Constraint Chains , 2018 .

[33]  Tao Zhang,et al.  Surface adjustment method for cable net structures considering measurement uncertainties , 2016 .

[34]  Qinchuan Li,et al.  Theory of Parallel Mechanisms , 2012 .

[35]  Duanling Li Kinematic Characteristic Analysis of Spherical Scissors Deployable Mechanisms , 2013 .

[36]  Jian S. Dai,et al.  Bifurcated configurations and their variations of an 8-bar linkage derived from an 8-kaleidocycle , 2018 .

[37]  J. E. Dyer,et al.  Deployable truss structure advanced technology , 1986 .

[38]  Jian S. Dai,et al.  Geometric Constraint of an Evolved Deployable Ball Mechanism , 2011 .

[39]  Denis Teissandier,et al.  Applying screw theory for summing sets of constraints in geometric tolerancing , 2017 .

[40]  Mohammed A. Balubaid,et al.  Free vibration investigation of FG nanoscale plate usingnonlocal two variables integral refined plate theory , 2019 .

[41]  A. Tounsi,et al.  A study on the structural behaviour of functionally graded porous plates on elastic foundation using a new quasi-3D model: Bending and free vibration analysis , 2020 .

[42]  Zongquan Deng,et al.  Modeling and analysis of a large deployable antenna structure , 2014 .