Multistable compliant mechanism and a steady-state analysis method thereof

Abstract

A multistable compliant mechanism is formed by connecting sequentially multiple basic units front to end to form a closed annular structure. Each basic unit includes two flexible hinges perpendicular to each other on different planes and two rigid connection parts for connecting the flexible hinges. The two flexible hinges are connected by a rigid connection part, and one of the flexible hinges is connected to a flexible hinge of an adjacent basic unit through the other rigid connection part. Lengths of two rigid connection parts in a same basic unit are equal, but lengths of rigid connection parts of different basic units are not necessarily equal. The multistable compliant mechanism features the continuous rotation and multi-steady state of a tri-compliant mechanism. The multistable compliant mechanism also features variable mechanism topology, an adjustable unit number, easy implementation, and promotion. A method for steady state analysis of the multistable compliant mechanism is also provided.

Claims

1. A multistable compliant mechanism comprising: multiple basic units connected sequentially front to end to form a closed annular structure; each basic unit comprising two flexible hinges perpendicular to each other on different planes, and two rigid connection parts for connecting the two flexible hinges, wherein the two flexible hinges are connected by a rigid connection part, and one of the two flexible hinges is connected to a flexible hinge of an adjacent basic unit through the other rigid connection part, wherein lengths of the two rigid connection parts in the basic unit are equal, and lengths of rigid connection parts of different basic units may be equal or not equal.

2. The multistable compliant mechanism according to claim 1, wherein the multistable compliant mechanism has four types: monostable, bistable, tristable, and quad-stable; wherein each basic unit meets size constraints according to a first formula: $\frac{{\omega }_{01}}{{\omega }_{02}}=\frac{\cos \left({\theta }_{n+1}\right)}{\cos \left({\theta }_{n-1}\right)}.Math.\left(\frac{L_{n-1}+L_n\cos \left({\theta }_n\right)}{L_n+L_{n-1}\cos \left({\theta }_n\right)}\right)$ wherein, ω.sub.01 and ω.sub.02 are input and output rotational angular velocities of the basic unit, L.sub.n−1 and L.sub.n are the lengths of the two rigid connection parts in the basic unit, θ.sub.n−1 and θ.sub.n are deflection angles of the two flexible hinges in the basic unit, θ.sub.n+1 is a joint offset angle between a next basic unit and a current basic unit; wherein to form the closed annular structure, each basic unit has a same rotational angular velocity according to the first formula, and then forms an annular structure that can be rotated stably; wherein the two adjacent hinges of each basic unit have a same angle change rules, and a kinematic relationship according to: $\{\begin{array}{c}{\theta }_1=2\arccos \left(\frac{\cos \left(\frac{\phi }{2}\right)}{\cos \left(\frac{{\theta }_2}{2}\right)}\right)\mathrm{sign}\left(\sin \left(\tau \right)\right)\\ {\theta }_2=2\arcsin \left(\sin \left(\tau \right)\sin \left(\frac{\phi }{2}\right)\right)\\ \phi =\frac{2\pi }{n}\end{array}$ wherein, θ.sub.1 and θ.sub.2 are the deflection angles of the two flexible hinges of the basic unit, τ is a rotational angle of the multistable compliant mechanism relative to an initial position, n is a number of basic units of the multistable compliant mechanism, and φ is a constant related to n; wherein steady-state positions of the multistable compliant mechanism are located at points where a potential energy of the multistable compliant mechanism is minimum according to: $\{\begin{array}{c}U=n\left(K_1.Math.\frac{{\left({\theta }_1-{\theta }_{01}\right)}^2}{2}+K_2.Math.\frac{{\left({\theta }_2-{\theta }_{02}\right)}^2}{2}\right);\\ U_r=\frac{U}{n};\\ r=\frac{K_2}{K_1};\\ f_1=\frac{{\theta }_1-{\theta }_{01}}{\tan \left({\theta }_1\right)};\\ f_2=\frac{{\theta }_2-{\theta }_{02}}{\tan \left({\theta }_2\right)};\\ \frac{{\mathrm{dU}}_r}{d\tau }=K_1.Math.\frac{d{\theta }_1}{d\tau }.Math.\tan \left({\theta }_1\right).Math.\left(f_1-r.Math.f_2\right);\\ \frac{d^2{U}_r}{d{\tau }^2}=0;\\ \frac{{\mathrm{dU}}_r}{d\tau }>0;\end{array}$ wherein, U is an overall strain energy of the multistable compliant mechanism, U.sub.r is a total strain energy of the basic unit, K.sub.1 and K.sub.2 are respectively stiffness of the two flexible hinges of the basic unit, θ.sub.1 and θ.sub.2 are respectively the deflection angles of the two flexibility hinges of the basic unit, θ.sub.01 and θ.sub.02 are zero offset angles of the two flexible hinges of the basic unit, r represents a ratio of stiffness coefficients of the two flexible hinges of the basic unit, ƒ.sub.1 and ƒ.sub.2 are respectively related to θ.sub.01, θ.sub.1 and θ.sub.02, θ.sub.2, and are used to analyze a steady-state transition function of the multistable compliant mechanism; wherein a plane formed by parameters θ.sub.01 and θ.sub.02 can be divided into a monostable area, a bistable area, a tri-stable area, and a quad-stable area according to a number of steady-states represented by the multistable compliant mechanism, and a parameterized formula of a boundary-curve: $\{\begin{array}{c}{\theta }_{01}={\theta }_1-\frac{{\theta }_2^{\prime }.Math.\left({\theta }_1^{{\prime }_2}+r.Math.{\theta }_2^{{\prime }_2}\right)}{{\theta }_1^{\prime }.Math.{\theta }_2^{″}-{\theta }_2^{\prime }.Math.{\theta }_1^{″}};\\ {\theta }_{02}={\theta }_2-\frac{{\theta }_1^{\prime }.Math.\left({\theta }_1^{{\prime }_2}+r.Math.{\theta }_2^{{\prime }_2}\right)}{r.Math.\left({\theta }_2^{\prime }.Math.{\theta }_1^{″}-{\theta }_1^{\prime }.Math.{\theta }_2^{″}\right)};\\ {\theta }_i^{\prime }=\frac{d{\theta }_i}{d\tau },i=1,2;\\ {\theta }_i^{″}=\frac{d^2{\theta }_i}{d{\tau }^2},i=1,2;\end{array}$ wherein θ′.sub.1 and θ″.sub.1 are respectively a first derivative and a second derivative of θ.sub.1 with respect to the rotational angle τ, θ′.sub.2 and θ″.sub.2 are respectively a first derivative and a second derivative of θ.sub.2 with respect to the rotational angle τ; along a direction of a curve, a number of tangents passing through coordinate point (θ.sub.01, θ.sub.02) corresponding to specific values of multistable compliant mechanism parameters θ.sub.01 and θ.sub.02 is the number of steady-states of the multistable compliant mechanism; and an intersection of the number of tangents and a kinematic relationship curve formed by θ.sub.01 and θ.sub.02 is a steady-state position of the multistable compliant mechanism.

3. The multistable compliant mechanism according to claim 1, wherein the two flexible hinges are spring hinges, straight beam flexible hinges or notch flexible hinges.

4. The multistable compliant mechanism according to claim 1, wherein the two rigid connection parts are connecting rods.

5. A steady-state analysis method for the multistable compliant mechanism according to claim 1, comprising the following steps: 1) determining a number n of basic units, wherein a basic shape and a basic size of each basic unit can vary, but corresponding rigidity coefficients of the two flexible hinges of the basic unit perpendicular to each other on different planes are the same; 2) determining a type of the two flexible hinges of the basic unit, and according to the determined type of the two flexible hinges, combining relevant theory of compliant mechanism to determine stiffness K.sub.1, K.sub.2 and stiffness coefficient ratio r; 3) determining zero offset angles θ.sub.01 and θ.sub.02 of the two flexible hinges of the basic unit of the multistable compliant mechanism, according to: $\{\begin{array}{c}r=\frac{K_2}{K_1};\\ f_1=\frac{{\theta }_1-{\theta }_{01}}{\tan \left({\theta }_1\right)};\\ f_2=\frac{{\theta }_2-{\theta }_{02}}{\tan \left({\theta }_2\right)};\end{array}$ wherein θ.sub.01 and θ.sub.02 are deflection angles of the two flexible hinges of the basic unit, and f1 and f2 are respectively related to θ.sub.01, θ.sub.01 and θ.sub.02, θ.sub.02; 4) drawing a plot of ƒ.sub.1/ƒ.sub.2, and find all intersection points with the stiffness coefficient ratio r of the flexible hinges of the basic unit, wherein, when an intersection point cannot be found or the plot of ƒ.sub.1/ƒ.sub.2 cannot be drawn, then directly go to step 6); 5) finding a steady-state point of the multistable compliant mechanism according to a numerical sign of expression: $K_1.Math.\frac{d{\theta }_1}{d\tau }.Math.\tan \left({\theta }_1\right)$ wherein, when the numerical sign of the expression is positive, the steady-state point appears at a point where ƒ.sub.1/ƒ.sub.2 crosses r positively from bottom to top; and when the numerical sign of the expression is negative, the steady-state point appears at a point where ƒ.sub.1/ƒ.sub.2 crosses r negatively from top to bottom; wherein after the steady state point is determined, when there is only one steady-state point, the multistable compliant mechanism is a monostable mechanism; when there are two steady-state points, the multistable compliant mechanism is a bistable mechanism; when there are three steady-state points, the multistable compliant mechanism is a tri-stable mechanism; when there are four steady-state points, the multistable compliant mechanism is a quad-stable mechanism; wherein a rotational angle τ corresponds to a steady-state point of the multistable compliant mechanism; 6) drawing an image according to parameterized formulas of a steady-state area boundary curve: $\{\begin{array}{c}{\theta }_{01}={\theta }_1-\frac{{\theta }_2^{\prime }.Math.\left({\theta }_1^{{\prime }_2}+r.Math.{\theta }_2^{{\prime }_2}\right)}{{\theta }_1^{\prime }.Math.{\theta }_2^{″}-{\theta }_2^{\prime }.Math.{\theta }_1^{″}};\\ {\theta }_{02}={\theta }_2-\frac{{\theta }_1^{\prime }.Math.\left({\theta }_1^{{\prime }_2}+r.Math.{\theta }_2^{{\prime }_2}\right)}{r.Math.\left({\theta }_2^{\prime }.Math.{\theta }_1^{″}-{\theta }_1^{\prime }.Math.{\theta }_2^{″}\right)};\\ {\theta }_i^{\prime }=\frac{d{\theta }_i}{d\tau },\left(i=1,2\right);\\ {\theta }_i^{″}=\frac{d^2{\theta }_i}{d{\tau }^2},\left(i=1,2\right);\end{array}$ determining a position of a point (θ.sub.01, θ.sub.02) corresponding to the zero offset angles θ.sub.01 and θ.sub.02 of the flexible hinges of actual basic units, and determining a steady-state area; determining a number of the steady-state, when the point locates in the monostable area, the multistable compliant mechanism is the monostable mechanism; when the point locates in a bi-stable area, the multistable compliant mechanism is the bistable mechanism; when the point locates in a tri-stable area, the multistable compliant mechanism is the tri-stable mechanism; when the point locates in a quad-stable area, the multistable compliant mechanism is the quad-stable mechanism; finding tangents of the boundary curve of the steady-state area passing through the point (θ.sub.01, θ.sub.02), and finding intersection points of the tangents and kinematics relationship curves of θ.sub.1 and θ.sub.2, the intersection points are the steady-state points of the multistable compliant mechanism; and finally, finding a steady-state position corresponding to the steady-state point of the multistable compliant mechanism according to: $\{\begin{array}{c}{\theta }_1=2\arccos \left(\frac{\cos \left(\frac{\phi }{2}\right)}{\cos \left(\frac{{\theta }_2}{2}\right)}\right)\mathrm{sign}\left(\sin \left(\tau \right)\right)\\ {\theta }_2=2\arcsin \left(\sin \left(\tau \right)\sin \left(\frac{\phi }{2}\right)\right)\\ \phi =\frac{2\pi }{n}\end{array}$ wherein φ is a constant related to n.

Description

BRIEF DESCRIPTION OF FIGURES

(1) FIG. 1 is a diagram of the topology of the multistable compliant mechanism of the present invention.

(2) FIG. 2 is a diagram of the kinematic relationship of the multistable compliant mechanism of the present invention.

(3) FIG. 3 is a diagram of the analysis of the number of steady states and the position of the steady state when the number and the individual zero offset angles of the basic units of the present invention are known.

(4) FIG. 4 is a diagram of the analysis of the number of steady states in the case where the number of the basic units and the stiffness ratio of basic units of the present invention are known.

(5) FIG. 5 is a diagram of the analysis of the steady-state position when the number of the basic units and the stiffness ratio of basic units of the present invention are known.

(6) FIG. 6 is a diagram of a hinge of a specific embodiment of the present invention.

(7) FIG. 7 is an overall diagram of a specific embodiment of the present invention.

DESCRIPTION

(8) The present invention will be further described below with reference to specific embodiments.

(9) As shown in FIG. 1, a multistable compliant mechanism provided in this embodiment is formed by connecting sequentially multiple basic units front to end to form a closed annular structure 1; the basic unit 101 comprises two flexible hinges 102, 103 perpendicular to each other on different planes, and two rigid connection parts 104, 105 (specifically, connecting rods) for connecting the flexible hinges; the flexible hinges 102, 103 have no specific structural limitations. The flexible hinges can be ordinary spring hinges, straight beam flexible hinges or notch flexible hinges etc., and can also be special flexible hinges designed through the relevant theory of the compliant mechanism; the rigidity of the flexible hinge 102 of each basic unit is the same, and the rigidity of the flexible hinge 103 is also the same. The lengths of the rigid parts 104, 105 connecting the two flexible hinges in the same basic unit must be equal, but the lengths of the rigid connecting parts of different basic units can be different; the input and output angular velocities of each basic unit (such as 106, 107 shown in the figure) meet the following size constraints:

(10) 0$\frac{{\omega }_{01}}{{\omega }_{02}}=\frac{\cos \left({\theta }_{n+1}\right)}{\cos \left({\theta }_{n-1}\right)}.Math.\left(\frac{L_{n-1}+L_n\cos \left({\theta }_n\right)}{L_n+L_{n-1}\cos \left({\theta }_n\right)}\right)$

(11) The number of basic units shown in the figure is 8. The mechanism can also form a variety of configurations by connecting basic units 101 to connecting rod of different sizes, thereby adapting to different working conditions.

(12) As shown in FIG. 2, the motion form of the multi-stable compliant mechanism is a rotating motion (as shown in FIG. 2), in which the angle 203 between the rotation axis 201 of the flexible hinge and the central axis of the conical surface 202 where other related hinge axes are located is defined as the rotational angle. When the axes of 201 and 203 are parallel, the two axes do not intersect, the rotational angle at this time is defined as 0 degrees or 180 degrees. The mechanism of the present invention is within the force constraint range. The mechanism movement exhibits underactuated performance, and the rotational angle and the deflection angles θ.sub.1 (204 as shown in the figure), θ.sub.2 (205 shown in the figure) of the flexible hinges of each unit are related to the multi-deformed inner angle φ (206 shown in the figure) formed by all the basic units, and their relationship expression is:

(13) $\{\begin{array}{c}{\theta }_1=2\arccos \left(\frac{\cos \left(\frac{\phi }{2}\right)}{\cos \left(\frac{{\theta }_2}{2}\right)}\right)\mathrm{sign}\left(\sin \left(\tau \right)\right)\\ {\theta }_2=2\arcsin \left(\sin \left(\tau \right)\sin \left(\frac{\phi }{2}\right)\right)\\ \phi =\frac{2\pi }{n}\end{array}$

(14) The mechanism of the present invention will have 1 to 4 steady states during a cycle of rotating, and the rotational angles corresponding to these steady states positions are the steady states positions.

(15) As shown in FIG. 3, under the condition that the number n of basic units and the respective zero offset angles θ.sub.01 and θ.sub.02 are known, the steady state number and steady state position of the mechanism according to the present invention mainly depend on the following formula:

(16) $\{\begin{array}{c}r=\frac{K_2}{K_1};\\ f_1=\frac{{\theta }_1-{\theta }_{01}}{\tan \left({\theta }_1\right)};\\ f_2=\frac{{\theta }_2-{\theta }_{02}}{\tan \left({\theta }_2\right)};\\ \frac{{\mathrm{dU}}_r}{d\tau }=K_1.Math.\frac{d{\theta }_1}{d\tau }.Math.\tan \left({\theta }_1\right).Math.\left(f_1-r.Math.f_2\right);\\ r-\frac{f_1}{f_2}=0;\end{array}$

(17) In the figure, the mechanism is described in detail with regard to the specific conditions of the number of basic units n=4, zero offset θ.sub.01=0.005π, θ.sub.01=0.01π. By analyzing the intersection point 302 of the stiffness ratio r=3 and the curve ƒ.sub.1/ƒ.sub.2 (301 shown in the figure), all the stagnation points of the potential energy function of the mechanism can be obtained. Combining the product sign of the three of dθ.sub.1/dτ and θ.sub.1 (303 shown in the figure) and ƒ.sub.2, the steady-state number and steady-state position of the mechanism can be determined from all stagnation points of the potential energy function: (1) If the sign of the product of the (dθ.sub.1/dτ, θ.sub.1, and ƒ.sub.2) is positive, the positive crossing point of curve 301 and straight line 3 from bottom to top is the steady-state position of the mechanism; (2) If the sign of the product of the (dθ.sub.1/dτ, θ.sub.1, and ƒ.sub.2) is negative, the negative crossing point of curve 301 and straight line 3 from top to bottom is the steady-state position of the mechanism.

(18) As shown in FIG. 4, when fixing the number of basic units n and the stiffness ratio r, by determining or changing the zero offsets θ.sub.01 and θ.sub.02 of the base unit, the steady state number and steady state positions of the mechanism described in the present invention can be intuitively analyzed and controlled.

(19) The plane formed by the parameters θ.sub.01 and θ.sub.02 can be divided into a monostable area 401, a bistable area 402, a tri-stable area 403, and a quad-stable area 404 according to the number of steady states exhibited by the mechanism. The parameterized formula of the boundary curve 405 dividing these areas is:

(20) $\{\begin{array}{c}{\theta }_{01}={\theta }_1-\frac{{\theta }_2^{\prime }.Math.\left({\theta }_1^{{\prime }_2}+r.Math.{\theta }_2^{{\prime }_2}\right)}{{\theta }_1^{\prime }.Math.{\theta }_2^{″}-{\theta }_2^{\prime }.Math.{\theta }_1^{″}};\\ {\theta }_{02}={\theta }_2-\frac{{\theta }_1^{\prime }.Math.\left({\theta }_1^{{\prime }_2}+r.Math.{\theta }_2^{{\prime }_2}\right)}{r.Math.\left({\theta }_2^{\prime }.Math.{\theta }_1^{″}-{\theta }_1^{\prime }.Math.{\theta }_2^{″}\right)};\\ {\theta }_i^{\prime }=\frac{d{\theta }_i}{d\tau },\left(i=1,2\right);\\ {\theta }_i^{″}=\frac{d^2{\theta }_i}{d{\tau }^2},\left(i=1,2\right);\end{array}$

(21) The specific parameters of the mechanism analyzed in the figure are as follows: n=4, r=1. For a set of determined θ.sub.01 and θ.sub.02, the point (θ.sub.01, θ.sub.02) locates in the steady-state area in the figure, and the mechanism using these parameters behaves as a responsive steady state. Taking the specific point 406 in the figure as an example, if the mechanism of the present invention adopts the parameters at this point, the mechanism will behave in a quad-stable performance.

(22) As shown in FIG. 5, when the number n of basic units and the stiffness ratio r are fixed, and after the steady-state number of the mechanism of the present invention is determined by the steady-state distribution diagrams of θ.sub.01 and θ.sub.02, then the steady-state position of the mechanism can be determined through the tangent aspect of the curve. Taking point 501 in the figure as an example, according to the curve direction 502, there are two tangents 503, 504. The intersection points 506, 507 of the curve and the kinematic relationship curve 505 formed by θ.sub.1 and θ.sub.2 are the steady-state positions of the mechanism. The steady state positions uniquely correspond to rotational angle τ. θ.sub.1 and θ.sub.2 at the intersections can be used to solve the specific rotational angle according to the following formula:

(23) $\{\begin{array}{c}{\theta }_1=2\arccos \left(\frac{\cos \left(\frac{\phi }{2}\right)}{\cos \left(\frac{{\theta }_2}{2}\right)}\right)\mathrm{sign}\left(\sin \left(\tau \right)\right)\\ {\theta }_2=2\arcsin \left(\sin \left(\tau \right)\sin \left(\frac{\phi }{2}\right)\right)\\ \phi =\frac{2\pi }{n}\end{array}$

(24) Referring to FIG. 6, the present invention can directly use straight beam flexible hinges to realize corresponding functions. The straight beam type flexible hinge is a thin sheet 6 with a rectangular cross section, wherein the length L (601 shown in the figure), the width b (602 shown in the figure), and the thickness h (603 in the figure) of the straight beam type flexible hinge and the Young's modulus E of the material can be used to change the stiffness of the flexible hinges according to the following formula:

(25) $\{\begin{array}{c}{K}_i=\frac{\mathrm{EI}}{L},\left(i=1,2\right);\\ I=\frac{{\mathrm{bh}}^3}{12};\end{array}$

(26) The zero offset angle of the hinge can be formed by bending the initial shape of the straight beam type flexible hinge into a circular arc, and the angle 604 of the circular arc is the zero offset angle θ.sub.01 θ.sub.02 of the hinge.

(27) Referring to FIG. 7, it is a specific structure 7 of the present invention using straight beam flexible hinges, which includes a straight beam flexible hinge 701 that are straightly distributed and perpendicular to each other on different planes, a fixing structure 702 connecting two adjacent hinges, and driving torque input and output terminals 703, 704. The structure can be used directly in the design of climbing rod robot, pipeline robot, tunnel robot, etc. Its multi-steady state manner can greatly improve the reliability of movement.

(28) The following is a steady-state analysis method of the above multistable compliant mechanism of this embodiment, comprises the following steps: 1) determining a number n of basic units, a basic shape and a basic size of each basic unit can vary, but corresponding stiffness of its flexible hinges that perpendicular to each other on different planes must be the same; 2) determining a type of flexible hinges of a basic unit, and according to the determined type of flexible hinges, combining relevant theory of compliant mechanism to determine its stiffness K.sub.1, K.sub.2 and the ratio r between them, if the selected flexible hinges are straight beam flexible hinges, their stiffness is obtained according to the following formula:

(29) $\{\begin{array}{c}{K}_i=\frac{\mathrm{EI}}{L},\left(i=1,2\right);\\ I=\frac{{\mathrm{bh}}^3}{12};\end{array}$
where E is the Young's modulus of the material of the straight beam type flexible hinges, b and h are respectively the cross-sectional width and thickness of a straight beam flexible hinge, and I is the cross-sectional moment of inertia of a straight beam flexible hinge; 3) determining zero offset angles θ.sub.01 and θ.sub.02 of the flexible hinges of the basic unit of the mechanism, according to the following formula:

(30) $\{\begin{array}{c}r=\frac{K_2}{K_1};\\ f_1=\frac{{\theta }_1-{\theta }_{01}}{\tan \left({\theta }_1\right)};\\ f_2=\frac{{\theta }_2-{\theta }_{02}}{\tan \left({\theta }_2\right)};\end{array}$ 4) drawing curves of the term ƒ.sub.1/ƒ.sub.2, and find an intersection point of it with the stiffness coefficient ratio r of the flexible hinges of the basic unit, if intersection point cannot be found or the curves of ƒ.sub.1/ƒ.sub.2 cannot be obtained, then directly go to step 6); 5) finding a steady-state point of the mechanism according to a numerical sign of the following expression:

(31) $K_1.Math.\frac{d{\theta }_1}{d\tau }.Math.\tan \left({\theta }_1\right)$
if it is positive, the steady-state point appears at a point where the function ƒ.sub.1/ƒ.sub.2 crosses r positively from bottom to top; if it is negative, the steady-state point appears at a point where the function ƒ.sub.1/ƒ.sub.2 crosses r negatively from top to bottom; after the steady state point is determined, if there is only one steady-state point, the mechanism is a monostable mechanism; if there are two steady-state points, the mechanism is a bistable mechanism; if there are three steady-state points, the mechanism is a tri-stable mechanism; if there are four steady-state points, the mechanism is a quad-stable mechanism; wherein the rotational angle τ corresponds to a steady-state point above is a steady-state position of the mechanism; 6) drawing a plot according to the parameterized formula of a steady-state area boundary curve of the following formula:

(32) $\{\begin{array}{c}{\theta }_{01}={\theta }_1-\frac{{\theta }_2^{\prime }.Math.\left({\theta }_1^{{\prime }_2}+r.Math.{\theta }_2^{{\prime }_2}\right)}{{\theta }_1^{\prime }.Math.{\theta }_2^{″}-{\theta }_2^{\prime }.Math.{\theta }_1^{″}};\\ {\theta }_{02}={\theta }_2-\frac{{\theta }_1^{\prime }.Math.\left({\theta }_1^{{\prime }_2}+r.Math.{\theta }_2^{{\prime }_2}\right)}{r.Math.\left({\theta }_2^{\prime }.Math.{\theta }_1^{″}-{\theta }_1^{\prime }.Math.{\theta }_2^{″}\right)};\\ {\theta }_i^{\prime }=\frac{d{\theta }_i}{d\tau },\left(i=1,2\right);\\ {\theta }_i^{″}=\frac{d^2{\theta }_i}{d{\tau }^2},\left(i=1,2\right);\end{array}$
determining a position of the point (θ.sub.01, θ.sub.02) corresponding to the zero offset angles θ.sub.01 and θ.sub.02 of the flexible hinges of actual basic units, and determining a steady-state area where it falls, then determining a number of its steady-state, if the point locates in the monostable area, the mechanism is a monostable mechanism; if the point locates in a bistable area, the mechanism is a bistable mechanism; if the point locates in a tri-stable area, the mechanism is a tri-stable mechanism; if the point locates in a quad-stable area, the mechanism is a quad-stable mechanism; finding tangents of the boundary curve of the steady-state area passing through the point (θ.sub.01, θ.sub.02), and finding intersection points of these tangents and kinematics curves of θ.sub.1 and θ.sub.2, these intersection points are the steady-state points of the mechanism;

(33) 0$\{\begin{array}{c}{\theta }_1=2\arccos \left(\frac{\cos \left(\frac{\phi }{2}\right)}{\cos \left(\frac{{\theta }_2}{2}\right)}\right)\mathrm{sign}\left(\sin \left(\tau \right)\right)\\ {\theta }_2=2\arcsin \left(\sin \left(\tau \right)\sin \left(\frac{\phi }{2}\right)\right)\\ \phi =\frac{2\pi }{n}\end{array}$
finally, finding a steady-state position corresponding to a steady-state point of the mechanism according to the above formula.

(34) It can be seen from FIGS. 1 and 2 that the present invention belongs to a type of centralized flexible hinges. Although the movement relationship is similar to the corresponding rigid mechanism, the multistable compliant mechanism provided by the present invention has a force constraint caused by the elastic deformation of the flexible hinge. Even with multiple degrees of freedom in the mechanism, a single r can still be used to achieve continuous rotational motion. Since the flexible hinge has no specific structural limitations, the number of basic units and the shape of the basic unit are variable, the present invention can adapt to different working conditions and has strong potential application value.

(35) It can be seen from FIGS. 3 to 5, the steady-state manner of the present invention is related to the stiffness, the ratio of the stiffness, the respective zero offset angles of two adjacent flexible hinges of the basic unit, and the number of their units. The steady-state performance analysis method of the multistable compliant mechanism of the present invention is simple and intuitive. Not only can it analyze the steady-state performance of known mechanisms, but also can design and control the number of steady-state and positions of steady-state of the multi-stable compliant mechanism.

(36) It can be seen from FIGS. 6 to 7 that the present invention can be implemented using a common compliant hinge. It has a lower design threshold and is more practical.

(37) The invention inherits the characteristics of the continuous rotation and multi-steady state of the existing three fold kaleidocycles compliant mechanism, and has the advantages of variable mechanism topology, measurable, controllable and adjustable steady state manner etc. Therefore, it can be directly applied to the posture maintaining devices such as solar panels, solar sails, antennas, new blood vessel supports, etc. and can also be used in the design of rod climbing robots, pipeline robots, tunnel robots, and metamorphic robots, and has huge potential application value.

(38) In summary, the present invention can effectively complete the functions of continuous rotation and multistability etc. of the compliant mechanism, and the topology of the mechanism is variable. The steady-state performance and the steady-state position are measurable, controllable, and adjustable, particularly suitable for complex working conditions. Therefore, compared with the prior art, the present invention is a new multistable compliant mechanism with simple structure, reliable motion and simple use, which is worthy of promotion.

(39) The above-mentioned embodiments are only preferred embodiments of the present invention, and are not intended to limit the scope of the present invention. Therefore, any changes made according to the shape and principle of the present invention should be included in the protection scope of the present invention.