CN112733265A - Design calculation and optimization method for electric vehicle power assembly suspension system - Google Patents
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Abstract
The invention discloses a design calculation and optimization method of an electric automobile power assembly suspension system, which comprises the following steps: firstly, establishing a power assembly mass center coordinate system, and acquiring parameters such as an inertia parameter, a mass center position, a mounting position of a rubber suspension, a static stiffness curve and the like of the power assembly on the basis; further establishing a dynamic model of the power assembly suspension system, and deriving a motion differential equation; establishing a target function according to an energy decoupling theory and transient response characteristics; the method is characterized by comprising the steps of selecting the purposes that the suspension system is highest in energy decoupling rate, the power assembly mass center longitudinal acceleration under transient response and the impact amplitude are minimum, taking the suspension linear section rigidity as a design variable, reasonably distributing natural frequency and changing range of the suspension rigidity as constraint conditions, optimizing by adopting a multi-island genetic algorithm, and finally verifying the feasibility of the method through an example.
Description
Technical Field
The invention belongs to the field of optimization design of an automobile power assembly suspension system, and particularly relates to a design calculation and optimization method of an electric automobile power assembly suspension system.
Background
The power assembly serves as a main excitation source of the automobile, and vibration generated by the power assembly is transmitted to the auxiliary frame through the suspension system and then transmitted to the automobile body, so that vibration of the automobile body is caused. The suspension system with good performance can not only reduce the vibration transmitted to the frame by the power assembly and improve the riding comfort, but also can better prolong the service life of the power assembly and other parts, so the design of the suspension system becomes more important. Different from the traditional fuel vehicle, the electric vehicle driving motor has the advantages of quick output response and large output torque. The output torque of the driving motor can rise to hundreds of Nm within a few milliseconds usually, and the driving motor has a relatively obvious impact characteristic, which puts new requirements on the design of an electric automobile suspension system.
In the current research on the suspension system of the power assembly, reasonable distribution of natural frequency of each order and maximum energy decoupling rate are generally optimized. The vibration isolation performance of the system under a specific working condition is neglected to a certain extent by purely considering the inherent characteristics of the power assembly suspension system. Particularly in the suspension system of the electric automobile, the excitation of the electric drive assembly has a relatively obvious impact characteristic, and if only the inherent characteristics of the suspension system of the power assembly are considered, the influence of the transient impact on the system cannot be evaluated. At present, no patent of invention relating to the aspect of the optimization design of the suspension system of the electric automobile under the impact working condition exists.
In a chinese granted patent "a design optimization method and optimization device of a powertrain suspension system" (CN102609551B), "the constructed powertrain suspension system model is a six-degree-of-freedom model, and the influence of a subframe widely used in an existing automobile on system vibration is not considered, and only the intrinsic characteristics of the powertrain suspension system are analyzed and optimized, that is, only static optimization is performed, and transient operating conditions frequently occurring in an electric automobile are not analyzed, so that the defect of such treatment is that the intrinsic characteristics may reach the optimization target, but the problem of poor vibration still exists in the actual operating conditions.
Disclosure of Invention
In order to solve the problems in the prior art, the invention provides a design calculation and optimization method of an electric automobile power assembly suspension system, which introduces two indexes of shock degree and longitudinal acceleration while considering the natural frequency and the energy decoupling rate of the power assembly suspension system, fully considers the natural characteristic and the transient response of the system, takes the reasonable distribution of the natural frequency, the highest energy decoupling rate and the optimal transient response index as optimization targets, and provides guidance for the design research and development of the electric automobile power assembly suspension system.
The object of the invention is achieved by at least one of the following solutions.
A design calculation and optimization method for an electric automobile power assembly suspension system comprises the following steps:
(1) establishing a reference coordinate system and acquiring inertia parameters of the power assembly and the auxiliary frame;
(2) acquiring the mounting position and the mounting angle of the suspension;
(3) establishing an undamped motion differential equation of the power assembly suspension system;
(4) establishing a parameterized dynamic model of the powertrain suspension system, calculating the mass center longitudinal acceleration and the impact degree of the powertrain by taking a step function as excitation, and taking the suspension rigidity and the installation position as model input parameters, wherein the mass center longitudinal acceleration (A)x) And the degree of impact (J) as output of the model;
(5) the method comprises the steps of establishing an optimization model by taking the linear section rigidity of a suspension as a design variable, the natural frequency of a power assembly as a constraint condition, the maximum energy decoupling rate of the power assembly and the minimum mass center longitudinal acceleration and impact amplitude of the power assembly under an impact working condition as optimization targets, and obtaining the design rigidity of the suspension according to the optimization model.
Further, the establishing of the reference coordinate system and the obtaining of the inertia parameters of the powertrain in the step (1) specifically includes: obtaining the mass m of the power assembly, establishing a fixed coordinate system O-XYZ by taking the centroid position O of the power assembly as a coordinate origin, wherein the Y axis is parallel to the output axis of the motor, the forward direction points to the free end of the output shaft of the motor, the forward direction of the Z axis is vertical upward, and the X axis is determined by a right-hand rule; obtaining the rotational inertia I of the power assembly to the X axis, the Y axis and the Z axis respectivelyxx、Iyy、IzzObtaining the inertia product I of the power assembly to the X axis and the Y axisxyProduct of inertia for Y-axis and Z-axis IyzAnd product of inertia I to X-axis and Z-axisxz。
Further, the mounting position in step (2) is defined as the intersection point of the elastic main axes of the suspension, and the mounting position of the ith suspension can be expressed as [ a ]xi ayi azi]。
Further, the undamped motion differential equation established in the step (3) is as follows:
wherein the mass matrix M is:
the stiffness matrix K is:
wherein:
Kgi=RKsiRT
the matrix R is a cosine matrix between the local coordinate system of the suspension and the coordinate system of the center of mass of the power assembly, and the value of the matrix R is determined by the installation angle of the suspension;
in the differential equation of motion, q ═ wx wy wz θx θy θz]TIs a power assembly mass center displacement vector,is an acceleration vector.
Further, in the step (4), when the parameterized dynamic model of the powertrain suspension system is established, rigid body models are adopted for both the electric drive assembly and the auxiliary frame.
Further, the stiffness of the suspension in the step (4) refers to the static stiffness of the elastic main shaft under the local coordinate system of the suspension: k is a radical ofui、kvi、kwiThe static stiffness of the suspension in the three elastic main shaft directions under the local coordinate system of the suspension, namely the static stiffness in the three directions of u, v and w, is respectively, the local coordinate system of the suspension is a coordinate system established by taking the elastic center of the suspension as the origin of coordinates and taking the three elastic main shafts as coordinate axes, and the static stiffness matrix form of the ith suspension can be expressed as follows: ksi=diag([kui kvikwi])。
Further, the calculation method of the impact degree in the step (4) is as follows:
wherein, aβThe angular acceleration of the powertrain about the Y-axis.
Further, in the step (5), establishing an objective function with the maximum energy decoupling rate of the powertrain as follows:
in the center of mass coordinate of the power assembly according to the mass matrix M and the rigidity matrixK is solved to obtain six-order natural frequency omega of power assembly suspension systemj(j 1, 2.... 6) and the mode shape matrix Φ, then the energy distribution of the system in each order of primary vibration can be obtained, and when the system is in the j (j 1, 2.. 6) th order of primary vibration, the maximum kinetic energy is:
the expansion is as follows:
then, the energy ratio of the k (k ═ 1, 2.., 6) th generalized coordinate at the j-th order primary vibration is:
energy distribution of the power assembly in six main vibration directions can be obtained through the formula;
if ejMax E (k, j), k 1,2,3.. 6, then EjFor the decoupling rate of the power assembly in a certain vibration direction, the optimization target is as follows: by varying the stiffness of the suspension so that ejAs close to 1 as possible if the constraint is satisfied.
Further, because the influence degree of vibration in each direction on the NVH performance of the whole vehicle is different, if the decoupling degree around the Y axis and in the vertical direction is the highest, a six-dimensional weight vector b ═ b is introduced for the purpose1 b2 b3 b4 b5 b6]To indicate the importance of the energy decoupling rate in each direction.
Further, in the step (5), the maximum energy decoupling rate of the power assembly and the minimum mass center longitudinal acceleration and impact amplitude of the power assembly under the impact working condition are set as optimization targets, and the established optimization model is as follows:
min f2=max(Ax)
min f3=max(J)
s.t.
kuil≤kui≤kuiu;
kvil≤kvi≤kviu;
kwil≤kwi≤kwiu;
ωj-ωj+1≤-1,(j=1,2,...,6);
5-ω1≤0;
ω6-40≤0;
90-e5≤0.
compared with the prior art, the invention at least has the following technical effects:
1) the design calculation and optimization method fully considers the inherent characteristics and transient response characteristics of the suspension system, takes the characteristics as an optimization target, establishes an optimization model for optimization, and gives consideration to both static and dynamic optimization effects;
2) the method simultaneously considers the static characteristic and the dynamic characteristic of the power assembly suspension system, can ensure that the natural frequency of the power assembly is reasonably distributed and has higher decoupling rate, and can also ensure that the power assembly has better vibration isolation effect under the transient impact working condition.
3) The method can predict the vibration characteristic and the optimization space of the suspension system in the initial stage of the design of the suspension system, can quickly and efficiently obtain an optimization scheme by modifying the relevant parameters of the suspension system, shortens the early-stage research and development period of the suspension system, reduces the research and development cost of enterprises, and has important engineering significance for ensuring the overall performance of the suspension system.
Drawings
FIG. 1 is a flow chart of a design calculation method for an electric vehicle powertrain suspension system.
FIG. 2 is a powertrain suspension system dynamics model.
Fig. 3 is a graph of the excitation torque applied in the simulation, which acts on the center of mass of the powertrain, the torque direction being positive about the Y-axis of the reference frame.
FIG. 4 is a comparison of transient responses for longitudinal acceleration of the powertrain centroid before and after optimization.
FIG. 5 is a comparison of transient responses for optimizing front and rear powertrain jerk.
Detailed Description
The invention is described in further detail below by way of an example with reference to the accompanying drawings.
The design calculation and optimization method for the suspension system of the power assembly of the electric automobile provided by the embodiment comprises the following steps:
(1) a center of mass coordinate system as shown in the dynamic model of the powertrain suspension system of fig. 2 is established. The center of mass position of the power assembly is a coordinate origin O, a fixed coordinate system O-XYZ is established by taking the O as the origin, the Y axis is parallel to the axis of the motor output shaft, the forward direction points to the free end of the motor output shaft, the forward direction of the Z axis is vertical upward, and the X axis is determined by the right-hand rule. Utilize three-wire pendulum inertial parameter measurement test bench to measure power assembly and respectively to X axle, Y axle, inertia I of Z axlexx、Iyy、IzzObtaining the inertia product I of the power assembly to the X axis and the Y axisxyProduct of inertia for Y-axis and Z-axis IyzAnd product of inertia I to X-axis and Z-axisxz. And simultaneously measuring the mass m of the power assembly. And obtaining inertia parameters of the subframe for subsequent dynamic simulation.
(2) And acquiring the installation position and the installation angle of the suspension. The mounting position of the suspension is defined as the intersection point of the elastic main shafts of the suspension, and the mounting position of the ith suspension is expressed as [ a ]xi ayi azi]。axi、ayi、aziRespectively, representing the coordinates of the mounting position of the suspension in the reference frame, i.e. the position of the elastic centre point of the suspension in the reference frame.
TABLE 1 Angle between the suspended elastic spindle and the reference coordinate axis
In the table, u, v and w are three elastic main shafts for suspension; alpha is alphaui、αvi、αwiRespectively representing the included angles beta between the u axis, the v axis and the w axis of the ith suspension and the X axis of the reference coordinate systemui、βvi、βwiRespectively representing the included angles between the u, v and w axes of the ith suspension and the Y axis of the reference coordinate system, gammaui、γvi、γwiRespectively representing the included angles between the u, v and w axes of the ith suspension and the Z axis of the reference coordinate system.
(3) According to the reference coordinate system established in the step (1) and the related parameters obtained in the step (2), the undamped motion differential equation of the power assembly suspension system can be derived as follows:
wherein the quality matrix is:
the stiffness matrix is:
in the above formula, the first and second carbon atoms are,
Kgi=RKsiRT
the matrix R is a cosine matrix between the suspension local coordinate system and the powertrain centroid coordinate system, and can be obtained from the data in table 3.
F (t) represents the acting force of the power assembly and is a vector of 6 multiplied by 1; ksiRepresenting the stiffness of the ith suspension in its local coordinate system; kgiRepresenting a stiffness matrix of the ith suspension in a reference coordinate system, namely a stiffness matrix in a center-of-mass coordinate system of the powertrain; kiRepresents the equivalent stiffness of the ith suspension at the center of mass of the powertrain from KsiTo KiThe transformation process of (2) is a process of enabling the rigidity of the suspension to be equivalent to the center of mass of the power assembly from a local coordinate system of the suspension; b isiIs a transformation matrix determined by the mounting position of the suspension; n represents the number of suspensions.
In the differential equation of motion, q ═ wx wy wz θx θy θz]TIs a power assembly mass center displacement vector,is an acceleration vector. w is ax、wy、wzRespectively representing the translational displacement of the center of mass of the power assembly in the x direction, the y direction and the z direction; thetax、θy、θzRespectively represent the rotational displacement of the center of mass of the power assembly in the x direction, the y direction and the z direction.
(4) Establishing a parameterized dynamic model (namely a simulation model) of the powertrain suspension system in multi-body dynamic software to facilitate subsequent optimization, increasing optimization efficiency, calculating the mass center longitudinal acceleration and the impact degree of the powertrain by taking a step function as excitation, and taking the suspension rigidity and the mounting position as model input parameters, wherein the mass center longitudinal acceleration (A) is a mass center longitudinal accelerationx) And the impact (J) as the output of the model, while taking these two parameters as one of the optimization objectives. The step function of this embodiment is a torque curve as shown in fig. 3. The multibody dynamics software used in this example was ADAMS, and it is understood that other ADAMS may be used in other examplesMultiple dynamics software of (1).
The rigidity of the suspension refers to the static rigidity of the elastic main shaft under a local coordinate system of the suspension: k is a radical ofui、kvi、kwiThe static stiffness of the suspension in the three elastic main shaft directions under the local coordinate system of the suspension, namely the static stiffness in the three directions of u, v and w, is respectively, the local coordinate system of the suspension is a coordinate system established by taking the elastic center of the suspension as the origin of coordinates and taking the three elastic main shafts as coordinate axes, and the static stiffness matrix form of the ith suspension can be expressed as follows: ksi=diag([kui kvi kwi])。
In the step, when a parameterized dynamic model of the powertrain suspension system is established, rigid body models are adopted for both the electric drive assembly and the auxiliary frame.
In this step, the method for calculating the impact degree is as follows:
wherein, aβThe angular acceleration of the powertrain about the Y-axis.
The longitudinal acceleration of the center of mass of the power assembly can be directly acquired through ADAMS.
(5) The method comprises the steps of establishing an optimization model by taking the linear section rigidity of a suspension as a design variable, the natural frequency of a power assembly as a constraint condition, the maximum energy decoupling rate of the power assembly and the minimum mass center longitudinal acceleration and impact amplitude of the power assembly under an impact working condition as optimization targets, and obtaining the design rigidity of the suspension according to the optimization model. The method comprises the following specific steps:
in the center of mass coordinate of the power assembly, the six-order natural frequency omega can be solved according to the mass matrix M and the rigidity matrix Kj(j ═ 1, 2.. 6) and the mode shape matrix Φ, it is further possible to obtain the energy distribution of the system when making primary vibrations of each order. When the system is subjected to j (j ═ 1, 2.., 6) th order primary vibration, the maximum kinetic energy is as follows:
φjrepresenting a j-th order mode vector of the power assembly,representing its transposed vector for the purpose of calculating the kinetic energy of the vibration; the expansion is as follows:
k is the number of rows in the mass matrix,lis the number of columns, mlkIs the element of the ith row and k columns in the quality matrix.
Then, the energy ratio of the k (k ═ 1, 2.., 6) generalized coordinates at the i-th order primary vibration is:
Tlmeaning represented is the l column vector, m, in the vibration energy matrixklThe element representing the kth row and the l column in the mass matrix M has the unit kg.
Energy distribution of the power assembly in six main vibration directions can be obtained through the formula;
if ejmaxE (k, j), k 1,2,3.. 6, then ejFor the decoupling rate of the power assembly in a certain vibration direction, the optimization target is as follows: by varying the stiffness of the suspension so that ejAs close to 1 as possible if the constraint is satisfied.
Because the vibration in each direction has different influence on the NVH performance of the whole vehicle, generally speaking, the decoupling degree in the Y-axis and the vertical direction is expected to be the highest. For this purpose, a six-dimensional weight vector b ═ b is introduced1 b2 b3 b4 b5 b6]To indicate the importance of the energy decoupling rate in each direction.
An optimization model can thus be obtained as follows:
min f2=max(Ax)
min f3=max(J)
s.t.
kuil≤kui≤kuiu;
kvil≤kvi≤kviu;
kwil≤kwi≤kwiu;
ωj-ωj+1≤-1,(j=1,2,...,6);
5-ω1≤0;
ω6-40≤0;
90-e5≤0.
wherein, minf1: the sum of six directions (1-energy decoupling rate) is minimized, namely the total energy decoupling rate is maximized; minf2: minimizing the peak value of the longitudinal acceleration curve of the center of mass of the power assembly; minf3: minimizing the peak value of the impact curve; k is a radical ofuil: represents the lower limit of the change of the u-direction stiffness of the ith suspension; k is a radical ofuiu: denotes the upper limit, k, of the change in the u-direction stiffness of the i-th suspensionvil、kviuRespectively representing the lower limit and the upper limit of the variation of the v-direction stiffness of the ith suspension; k is a radical ofwil、kwiuRespectively representing the lower limit and the upper limit of the variation of the w-direction rigidity of the ith suspension; e.g. of the type5The decoupling rate in the direction of the powertrain Pitch, i.e., the decoupling rate in the Pitch direction, is indicated.
TABLE 2 initial stiffness of each suspension and its variation range
The system transient response pairs before and after optimization are shown in fig. 4 and 5, for example. FIG. 4 is a transient response of optimized fore and aft powertrain longitudinal acceleration, and FIG. 5 is a comparison of optimized fore and aft powertrain jerk. Through comparison, the energy decoupling rate of the power assembly suspension system is improved after the design calculation and optimization method is used for optimization; meanwhile, the longitudinal acceleration and the impact degree of the power assembly under impact excitation are both reduced, and the transient response is improved, so that the effectiveness of the design calculation and optimization method is demonstrated.
It should be understood that the above-mentioned embodiments of the present invention are only examples for clearly illustrating the present invention, and are not intended to limit the embodiments of the present invention. Other variations and modifications will be apparent to persons skilled in the art in light of the above description. And are neither required nor exhaustive of all embodiments. Any modification, equivalent replacement, and improvement made within the spirit and principle of the present invention should be included in the protection scope of the claims of the present invention.
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