CN214309421U - Strength test device of suspension frame framework of magnetic levitation vehicle - Google Patents
Strength test device of suspension frame framework of magnetic levitation vehicle Download PDFInfo
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- CN214309421U CN214309421U CN202023105257.3U CN202023105257U CN214309421U CN 214309421 U CN214309421 U CN 214309421U CN 202023105257 U CN202023105257 U CN 202023105257U CN 214309421 U CN214309421 U CN 214309421U
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Abstract
The utility model discloses a strength test device of maglev vehicle suspension frame framework, including suspension frame framework body, experimental supporting platform, horizontal load loading mechanism, vertical load loading mechanism and vertical load loading mechanism, suspension frame framework body includes the vertical roof beam of first suspension frame, the vertical roof beam of second suspension frame and two suspension frame crossbeams, two suspension frame crossbeams cross-over connect respectively at the both ends of the vertical roof beam of first suspension frame and the vertical roof beam of second suspension frame, the below of the vertical roof beam of first suspension frame and the vertical roof beam of second suspension frame all is equipped with electro-magnet simulation roof beam, all install linear electric motor simulation roof beam between the vertical roof beam of first suspension frame and the electro-magnet simulation roof beam and between the vertical roof beam of second suspension frame and the electro-magnet simulation roof beam. The utility model discloses a strength test device of maglev vehicle suspension frame can transversely, vertically reach vertical restraint and loading to suspension frame framework body according to maglev vehicle actual operation operating mode, and its structure scientific and reasonable, has improved experimental efficiency greatly.
Description
Technical Field
The utility model relates to a railway rolling stock tests technical field, concretely relates to strength test device of maglev vehicle suspension frame framework.
Background
The suspension frame of the magnetic suspension vehicle is a running mechanism of the magnetic suspension vehicle, is equivalent to a bogie of a traditional railway wheel-track vehicle, and is one of core components for realizing suspension, guiding, traction and braking of the magnetic suspension vehicle. Therefore, after the suspension frame is designed, the suspension frame produced at first time needs to be subjected to static strength and fatigue strength bench tests, because the electromagnet of the suspension frame of the magnetic levitation vehicle is electrified and then interacts with the track, the magnetic levitation vehicle is suspended, and the weight of the vehicle body above the suspension frame in the vertical direction is balanced with the electromagnetic force below the suspension frame; when the vehicle body passes through a curve, a transverse centrifugal force effect is generated or the vehicle body receives a cross wind effect, and the electromagnet encircles the track to generate transverse restraint; the traveling wave magnetic field generated after the linear motor is electrified pushes the magnetic suspension train to move in the longitudinal direction, and the traction pull rod drives the train body to move, so that the action of the linear motor on the suspension frame framework and the action of the train body on the suspension frame framework are a pair of counter forces in the longitudinal direction. Therefore, when the suspension frame of the magnetic suspension vehicle is subjected to a bench test, how to simulate the independent action or the combined action of various loads in the actual operation of the magnetic suspension vehicle to carry out vertical, transverse and longitudinal loading on the suspension frame and how to carry out constraint on the suspension frame in various directions without generating excessive constraint is directly related to the accuracy of the test. The suspension frame is restrained according to the actual stress characteristics, the suspension frame is subjected to vertical, longitudinal and transverse load under the same working conditions at the corresponding load application positions so as to test whether the stress level of the key position of the suspension frame meets the requirements of relevant standards, the unnoticed risk points in the structural design are found through flaw detection after the fatigue strength test, and a test reference basis is provided for further structural optimization.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an intensity test device of maglev vehicle suspension frame framework, its structure scientific and reasonable can carry out horizontal, vertical and vertical restraint and loading to suspension frame framework body according to maglev vehicle actual operation operating mode to solve the technical problem who mentions in the background art.
The purpose of the utility model is realized through the following technical scheme:
a strength test device for a suspension frame of a magnetic levitation vehicle comprises a suspension frame body, a test supporting platform, a transverse load loading mechanism, a longitudinal load loading mechanism and a vertical load loading mechanism, the suspension frame framework body comprises a first suspension frame longitudinal beam, a second suspension frame longitudinal beam and two suspension frame cross beams, the two suspension frame cross beams are respectively bridged at two ends of the first suspension frame longitudinal beam and the second suspension frame longitudinal beam, electromagnet simulation beams are arranged below the first suspension frame longitudinal beam and the second suspension frame longitudinal beam, linear motor simulation beams are respectively arranged between the first suspension frame longitudinal beam and the electromagnet simulation beam and between the second suspension frame longitudinal beam and the electromagnet simulation beam, electromagnet mounting seats are arranged at four corners of the bottom wall of the suspension frame body, and two ends of each electromagnet simulation beam are connected to the side walls of two adjacent electromagnet mounting seats respectively;
the four corners of the top wall of the suspension frame framework body are respectively provided with an air spring loading seat, one end of the transverse load loading mechanism is connected to the side wall of the air spring loading seat, the other end of the transverse load loading mechanism is connected to the test supporting platform, and the transverse load loading mechanism transmits transverse load to the suspension frame framework body through the air spring loading seats; one end of the vertical load loading mechanism is connected to the top wall of the air spring loading seat, the other end of the vertical load loading mechanism is connected to the test supporting platform, and the vertical load loading mechanism carries out vertical load loading on the suspension frame body through the air spring loading seat; one end of the longitudinal load loading mechanism penetrates through the air spring loading seat and is connected with the first suspension frame longitudinal beam and the second suspension frame longitudinal beam, and the other end of the longitudinal load loading mechanism is connected with the test supporting platform; the transverse load loading mechanism, the longitudinal load loading mechanism and the vertical load loading mechanism are mutually vertical;
furthermore, the transverse load loading mechanism comprises a transverse loading assembly and a transverse restraining assembly, the test supporting platform is a concave platform, the supporting platform comprises two platform ends and a concave part, and the concave part is arranged in the middle of the two platform ends;
the transverse restraining component is installed at the platform end and is arranged in parallel with the suspension frame beam, one end of the transverse loading component is connected with the transverse restraining component, the other end of the transverse loading component is connected with the side wall of the air spring loading seat, and transverse loads are transmitted to the suspension frame body.
The vertical load of the utility model mainly comes from the weight of the upper vehicle body, so that the vertical loading is needed to be carried out on the four air spring loading seats through the vertical load loading mechanism; the transverse load is mainly from the centrifugal force when the vehicle passes through a curve or the side wall of the vehicle body is acted by side wind and is transmitted to the suspension frame body through the four air spring loading seats; therefore, the transverse load is loaded on the four air spring loading seats through the transverse load loading mechanism. The longitudinal load is mainly generated at the joint between the vehicle body and the suspension frame body when the vehicle starts braking or accelerates and decelerates.
Furthermore, the air spring loading seat comprises connecting columns and an installation frame body, the connecting columns are installed on four corners of the top wall of the suspension frame framework body, and the installation frame body is used for connecting the transverse load loading mechanism, the longitudinal load loading mechanism and the vertical load loading mechanism.
The beneficial effects of the preferred embodiment are as follows: the air spring loading seat adopts the structural form of a connecting column and an installation frame body, and is convenient to connect the transverse load loading mechanism, the longitudinal load loading mechanism and the vertical load loading mechanism.
Further, horizontal restraint subassembly includes four horizontal restraint units, and four horizontal restraint units divide into two sets ofly, and is two sets of horizontal restraint unit is installed two respectively the platform end and with suspension frame crossbeam parallel arrangement, every horizontal restraint unit all include first support column, horizontal counter-force seat and horizontal bracing piece, four first support column and four horizontal counter-force seat is all installed the platform end, the first end of horizontal bracing piece with the electro-magnet simulation roof beam is connected, the second end of horizontal bracing piece with the lateral wall of horizontal counter-force seat is connected.
The beneficial effects of the preferred embodiment are as follows: one end of the transverse restraint assembly is fixed on the side face of the electromagnet simulation beam through the pulling plate, the other end of the transverse restraint assembly is fixed on the transverse counter-force seat, and the transverse counter-force seat is fixedly installed at the platform end of the test platform and provides transverse restraint for the suspension frame.
Further, horizontal loading subassembly includes horizontal loading actuator, the end ball pivot support that stretches out of horizontal loading actuator connect in the lateral wall of installation framework, the afterbody ball pivot support of horizontal loading actuator connect in the lateral wall of first support column.
The beneficial effects of the preferred embodiment are as follows: each transverse loading actuator acts on the side surface of the air spring loading seat, and then the transverse load is transferred to the suspension frame.
Furthermore, an anti-diamond beam is connected between the first end and the second end of each of the two electromagnet simulation beams.
The beneficial effects of the preferred embodiment are as follows: in order to prevent the whole system from generating diamond dislocation deformation in the loading process, the ends of the left and right electromagnet simulation beams are restrained by one diamond-resistant beam.
Further, the vertical load loading mechanism comprises a vertical loading component and a vertical restraining component,
the vertical restraint assembly is installed on the tested supporting platform and is perpendicular to the suspension frame cross beam, one end of the vertical loading assembly is connected with the vertical restraint assembly, the other end of the vertical loading assembly is connected with the top wall of the air spring loading seat, and vertical loads are transmitted to the suspension frame body.
The beneficial effects of the preferred embodiment are as follows: the vertical restraint assembly is installed the experimental supporting platform provides the supporting role for vertical loading subassembly, and vertical loading subassembly connection air spring loading seat's roof realizes reaching vertical load the suspension frame framework body.
Furthermore, the vertical restraint assembly comprises two vertical loading beams and a plurality of vertical support rods, the two vertical loading beams are respectively bridged between first support columns on two sides of the platform end distributed on two sides of the recessed portion, the plurality of vertical support rods are divided into two groups, the first ends of the two groups of vertical support rods are both mounted on the bottom wall of the electromagnet simulation beam through bearing seats, and the second ends of the two groups of vertical support rods are both mounted on the recessed portion through the bearing seats;
the vertical loading assembly comprises a vertical loading actuator, an extending end spherical hinge support of the vertical loading actuator is connected to the top wall of the installation frame body, and a tail spherical hinge support of the vertical loading actuator is connected to the bottom wall of the vertical loading cross beam.
The beneficial effects of the preferred embodiment are as follows: four vertical loading actuators are suspended on the front vertical loading cross beam and the rear vertical loading cross beam, and the four vertical loading actuators are loaded on the upper surfaces of the four air spring loading seats, so that vertical loads are transmitted to the suspension frame body.
Furthermore, the longitudinal load loading mechanism comprises a longitudinal loading assembly and a longitudinal restraining assembly, the longitudinal restraining assembly is installed at the platform end and located at the outer edge of the suspension frame body, the first suspension frame longitudinal beam and the second suspension frame longitudinal beam are both provided with installation bases, one end of the longitudinal loading assembly is connected with the longitudinal restraining assembly, and the other end of the longitudinal loading assembly penetrates through the air spring loading seat and is installed on the first suspension frame longitudinal beam and the second suspension frame longitudinal beam through the installation bases, so that the longitudinal load is transmitted to the suspension frame body.
The beneficial effects of the preferred embodiment are as follows: the longitudinal load loading mechanism is characterized in that a longitudinal restraining component of the longitudinal load loading mechanism is arranged at the platform end and located at the outer edge of the suspension frame body to provide a supporting function for the longitudinal load loading mechanism, the longitudinal load loading component penetrates through the air spring loading seat and is connected with the first suspension frame longitudinal beam and the second suspension frame longitudinal beam through the mounting base, and the longitudinal load is transmitted to the suspension frame body.
Further, the longitudinal restraint assembly comprises two second support columns, a longitudinal loading cross beam and a longitudinal restraint counterforce seat, the two second support columns are oppositely arranged on the platform ends on two sides of the concave part, and the longitudinal loading cross beam is bridged between the two second support columns;
the longitudinal loading assembly comprises two longitudinal loading actuators, the extending ends of the longitudinal loading actuators penetrate through the through holes of the mounting frame body to be connected with the mounting base, and the tail spherical hinge support of each longitudinal loading actuator is connected to the side wall of the longitudinal loading cross beam;
longitudinal restraint counter-force seat fixed mounting is in the concave yield portion is located the homonymy all be equipped with the restraint steel sheet between the horizontal counter-force seat, first vertical roof beam of suspension with all be equipped with vertical backstop seat on the diapire of the vertical roof beam of second suspension, arbitrary restraint steel sheet with all be equipped with vertical restraint roof beam between the horizontal counter-force seat, the pot head of vertical restraint roof beam is located the top of longitudinal restraint counter-force seat, the other end of vertical restraint roof beam passes vertical backstop seat with the restraint steel sheet is connected.
The beneficial effects of the preferred embodiment are as follows: the two second supporting columns are arranged at the platform ends at the left side and the right side of the test supporting platform, the two second supporting columns support a longitudinal loading beam, and the longitudinal loading beam provides support for two longitudinal loading actuators; and the restraint steel plate between the transverse counter-force seats at the same side and the longitudinal restraint counter-force seat provide restraint for the longitudinal restraint beam, and the middle part of the longitudinal restraint beam is tightly attached to the longitudinal stop seat on the lower surface of the suspension frame framework so as to restrain the longitudinal displacement of the suspension frame framework.
The utility model has the advantages that:
(1) the suspension frame of the magnetic suspension vehicle mainly needs to consider vertical, transverse and longitudinal loads when strength test is carried out, wherein the vertical load mainly comes from the weight of an upper vehicle body, so that vertical loading is carried out on four air spring loading seats through a vertical load loading mechanism; the transverse load is mainly from the centrifugal force when the vehicle passes through a curve or the side wall of the vehicle body is acted by side wind and is transmitted to the suspension frame body through the four air spring loading seats; therefore, the transverse load is loaded on the four air spring loading seats through the transverse load loading mechanism. The longitudinal load is mainly generated at the joint between the vehicle body and the suspension frame body when the vehicle starts to brake or accelerates and decelerates, so that the longitudinal load can be loaded at the joint between the vehicle body and the suspension frame body through the longitudinal actuator; the utility model discloses a strength test device of maglev vehicle suspension frame can transversely, vertically reach vertical restraint and loading to suspension frame framework body according to maglev vehicle actual operation operating mode, and its structure scientific and reasonable, has improved experimental efficiency greatly.
(2) The utility model has four vertical loading actuators, the simulated actual vehicle body is supported on the suspension frame framework through the air springs at four corners, and the vertical acting force of the actual vehicle body weight on the suspension frame framework can be simulated when the vertical actuator is used for force loading; when the vertical actuators are subjected to displacement loading, the action phases and amplitude values of the four vertical actuators are changed, and various motion postures of nodding and shaking of the vehicle body in actual operation can be simulated; and the suspension bracket is supported and restrained by the electromagnet in the vertical direction, so that the electromagnetic force action between the electromagnet of the suspension bracket and the track in practice is simulated. The transverse force applied to the vehicle body under the action of the transverse wind is calculated according to the size of the curve radius and the size of the transverse wind load in actual operation, and the transverse force applied to the vehicle body is transmitted to the suspension frame body through the air spring. Therefore, during the test, the four transverse loading actuators on the side face of the air spring loading seat apply transverse loads to the suspension frame body, and meanwhile transverse restraint is applied to the electromagnet simulation beam, so that transverse restraint of the suspension frame electromagnet in actual operation is simulated. The linear motor is electrified to generate a traveling wave magnetic field to push the suspension frame body to move longitudinally, the suspension frame body drives the vehicle body to move longitudinally through the traction pull rod, and the action of the linear motor on the suspension frame and the action of the vehicle body on the suspension frame body are a pair of counter forces. Through the utility model discloses a when test device carries out vertical loading, the longitudinal motion of suspension frame framework body has been retrained, convert load to traction pull rod department, carry out vertical loading to the suspension frame framework, it is certain contained angle to have considered simultaneously between the vertical roof beam upper surface of actual well traction pull rod and suspension frame, all adopt radial spherical plain bearing at each restraint tip, can bear great load, can adjust installation angle according to actual need, radial spherical plain bearing tip has the internal thread, the actual installation size is adjusted to the internal threaded length of accessible control bracing piece screw in, make application scope wider.
Drawings
FIG. 1 is a schematic view of the overall structure of the strength testing device of the suspension frame structure of the magnetic levitation vehicle of the present invention;
FIG. 2 is a schematic structural view of the suspension frame body of the present invention;
fig. 3 is a second schematic structural view of the suspension frame body of the present invention;
FIG. 4 is a view of the installation structure among the suspension frame body, the electromagnet simulation beam and the anti-diamond beam of the present invention;
FIG. 5 is a schematic structural view of the air spring loading seat of the present invention;
FIG. 6 is a schematic structural view of the test support platform of the present invention;
fig. 7 is a schematic structural view of the lateral load loading mechanism of the present invention;
fig. 8 is a schematic structural view of the vertical load loading mechanism of the present invention;
fig. 9 is a schematic structural view of the longitudinal load loading mechanism of the present invention;
in the figure, 1-a suspension frame body, 101-a first suspension frame longitudinal beam, 102-a second suspension frame longitudinal beam, 103-a suspension frame beam, 104-a mounting base, 2-a test supporting platform, 201-a platform end, 202-a concave part, 3-a transverse load loading mechanism, 4-a longitudinal load loading mechanism, 5-a vertical load loading mechanism, 6-an electromagnet simulation beam, 7-a linear motor simulation beam, 8-an electromagnet mounting seat, 9-an air spring loading seat, 901-a connecting column, 902-a mounting frame body, 10-a transverse loading assembly, 1001-a transverse loading actuator, 11-a transverse constraint assembly, 1101-a first supporting column, 1102-a transverse counter-force seat, 1103-a transverse supporting rod, 12-an anti-diamond beam, 13-vertical loading assembly, 1301-vertical loading actuator, 14-vertical constraint assembly, 1401-vertical loading beam, 1402-vertical support rod, 15-bearing seat, 16-longitudinal loading assembly, 1601-longitudinal loading actuator, 17-longitudinal constraint assembly, 1701-second support column, 1702-longitudinal loading beam, 1703-longitudinal constraint counterforce seat, 18-constraint steel plate and 19-longitudinal constraint beam.
Detailed Description
The technical solution of the present invention will be described clearly and completely with reference to the following embodiments, and it should be understood that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. Based on the embodiments in the present invention, all other embodiments obtained by those skilled in the art without creative efforts belong to the protection scope of the present invention.
Example 1
Referring to fig. 1-9, the present invention provides a technical solution:
referring to fig. 1-4, a strength testing device for a suspension frame framework of a magnetic levitation vehicle comprises a suspension frame framework body 1, a testing support platform 2, a transverse load loading mechanism 3, a longitudinal load loading mechanism 4 and a vertical load loading mechanism 5, wherein the suspension frame framework body 1 comprises a first suspension frame longitudinal beam 101, a second suspension frame longitudinal beam 102 and two suspension frame cross beams 103, the two suspension frame cross beams 103 are respectively bridged at two ends of the first suspension frame longitudinal beam 101 and the second suspension frame longitudinal beam 102, electromagnet simulation beams 6 are respectively arranged below the first suspension frame longitudinal beam 101 and the second suspension frame longitudinal beam 102, linear motor simulation beams 7 are respectively arranged between the first suspension frame longitudinal beam 101 and the electromagnet simulation beams 6 and between the second suspension frame longitudinal beam 102 and the electromagnet simulation beams 6, electromagnet installation seats 8 are arranged at four corners of the bottom wall of the suspension frame framework body 1, and two ends of each electromagnet simulation beam 6 are connected to the side walls of two adjacent electromagnet installation seats 8 respectively;
the four corners of the top wall of the suspension frame framework body 1 are respectively provided with an air spring loading seat 9, one end of the transverse load loading mechanism 3 is connected to the side wall of the air spring loading seat 9, the other end of the transverse load loading mechanism 3 is connected to the test supporting platform 2, and the transverse load loading mechanism 3 transmits a transverse load to the suspension frame framework body 1 through the air spring loading seat 9; one end of the vertical load loading mechanism 5 is connected to the top wall of the air spring loading seat 9, the other end of the vertical load loading mechanism 5 is connected to the test supporting platform 2, and the vertical load loading mechanism 5 carries out vertical load loading on the suspension frame body 1 through the air spring loading seat 9; one end of the longitudinal load loading mechanism 4 is arranged in the air spring loading seat 9 in a penetrating manner and connected with the first suspension frame longitudinal beam 101 and the second suspension frame longitudinal beam 102, and the other end of the longitudinal load loading mechanism 4 is connected with the test supporting platform 2; and the transverse load loading mechanism 3, the longitudinal load loading mechanism 4 and the vertical load loading mechanism 5 are mutually vertical.
The suspension frame of the magnetic suspension vehicle of the utility model mainly needs to consider vertical, transverse and longitudinal loads when carrying out strength test, wherein, the vertical load mainly comes from the weight of the vehicle body above, therefore, the vertical loading is needed to be carried out on the four air spring loading seats 9 through the vertical load loading mechanism 5; the transverse load is mainly from the centrifugal force when the vehicle body passes through a curve or the side wall of the vehicle body is acted by side wind and is transmitted to the suspension frame framework body 1 through the four air spring loading seats 9; therefore, the transverse load is loaded on the four air spring loading seats through the transverse load loading mechanism 3. The longitudinal load is mainly generated at the joint between the vehicle body and the suspension frame body 1 when the vehicle starts to brake or accelerates and decelerates, so that the longitudinal load can be loaded at the joint between the vehicle body and the suspension frame body 1 through a longitudinal actuator; the utility model discloses a strength test device of maglev vehicle suspension frame can transversely, vertically reach vertical restraint and loading to suspension frame framework body 1 according to maglev vehicle actual operation operating mode, and its structure scientific and reasonable, has improved experimental efficiency greatly.
Suspension frame framework body 1 whole realize supporting the restraint through fastening the electro-magnet on electro-magnet mount pad 8, when carrying out the intensity test, the test object is uncharged magnet and linear electric motor's suspension frame framework amount, consequently need simulate electro-magnet and linear electric motor through experimental frock to restraint and loading.
Preferably, the left and right of the linear motor simulation beam 7 are respectively in a channel steel form, the lower surface of the channel steel is provided with eight through holes which are matched with eight bolt holes on the lower surfaces of the left and right longitudinal beams of the suspension frame framework body 1, the linear motor simulation beam 7 is suspended below the left and right longitudinal beams of the suspension frame framework body 1 through a lead screw, and a balance weight can be added in the channel steel according to the actual mass of the linear motor. The electromagnet simulation beams 6 are arranged on the left and right sides respectively, steel plates with threaded holes are welded on the front outer side face and the rear outer side face of each beam respectively, and the threaded holes in the steel plates are matched with through holes in the electromagnet mounting seats 8 of the suspension frame.
Referring to fig. 5, the air spring loading seat 9 includes a connecting column 901 and a mounting frame 902, the connecting column 901 is mounted at four corners of the top wall of the suspension frame body 1, and the mounting frame 902 is used for connecting the transverse load loading mechanism 3, the longitudinal load loading mechanism 4 and the vertical load loading mechanism 5.
The utility model discloses an air spring loading seat 9 adopts spliced pole 901 and installation frame body 902's structural style, conveniently connects horizontal load loading mechanism 3, vertical load loading mechanism 4 and vertical load loading mechanism 5.
Preferably, the air spring loading seat 9 is formed by welding an upper part and a lower part, the upper part is of a square structure formed by welding four steel plates, the upper surface of the air spring loading seat is connected with the vertical load loading mechanism 5, the side surface of the air spring loading seat is connected with the transverse load loading mechanism 3, and the upper part of the air spring loading seat 9 is communicated with the front and the back in order to avoid interference with the longitudinal load loading mechanism 4. The lower part of the air spring loading seat 9 is a hollow cylinder, the outer surface of the cylinder is milled smoothly, and the air spring loading seat and the inner side surface of the air spring mounting seat of the suspension frame framework adopt small clearance fit, so that the transverse load is transferred to the suspension frame framework body 1 through the air spring loading seat 9.
Referring to fig. 6, the transverse load loading mechanism 3 includes a transverse loading assembly 10 and a transverse restraining assembly 11, the test support platform 2 is a concave platform, the support platform includes two platform ends 201 and a concave portion 202, and the concave portion 202 is disposed in the middle of the two platform ends 201;
the transverse restraining component 11 is installed at the platform end 201 and is parallel to the suspension frame cross beam 103, one end of the transverse loading component 10 is connected with the transverse restraining component 11, the other end of the transverse loading component 10 is connected with the side wall of the air spring loading seat 9, and transverse loads are transmitted to the suspension frame framework body 1.
The utility model discloses horizontal restraint subassembly 11 of horizontal load loading mechanism 3 is installed and is provided the supporting role for horizontal loading subassembly 10 on concave type platform, and the lateral wall of air spring loading seat 9 is connected to the other end of horizontal loading subassembly 10, realizes transmitting horizontal load suspension frame body 1.
Referring to fig. 7, the lateral constraint assembly 11 includes four lateral constraint units, the four lateral constraint units are divided into two groups, the two groups of lateral constraint units are respectively installed at the two platform ends 201 and are parallel to the suspension frame cross beam 103, each lateral constraint unit includes a first support column 1101, a lateral reaction force seat 1102 and a lateral support rod 1103, the four first support columns 1101 and the four lateral reaction force seats 1102 are all installed at the platform ends 201, a first end of the lateral support rod 1103 is connected to the electromagnet simulation beam 6, and a second end of the lateral support rod 1103 is connected to a side wall of the lateral reaction force seat 1102.
The utility model discloses a four first support columns 1101 can play simultaneously and provide the supporting role for four horizontal loading actuators 1001, and every horizontal loading actuator 1001 acts on the side of air spring loading seat 9, and then transmits horizontal load to the suspension frame framework. One end of the transverse restraint assembly 11 is fixed on the side surface of the electromagnet simulation beam 6 through a pulling plate, the other end of the transverse restraint assembly is fixed on a transverse counter force seat 1102, and the transverse counter force seat 1102 is fixedly installed at the platform end 201 of the test platform to provide transverse restraint for the suspension frame.
Referring to fig. 7, the transversal loading assembly 10 includes a transversal loading actuator 1001, an extending end spherical hinge support of the transversal loading actuator 1001 is connected to a side wall of the mounting frame 902, and a tail spherical hinge support of the transversal loading actuator 1001 is connected to a side wall of the first supporting column 1101.
Specifically, the transverse loading actuator 1001 is connected to the side surface of the air spring loading seat 9 through an actuator extending end spherical hinge support, and a tail spherical hinge support of the transverse loading actuator 1001 is connected to the first support columns 1101 distributed on the left and right through bolts. By adopting the connection mode, the installation of the transverse loading actuator 1001 is stable, and parts can be replaced conveniently.
Referring to fig. 4 and 7, a diamond-resistant beam 12 is connected between the first end and the second end of each of the two electromagnet simulating beams 6.
The utility model discloses a prevent that entire system from producing rhombus dislocation deformation among the loading process, control 6 tip of two electro-magnet simulation roof beams and retrain through an anti rhombus roof beam.
Referring to fig. 8, the vertical load loading mechanism 5 includes a vertical loading assembly 13 and a vertical constraint assembly 14, the vertical constraint assembly 14 is mounted on the test support platform 2 and is perpendicular to the suspension frame beam 103, one end of the vertical loading assembly 13 is connected to the vertical constraint assembly 14, and the other end of the vertical loading assembly 13 is connected to the top wall of the air spring loading seat 9, so that a vertical load is transferred to the suspension frame body 1.
The utility model discloses vertical restraint subassembly 14 is installed experimental supporting platform 2 provides the supporting role for vertical loading subassembly 13, and vertical loading subassembly 13 is connected the roof of air spring loading seat 9, realizes transmitting vertical load suspension frame framework body 1.
Referring to fig. 8, the vertical restraint assembly 14 includes two vertical loading beams 1401 and a plurality of vertical supporting rods 1402, the two vertical loading beams 1401 are respectively bridged between the first supporting columns 1101 distributed on the platform ends 201 at the two sides of the recessed portion 202, the plurality of vertical supporting rods 1402 are divided into two groups, first ends of the two groups of vertical supporting rods 1402 are both mounted on the bottom wall of the electromagnet simulation beam 6 through bearing seats 15, and second ends of the two groups of vertical supporting rods 1402 are both mounted on the recessed portion 202 through the bearing seats 15;
the vertical loading assembly 13 comprises a vertical loading actuator 1301, wherein an extending end spherical hinge support of the vertical loading actuator 1301 is connected to the top wall of the mounting frame 902, and a tail spherical hinge support of the vertical loading actuator 1301 is connected to the bottom wall of the vertical loading beam 1401.
The utility model discloses a 4 first support columns 1101 are installed to the 2 left and right sides of experimental supporting platform, support a vertical loading crossbeam 1401 between per two first support columns 1101, and two vertical loading crossbeams 1401 hang four vertical loading actuators 1301 around, and four vertical loading actuators 1301 load in the upper surface of four air spring loading seats 9, and then with vertical load transmission to suspension frame framework body 1 on. The suspension frame framework body 1 is fixedly connected with the left electromagnet simulation beam and the right electromagnet simulation beam 6, and each electromagnet simulation beam 6 is supported in the concave part 202 of the test supporting platform 2 through four sets of vertical supporting tools.
In order to restrain the transverse displacement and the vertical displacement of the suspension frame framework body 1, the electromagnet simulation beam 6 and the suspension frame framework body 1 are fixedly connected, and the vertical restraint assembly 14 and the transverse restraint assembly 11 are connected to the electromagnet simulation beam 6 and can provide vertical support and transverse restraint for the whole suspension frame framework body 1.
Referring to fig. 9, the longitudinal load loading mechanism 4 includes a longitudinal loading component 16 and a longitudinal restraining component 17, the longitudinal restraining component 17 is installed at the platform end 201 and located at the outer edge of the suspension frame body 1, the first suspension frame longitudinal beam 101 and the second suspension frame longitudinal beam 102 are both provided with an installation base 104, one end of the longitudinal loading component 16 is connected to the longitudinal restraining component 17, and the other end of the longitudinal loading component 16 passes through the air spring loading seat 9 and is installed on the first suspension frame longitudinal beam 101 and the second suspension frame longitudinal beam 102 through the installation base 104, so as to transmit a longitudinal load to the suspension frame body 1.
The utility model discloses a vertical restraint subassembly 17 of longitudinal load loading mechanism 4 is installed platform end 201 just is located suspension frame framework body 1's outer fringe provides the supporting role for vertical loading subassembly 16, and vertical loading subassembly 16 passes air spring loading seat 9 and connects vertical roof beam 101 of first suspension and the vertical roof beam 102 of second suspension through installation base 104, realizes transmitting vertical load suspension frame framework body 1.
Referring to fig. 9, the longitudinal restraint assembly 17 includes two second support posts 1701, a longitudinal loading beam 1702 and a longitudinal restraint reaction seat 1703, the two second support posts 1701 being oppositely mounted on the platform end 201 on both sides of the recess 202, the longitudinal loading beam 1702 bridging between the two second support posts 1701;
the longitudinal loading assembly 16 comprises two longitudinal loading actuators 1601, the extending ends of the longitudinal loading actuators 1601 penetrate through the through holes of the mounting frame 902 to be connected with the mounting base 104, and the tail spherical hinge supports of the longitudinal loading actuators 1601 are connected with the side walls of the longitudinal loading beam 1702;
longitudinal restraint counter-force seat 1703 fixed mounting be located the homonymy all be equipped with restraint steel sheet 18 between the horizontal counter-force seat 1102, first suspension frame vertical roof beam 101 with all be equipped with vertical backstop seat on the diapire of second suspension frame vertical roof beam 102, arbitrary restraint steel sheet 18 with all be equipped with longitudinal restraint roof beam 19 between the horizontal counter-force seat 1102, the pot head of longitudinal restraint roof beam 19 is located longitudinal restraint counter-force seat 1703's top, the other end of longitudinal restraint roof beam 19 passes longitudinal backstop seat with restraint steel sheet 18 is connected.
The utility model discloses a test support platform 2 left and right sides platform end 201 installs two second support columns 1701, and a longitudinal loading crossbeam 1702 is propped up to two second support columns 1701, and longitudinal loading crossbeam 1702 provides the support for two longitudinal loading actuators 1601; the restraint steel plate 18 and the longitudinal restraint counter force seat 1703 between the transverse counter force seats 1102 on the same side provide restraint for the longitudinal restraint beam 19, the middle part of the longitudinal restraint beam 19 is tightly attached to the longitudinal stop seat on the lower surface of the suspension frame framework, and the suspension frame framework is restrained from longitudinal displacement. The loading end of the longitudinal loading actuator 1601 penetrates through the air spring loading seat 9 to be connected with the mounting base, and the longitudinal load is transmitted to the suspension frame body.
The lower surfaces of the first suspension frame longitudinal beam 101 and the second suspension frame longitudinal beam 102 of the suspension frame framework body 1 are provided with longitudinal stopping seats, the longitudinal stopping seats are tightly attached to the longitudinal restraining beam 19, one end of the longitudinal restraining beam 19 is fixed on the longitudinal restraining supporting seat 1704, and the other end of the longitudinal restraining beam 19 is fixed on the transverse counterforce seat 1102, so that longitudinal restraint is provided for the suspension frame framework.
Specifically, longitudinal loading actuator 1601 with install and connect through the longitudinal thrust pole between the base 104, longitudinal loading actuator 1601 stretches out end lead screw and is connected with longitudinal thrust pole one end screw hole through the actuator, longitudinal thrust pole other end lead screw and radial spherical joint bearing internal thread are connected, and radial spherical joint bearing passes through the installation base 104 of round pin hub connection on suspension frame framework body 1, and longitudinal loading actuator 1601 afterbody ball pivot support is connected in longitudinal loading crossbeam 1702 side, has realized providing counter-force support for longitudinal loading actuator 1601, and the longitudinal thrust pole passes the air spring that link up around 9 upper portions, is connected with the installation base 104 of suspension frame framework longitudinal beam top, transmits longitudinal load to the suspension frame framework.
The utility model discloses a strength test device of maglev vehicle suspension frame's load and restraint transmission route are respectively:
lateral load and lateral restraint: four first support columns 1101 can play the effect of providing the support for four transverse loading actuators 1001 simultaneously, the one end of transverse restraint subassembly 11 is fixed in the side of electro-magnet simulation roof beam 6 through the arm-tie, the other end is fixed in transverse reaction seat 1102, transverse reaction seat 1102 fixed mounting is in test platform's platform end 201, for the suspension framework provides transverse restraint, every transverse loading actuator 1001 acts on the side of air spring loading seat 9 dress, and then transmits transverse load to suspension framework body 1 on.
Vertical load and vertical restraint: the left side and the right side of the test support platform 2 are provided with 4 first support columns 1101, a vertical loading beam 1401 is supported between every two first support columns 1101, four vertical loading actuators 1301 are suspended on the front vertical loading beam 1401 and the rear vertical loading beam 1401, the four vertical loading actuators 1301 are loaded on the upper surfaces of four air spring loading seats 9, then vertical loads are transmitted to the suspension frame framework body 1, four sets of vertical support rods 1402 are supported below each electromagnet simulation beam 6 which is tightly connected with the suspension frame framework body 1, and vertical displacement constraint is provided for the suspension frame framework body 1.
Longitudinal load and longitudinal restraint: two second supporting columns 1701 are installed at the platform ends 201 on the left side and the right side of the test supporting platform 2, a longitudinal loading cross beam 1702 is supported by the two second supporting columns 1701, one end of a longitudinal restraining beam 19 is fixed on a longitudinal restraining counter-force seat 1703, the other end of the longitudinal restraining beam is fixed on a transverse counter-force seat 1102, meanwhile, the middle of the longitudinal restraining beam 19 is tightly attached to a longitudinal stop seat on the lower surface of a first longitudinal beam 101 and a second longitudinal beam 102 of the suspension frame framework body 1 to provide longitudinal restraint for the suspension frame framework body 1, the longitudinal loading cross beam 1702 provides support for two longitudinal loading actuators 1601, the loading end of a longitudinal loading actuator 160 is connected with the installation base 104 to transmit longitudinal loads to the suspension frame framework body 1.
At present, although there is a loading device for performing a strength test on a suspension frame, the existing loading device is only for loading a single-side suspension frame; compared with the prior art, the mode is applyed to vertical load and the vertical restraint mode is different, the utility model provides a vertical load is applyed through the installation base 104 of suspension frame framework body 1 top, and vertical restraint is applyed at the vertical stop seat of the vertical roof beam of first suspension frame 101 and the vertical roof beam 102 below of second suspension frame, and the atress condition of suspension frame framework is unanimous when the mode of application of load and restraint all with magnetic levitation vehicle actual operation, and the vertical load of current device advances horizontal loading at the object both ends of being tried, and the restraint is in the object top of being tried.
The vertical load is applied and the vertical constraint mode is different, the vertical load is loaded at the air spring above the suspension frame, and the vertical constraint is applied at the electromagnet below the suspension frame framework body 1; the suspension force generated between the suspension frame electromagnet and the track provides vertical support for the whole system, the existing vertical load is vertically loaded below a tested object and restrained above the tested object, and the loading and restraining modes of the suspension frame electromagnet and the track are just opposite.
Transverse load's application method and transverse restraint mode are different, the utility model discloses when in actual operation according to maglev vehicle, the top automobile body can receive crosswind effect or curve centrifugal force effect and then produce transverse force to suspension frame framework body 1, consider the transverse force effect that comes from the top automobile body that suspension frame framework body 1 received to act on the side of air spring, simultaneously, arrange transverse restraint at 6 departments of electro-magnet simulation roof beam with suspension frame framework body 1 fastening connection, unanimous with the actual atress condition. In the prior art, the transverse load is directly applied to the middle of the longitudinal beam of the suspension frame, and the end part of the longitudinal beam is clamped to realize transverse restraint.
The foregoing is illustrative of the preferred embodiments of the present invention, and it is to be understood that the invention is not limited to the precise forms disclosed herein, and that various other combinations, modifications, and environments may be resorted to, falling within the scope of the invention as defined by the appended claims. But that modifications and variations may be effected by those skilled in the art without departing from the spirit and scope of the invention, which is to be limited only by the claims appended hereto.
Claims (9)
1. The utility model provides a strength test device of maglev vehicle suspension frame framework which characterized in that: the device comprises a suspension frame framework body (1), a test supporting platform (2), a transverse load loading mechanism (3), a longitudinal load loading mechanism (4) and a vertical load loading mechanism (5), wherein the suspension frame framework body (1) comprises a first suspension frame longitudinal beam (101), a second suspension frame longitudinal beam (102) and two suspension frame cross beams (103), the two suspension frame cross beams (103) are respectively bridged at two ends of the first suspension frame longitudinal beam (101) and the second suspension frame longitudinal beam (102), electromagnet simulation beams (6) are respectively arranged below the first suspension frame longitudinal beam (101) and the second suspension frame longitudinal beam (102), linear motor simulation beams (7) are respectively arranged between the first suspension frame longitudinal beam (101) and the electromagnet simulation beams (6) and between the second suspension frame longitudinal beam (102) and the electromagnet simulation beams (6), electromagnet installation seats (8) are arranged at four corners of the bottom wall of the suspension frame body (1), and two ends of each electromagnet simulation beam (6) are connected to the side walls of two adjacent electromagnet installation seats (8) respectively;
air spring loading seats (9) are arranged at four corners of the top wall of the suspension frame framework body (1), one end of the transverse load loading mechanism (3) is connected to the side wall of the air spring loading seat (9), the other end of the transverse load loading mechanism (3) is connected to the test supporting platform (2), and the transverse load loading mechanism (3) transmits transverse load to the suspension frame framework body (1) through the air spring loading seats (9); one end of the vertical load loading mechanism (5) is connected to the top wall of the air spring loading seat (9), the other end of the vertical load loading mechanism (5) is connected to the test supporting platform (2), and the vertical load loading mechanism (5) carries out vertical load loading on the suspension frame framework body (1) through the air spring loading seat (9); one end of the longitudinal load loading mechanism (4) is arranged on the air spring loading seat (9) in a penetrating mode and connected with the first suspension frame longitudinal beam (101) and the second suspension frame longitudinal beam (102), and the other end of the longitudinal load loading mechanism (4) is connected to the test supporting platform (2); the transverse load loading mechanism (3), the longitudinal load loading mechanism (4) and the vertical load loading mechanism (5) are mutually vertical;
the transverse load loading mechanism (3) comprises a transverse loading assembly (10) and a transverse restraining assembly (11), the test supporting platform (2) is a concave platform, the supporting platform comprises two platform ends (201) and a concave part (202), and the concave part (202) is arranged in the middle of the two platform ends (201);
the horizontal restraint subassembly (11) install platform end (201) and with suspension frame crossbeam (103) parallel arrangement, the one end of horizontal loading subassembly (10) is connected horizontal restraint subassembly (11), the other end of horizontal loading subassembly (10) is connected the lateral wall of air spring loading seat (9), realizes transmitting horizontal load to suspension frame framework body (1).
2. The strength test device for the suspension frame of the magnetic suspension vehicle of claim 1, which is characterized in that: the air spring loading seat (9) comprises connecting columns (901) and mounting frame bodies (902), the connecting columns (901) are mounted at four corners of the top wall of the suspension frame framework body (1), and the mounting frame bodies (902) are used for connecting the transverse load loading mechanism (3), the longitudinal load loading mechanism (4) and the vertical load loading mechanism (5).
3. The strength test device for the suspension frame of the magnetic suspension vehicle of claim 2, which is characterized in that: horizontal restraint subassembly (11) include four horizontal restraint units, and four horizontal restraint units divide into two sets ofly, and are two sets of horizontal restraint unit installs two respectively platform end (201) and with suspension frame crossbeam (103) parallel arrangement, every horizontal restraint unit all include first support column (1101), horizontal counter-force seat (1102) and horizontal bracing piece (1103), four first support column (1101) and four horizontal counter-force seat (1102) are all installed platform end (201), the first end of horizontal bracing piece (1103) with the connection of electro-magnet simulation roof beam (6), the second end of horizontal bracing piece (1103) with the lateral wall of horizontal counter-force seat (1102) is connected.
4. The strength test device for the suspension frame of the magnetic suspension vehicle of claim 3, which is characterized in that: horizontal loading subassembly (10) include horizontal loading actuator (1001), the end ball pivot support that stretches out of horizontal loading actuator (1001) connect in the lateral wall of installation frame body (902), the afterbody ball pivot support of horizontal loading actuator (1001) connect in the lateral wall of first support column (1101).
5. The strength test device for the suspension frame of the magnetic suspension vehicle of claim 4, which is characterized in that: an anti-diamond beam (12) is connected between the first end and the second end of each of the two electromagnet simulation beams (6).
6. The strength test device for the suspension frame of the magnetic suspension vehicle of claim 5, which is characterized in that: the vertical load loading mechanism (5) comprises a vertical loading assembly (13) and a vertical restraining assembly (14),
vertical restraint subassembly (14) are installed experimental supporting platform (2) and with suspension frame crossbeam (103) are perpendicular, the one end of vertical loading subassembly (13) is connected vertical restraint subassembly (14), the other end of vertical loading subassembly (13) is connected the roof of air spring loading seat (9), realize reaching vertical load the suspension frame framework body (1).
7. The strength test device for the suspension frame of the magnetic suspension vehicle of claim 6, which is characterized in that: the vertical constraint assembly (14) comprises two vertical loading cross beams (1401) and a plurality of vertical supporting rods (1402), the two vertical loading cross beams (1401) are respectively bridged between first supporting columns (1101) distributed on platform ends (201) on two sides of the recessed portion (202), the plurality of vertical supporting rods (1402) are divided into two groups, first ends of the two groups of vertical supporting rods (1402) are respectively installed on the bottom wall of the electromagnet simulation beam (6) through bearing seats (15), and second ends of the two groups of vertical supporting rods (1402) are respectively installed on the recessed portion (202) through the bearing seats (15);
the vertical loading assembly (13) comprises a vertical loading actuator (1301), an extending end spherical hinge support of the vertical loading actuator (1301) is connected to the top wall of the mounting frame body (902), and a tail spherical hinge support of the vertical loading actuator (1301) is connected to the bottom wall of the vertical loading cross beam (1401).
8. The strength test device for the suspension frame of the magnetic suspension vehicle of claim 3, which is characterized in that: the longitudinal load loading mechanism (4) comprises a longitudinal loading assembly (16) and a longitudinal restraining assembly (17), the longitudinal restraining assembly (17) is installed at the platform end (201) and located at the outer edge of the suspension frame framework body (1), the first suspension frame longitudinal beam (101) and the second suspension frame longitudinal beam (102) are both provided with installation bases (104), one end of the longitudinal loading assembly (16) is connected with the longitudinal restraining assembly (17), the other end of the longitudinal loading assembly (16) penetrates through the air spring loading seat (9) and is installed on the first suspension frame longitudinal beam (101) and the second suspension frame longitudinal beam (102) through the installation bases (104), and longitudinal loads are transmitted to the suspension frame framework body (1).
9. The strength testing device for the suspension frame of the magnetic suspension vehicle of claim 8, which is characterized in that: the longitudinal restraint assembly (17) comprises two second support columns (1701), a longitudinal loading beam (1702) and a longitudinal restraint counterforce seat (1703), wherein the two second support columns (1701) are oppositely installed on the platform ends (201) on two sides of the recess (202), and the longitudinal loading beam (1702) is bridged between the two second support columns (1701);
the longitudinal loading assembly (16) comprises two longitudinal loading actuators (1601), the extending ends of the longitudinal loading actuators (1601) penetrate through the through holes of the mounting frame body (902) to be connected with the mounting base (104), and the tail spherical hinge supports of the longitudinal loading actuators (1601) are connected to the side walls of the longitudinal loading cross beam (1702);
longitudinal restraint counter-force seat (1703) fixed mounting be located homonymy all be equipped with between horizontal counter-force seat (1102) and retrain steel sheet (18), first vertical roof beam of suspension (101) with all be equipped with vertical backstop seat on the diapire of the vertical roof beam of second suspension (102), arbitrary restraint steel sheet (18) with all be equipped with vertical restraint roof beam (19) between horizontal counter-force seat (1102), the pot head of vertical restraint roof beam (19) is located the top of longitudinal restraint counter-force seat (1703), the other end of longitudinal restraint roof beam (19) passes vertical backstop seat with restraint steel sheet (18) are connected.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023105257.3U CN214309421U (en) | 2020-12-21 | 2020-12-21 | Strength test device of suspension frame framework of magnetic levitation vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023105257.3U CN214309421U (en) | 2020-12-21 | 2020-12-21 | Strength test device of suspension frame framework of magnetic levitation vehicle |
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| CN214309421U true CN214309421U (en) | 2021-09-28 |
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| CN202023105257.3U Withdrawn - After Issue CN214309421U (en) | 2020-12-21 | 2020-12-21 | Strength test device of suspension frame framework of magnetic levitation vehicle |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112629845A (en) * | 2020-12-21 | 2021-04-09 | 西南交通大学 | Strength test device of suspension frame framework of magnetic levitation vehicle |
| CN116429396A (en) * | 2023-03-28 | 2023-07-14 | 浙江骏融汽车零部件有限公司 | New energy automobile front anti-collision beam detection equipment |
-
2020
- 2020-12-21 CN CN202023105257.3U patent/CN214309421U/en not_active Withdrawn - After Issue
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112629845A (en) * | 2020-12-21 | 2021-04-09 | 西南交通大学 | Strength test device of suspension frame framework of magnetic levitation vehicle |
| CN112629845B (en) * | 2020-12-21 | 2024-05-03 | 西南交通大学 | Intensity test device of magnetic levitation vehicle suspension frame |
| CN116429396A (en) * | 2023-03-28 | 2023-07-14 | 浙江骏融汽车零部件有限公司 | New energy automobile front anti-collision beam detection equipment |
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