CN217587625U - High-compatibility space radiation detector ground calibration device - Google Patents
High-compatibility space radiation detector ground calibration device Download PDFInfo
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- CN217587625U CN217587625U CN202220982613.XU CN202220982613U CN217587625U CN 217587625 U CN217587625 U CN 217587625U CN 202220982613 U CN202220982613 U CN 202220982613U CN 217587625 U CN217587625 U CN 217587625U
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Abstract
The utility model discloses a high compatibility space radiation detector ground calibration device, including two segmentation elevating platforms, translation transport table and interface board. The utility model discloses ground calibration device structural planning is reasonable, and the integrated level is high, and is favorable to satisfying space radiation detector required height in the ground calibration test process and bears, the requirement such as big stroke and minimum mesa height. And simultaneously, the utility model discloses have great compatibility, can satisfy the space radiation detector of different grade type, like the demarcation test demand of loads such as X ray detector, space energy ware, and the utility model discloses can realize demarcation platform and the quick alignment of line beam ray export, satisfy different detectors and help shortening test time to the demand of the different inclinations of demarcation platform mesa, improve test efficiency, be fit for using widely in this area.
Description
Technical Field
The utility model belongs to the technical field of the space is surveyed, concretely relates to high compatibility ground calibration device, the device are used for space radiation detector to mark the test on ground.
Background
The development history of domestic space radiation detectors is earlier, but large-scale special space observation begins from the starting of special spatial science leader items, such as dark matter particle detection satellites, hard X-ray telescopes, advanced astronomical solar astronomical stage satellites and the like. Before the space radiation detector emits the light, a large number of tests need to be carried out on the ground, and particularly, performance calibration related to the detector, such as detector imaging calibration, efficiency calibration and the like.
The space high-energy particle detection ground calibration is generally carried out under the condition of a beam with a fixed height, and the central height of the beam is usually determined and is lower. The most famous European nucleus center has the beam center height of only 1.3m, and the beam center height for pulsar navigation in China is 1.25m. The space high-energy particle detector mostly uses a larger area for higher acceptance, and in consideration of installation of a tool and other combined test equipment, the lower the supporting platform surface of the calibration platform is, the better the supporting platform surface is, generally the supporting platform surface is required to be less than 550mm, and the supporting platform surface can be preferably less than 500mm (the turntable is not considered in two values). The existing calibration platform is generally lifted by a scissor-type lifting mechanism, and if the supporting platform surface is too low, the bearing capacity is rapidly reduced (mainly, the bearing capacity is generally limited in a lifting stage). Moreover, no calibration platform capable of adapting to different radiation detectors is available at home, and the requirements of each detector on each index of the platform are different. Therefore, a high-compatibility calibration device is designed, on the premise of large bearing, a high-precision large-stroke range is realized, the initial height of the table top is reduced as much as possible, the function of adjusting the inclination angle of the table top is provided, the time required by a calibration test can be shortened, repeated construction can be reduced, expenditure is saved, and great challenges are faced.
SUMMERY OF THE UTILITY MODEL
The utility model discloses a technical purpose designs one kind and can realize the big stroke scope of high accuracy, reduces the minimum stroke height of demarcation platform simultaneously as far as to have the high compatibility space radiation detector ground calibration device of the adjustable function in mesa inclination.
The utility model discloses a scheme as follows:
the utility model provides a high compatibility space radiation detector ground calibration device, includes interface platform, two segmentation elevating platforms and translation transport table, the interface platform includes the interface board, its characterized in that:
the two-section type lifting platform comprises a first section lifting mechanism and a second section lifting mechanism;
the first section of lifting mechanism is a scissor type lifting machine, the scissor type lifting machine comprises a top frame, a bottom frame and a scissor pair for connecting the top frame and the bottom frame, an interface table is installed on the top frame, a return force supporting mechanism is installed on the upper surface of the bottom frame and comprises a plurality of spring pieces which are symmetrically distributed on the bottom frame, when the top frame is lowered to an initial position, the top frame presses on the spring pieces, and the spring pieces are in a compressed state;
the second section of lifting mechanism comprises screw rod lifters distributed at four corners of the bottom frame, the screw rod lifters are vertically arranged at the outer side of the bottom frame, nut sleeves of the screw rod lifters are connected with the bottom frame, and the bottom frame moves up and down along with the nut sleeves under the driving of a motor;
the translation transport table is equipped with and lifts the platform and install the gyro wheel in lifting the platform below, it is less than during lead screw lift up-motion to the maximum stroke to lift the height of platform upper surface bottom frame lower surface, the translation transport table passes through the bottom frame of lifting and the below mesa or the below of the space passageway motion bottom frame that forms between the ground.
On the basis of the scheme, the improved scheme further comprises the following steps:
furthermore, the frame matrixes of the top frame and the bottom frame are in a shape of Chinese character ri and comprise rectangular outer frames and cross beams fixedly arranged in the middle of the outer frames, first lead screw installation seats are arranged on the cross beams and arranged downwards, and first lead screw installation seats of the bottom frame are arranged upwards; the inner side surfaces of two frames of the outer frame are provided with a left transverse linear chute, a right transverse linear chute and a left shaft lever mounting seat and a right shaft lever mounting seat which are opposite, the transverse linear chutes and the shaft lever mounting seats are respectively positioned at the front side and the rear side of the cross beam, and in the vertical direction, the transverse linear chute and the shaft lever mounting seat of the top frame respectively correspond to the transverse linear chute and the shaft lever mounting seat of the bottom frame up and down; the end part of the scissor arm at one side of the scissor pair is connected with the transverse linear sliding chute through a sliding block type connecting shaft, and the end part of the scissor arm at the other side of the scissor pair is connected with the shaft lever mounting seat through a hinged shaft; the scissor lift comprises a first linear motion module arranged on a top frame and a second linear motion module arranged on a bottom frame, the two linear motion modules comprise a screw rod, a nut sleeve and a servo motor, the two linear motion modules are arranged in the front and rear directions oppositely, one end of the screw rod is arranged on the top frame or the bottom frame through a second shaft rod mounting seat, and the other end of the screw rod is arranged in a first shaft rod mounting seat of a corresponding cross beam.
Furthermore, the translation transport table is a remote control universal translation transport table, and the rollers below the lifting platform are universal wheel sets and driven by a servo motor provided with a remote control circuit.
Furthermore, the bottom of the screw rod lifter is provided with a disc type support leg.
Furthermore, a limiting mechanism fixedly connected with the bottom frame is arranged on the lifting platform of the translation transport table.
Furthermore, the spring part of the return force supporting mechanism is a column type spring ring, and a limiting shaft core inserted into the spring ring from the upper part is fixedly arranged on the lower surface of the top frame at a position corresponding to the spring ring.
Further, the utility model discloses calibration device is equipped with the detection the measurement feedback mechanism of first section elevating system and second section elevating system stroke.
Furthermore, the interface board is provided with array threaded holes, a turntable interface, a temperature and humidity sensor interface and level meter measuring positions, wherein the array threaded holes are uniformly distributed on the surface of the interface board, the temperature and humidity sensor interface is arranged on the opposite side of the interface board, and the level meter measuring positions are uniformly distributed on the edge side of the interface board.
Furthermore, a servo motor of the first linear motion module is positioned below the interface board, and the interface board is provided with a door plate which can be opened and closed or detached at a position corresponding to the servo motor.
The beneficial effects of the utility model are that:
1) The utility model realizes the split of the lifting mechanism and the translation mechanism through the design of the two-section lifting mechanism, the lowest calibration height of the device can be further reduced after the lifting mechanism is separated from the translation mechanism, and meanwhile, the second-section lifting mechanism adopts the screw lifting platform, and the posture adjustment of the inclination angle of the interface plate can be realized in a certain range by utilizing the fit clearance of the screw and the nut pair, thereby meeting the calibration requirements of different conditions;
2) The utility model discloses a contained angle between the scissors arm of scissor lift can further increase through the design of back force supporting mechanism to reduce the minimum calibration height of device, specifically speaking, utilize the spring part of the gravity compression bottom back force supporting mechanism of scissor lift supporting platform in the descending process, make the spring part deposit potential energy, utilize this potential energy compensation to increase because of the scissors arm contained angle increases the motor starting resistance when scissor lift lifts, thereby realize further reducing the minimum calibration height of calibration platform;
3) The utility model discloses the design of the external interface board that the device is relatively independent can provide humiture environment, mesa inclination in the space high energy radiation detector calibration test process to integrate the revolving stage of different grade type as required and provide the required corner demand of detector calibration;
4) The utility model discloses device structural planning is reasonable, and the integrated level is high, and is favorable to satisfying space radiation detector required height in the ground calibration test process and bears, the big stroke reaches minimum mesa height etc.. The utility model discloses calibration device has great compatibility, can satisfy the space radiation detector of different grade type, like the demarcation test demand of loads such as X ray detector, space energy meter to and can realize demarcating platform and the quick alignment of line beam ray export, satisfy the demand of different detectors to the different inclinations of demarcation platform mesa, help shortening test time, improve test efficiency.
Drawings
Fig. 1 is a schematic perspective view of the device of the present invention;
FIG. 2 is a schematic perspective view of the device of the present invention;
FIG. 3 is a schematic view of a partial structure of the supporting frame of the present invention;
FIG. 4 is a schematic view of the bottom frame of the device of the present invention;
FIG. 5 is a schematic view of the structure of the translation stage;
FIG. 6 is a diagram comparing the lowered and raised states of the device of the present invention;
fig. 7 is a schematic structural diagram of the interface board of the present invention.
The reference numbers in the above figures are respectively:
1-interface table, 101-interface board;
2-two-section type lifting mechanism, 201-top frame, 202-bottom frame, 203-servo motor, 204-nut sleeve, 205-spring part, 206-screw rod, 207-servo motor, 208-scissor pair, 209-slide block type connecting shaft, 210-shaft rod mounting seat, 212-transverse linear sliding groove, 213-screw rod, 214-disc type base;
3-a translation transport table, 301-a lifting platform, 302-a roller and 303-a limiting mechanism;
4-measurement feedback mechanism.
Detailed Description
The present invention will now be described in further detail with reference to the accompanying drawings.
The utility model provides a high compatibility space radiation detector ground calibration device, includes main components such as interface platform 1, two segmentation elevating platforms 2, translation transport table 3, measurement feedback mechanism 4, as shown in fig. 1 to 7, the concrete structure of its each part is constituteed as follows:
interface table 1
The interface platform 1 comprises a grid plate and an interface plate 101 which is tiled and fixedly arranged above the grid plate.
An array threaded hole 101-5, a rotary table interface, a temperature and humidity sensor interface 101-3 and a level meter measuring position 101-2 are designed on the interface board 101, wherein:
the array threaded holes 101-5 are uniformly distributed on the surface of the interface board 101 and are used for fixedly connecting a high-energy radiation detector in the test process, and the working table can be further expanded according to the requirement;
more than one turntable interface for installing the turntable 101-4 is reserved on the interface board 101 so as to meet the installation requirements of different turntables selected by different detector calibration experiments;
temperature and humidity sensor interfaces 101-3 are designed on two opposite sides of the interface board 101 in at least one direction and used for monitoring temperature and humidity environments in the calibration test process;
the two ends and the middle position of the edge part of the opposite side in at least one direction of the interface board 101 are reserved with a level meter measuring position 101-2 (the position for installing or placing the level meter measuring position 101-2) for matching and adjusting the inclination angle (generally required to be horizontal 0 degree) required by the calibration platform in the test process.
A removable or openable door panel 101-1 may be reserved in this position when there is a possibility of interference with equipment below the replacement service interface board 101.
In this embodiment: the interface board 101 is made of stainless steel materials, the length and the width of the interface board are 2000mm multiplied by 1200mm, the thickness of the interface board is 10mm, the unevenness of the board surface is better than 0.01mm, the bearing capacity exceeds 1500kg, M6 array threaded holes are reserved, and the hole spacing is 100mm; 2 high-precision temperature and humidity integrated sensors capable of remotely monitoring the temperature and the humidity are arranged at the top of the interface board 101, the temperature precision is 0.1 ℃, and the relative humidity precision is +/-2%; the top of the interface board 101 is reserved with measuring positions of 6 small gradienters, and the inclination angle measuring precision of the gradienters is 0.01 degree; the installation interfaces of 2 rotating tables 101-4 are reserved, two rotating tables 101-4 can be installed independently or used simultaneously according to requirements, one rotating table bears 250kg, the rotation angle resolution is 0.1 'and the precision is 2', the other rotating table bears more than 500kg and the rotation angle resolution is 2.6 'and the precision is 18' (the two rotating tables can be used independently or simultaneously according to requirements). The instrument installed on the interface board 101 can be configured with different parameters according to specific requirements in other projects, and other light and high-strength materials such as aluminum alloy, titanium alloy and the like can be considered if the weight reduction of the device is required to be considered.
(II) two-section type lifting platform
The two-section type lifting platform comprises a first section lifting mechanism and a second section lifting mechanism.
The first stage of the lifting mechanism is a scissor lift, which comprises a top frame 201, a bottom frame 202 and a pair of scissor forks 208 connecting the two.
The top frame 201 and the bottom frame 202 are both rectangular frames, and the frame matrixes of the top frame and the bottom frame are in a shape of Chinese character 'ri'. Taking the bottom frame 202 as an example, as shown in fig. 4, the frame structure shaped like a Chinese character ri includes a rectangular outer frame and a beam fixedly disposed in the middle of the outer frame, the beam is provided with a first lead screw mounting seat, the first lead screw mounting seat of the top frame 201 is disposed downward, and the first lead screw mounting seat of the bottom frame 202 is disposed upward.
In this embodiment, a single-layer scissor pair (or a multi-layer scissor pair according to actual conditions) is adopted, and the scissor pair includes two sets of parallel and symmetrical scissor arms.
The inner side surface of the outer frame is provided with a left transverse linear sliding groove 212, a right transverse linear sliding groove 212, a left shaft lever mounting seat 210 and a right shaft lever mounting seat 210, the transverse linear sliding grooves 212 and the shaft lever mounting seats 210 are respectively located on the front side and the rear side of the cross beam, as shown in fig. 3, the transverse linear sliding groove of the top frame 201 corresponds to the transverse linear sliding groove of the bottom frame 202 up and down, the shaft lever mounting seat of the top frame 201 corresponds to the shaft lever mounting seat of the bottom frame 202 up and down, the end part of the scissors arm at the front side of the scissors fork pair 208 is limited and installed in the transverse linear sliding groove 212 through a slider type connecting shaft 209, and the end part of the scissors arm at the rear side is connected with the shaft lever mounting seat 210 through a hinged shaft. When the included angle of the scissor arm changes, the front side scissor arm end part does linear reciprocating motion along the extending direction of the transverse linear sliding groove 212 (one end of the slider type connecting shaft 209 is a slider installed in the transverse linear sliding groove 212, and the other end is a shaft rod hinged with the scissor arm), while the rear side scissor arm end part only rotates by taking a hinged shaft thereof as a center, and does not generate displacement in the front-rear direction.
The scissor lift comprises a first linear motion module and a second linear motion module which are oppositely arranged in the front and rear directions, and the two linear motion modules comprise a screw rod, a nut sleeve and a servo motor.
As shown in fig. 3, the motor 203 of the first linear motion module is installed at the rear side of the top frame 201, one end of the lead screw is connected with the top frame 201 through the shaft rod installation seat, and the other end of the lead screw is installed in the shaft rod installation seat of the top frame beam in a limiting manner. The servo motor 207 of the second linear motion module is installed at the front side of the bottom frame 202, one end of a screw rod of the second linear motion module is connected with the bottom frame 202 through a second shaft rod installation seat, and the other end of the screw rod is installed in a first shaft rod installation seat of a bottom frame beam in a limiting manner.
After the servo motors of the two linear motion modules are synchronously started, the nut sleeves on the respective screw rods are controlled to move longitudinally in a push-pull mode, so that the included angle of the scissor arms is changed, the included angle is further converted into the lifting motion of the scissor lift, and the height of the interface platform 1 is controlled, as shown in fig. 6. Therefore, the length of the transverse straight sliding groove 212 determines the lifting height of the scissor lift, and the stroke range of the scissor lift can be adjusted by changing the length of the transverse straight sliding groove 212 according to the requirements of actual conditions.
The grating plate of the interface platform 1 is fixed on the top frame 201, the servo motor 203 of the first linear motion module is located below the interface board 101, and the interface board 101 is provided with a door plate which can be opened and closed or detached at the edge position corresponding to the servo motor 203, so as to facilitate detection and maintenance and avoid interference.
The second section of lifting mechanism comprises four lead screw lifters respectively arranged at four corners of the bottom frame 202. The screw rod lifter comprises a screw rod, a nut sleeve and a servo motor 201, wherein a disc type supporting leg 214 is installed at the bottom of the screw rod, the nut sleeve is rigidly connected with the bottom frame 202 through a connecting seat, and a shell of the servo motor 201 is also fixed on the connecting seat. Each screw rod lifter is vertically arranged on the outer side of the bottom frame 202, and the bottom frame 202 can move up and down along with the nut sleeve on the screw rod 213 under the driving of the servo motor 201.
When the top frame 202 descends to an initial position, the top frame 201 presses on the spring piece, and the spring piece 205 is in a compressed state. As shown in fig. 1 and 6, in the present embodiment, the spring element of the return support mechanism is a column-type spring ring, and a position-limiting shaft core inserted into the spring ring from above is fixedly installed on the lower surface of the top frame 201 at a position corresponding to the spring ring, so that the spring ring is axially offset.
(III) translational transport table
Translation transport table 3 is equipped with and lifts platform 301 and installs gyro wheel 302 in lifting platform below, the upper surface height of lifting platform 301 will be less than when the lead screw lift upwards moves to the maximum stroke the height of bottom frame 202 lower surface, translation transport table 3 can move the below of bottom frame 202 through the space passageway that forms between the bottom frame 202 of lifting and below mesa or the ground to the bottom frame 202 contact that descends. Meanwhile, a limiting mechanism such as a positioning pin and the like for fixing the bottom frame 202 is arranged on the lifting platform 301, so that the two-section type lifting table is prevented from moving on the surface of the lifting platform in the process of translation or posture adjustment.
In practice, translation transport table 3 preferably adopts the universal translation transport table of remote control, and its gyro wheel of lifting the platform below is universal wheelset, drives through the servo motor that is equipped with remote control circuit, and translation transport table 3 can be convenient the transfer of realization arbitrary direction, and here is prior art, does not detailed again promptly. In this embodiment, the lifting platform 301 is 1000mm × 800mm × 10mm, and is made of a steel material.
(IV) measuring feedback mechanism
The measurement feedback mechanism 4 comprises a sensor for detecting the motion stroke of the first section of lifting mechanism and the second section of lifting mechanism. In this embodiment, both use linear displacement grating chi, possess high accuracy measurement display and feedback function, measurement accuracy is superior to 0.01mm. After the device is integrated integrally, the displacement precision is better than 0.02mm through calibration. The signal output end of the sensor is connected with the remote control platform through wireless communication equipment, and the influence on human irradiation in the test process of the high-energy radiation detector can be greatly avoided. The grating ruler selected in the embodiment considers the calibration requirements of most high-energy radiation detectors, but the grating ruler with higher precision or other types of spherical grating rulers and magnetic grating rulers with measurement and feedback functions can be further optimized and changed according to the requirements.
In the embodiment, the maximum horizontal displacement stroke of the screw rod of the scissor-type lifting platform is designed to be 700mm, the height of the lowest table top of the interface board is 460mm, and the maximum lifting stroke is 550mm; the maximum effective displacement stroke of the screw rod lifter is 270mm.
The working principle is as follows:
the utility model discloses two sections elevating system of ground calibration device all can realize the high lifting to interface platform 1, but work phase mainly accomplishes lifting by a wide margin and the height adjustment to interface platform 1 through first section elevating system's scissors fork formula elevating platform, and second section elevating system lead screw elevating platform mainly used is to the fine setting of interface platform slope gesture to and the lifting of mechanism more than the bottom frame 202 is realized to cooperation translation transport table 3. The method comprises the following specific steps:
1) Lifting operation
When the interface platform 1 is at the lowest height, the included angle of the two arms of the scissor pair 208 is close to 180 degrees, and the lifting with load has high requirement on the output torque of the motor at the moment; in the lifting process, along with the gradual reduction of the included angle of the two arms of the scissor pair 208, the demand of the vertical displacement motion on the output torque of the motor is rapidly reduced. In order to reduce the difficulty of initial lifting, spring elements are arranged at four corners below the top frame, and when the interface platform 1 is lifted from the lowest position, the spring elements are in a compressed state to release elastic potential energy, so that the requirement of actual load on the output torque of the motor is reduced.
2) Translational operation
The control system of the remote control platform lifts the bottom frame 202 by controlling four servo motors 201 at four corners of the second lifting mechanism to work cooperatively until the height distance between the bottom frame 202 and the lower table surface or the ground can be inserted into the translation transport table 3, then the translation transport table 3 is remotely controlled to move to the lower part of the bottom frame 202 automatically, the bottom frame 202 with the upper layer structure is lowered until the bottom frame 202 is contacted with the lifting table surface 301 of the translation transport table 3, at the moment, the four servo motors 201 continue to work, as the bottom frame 202 with the nut sleeve on the screw rod lifting table can not be lowered continuously, the screw rod can drive the disc type supporting legs 214 at the bottom to lift relative to the bottom frame, when the disc type supporting legs 214 are separated from the ground, the servo motors 201 can stop moving, after the bottom frame 202 and the lifting table 301 are fixed through the limiting mechanism, the translation transport table 3 is started, and the whole calibration device is transferred to a proper position.
When the calibration device works, the reverse operation of the process is implemented, the translation transport table 3 is evacuated, and the detection device on the interface board 101 can work at the lowest height.
3) Posture adjustment operation
Because a fit clearance exists between the screw rod structure and the nut sleeve, the remote control platform can realize the fine adjustment of the inclination angle of the interface board 101 by independently controlling the servo motors 201 at the four corners of the second lifting mechanism to independently work, and adjust the interface board to a horizontal state or a non-horizontal state. The model number YS80B5-0.75KW of the screw rod lifter is adopted in the embodiment, the specification of the screw rod is Tr40 x 7, and the maximum horizontal inclination angle of each side of the interface board 101 can be controlled between 2 and 5 degrees.
The utility model discloses calibration device can adjust equipment such as the detector on the interface board 101 to the suitable position of ray beam and direction through above-mentioned operation. The utility model discloses calibration device is at the during operation, and the bottom is direct to contact with ground (or in order to avoid the influence that the unevenness in ground brought, also can only support through the disc type base 214 in four corners, and control bottom frame 202 exceeds ground 1 ~ 2 mm). Before and after the test, the calibration device needs to be preliminarily calibrated with the beam incident direction, manual adjustment can be used in the stage, short-distance transportation is carried out through translation operation, and remote control circuit board interfaces for controlling all servo motors are reserved on the table board of the interface board 101, so that remote control transportation and angle adjustment inside a factory building are finally realized.
The irradiation in the beam testing process is considered, and the calibration platform with the remote control function is commonly used. However, a calibration device which simultaneously meets the following conditions does not exist at present in China: the bearing capacity is 1500kg or more, the lowest height (from the ground) of the table top is not more than 500mm, the displacement precision reaches 0.03mm or more, and the turntable is compatible with different requirements; the calibration platform with the indexes can be compatible with the calibration test of most of space radiation detectors which are developed at home at present or may be developed in the future.
Practice proves that the highest safe load of the calibration device can reach 1620kg (design value 1200kg, design margin is 1.35) at present, the displacement precision can be controlled to be about 0.01mm based on the existing high-precision screw rod mechanism, the calibration device is superior to the existing calibration device, the calibration device can be compatible with the calibration test of most of the currently developed space radiation detectors in China, and further optimized space exists. Meanwhile, according to the result of actual test, under the condition of full load, the output current of the servo motor of the scissor lift is reduced to 2A from 5A by means of the auxiliary supporting mechanism, and is reduced by more than half. The calibration device of the embodiment is designed for the outer interface board, can provide a temperature and humidity environment and a table top inclination angle in the calibration test process of the space high-energy radiation detector, and integrates different types of rotary tables as required to provide the rotation angle requirement required by the calibration of the detector. The calibration device can meet the calibration requirement for adjusting the inclination angle of the table board as required, overcomes the adverse effect caused by the fact that the ground of a test field is not smooth enough, and solves the problem of quick assembly, calibration and alignment of the ground calibration platform.
It should be noted that, in the present invention, the terms "upper", "lower", "left", "right", "front", "back", etc. are used for the sake of clarity only, and are not used to limit the scope of the present invention, and the relative relationship changes or adjustments may be made without substantial technical changes.
Above only the utility model discloses an it is preferred embodiment, the utility model discloses a scope of protection not only limits in above-mentioned embodiment, and the all belongs to the utility model discloses a technical scheme under the thinking all belongs to the utility model discloses a scope of protection. It should be noted that various modifications and decorations can be made by those skilled in the art without departing from the principle of the present invention, and the scope of the present invention should be considered as the protection scope of the present invention.
Claims (9)
1. The utility model provides a high compatibility space radiation detector ground calibration device, includes interface platform (1), two segmentation elevating platforms (2) and translation transport table (3), interface platform (1) is including interface board (101), its characterized in that:
the two-section type lifting platform (2) comprises a first section lifting mechanism and a second section lifting mechanism;
the first section of lifting mechanism is a scissor type lifter, the scissor type lifter comprises a top frame (201), a bottom frame (202) and a scissor pair (208) for connecting the top frame and the bottom frame, an interface platform (1) is installed on the top frame (201), a return force supporting mechanism is installed on the upper surface of the bottom frame (202), the return force supporting mechanism comprises a plurality of spring pieces (205) which are symmetrically distributed on the bottom frame, when the top frame (201) descends to an initial position, the top frame (201) presses the spring pieces (205), and the spring pieces (205) are in a compression state;
the second section of lifting mechanism comprises screw rod lifters arranged at four corners of the bottom frame (202), the screw rod lifters are vertically arranged on the outer side of the bottom frame (202), nut sleeves of the screw rod lifters are connected with the bottom frame (202), and the bottom frame (202) moves up and down along with the nut sleeves under the driving of a motor;
translation transport table (3) are equipped with lift platform (301) and install gyro wheel (302) of lifting the platform below, the height of lifting platform (301) upper surface is less than when lead screw lift up motion reaches the maximum stroke bottom frame (202) lower surface's height, translation transport table (3) move to the below of bottom frame (202) through the space passageway that forms between bottom frame (202) of lifting and below mesa or the ground.
2. The ground calibration device for the high-compatibility space radiation detector according to claim 1, characterized in that:
the frame matrixes of the top frame (201) and the bottom frame (202) are in a shape of Chinese character 'ri', and comprise a rectangular outer frame and a cross beam fixedly arranged in the middle of the outer frame, wherein the cross beam is provided with a first lead screw mounting seat, the first lead screw mounting seat of the top frame is arranged downwards, and the second lead screw mounting seat of the bottom frame is arranged upwards;
the inner side surfaces of two frames of the outer frame are provided with a left transverse linear sliding groove (212) and a right transverse linear sliding groove (212) which are opposite to each other, and a left shaft lever mounting seat (210) and a right shaft lever mounting seat (210) which are opposite to each other, the transverse linear sliding grooves (212) and the shaft lever mounting seats (210) are respectively positioned on the front side and the rear side of the cross beam, and in the vertical direction, the transverse linear sliding grooves and the shaft lever mounting seats of the top frame (201) respectively correspond to the transverse linear sliding grooves and the shaft lever mounting seats of the bottom frame (202) up and down; the end part of the scissor arm at one side of the scissor pair (208) is connected with the transverse linear sliding groove (212) through a sliding block type connecting shaft (209), and the end part of the scissor arm at the other side is connected with the shaft lever mounting seat (210) through a hinged shaft;
the scissor lift comprises a first linear motion module arranged on a top frame (201) and a second linear motion module arranged on a bottom frame (202), wherein the two linear motion modules comprise a screw rod, a nut sleeve and a servo motor, the two linear motion modules are arranged in the front direction and the rear direction oppositely, one end of the screw rod is arranged on the top frame (201) or the bottom frame (202) through a second shaft rod mounting seat, and the other end of the screw rod is arranged in a first shaft rod mounting seat of a corresponding cross beam.
3. The ground calibration device for the high-compatibility space radiation detector according to claim 1, wherein:
the translation transport table (3) is a remote control universal translation transport table, and rollers below the lifting platform (301) are universal wheel sets and driven by a motor provided with a remote control circuit.
4. The ground calibration device for the high-compatibility space radiation detector according to claim 1, wherein:
and a disc type supporting leg (214) is arranged at the bottom of the screw rod lifter.
5. The ground calibration device for the high-compatibility space radiation detector according to claim 1, wherein:
and a limiting mechanism (303) fixedly connected with the bottom frame (202) is arranged on the lifting platform (301) of the translation transport table (3).
6. The ground calibration device for the high-compatibility space radiation detector according to claim 1, characterized in that:
the spring part (205) of the return force supporting mechanism is a column type spring ring, and a limiting shaft core inserted into the spring ring from the upper side is fixedly arranged on the lower surface of the top frame (201) at a position corresponding to the spring ring.
7. The ground calibration device for the high-compatibility space radiation detector according to claim 1, wherein:
and a measurement feedback mechanism (4) for detecting the strokes of the first section of lifting mechanism and the second section of lifting mechanism is arranged.
8. The ground calibration device for the high-compatibility space radiation detector according to claim 1, wherein:
the interface board (101) is provided with array threaded holes, a rotary table interface, a temperature and humidity sensor interface (101-3) and level meter measuring positions (101-2), wherein the array threaded holes are uniformly distributed on the surface of the interface board (101), the temperature and humidity sensor interface (101-3) is arranged on the opposite side of the interface board, and the level meter measuring positions (101-2) are uniformly distributed on the edge side of the interface board.
9. The ground calibration device for the high-compatibility space radiation detector according to claim 2, wherein:
the servo motor of the first linear motion module is positioned below the interface board (101), and the interface board (101) is provided with a door panel (101-1) which can be opened, closed or disassembled at a position corresponding to the servo motor.
Priority Applications (1)
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