CN112693634A - Satellite solar wing positioning tool - Google Patents
Satellite solar wing positioning tool Download PDFInfo
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- CN112693634A CN112693634A CN202110304612.XA CN202110304612A CN112693634A CN 112693634 A CN112693634 A CN 112693634A CN 202110304612 A CN202110304612 A CN 202110304612A CN 112693634 A CN112693634 A CN 112693634A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/42—Arrangements or adaptations of power supply systems
- B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
- B64G1/443—Photovoltaic cell arrays
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Abstract
The invention discloses a satellite solar wing positioning tool, which belongs to the technical field of satellite installation and comprises a carrying platform, a plane moving mechanism, a rotating mechanism, a lifting adjusting mechanism, a supporting mechanism and a grabbing mechanism, wherein the carrying platform can be fixedly arranged on a transfer carriage, the plane moving mechanism is fixedly arranged on the carrying platform, the rotating mechanism is arranged on the plane moving mechanism, the lifting adjusting mechanism is arranged on the rotating mechanism, the supporting mechanism is arranged on the rotating mechanism, and the grabbing mechanism is arranged on the lifting adjusting mechanism. According to the satellite solar wing positioning tool, the grabbing mechanism is used for clamping the satellite solar wing, the plane moving mechanism is used for adjusting the horizontal position of the satellite solar wing, the rotating mechanism is used for adjusting the horizontal angle of the satellite solar wing, the lifting adjusting mechanism is matched with the supporting mechanism, and the height and the multi-direction angle of the satellite solar wing are adjusted, so that the satellite solar wing positioning tool is accurate in positioning.
Description
Technical Field
The invention relates to the technical field of satellite installation, in particular to a satellite solar wing positioning tool.
Background
The solar wing is an energy source of the satellite, the solar wing is in a folded state when the satellite launches, the satellite and the arrow are opened after being separated, and the direction is continuously adjusted in the flying process of the satellite, so that the solar cell is aligned to the sun, and energy is provided for the whole satellite to work. The solar sailboard has two functions of power supply and charging, is equivalent to a small power station, is not the same thing as the solar sail, is a device for collecting solar energy, and the solar sail is a spacecraft for space navigation by utilizing the light pressure of sunlight.
The invention discloses a satellite solar wing positioning tool with the prior publication number of CN105834987B, and relates to a satellite solar wing positioning tool, which comprises a transfer trolley, wherein the transfer trolley is provided with a carrying platform, and a translation mechanism is arranged on the carrying platform; the translation mechanism comprises a first flange plate, a cross beam, a second flange plate, a first ball screw fixedly arranged on the first flange plate and a second ball screw fixedly arranged on the second flange plate; when the first ball screw is rotated, the cross beam can slide on the first flange plate along the direction of the first ball screw; when the second ball screw is rotated, the second flange plate can slide on the cross beam along the direction of the second ball screw.
According to the invention, in the process of positioning the solar wing, the solar wing is always horizontally placed, when an angle deviation exists between the satellite and the solar wing, fine adjustment cannot be carried out, the positioning is not accurate, and meanwhile, the ball is adopted for moving, so that the accuracy rate is low.
Disclosure of Invention
The embodiment of the invention provides a satellite solar wing positioning tool, which aims to solve the technical problem.
The embodiment of the invention adopts the following technical scheme: the utility model provides a satellite solar wing location frock, includes cargo platform, plane moving mechanism, rotary mechanism, lift adjustment mechanism, supporting mechanism and snatchs the mechanism, cargo platform fixed mounting is on transporting the carriage, plane moving mechanism fixed mounting is on cargo platform, rotary mechanism installs on plane moving mechanism, lift adjustment mechanism installs on rotary mechanism, supporting mechanism installs on rotary mechanism, it installs on lift adjustment mechanism to snatch the mechanism.
Further, the plane moving mechanism includes first lead screw slip table, second lead screw slip table, removal track, removal telescopic link, removal slider and lower bearing board, first lead screw slip table fixed mounting is on objective platform, second lead screw slip table fixed mounting is on objective platform and is perpendicular contained angle with first lead screw slip table direction of installation, remove orbital one end and install on the slip table of first lead screw slip table, be equipped with the removal spout on the removal track, it slides and sets up in removing orbital removal spout to remove the slider, the lower bearing board welding is at the bottom of removing the slider and lower bearing board and removal track sliding fit, the one end of removing the telescopic link is installed on the slip table of second lead screw slip table and the other end is installed under on the bearing board.
Further, rotary mechanism includes loading board, swivel bearing, rotary disk, rotatory ring gear, support frame, rotary gear, bears frame and rotating electrical machines, it welds at the top of removing the slider and goes up loading board and removal track sliding fit to go up the loading board, swivel bearing installs the top at last loading board, the rotary disk cover is established on swivel bearing's outer lane and rotary disk and last loading board normal running fit, rotatory ring gear fixed cover is established on the outer lane of rotary disk, the support frame welds on the lateral wall of last loading board, bear the welding on the support frame, rotating electrical machines installs on bearing frame, rotating electrical machines's main shaft runs through the support frame setting, the rotary gear rotates and installs on the support frame and connect on rotating electrical machines's main shaft, rotary gear meshes with rotatory ring gear mutually.
Further, the lifting adjusting mechanism comprises a supporting plate, an adjusting plate and three lifting adjusting components, when the supporting plate is welded on the rotating disk, the three lifting adjusting components are all arranged on the supporting plate, each lifting adjusting component comprises a lifting motor, a lifting mounting plate, a lifting threaded rod, a lifting slider, two lifting rods, two lifting support rods and four rotating mounting pins, one end of each lifting rod is arranged on the supporting plate, the lifting mounting plate is arranged at the other end of the lifting rod, the lifting motor is arranged on the lifting mounting plate, a main shaft of the lifting motor penetrates through the lifting mounting plate, the lifting threaded rod is rotatably arranged on the lifting mounting plate, one end of the lifting threaded rod is connected to the main shaft of the lifting motor, the lifting slider is sleeved on the lifting threaded rod and the two lifting rods, the lifting slider is in sliding fit with the two lifting rods, and the lifting slider is in threaded, wherein two rotate the mounting pin symmetry and rotate and install on lifting slide, two lifting support pole's one end rotates respectively and installs on two rotate the mounting pin, two in addition rotate the mounting pin and rotate the other end of installing two lifting slide respectively, six on six lifting support pole rotate the mounting pin, the regulating plate is installed on six.
Further, supporting mechanism is including promoting electric jar and universal joint, promote the electric jar and install the top at last loading board, the flexible end at the electric jar of promotion is installed to the other end at the bottom of regulating plate and universal joint to the one end of universal joint.
Further, the grabbing mechanism comprises a grabbing frame, a grabbing electric cylinder, a grabbing moving block, two grabbing sliding plates and two grabbing clamps, the grabbing frame is fixedly installed at the top of the adjusting plate, sliding grooves are formed in the grabbing frame, the two grabbing sliding plates are symmetrically installed in the sliding grooves of the grabbing frame, the grabbing sliding plates are in sliding fit with the grabbing frame, the two grabbing clamps are installed on the two grabbing sliding plates, sliding rails are arranged on the grabbing sliding plates, two sides of the grabbing moving block are installed on the sliding rails of the two grabbing sliding plates, the grabbing electric cylinder is installed at the top of the adjusting plate, and the telescopic end of the grabbing electric cylinder penetrates through the grabbing frame and is hinged to the grabbing moving block.
Further, the bottom of lower loading board is equipped with the universal wheel.
The embodiment of the invention adopts at least one technical scheme which can achieve the following beneficial effects:
the plane moving mechanism drives the moving rail to move by the first screw rod sliding table, drives the moving slide block to move, so that the moving telescopic rod is stretched or contracted, the moving slide block is controlled to transversely move on the carrying platform, then the moving telescopic rod is driven to move by the second screw rod sliding table, the moving telescopic rod moves to drive the moving slide block to move in a moving chute in the moving rail, the moving slide block is controlled to longitudinally move on the carrying platform, and the first screw rod sliding table and the second screw rod sliding table are matched to control a satellite sun wing to align a satellite for positioning; before work begins, the objective platform is horizontally placed, when the satellite solar wing is positioned and installed, the first screw rod sliding table and the second screw rod sliding table are operated to drive the movable sliding block to move on the objective platform, so that the device drives the satellite solar wing to align to the satellite installation position, and the satellite solar wing is accurately positioned.
The rotating mechanism is characterized in that a rotating gear ring is driven by a rotating motor to rotate, the rotating gear ring rotates to drive a rotating disc to rotate, the rotating disc rotates on the upper bearing plate under the action of a rotating bearing, and the rotating gear ring adopt a structure that a small circle drives a large circle, so that the rotating precision of the device is improved, the satellite solar wing is positioned conveniently, and the satellite solar wing is accurately installed on a satellite; after the horizontal position of the plane moving mechanism is adjusted, the rotating motor operates to drive the rotating gear to rotate, the rotating gear rotates to drive the rotating gear ring to rotate, and the rotating gear ring rotates to drive the rotating disk to rotate, so that the orientation of the satellite solar wing can be adjusted, and the satellite solar wing can be conveniently positioned and installed.
Thirdly, the lifting adjusting mechanism drives the lifting threaded rod to rotate by the lifting motor, the lifting threaded rod rotates to drive the lifting sliding block to slide up and down on the lifting threaded rod and the lifting rod, so that one side of the adjusting plate is driven to lift, the angle and the height of the adjusting plate can be adjusted, the three lifting adjusting components operate simultaneously, the angle and the height of the satellite solar wing can be adjusted in an all-dimensional mode, the satellite solar wing is accurately positioned, meanwhile, the two ends of the lifting supporting rod between the lifting sliding block and the adjusting plate are connected through rotating mounting pins, and the adjusting accuracy is improved; when work goes on, three elevator motor functions, drives three lifting slide and removes, under supporting mechanism's cooperation, carries out angle regulation and height to the adjusting plate, is favorable to driving satellite sun wing and aims at the satellite mounting hole, can realize carrying out diversified angle modulation with satellite sun wing, fixes a position accurately.
Drawings
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the invention and not to limit the invention. In the drawings:
FIG. 1 is a first perspective view of the present invention;
FIG. 2 is a second perspective view of the present invention;
FIG. 3 is a schematic perspective view of the planar moving mechanism of the present invention;
fig. 4 is a schematic perspective view of the rotating mechanism of the present invention;
FIG. 5 is a schematic perspective view of the lift adjustment mechanism of the present invention;
FIG. 6 is a schematic perspective view of the supporting mechanism of the present invention;
FIG. 7 is a schematic perspective view of the grasping mechanism according to the present invention;
fig. 8 is a partial perspective view of the present invention.
Reference numerals:
the object carrying platform 1, the plane moving mechanism 2, the rotating mechanism 3, the lifting adjusting mechanism 4, the supporting mechanism 5, the grabbing mechanism 6, the first lead screw sliding table 21, the second lead screw sliding table 22, the moving track 23, the moving telescopic rod 24, the moving slider 25, the lower bearing plate 26, the upper bearing plate 31, the rotating bearing 32, the rotating disk 33, the rotating gear ring 34, the supporting frame 35, the rotating gear 36, the bearing frame 37, the rotating motor 38, the supporting plate 41, the adjusting plate 42, the lifting adjusting assembly 43, the lifting motor 44, the lifting mounting plate 45, the lifting threaded rod 46, the lifting slider 47, the lifting rod 48, the lifting support rod 49, the rotating mounting pin 491, the pushing electric cylinder 51, the universal joint 52, the grabbing frame 61, the grabbing electric cylinder 62, the grabbing moving block 63, the grabbing sliding plate 64, the grabbing clamp 65 and.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the technical solutions of the present invention will be clearly and completely described below with reference to the specific embodiments of the present invention and the accompanying drawings. It is to be understood that the described embodiments are merely exemplary of the invention, and not restrictive of the full scope of the invention. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
The technical solutions provided by the embodiments of the present invention are described in detail below with reference to the accompanying drawings.
Referring to fig. 1 to 8, an embodiment of the invention provides a satellite solar wing positioning tool, which includes a carrying platform 1, a planar moving mechanism 2, a rotating mechanism 3, a lifting adjusting mechanism 4, a supporting mechanism 5 and a grabbing mechanism 6, wherein the carrying platform 1 can be fixedly installed on a transfer carriage, the planar moving mechanism 2 is fixedly installed on the carrying platform 1, the rotating mechanism 3 is installed on the planar moving mechanism 2, the lifting adjusting mechanism 4 is installed on the rotating mechanism 3, the supporting mechanism 5 is installed on the rotating mechanism 3, and the grabbing mechanism 6 is installed on the lifting adjusting mechanism 4.
Preferably, referring to fig. 3, the plane moving mechanism 2 includes a first screw rod sliding table 21, a second screw rod sliding table 22, a moving track 23, a moving telescopic rod 24, a moving slider 25 and a lower bearing plate 26, the first screw rod sliding table 21 is fixedly arranged on the carrying platform 1, the second screw rod sliding table 22 is fixedly arranged on the carrying platform 1 and forms a vertical included angle with the installation direction of the first screw rod sliding table 21, one end of the moving track 23 is arranged on the sliding table of the first screw rod sliding table 21, a moving sliding groove is arranged on the moving track 23, the moving slide block 25 is arranged in the moving slide groove of the moving track 23 in a sliding manner, the lower bearing plate 26 is welded at the bottom of the moving slide block 25, the lower bearing plate 26 is in sliding fit with the moving track 23, one end of the movable telescopic rod 24 is installed on the sliding table of the second screw rod sliding table 22, and the other end is installed on the lower bearing plate 26; the plane moving mechanism 2 drives the moving rail 23 to move by the first screw rod sliding table 21, drives the moving slide block 25 to move, so as to stretch or contract the moving telescopic rod 24, controls the moving slide block 25 to move transversely on the object carrying platform 1, drives the moving telescopic rod 24 to move by the second screw rod sliding table 22, moves the moving telescopic rod 24 to drive the moving slide block 25 to move in the moving chute in the moving rail 23, controls the moving slide block 25 to move longitudinally on the object carrying platform 1, and controls the sun wing of the satellite to align to the satellite by the cooperation of the first screw rod sliding table 21 and the second screw rod sliding table 22 to position; before the work begins, the objective platform 1 is horizontally placed, when the satellite solar wing is positioned and installed, the first screw rod sliding table 21 and the second screw rod sliding table 22 operate to drive the movable sliding block 25 to move on the objective platform 1, so that the device drives the satellite solar wing to align to the satellite installation position, and the satellite solar wing is accurately positioned.
Preferably, referring to fig. 4, the rotating mechanism 3 includes an upper bearing plate 31, a rotating bearing 32, a rotating disc 33, a rotating ring gear 34, a supporting frame 35, a rotating gear 36, a bearing frame 37 and a rotating motor 38, the upper bearing plate 31 is welded on the top of the moving slider 25, the upper bearing plate 31 is in sliding fit with the moving track 23, the rotating bearing 32 is installed on the top of the upper bearing plate 31, the rotating disc 33 is sleeved on the outer ring of the rotating bearing 32, the rotating disc 33 is in rotating fit with the upper bearing plate 31, the rotating ring gear 34 is fixedly sleeved on the outer ring of the rotating disc 33, the supporting frame 35 is welded on the side wall of the upper bearing plate 31, the bearing frame 37 is welded on the supporting frame 35, the rotating motor 38 is installed on the bearing frame 37, the main shaft of the rotating motor 38 penetrates through the supporting frame 35, the rotating gear 36 is rotatably, the rotary gear 36 is meshed with the rotary gear ring 34; the rotating mechanism 3 is characterized in that a rotating motor 38 drives a rotating gear ring 34 to rotate, the rotating gear ring 34 rotates to drive a rotating disc 33 to rotate, the rotating disc 33 rotates on the upper bearing plate 31 under the action of a rotating bearing 32, and a structure that a small circle drives a large circle is adopted by a rotating gear 36 and the rotating gear ring 34, so that the rotating accuracy of the device is improved, the satellite sun wing is positioned conveniently, and the satellite sun wing is accurately installed on a satellite; after the horizontal position of the plane moving mechanism 2 is adjusted, the rotating motor 38 operates to drive the rotating gear 36 to rotate, the rotating gear 36 rotates to drive the rotating gear ring 34 to rotate, and the rotating gear ring 34 rotates to drive the rotating disk 33 to rotate, so that the orientation of the satellite sun wing can be adjusted, and the satellite sun wing can be conveniently positioned and installed.
Preferably, referring to fig. 5, the lifting adjusting mechanism 4 includes a supporting plate 41, an adjusting plate 42 and three lifting adjusting assemblies 43, when the supporting plate 41 is welded on the rotating disk 33, three lifting adjusting assemblies 43 are mounted on the supporting plate 41, each lifting adjusting assembly 43 includes a lifting motor 44, a lifting mounting plate 45, a lifting threaded rod 46, a lifting slider 47, two lifting rods 48, two lifting support rods 49 and four rotating mounting pins 491, one end of each of the two lifting rods 48 is mounted on the supporting plate 41, the lifting mounting plate 45 is mounted at the other end of the lifting rod 48, the lifting motor 44 is mounted on the lifting mounting plate 45, the main shaft of the lifting motor 44 penetrates through the lifting mounting plate 45, the lifting threaded rod 46 is rotatably mounted on the lifting mounting plate 45, and one end of the lifting threaded rod is connected to the main shaft of the lifting motor 44, the lifting slide block 47 is sleeved on the lifting threaded rod 46 and the two lifting rods 48, the lifting slide block 47 is in sliding fit with the two lifting rods 48, the lifting slide block 47 is in threaded fit with the lifting threaded rod 46, two rotating mounting pins 491 are symmetrically and rotatably mounted on the lifting slide block 47, one ends of two lifting support rods 49 are respectively rotatably mounted on the two rotating mounting pins 491, the other two rotating mounting pins 491 are respectively rotatably mounted at the other ends of the two lifting slide blocks 47, and the adjusting plate 42 is mounted on six rotating mounting pins 491 on the six lifting support rods 49; the lifting adjusting mechanism 4 is characterized in that a lifting motor 44 drives a lifting threaded rod 46 to rotate, the lifting threaded rod 46 rotates to drive a lifting slider 47 to slide up and down on the lifting threaded rod 46 and a lifting rod 48, so that one side of an adjusting plate 42 is driven to lift, the angle and height of the adjusting plate 42 can be adjusted, the three lifting adjusting components 43 operate simultaneously, the angle and height of a satellite solar wing can be adjusted in an omnibearing manner, the satellite solar wing is accurately positioned, and meanwhile, the two ends of a lifting support rod 49 between the lifting slider 47 and the adjusting plate 42 are connected through rotating mounting pins 491, so that the adjusting accuracy is improved; when work goes on, three elevator motor 44 functions, drives three lifting slide 47 and removes, under the cooperation of supporting mechanism 5, carries out angle regulation and height to adjusting plate 42, is favorable to driving satellite sun wing and aims at the satellite mounting hole, can realize carrying out diversified angle modulation with satellite sun wing, and the location is accurate.
Preferably, as shown in fig. 6, the support mechanism 5 comprises an electric pushing cylinder 51 and a universal joint 52, the electric pushing cylinder 51 is mounted on the top of the upper bearing plate 31, one end of the universal joint 52 is mounted on the bottom of the adjusting plate 42, and the other end of the universal joint 52 is mounted on the telescopic end of the electric pushing cylinder 51; the supporting mechanism 5 drives the adjusting plate 42 to ascend and descend among the three ascending and descending adjusting assemblies 43 by pushing the electric cylinder 51, and adjusts the adjusting plate 42 by matching with the ascending and descending adjusting assemblies 43 so as to prevent the adjusting plate 42 from being clamped due to the gravity problem; when the lifting adjusting mechanism 4 is operated, the electric cylinder 51 is pushed to start operating, the vertical height of the adjusting plate 42 is controlled, and the universal joint 52 is matched, so that the adjusting plate 42 is not blocked from steering.
Preferably, referring to fig. 7, the grabbing mechanism 6 includes a grabbing frame 61, a grabbing electric cylinder 62, a grabbing moving block 63, two grabbing sliding plates 64 and two grabbing clamps 65, the grabbing frame 61 is fixedly mounted on the top of the adjusting plate 42, a sliding slot is formed in the grabbing frame 61, the two grabbing sliding plates 64 are symmetrically mounted in the sliding slot of the grabbing frame 61, the two grabbing sliding plates 64 are in sliding fit with the grabbing frame 61, the two grabbing clamps 65 are mounted on the two grabbing sliding plates 64, a sliding rail is formed on each of the two grabbing sliding plates 64, two sides of the grabbing moving block 63 are mounted on the sliding rails of the two grabbing sliding plates 64, the grabbing electric cylinder 62 is mounted on the top of the adjusting plate 42, and a telescopic end of the grabbing electric cylinder 62 penetrates through the grabbing frame 61 and is hinged to the grabbing moving block 63; the grabbing mechanism 6 drives the grabbing moving block 63 to move on the two grabbing sliding plates 64 by the grabbing electric cylinder 62, and controls the two grabbing sliding plates 64 to move on the grabbing frame 61, so that the two grabbing clamps 65 are driven to clamp the satellite solar wing, the satellite solar wing is conveniently positioned and installed, and the satellite solar wing is prevented from sliding to interfere with positioning in the installation process; before the work begins, the grabbing electric cylinder 62 starts to operate, drives the two grabbing clamps 65 to clamp the satellite solar wing, and then the grabbing mechanism 6 drives the satellite solar wing to move to the installation position to be installed under the driving of the plane moving mechanism 2 and the lifting adjusting mechanism 4.
Preferably, referring to fig. 8, the bottom of the lower bearing plate 26 is provided with universal wheels 7; the universal wheel 7 is installed in the bottom of lower bearing board 26, and universal wheel 7 direct contact carries the thing plane, for providing the holding power for lower bearing board 26, prevents to remove slider 25 under the influence of device gravity, and the card is on removing track 23, prevents to damage and removes track 23 and remove slider 25.
The working principle of the invention is as follows: before the work starts, the grabbing electric cylinder 62 starts to operate to drive the two grabbing clamps 65 to clamp the satellite solar wing, the plane moving mechanism 2 drives the moving rail 23 to move by the first screw rod sliding table 21 to drive the moving slide block 25 to move, so that the moving telescopic rod 24 is stretched or contracted, the moving slide block 25 is controlled to transversely move on the carrying platform 1, then the moving telescopic rod 24 is driven to move by the second screw rod sliding table 22, the moving telescopic rod 24 moves to drive the moving slide block 25 to move in a moving chute in the moving rail 23, the moving slide block 25 is controlled to longitudinally move on the carrying platform 1, and the first screw rod sliding table 21 and the second screw rod sliding table 22 are matched to control the satellite solar wing to align to a satellite for positioning; before the work starts, the loading platform 1 is horizontally placed, when the satellite solar wing is positioned and installed, the first screw rod sliding table 21 and the second screw rod sliding table 22 operate to drive the movable sliding block 25 to move on the loading platform 1, so that the device drives the satellite solar wing to align with the satellite installation position, the satellite solar wing is accurately positioned, the rotating mechanism 3 drives the rotating gear ring 34 to rotate by the rotating motor 38, the rotating gear ring 34 rotates to drive the rotating disc 33 to rotate, the rotating disc 33 rotates on the upper bearing plate 31 under the action of the rotating bearing 32, the rotating gear 36 and the rotating gear ring 34 adopt a structure that a small circle drives a large circle, the rotating accuracy of the device is improved, the satellite solar wing is conveniently positioned and accurately installed on a satellite; after the plane moving mechanism 2 has adjusted the horizontal position, the rotating motor 38 operates to drive the rotating gear 36 to rotate, the rotating gear 36 rotates to drive the rotating gear ring 34 to rotate, the rotating gear ring 34 rotates to drive the rotating disk 33 to rotate, thereby the orientation of the satellite solar wing can be adjusted, and the positioning and installation of the satellite solar wing are convenient, the lifting adjusting mechanism 4 drives the lifting threaded rod 46 to rotate by the lifting motor 44, the lifting threaded rod 46 rotates to drive the lifting slider 47 to slide up and down on the lifting threaded rod 46 and the lifting rod 48, thereby driving one side of the adjusting plate 42 to lift, which can play a role in adjusting the angle and height of the adjusting plate 42, the three lifting adjusting components 43 operate simultaneously, can adjust the angle and height of the satellite solar wing in all directions, make the satellite solar wing positioned accurately, and simultaneously, the two ends of the lifting support rod 49 between the lifting slider 47 and the adjusting plate 42 are connected by the rotating installation, the accuracy of adjustment is improved; when the satellite sun wing positioning device works, the three lifting motors 44 operate to drive the three lifting slide blocks 47 to move, the adjusting plates 42 are adjusted in angle and height under the matching of the supporting mechanism 5, the satellite sun wing is driven to be aligned with a satellite mounting hole, the satellite sun wing can be adjusted in multi-direction angle, positioning is accurate, the supporting mechanism 5 drives the adjusting plates 42 to lift among the three lifting adjusting assemblies 43 by the aid of the electric pushing cylinders 51, the adjusting plates 42 are adjusted by the matching of the lifting adjusting assemblies 43, and the adjusting plates 42 are prevented from being clamped due to gravity; when lifting adjusting mechanism 4 operates, promote electric cylinder 51 and begin to operate, control the vertical height of regulating plate 42, cooperate universal joint 52 simultaneously, it turns to not hinder regulating plate 42 to take place, it snatchs movable block 63 and removes on two snatchs sliding plate 64 by snatching the electric cylinder 62 drive to snatch mechanism 6, control two and snatch sliding plate 64 and remove on snatching frame 61, thereby it snatchs clamp 65 and carries out the centre gripping to satellite solar wing to drive two, conveniently fix a position the satellite solar wing and install, prevent simultaneously that satellite solar wing from producing the slip interference location in the installation, afterwards under planar moving mechanism 2 and lifting adjusting mechanism 4's drive, it drives satellite solar wing and removes to the installation department to snatch mechanism 6, install.
The above description is only an example of the present invention, and is not intended to limit the present invention. Various modifications and alterations to this invention will become apparent to those skilled in the art. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention should be included in the scope of the claims of the present invention.
Claims (7)
1. The utility model provides a satellite solar wing location frock, its characterized in that includes cargo platform (1), plane moving mechanism (2), rotary mechanism (3), lift adjustment mechanism (4), supporting mechanism (5) and snatchs mechanism (6), cargo platform (1) fixed mounting is on transporting the carriage, plane moving mechanism (2) fixed mounting is on cargo platform (1), rotary mechanism (3) are installed on plane moving mechanism (2), lift adjustment mechanism (4) are installed on rotary mechanism (3), supporting mechanism (5) are installed on rotary mechanism (3), snatch mechanism (6) and install on lift adjustment mechanism (4).
2. The satellite solar wing positioning tool according to claim 1, wherein the plane moving mechanism (2) comprises a first lead screw sliding table (21), a second lead screw sliding table (22), a moving track (23), a moving telescopic rod (24), a moving sliding block (25) and a lower bearing plate (26), the first lead screw sliding table (21) is fixedly installed on the object carrying platform (1), the second lead screw sliding table (22) is fixedly installed on the object carrying platform (1) and forms a vertical included angle with the installation direction of the first lead screw sliding table (21), one end of the moving track (23) is installed on the sliding table of the first lead screw sliding table (21), the moving track (23) is provided with a moving sliding groove, the moving sliding block (25) is arranged in the moving sliding groove of the moving track (23), the lower bearing plate (26) is welded at the bottom of the moving sliding block (25) and the lower bearing plate (26) is in sliding fit with the moving track (23), one end of the movable telescopic rod (24) is arranged on the sliding table of the second screw rod sliding table (22) and the other end is arranged on the lower bearing plate (26).
3. The satellite solar wing positioning tool according to claim 2, wherein the rotating mechanism (3) comprises an upper bearing plate (31), a rotating bearing (32), a rotating disc (33), a rotating gear ring (34), a support frame (35), a rotating gear (36), a bearing frame (37) and a rotating motor (38), the upper bearing plate (31) is welded on the top of the moving slider (25) and the upper bearing plate (31) is in sliding fit with the moving track (23), the rotating bearing (32) is installed on the top of the upper bearing plate (31), the rotating disc (33) is sleeved on the outer ring of the rotating bearing (32) and the rotating disc (33) is in rotating fit with the upper bearing plate (31), the rotating gear ring (34) is fixedly sleeved on the outer ring of the rotating disc (33), the support frame (35) is welded on the side wall of the upper bearing plate (31), the bearing frame (37) is welded on the support frame (35), the rotary motor (38) is installed on the bearing frame (37), the main shaft of the rotary motor (38) penetrates through the supporting frame (35) and is arranged, the rotary gear (36) is rotatably installed on the supporting frame (35) and connected to the main shaft of the rotary motor (38), and the rotary gear (36) is meshed with the rotary gear ring (34).
4. The satellite solar wing positioning tool according to claim 3, characterized in that the lifting adjusting mechanism (4) comprises a supporting plate (41), an adjusting plate (42) and three lifting adjusting components (43), when the supporting plate (41) is welded on the rotating disk (33), three lifting adjusting components (43) are mounted on the supporting plate (41), each lifting adjusting component (43) comprises a lifting motor (44), a lifting mounting plate (45), a lifting threaded rod (46), a lifting slider (47), two lifting rods (48), two lifting support rods (49) and four rotating mounting pins (491), one ends of the two lifting rods (48) are mounted on the supporting plate (41), the lifting mounting plate (45) is mounted at the other end of the lifting rods (48), the lifting motor (44) is mounted on the lifting mounting plate (45) and a main shaft of the lifting motor (44) penetrates through the lifting mounting plate (45) to be arranged, lifting screw rod (46) rotate install on lifting mounting panel (45) and one end is connected on the main shaft of elevator motor (44), lifting slide (47) cover is established on lifting screw rod (46) and two lifter (48), lifting slide (47) and two lifter (48) sliding fit and lifting slide (47) and lifting screw rod (46) screw-thread fit, wherein two rotate mounting pin (491) symmetry and rotate and install on lifting slide (47), two the one end of lifting support pole (49) is rotated respectively and is installed on two rotation mounting pin (491), two in addition rotate mounting pin (491) and rotate the other end of installing two lifting slide (47) respectively, six rotation mounting pins (491) on six lifting support poles (49) are installed in regulating plate (42).
5. The satellite solar wing positioning tool according to claim 4, characterized in that the supporting mechanism (5) comprises an electric pushing cylinder (51) and a universal joint (52), the electric pushing cylinder (51) is mounted on the top of the upper bearing plate (31), one end of the universal joint (52) is mounted on the bottom of the adjusting plate (42) and the other end of the universal joint (52) is mounted on the telescopic end of the electric pushing cylinder (51).
6. The satellite solar wing positioning tool according to claim 4, wherein the grabbing mechanism (6) comprises a grabbing frame (61), a grabbing electric cylinder (62), a grabbing moving block (63), two grabbing sliding plates (64) and two grabbing clamps (65), the grabbing frame (61) is fixedly installed at the top of the adjusting plate (42), a sliding slot is formed in the grabbing frame (61), the two grabbing sliding plates (64) are symmetrically installed in the sliding slot of the grabbing frame (61), the two grabbing sliding plates (64) are in sliding fit with the grabbing frame (61), the two grabbing clamps (65) are installed on the two grabbing sliding plates (64), a sliding rail is formed on each grabbing sliding plate (64), two sides of the grabbing moving block (63) are installed on the sliding rails of the two grabbing sliding plates (64), the grabbing electric cylinder (62) is installed at the top of the adjusting plate (42), the telescopic end of the grabbing electric cylinder (62) penetrates through the grabbing frame (61) and is hinged to the grabbing moving block (63).
7. The satellite solar wing positioning tool according to claim 2, characterized in that universal wheels (7) are arranged at the bottom of the lower bearing plate (26).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110304612.XA CN112693634B (en) | 2021-03-23 | 2021-03-23 | Satellite solar wing positioning tool |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
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| CN105834987A (en) * | 2016-04-15 | 2016-08-10 | 上海微小卫星工程中心 | Satellite solar wing locating tool |
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| CN109352627A (en) * | 2018-11-06 | 2019-02-19 | 昆明理工大学 | A kind of space three-dimensional parallel manipulator hand |
| CN110775297A (en) * | 2019-09-26 | 2020-02-11 | 上海宇航***工程研究所 | Hinged type extending arm capable of being repeatedly compressed |
| CN210703125U (en) * | 2019-10-30 | 2020-06-09 | 余霞东 | Four sides linkage positioning fixture |
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| SU831606A1 (en) * | 1979-03-05 | 1981-05-23 | Институт Технической Кибернетикиан Белорусской Ccp | Module of industrial robot |
| KR100717641B1 (en) * | 2006-04-18 | 2007-05-11 | 김영구 | A multistage bolt socket |
| JP2015085400A (en) * | 2013-10-28 | 2015-05-07 | 国立大学法人東京工業大学 | Surgical robot arm, and method for correcting fixed point error of the same |
| CN106826782A (en) * | 2015-12-04 | 2017-06-13 | 重庆足首自动化技术服务有限公司 | A kind of circular cylindrical coordinate formula robot |
| CN105834987A (en) * | 2016-04-15 | 2016-08-10 | 上海微小卫星工程中心 | Satellite solar wing locating tool |
| CN205703890U (en) * | 2016-06-13 | 2016-11-23 | 苏州博众精工科技有限公司 | Orientation maintaining means |
| CN208496866U (en) * | 2018-06-29 | 2019-02-15 | 苏州晶旭新能源科技有限公司 | A kind of mounting device being easily installed solar energy photovoltaic panel |
| CN109352627A (en) * | 2018-11-06 | 2019-02-19 | 昆明理工大学 | A kind of space three-dimensional parallel manipulator hand |
| CN110775297A (en) * | 2019-09-26 | 2020-02-11 | 上海宇航***工程研究所 | Hinged type extending arm capable of being repeatedly compressed |
| CN210703125U (en) * | 2019-10-30 | 2020-06-09 | 余霞东 | Four sides linkage positioning fixture |
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|---|---|
| CN112693634B (en) | 2021-06-01 |
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