Integrated flipping and parking device for small satellites
By designing an integrated flip-parking device suitable for small satellites, three-dimensional adjustments and attitude flips are realized front-back, left and right, and lifting, which solves the rapid development and low-cost needs in the integration process of small satellite assembly, and improves satellite development efficiency.
Patent Information
- Application Number
- CN202211519645.7
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2022-11-30
- Publication Date
- 2025-08-19
- Estimated Expiration
- 2042-11-30
AI Technical Summary
The prior art cannot meet the fast and low-cost parking, transport and attitude flip of small satellites during the assembly integration process, especially the three-dimensional adjustment and deployment test of moving parts.
A flip-parking integrated device including a base assembly, a lifting column assembly, a posture adjustment assembly and a general installation frame is designed. Through adjustments in the three linear directions of front and rear, left and right, and lifting, and rotation about two orthogonal axes in the horizontal plane, the parking, transport and flip of small satellites are realized.
It realizes the rapid development needs of small satellites, reduces high-risk operations, improves satellite development efficiency, and meets the attitude flip requirements of assembly integration, test transport and moving parts.
Smart Images

Figure CN115816397B_ABST
Abstract
Description
Technical Field
[0001] The present invention relates to the field of satellite technology, and in particular to a flipping and parking integrated device suitable for small satellites. Background Art
[0002] With the continuous improvement of basic technological capabilities, the diversified development of the application market, and the strong support of national policies, the industrialization and commercialization of small satellites are becoming increasingly evident, and they are widely used in communications, space science, Earth observation, and technology demonstration. Multi-satellite coordination and network formation are the most prominent features of small satellites. The demand for satellite constellation construction has led to a significant increase in the development of small satellites.
[0003] Small satellites are significantly smaller in mass and volume than large and medium-sized satellites, resulting in shorter development cycles and lower costs. During the final assembly and integration process, large and medium-sized satellites are parked and transported using transfer and parking vehicles, with attitude flips achieved using a two-axis turntable. This requires the constant switching of tooling to meet the satellite's varying state requirements at different stages. This is a time-consuming and labor-intensive process, with numerous operational risks, and cannot meet the low-cost, rapid development needs of small satellites. Therefore, it is necessary to develop an integrated flip and parking device suitable for small satellites that can meet the requirements for parking, test transport, and attitude flips during active component deployment testing or polarity testing during the final assembly and integration process.
[0004] Patent document CN215469230U discloses an automatic flipping platform for satellite installation and debugging, comprising a base frame, a vertical plate fixedly connected to one side of the top of the base frame, a slider having a gap in the inner wall of the vertical plate, a first threaded rod threadedly connected to the inner wall of the slider, and the top of the first threaded rod rotatably connected to the inner wall of the vertical plate via a bearing. This utility model relates to the field of flipping platform technology. This automatic flipping platform for satellite installation and debugging has a stable structure, is easy to operate, and has a high degree of automation, reducing labor costs. Its specific beneficial effects are as follows: through the cooperation of a servo motor, a second threaded rod, and a clamping rod, the position of the second robotic arm can be freely adjusted, facilitating operation by staff and improving work efficiency. The clamping rod also serves to limit the second robotic arm, ensuring that the second robotic arm does not deviate during operation, thereby improving the working quality of the equipment. However, this device cannot achieve adjustment of small satellites along three linear directions. Summary of the Invention
[0005] In view of the defects in the prior art, the purpose of the present invention is to provide an integrated flipping and parking device suitable for small satellites.
[0006] The flipping and parking integrated device for a small satellite provided by the present invention comprises a base assembly, a lifting column assembly, an attitude adjustment assembly, and a universal mounting frame. The lifting column assembly is disposed on the base assembly, the attitude adjustment assembly is disposed on top of the lifting column assembly, and the universal mounting frame is disposed on the attitude adjustment assembly. The universal mounting frame is used to mount the small satellite.
[0007] The posture adjustment assembly includes a mounting support, a front and rear fine-tuning assembly, an up and down adjustment screw, a left and right adjustment screw, and a pitch adjustment assembly. The mounting support and the pitch adjustment assembly are both arranged on the lifting column assembly;
[0008] The upper end of the mounting bracket is connected to the front and rear fine-tuning assembly, the end of the front and rear fine-tuning assembly is connected to the upper and lower adjustment screws, the upper ends of the upper and lower adjustment screws are connected to the left and right adjustment screws, the left and right adjustment screws are arranged at the lower end of the universal mounting frame, and the upper end of the pitch adjustment assembly is connected to the universal mounting frame;
[0009] The universal mounting frame can move in the front-rear, up-down and left-right directions respectively under the drive of the front-rear fine adjustment assembly, the up-down adjustment screw and the left-right adjustment screw, and can be folded around the left-right adjustment screw under the drive of the pitch adjustment assembly.
[0010] Preferably, the base assembly includes a base frame, a plurality of universal wheels, a plurality of universal balls, a plurality of foot cups and a plurality of directional wheels;
[0011] The universal wheels and fixed wheels are respectively arranged at the front and rear ends of the base frame, the universal ball is arranged at the bottom of the base frame and can protrude or retract downward, the foot cups are arranged on both sides of the base frame and can move up and down, and the universal wheels are provided with a locking structure;
[0012] When the foot cup moves downward until it touches the ground, the position of the base assembly remains fixed; when the universal ball protrudes downward until it touches the ground at the same time as the universal wheel, the base assembly can move left and right; when the universal ball is retracted into the base frame, the universal wheel and the directional wheel touch the ground at the same time, and the base assembly can move forward and backward.
[0013] Preferably, the lifting column assembly includes an electric push rod, a mounting plate, a fixed column and a lifting column;
[0014] The mounting plate is mounted on the base assembly, the fixed column is arranged on the mounting plate, the lifting column is sleeved on the fixed column, the fixed end of the electric push rod is mounted on the lower end of the fixed column, the other end of the electric push rod is located inside the fixed column and extends upward until it extends out of the top of the fixed column and forms an extended end, a push rod connecting support is provided on the extended end, and the push rod connecting support is connected to the lifting column.
[0015] Preferably, the fixed column and the lifting column are both evenly provided with a plurality of adjustment holes along the height direction.
[0016] Preferably, limit blocks are provided at both ends of the fixed column to limit the lifting range of the lifting column.
[0017] Preferably, a push rod motor is provided on the fixed end of the electric push rod, a motor protection cover is provided on the outer side of the push rod motor, and the limit block at the lower end of the fixed column is located above the motor protection cover.
[0018] Preferably, the front and rear fine-tuning assembly includes a front and rear push rod and a front and rear adjustment hand wheel, a fixing sleeve, a tightening sleeve and an adjustment sleeve connected in sequence;
[0019] One end of the front and rear push rods is connected to the front and rear adjustment hand wheel, and the other end of the front and rear push rods passes through the fixed sleeve and the tightening sleeve in sequence to connect to the adjustment sleeve, the fixed sleeve is arranged at the upper end of the mounting support, and the upper and lower adjustment screws are arranged in the adjustment sleeve, and the front and rear adjustment hand wheel can drive the front and rear push rods to slide in the fixed sleeve and the tightening sleeve;
[0020] The tightening sleeve is provided with a tightening handwheel, and the tightening handwheel can tighten the tightening sleeve to fix the position between the front and rear push rods and the fixed sleeve.
[0021] Preferably, the pitch adjustment assembly includes a screw elevator, a mounting seat, a mounting bracket and a universal joint assembly, the screw elevator is arranged on the mounting seat, the mounting seat is arranged on the mounting bracket, and the mounting bracket is arranged at the upper end of the lifting column assembly;
[0022] The screw elevator includes a base, an elevator handwheel and a lifting rod, wherein the elevator handwheel and the lifting rod are both arranged on the base, the base is mounted on the mounting seat, and the upper end of the lifting rod is connected to the upper end of the universal mounting frame through a universal joint assembly;
[0023] The elevator hand wheel can drive the lifting rod to move up and down, thereby driving the universal mounting frame to fold around the left and right adjusting screw rods through the universal joint assembly.
[0024] Preferably, a handle is provided on the mounting bracket.
[0025] Preferably, the universal mounting frame comprises a mounting frame, an upper connecting bracket and a lower connecting bracket, wherein the upper connecting bracket and the lower connecting bracket are respectively arranged at the upper and lower ends of the mounting frame;
[0026] The lower connecting bracket is arranged on the left and right adjusting screws, and the upper connecting bracket is connected to the pitch adjusting assembly.
[0027] Compared with the prior art, the present invention has the following beneficial effects:
[0028] 1. The present invention has a simple structure and is easy to operate. It uses an attitude adjustment component to adjust the attitude of small satellites. It can achieve adjustment in three linear directions: front and back, left and right, and up and down, and in the rotation direction around two orthogonal axes in the horizontal plane. It integrates the functions of parking, transporting and flipping small satellites. It has a compact structure, adjustable height, wide operating space, and can meet the needs of rapid development of small satellites.
[0029] 2. The present invention can simultaneously meet the requirements of small satellite assembly, integrated parking, test transportation, and deployment and test attitude flipping of movable parts such as solar panels and antennas, reduce extremely high-risk operations such as hoisting during satellite assembly, effectively improve satellite development efficiency, and meet the needs of rapid development of small satellites. BRIEF DESCRIPTION OF THE DRAWINGS
[0030] Other features, objects and advantages of the present invention will become more apparent upon reading the detailed description of non-limiting embodiments with reference to the following drawings:
[0031] Figure 1 It is a structural schematic diagram of the present invention;
[0032] Figure 2 It is a structural schematic diagram of the base assembly in the present invention;
[0033] Figure 3 This is a structural schematic diagram of the lifting column assembly at one angle in the present invention;
[0034] Figure 4 This is a structural diagram of the lifting column assembly of the present invention from another angle;
[0035] Figure 5 Schematic diagram of the structure of the posture adjustment component of the present invention;
[0036] Figure 6 It is a structural schematic diagram of the universal installation frame in the present invention;
[0037] Figure 7 It is a structural schematic diagram of the front and rear fine-tuning components in the present invention.
[0038] The figure shows:
[0039] Base assembly 1 Up and down adjustment screw 20
[0040] Lifting column assembly 2 left and right adjustment screw 21
[0041] Attitude adjustment component 3 adapter 22
[0042] Universal mounting frame 4 Pitch adjustment assembly 23
[0043] Base frame 5 front and rear adjustment hand wheel 24
[0044] Universal wheel 6 fixed sleeve 25
[0045] Universal ball 7 Tightening sleeve 26
[0046] Foot cup 8 Tightening hand wheel 27
[0047] Steering wheel 9 Adjusting sleeve 28
[0048] Electric linear actuator 10 Screw jack 29
[0049] Motor protection cover 11 Lifter handwheel 30
[0050] Push rod connecting support 12 mounting seat 31
[0051] Mounting plate 13 Mounting bracket 32
[0052] Fixed column 14 Handle 33
[0053] Lifting column 15 universal joint assembly 34
[0054] Limit block 16 Installation frame 35
[0055] Column protection cover 17 upper connecting bracket 36
[0056] Mounting bracket 18 Lower connecting bracket 37
[0057] Front and rear fine-tuning components 19 DETAILED DESCRIPTION
[0058] The present invention will be described in detail below with reference to specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but are not intended to limit the present invention in any form. It should be noted that, for those skilled in the art, several changes and improvements can be made without departing from the scope of the present invention. These all fall within the scope of protection of the present invention.
[0059] The present invention discloses an integrated flipping and parking device suitable for small satellites. The device is adaptable to the size and weight of small satellites, has an adjustable operating height, and a wide operating space. It is suitable for the assembly characteristics of small satellites and can simultaneously meet the requirements of small satellite assembly, integrated parking, test transportation, and attitude flipping for deployment tests of movable parts such as solar panels and antennas. It reduces extremely high-risk operations such as hoisting during satellite assembly, effectively improves satellite development efficiency, and meets the needs of rapid small satellite development.
[0060] According to the present invention, a flipping and parking integrated device suitable for small satellites is disclosed. Figure 1-7As shown, it includes a base assembly 1, a lifting column assembly 2, an attitude adjustment assembly 3 and a universal mounting frame 4. The lifting column assembly 2 is vertically arranged on the base assembly 1, the attitude adjustment assembly 3 is arranged on the top of the lifting column assembly 2, and the universal mounting frame 4 is arranged on the attitude adjustment assembly 3. The universal mounting frame 4 is used to install small satellites; the device can realize adjustment in three linear directions of front and back, left and right, and lifting and lowering, and in the rotation direction around two orthogonal axes in the horizontal plane, meeting the requirements of small satellite assembly and integration, test transportation and attitude flipping of solar wing deployment test.
[0061] like Figure 5 As shown, the posture adjustment assembly 3 includes a mounting support 18, a front and rear fine-tuning assembly 19, an up and down adjustment screw 20, a left and right adjustment screw 21 and a pitch adjustment assembly 23. The mounting support 18 and the pitch adjustment assembly 23 are both arranged on the lifting column assembly 2; the upper end of the mounting support 18 is connected to the front and rear fine-tuning assembly 19, the end of the front and rear fine-tuning assembly 19 is connected to the up and down adjustment screw 20, the upper end of the up and down adjustment screw 20 is connected to the left and right adjustment screw 21, the left and right adjustment screw 21 is arranged at the lower end of the universal mounting frame 4, and the upper end of the pitch adjustment assembly 23 is connected to the universal mounting frame 4; preferably, the mounting support 18 and the lifting column assembly 2 are screwed and fixed by M12×110, the upper end of the up and down adjustment screw 20 is connected to the left and right adjustment screw 21 through an adapter 22, the adjustment range of the left and right adjustment screw 21 is ±30mm, and the adjustment range of the front and rear adjustment assembly 19 is ±30mm.
[0062] like Figure 7 As shown, the front and rear fine-tuning assembly 19 includes a front and rear push rod and a front and rear adjustment handwheel 24, a fixed sleeve 25, a tightening sleeve 26 and an adjusting sleeve 28 connected in sequence; one end of the front and rear push rod is connected to the front and rear adjustment handwheel 24, and the other end of the front and rear push rod passes through the fixed sleeve 25 and the tightening sleeve 26 in sequence to connect to the adjusting sleeve 28, the fixed sleeve 25 is arranged at the upper end of the mounting support 18, and the upper and lower adjustment screws 20 are arranged in the adjusting sleeve 28, the front and rear adjustment handwheel 24 can drive the front and rear push rod to slide in the fixed sleeve 25 and the tightening sleeve 26; the tightening sleeve 26 is provided with a tightening handwheel 27, and the tightening handwheel 27 can tighten the tightening sleeve 26 to fix the position between the front and rear push rod and the fixed sleeve 25.
[0063] like Figure 5As shown, the pitch adjustment assembly 23 includes a screw elevator 29, a mounting seat 31, a mounting bracket 32 and a universal joint assembly 34, the screw elevator 29 is arranged on the mounting seat 31, the mounting seat 31 is arranged on the mounting bracket 32, and the mounting bracket 32 is arranged at the upper end of the lifting column assembly 2; the screw elevator 29 includes a base, an elevator handwheel 30 and a lifting rod, the elevator handwheel 30 and the lifting rod are both arranged on the base, the base is mounted on the mounting seat 31, and the upper end of the lifting rod is connected to the upper end of the universal mounting frame 4 through the universal joint assembly 34; the elevator handwheel 30 can drive the lifting rod to rise and fall, thereby driving the universal mounting frame 4 to fold around the left and right adjustment screws 21 through the universal joint assembly 34, thereby realizing flipping in the pitch direction from 0° (horizontal) to 90° (vertical).
[0064] Preferably, a handle 33 is provided on the mounting bracket 32, and the four corners of the base of the spiral elevator 29 are screwed to the mounting base 31 by M8×30 screws. The mounting base 31 and the mounting bracket 32 are connected by a pin shaft, and the mounting bracket 32 is mounted on the fixed column 14 by M8×30 screws.
[0065] The universal mounting frame 4 can move in the front-back, up-down and left-right directions respectively under the drive of the front-back fine-tuning assembly 19, the up-down adjustment screw 20 and the left-right adjustment screw 21, and can be folded around the left-right adjustment screw 21 under the drive of the pitch adjustment assembly 23.
[0066] like Figure 2 As shown, the base assembly 1 includes a base frame 5, multiple universal wheels 6, multiple universal balls 7, multiple foot cups 8 and multiple fixed wheels 9; the universal wheels 6 and fixed wheels 9 are respectively arranged at the front and rear ends of the base frame 5, the universal ball 7 is arranged at the bottom of the base frame 5 and can protrude or retract downward, the foot cups 8 are arranged on both sides of the base frame 5 and can move up and down, and a locking structure is provided on the universal wheel 6; when the foot cup 8 moves downward until it touches the ground, the position of the base assembly 1 remains fixed; when the universal ball 7 protrudes downward until it touches the ground at the same time as the universal wheel 6, the base assembly 1 can move left and right; when the universal ball 7 is retracted into the base frame 5, the universal wheel 6 and the fixed wheel 9 touch the ground at the same time, and the base assembly 1 can move forward and backward. Preferably, as Figure 2 As shown, the universal wheel 6, universal ball 7, foot cup 8 and fixed wheel 9 are all two
[0067] like Figure 3-4As shown, the lifting column assembly 2 includes an electric push rod 10, a mounting plate 13, a fixed column 14, and a lifting column 15; the mounting plate 13 is mounted on the base assembly 1, the fixed column 14 is set on the mounting plate 13, and the lifting column 15 is sleeved on the fixed column 14. The fixed end of the electric push rod 10 is mounted on the lower end of the fixed column 14, and the other end of the electric push rod 10 is located inside the fixed column 14 and extends upward until it extends out of the top of the fixed column 14 and forms an extended end. The extended end is provided with a push rod connecting support 12, and the push rod connecting support 12 is connected to the lifting column 15. Multiple adjustment holes are evenly arranged on the fixed column 14 and the lifting column 15 along the height direction. Preferably, the fixed column 14 and the lifting column 15 can be adjusted in 40mm increments within a 200mm range through adjustment holes. The electric push rod 10 can achieve continuous height adjustment within a 400mm range. The up and down adjustment screw 20 can achieve continuous height adjustment of ±25mm. The universal mounting frame 4 can also be driven to achieve height adjustment in different directions to meet different operating height requirements.
[0068] Limit blocks 16 are provided at both ends of the fixed column 14 to limit the lifting range of the lifting column 15. The lifting column 15 is prevented from exceeding the working range upwards and from interfering with the electric push rod motor protection cover 11 downwards. A push rod motor is provided on the fixed end of the electric push rod 10, and a motor protection cover 11 is provided on the outside of the push rod motor. The limit block 16 at the lower end of the fixed column 14 is located above the motor protection cover 11. An opening is provided on the front side of the lifting column 15, and a column protection cover 17 is provided on the opening. In one embodiment of the present invention, the driving force of the electric push rod 10 is 1000kg and the locking force is 800kg. The fixed column 14 is screwed to the L-shaped mounting plate 13 by M10×30 screws; the bottom of the lifting column assembly 2 is mounted on the base frame 5 through the L-shaped mounting plates 13 on both sides.
[0069] like Figure 6 As shown, the universal mounting frame 4 includes a mounting frame 35, an upper connecting bracket 36 and a lower connecting bracket 37. The upper connecting bracket 36 and the lower connecting bracket 37 are respectively arranged at the upper and lower ends of the mounting frame 35; the lower connecting bracket 37 is arranged on the left and right adjusting screws 21, and the upper connecting bracket 36 is connected to the pitch adjustment assembly 23.
[0070] The mounting frame 35 is provided with five φ12 mounting holes. Small satellites of different models can be mounted on the universal mounting frame 4 through an adapter plate. In the vertical parking state, the lower edge of the mounting frame 35 is 1000 mm from the ground. After the full stroke is raised, the lower edge of the mounting frame 35 is 1600±25 mm from the ground. When installing a single satellite and payload and laying cables, the mounting frame 35 is in a horizontal direction. In the horizontal parking state, the mounting frame 35 is 900 mm from the ground, which is suitable for operators to perform on-board operations during the small satellite assembly process.
[0071] The flipping and parking integrated device for small satellites provided by the present invention has integrated functions of parking, transportation and flipping, is adaptable to small satellites of different models, and can meet the requirements of parking, transportation and flipping of small satellites in the final assembly process.
[0072] In the description of this application, it should be understood that the terms "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside", etc., indicating the orientation or position relationship, are based on the orientation or position relationship shown in the accompanying drawings, and are only for the convenience of describing this application and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on this application.
[0073] The above describes specific embodiments of the present invention. It should be understood that the present invention is not limited to the specific embodiments described above, and those skilled in the art may make various changes or modifications within the scope of the claims, which do not affect the essence of the present invention. The embodiments of this application and the features in the embodiments may be combined with each other in any manner unless there is a conflict.
Claims
1. A flip and parking integrated device suitable for small satellites, characterized in that: The invention comprises a base assembly (1), a lifting column assembly (2), an attitude adjustment assembly (3) and a universal mounting frame (4), wherein the lifting column assembly (2) is arranged on the base assembly (1), the attitude adjustment assembly (3) is arranged on the top of the lifting column assembly (2), and the universal mounting frame (4) is arranged on the attitude adjustment assembly (3), and the universal mounting frame (4) is used for mounting a small satellite; The posture adjustment assembly (3) comprises a mounting support (18), a front-back fine-tuning assembly (19), an up-down adjustment screw (20), a left-right adjustment screw (21), and a pitch adjustment assembly (23); the mounting support (18) and the pitch adjustment assembly (23) are both arranged on the lifting column assembly (2); The upper end of the mounting support (18) is connected to the front and rear fine-tuning assembly (19), the end of the front and rear fine-tuning assembly (19) is connected to the upper and lower adjusting screws (20), the upper ends of the upper and lower adjusting screws (20) are connected to the left and right adjusting screws (21), the left and right adjusting screws (21) are arranged at the lower end of the universal mounting frame (4), and the upper end of the pitch adjustment assembly (23) is connected to the universal mounting frame (4); The universal mounting frame (4) can move in the front-back, top-bottom, and left-right directions respectively under the drive of the front-back fine-tuning assembly (19), the up-down adjusting screw (20), and the left-right adjusting screw (21), and can be folded around the left-right adjusting screw (21) under the drive of the pitch adjusting assembly (23).
2. The integrated flipping and parking device for small satellites according to claim 1, characterized in that: The base assembly (1) comprises a base frame (5), a plurality of universal wheels (6), a plurality of universal balls (7), a plurality of foot cups (8) and a plurality of directional wheels (9); The universal wheel (6) is arranged at the front end of the base frame (5), the directional wheel (9) is arranged at the rear end of the base frame (5), the universal ball (7) is arranged at the bottom of the base frame (5) and can protrude downward or retract, the foot cup (8) is arranged on both sides of the base frame (5) and can move up and down, and a locking structure is provided on the universal wheel (6); When the foot cup (8) moves downward until it touches the ground, the position of the base assembly (1) remains fixed; when the universal ball (7) protrudes downward until it touches the ground simultaneously with the universal wheel (6), the base assembly (1) can move left and right; when the universal ball (7) is retracted into the base frame (5), the universal wheel (6) and the directional wheel (9) touch the ground simultaneously, and the base assembly (1) can move forward and backward.
3. The integrated flipping and parking device for small satellites according to claim 1, characterized in that: The lifting column assembly (2) comprises an electric push rod (10), a mounting plate (13), a fixed column (14) and a lifting column (15); The mounting plate (13) is mounted on the base assembly (1), the fixed column (14) is arranged on the mounting plate (13), the lifting column (15) is sleeved on the fixed column (14), the fixed end of the electric push rod (10) is mounted on the lower end of the fixed column (14), the other end of the electric push rod (10) is located inside the fixed column (14) and extends upward until it extends out of the top of the fixed column (14) and forms an extended end, and a push rod connecting support (12) is provided on the extended end, and the push rod connecting support (12) is connected to the lifting column (15).
4. The integrated flipping and parking device for small satellites according to claim 3, characterized in that: The fixed column (14) and the lifting column (15) are both evenly provided with a plurality of adjustment holes along the height direction.
5. The integrated flipping and parking device for small satellites according to claim 3, characterized in that: Limiting blocks (16) are provided at both ends of the fixed column (14), thereby limiting the lifting range of the lifting column (15).
6. The integrated flipping and parking device for small satellites according to claim 5, characterized in that: A push rod motor is provided on the fixed end of the electric push rod (10), a motor protection cover (11) is provided on the outside of the push rod motor, and a limit block (16) at the lower end of the fixed column (14) is located above the motor protection cover (11).
7. The integrated flipping and parking device for small satellites according to claim 1, characterized in that: The front and rear fine-tuning assembly (19) comprises front and rear push rods and sequentially connected front and rear adjustment hand wheels (24), a fixing sleeve (25), a tightening sleeve (26) and an adjustment sleeve (28); One end of the front and rear push rods is connected to the front and rear adjustment hand wheels (24), and the other ends of the front and rear push rods pass through the fixed sleeve (25) and the tightening sleeve (26) in sequence to connect the adjustment sleeve (28). The fixed sleeve (25) is arranged on the upper end of the mounting support (18), and the upper and lower adjustment screws (20) are arranged in the adjustment sleeve (28). The front and rear adjustment hand wheels (24) can drive the front and rear push rods to slide in the fixed sleeve (25) and the tightening sleeve (26). The tightening sleeve (26) is provided with a tightening hand wheel (27), and the tightening hand wheel (27) can tighten the tightening sleeve (26) so as to fix the position between the front and rear push rods and the fixed sleeve (25).
8. The integrated flipping and parking device for small satellites according to claim 1, characterized in that: The pitch adjustment assembly (23) comprises a screw elevator (29), a mounting seat (31), a mounting bracket (32) and a universal joint assembly (34), wherein the screw elevator (29) is arranged on the mounting seat (31), the mounting seat (31) is arranged on the mounting bracket (32), and the mounting bracket (32) is arranged at the upper end of the lifting column assembly (2); The spiral elevator (29) includes a base, an elevator handwheel (30) and a lifting rod, wherein the elevator handwheel (30) and the lifting rod are both arranged on the base, the base is mounted on a mounting seat (31), and the upper end of the lifting rod is connected to the upper end of the universal mounting frame (4) via a universal joint assembly (34); The elevator hand wheel (30) can drive the lifting rod to move up and down, thereby driving the universal mounting frame (4) to fold around the left and right adjusting screws (21) through the universal joint assembly (34).
9. The integrated flipping and parking device for small satellites according to claim 8, characterized in that: The mounting bracket (32) is provided with a handle (33).
10. The integrated flipping and parking device for small satellites according to claim 1, characterized in that: The universal mounting frame (4) comprises a mounting frame (35), an upper connecting bracket (36) and a lower connecting bracket (37), wherein the upper connecting bracket (36) is arranged at the upper end of the mounting frame (35), and the lower connecting bracket (37) is arranged at the lower end of the mounting frame (35); The lower connecting bracket (37) is arranged on the left and right adjusting screws (21), and the upper connecting bracket (36) is connected to the pitch adjusting assembly (23).
Citation Information
Patent Citations
Automatic overturning table for satellite installation and debugging
CN215469230U
Novel satellite side plate satellite-borne rack car
CN105600710A
Novel six-degree-of-freedom satellite side plate mounting equipment
CN106429960A