Space operation auxiliary device based on computer
By designing a combination of a manned frame and auxiliary components, the problem that existing space operation auxiliary devices are difficult to balance walking flexibility and support stability in mechanical structure is solved, thereby improving the safety and efficiency of astronauts' stable walking in space.
Patent Information
- Application Number
- CN202510986513.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-07-17
- Publication Date
- 2025-09-05
AI Technical Summary
The mechanical structure of existing space operation assistance devices makes it difficult to balance walking flexibility and support stability, resulting in astronauts being unable to respond to complex movement requirements in real time when performing extravehicular missions, and there is a risk of imbalance and accidental falls.
The design of a computer-based space operation auxiliary device includes a manned frame, a support assembly and an auxiliary assembly. The support assembly consists of a mounting box, a fixing ring, a tripod bracket and a slot. The auxiliary assembly consists of a groove, a track, a protective plate, a controller, an operating screen, a camera, a lighting, a fixing frame and a robotic arm. Through the cooperation of the tripod bracket and the telescopic cylinder, it provides stable support and height adjustment to meet the needs of astronauts of different heights.
Ensure that astronauts operate smoothly during spacewalks, prevent accidental falls or loss of balance, ensure safety, ensure the smooth progress of spacewalk missions, and provide optimal support and comfort.
Smart Images
Figure CN120589205A_ABST
Abstract
Description
Technical Field
[0001] The present invention relates to the field of space operation assistance technology, and in particular to a computer-based space operation assistance device. Background Art
[0002] Space is an extreme environment that is completely different from the Earth, which brings huge challenges to human space operations. In space, in a microgravity environment, objects are almost not bound by gravity. When astronauts perform equipment installation, maintenance and other operations, they cannot use gravity to maintain a stable posture and find it difficult to operate tools accurately, resulting in a significant reduction in work efficiency and safety. Therefore, space operation assistance devices are needed to assist astronauts in their work, helping astronauts to repair and replace extravehicular equipment, reducing the astronauts' workload and improving work efficiency.
[0003] Existing work assist devices mostly adopt a fixed-form design in mechanical structure, which makes it difficult to balance walking flexibility and support stability. As a result, when astronauts perform extravehicular missions, they often face the risk of imbalance and accidental falls because the device cannot respond to complex movement requirements in real time. This not only seriously threatens the life safety of astronauts, but may also lead to the forced interruption of space operations, causing immeasurable losses to the continuity of space missions and the realization of scientific research goals.
[0004] Therefore, since the above-mentioned operation assistance devices mostly adopt a fixed-form design in mechanical structure, it is difficult to take into account both walking flexibility and support stability. As a result, when astronauts perform extravehicular tasks, they often face the risk of imbalance of center of gravity and accidental falls because the devices cannot respond to complex movement requirements in real time. Therefore, a computer-based space operation assistance device can be designed. Summary of the Invention
[0005] In order to overcome the problem that work assist devices mostly adopt fixed-form design in mechanical structure, it is difficult to take into account both walking flexibility and support stability. As a result, astronauts often face the risk of imbalance and accidental falls when performing extravehicular missions because the devices cannot respond to complex movement requirements in real time.
[0006] The technical solution of the present invention is: a computer-based space operation auxiliary device, including a manned frame; it also includes a support assembly and an auxiliary assembly, the rear end of the manned frame is equipped with a support assembly for auxiliary support, and the manned frame is equipped with an auxiliary assembly for assisting walking, the support assembly includes an installation box, a fixing ring, a triangular bracket and a slot, the rear end of the manned frame is equipped with an installation box, the left and right sides of the bottom end of the installation box are magnetically connected to the fixing ring, the outer side of the fixing ring is movably connected to the triangular bracket, the left and right sides of the bottom end of the manned frame are provided with slots, and the center of the fixing ring is symmetrical to the bottom end of the slot; the auxiliary assembly includes a groove, a track, a protective plate, a controller, an operating screen, a card slot, a camera, a lighting lamp, a fixing frame and a robotic arm, and the bottom end of the manned frame is provided with a groove.
[0007] Preferably, a stable structure is formed by setting up a tripod bracket to provide support for astronauts when walking, ensuring that the astronauts operate more smoothly, and helping to prevent astronauts from accidentally falling or losing balance during spacewalks, thereby protecting the astronauts' safety and ensuring the smooth progress of spacewalk missions; at the same time, the cooperation of the tripod bracket and the telescopic cylinder can adjust the height of the tripod bracket to suit astronauts of different heights, providing optimal support and comfort, helping astronauts to better complete their tasks, and avoiding operational inconveniences or safety hazards caused by inappropriate height.
[0008] Preferably, a partition is provided inside the installation box, telescopic cylinders are provided at both left and right ends of the top of the partition, and a mounting ring is symmetrically installed at the center of the outer side of the top of the slot.
[0009] Preferably, the telescopic end of the telescopic cylinder is connected to a movable rod, and the movable rod is movably connected to the slot and the triangular bracket. Handrails are provided on both sides of the top of the installation box, and sponge pads are sleeved on the outer side of the handrails.
[0010] Preferably, a crawler track is rotatably mounted inside the groove, and a protective plate is mounted on the back side of the crawler track, and the protective plate is arranged inside the crawler track.
[0011] Preferably, a controller is installed at the top of the people carrier, an operation screen is provided on the inner wall opposite to the controller, and a card slot is provided at the front end of the controller.
[0012] Preferably, a camera is installed at the left end of the manned frame, and lighting lamps are provided at the middle positions of the left and right sides of the front end of the manned frame.
[0013] Preferably, fixed frames are installed at the front ends of the left and right sides of the manned frame, the internal rotation of the fixed frames is connected to the mechanical arms, and the fixed frames and the mechanical arms are connected by a connecting rod.
[0014] Preferably, a display screen is provided on the side wall of the controller, and drive rods are rotatably connected on both sides of the inside of the crawler.
[0015] Preferably, a control button is provided at the middle position of the front end of the robotic arm, and the robotic arm is made of titanium alloy.
[0016] The beneficial effects of the present invention are as follows: through the setting of the tripod bracket, a stable structure is formed to provide support for astronauts when walking, ensuring that the astronauts operate relatively smoothly, and helping to prevent astronauts from accidentally falling or losing balance during spacewalks, thereby protecting the astronauts' safety and ensuring the smooth progress of spacewalk missions; at the same time, the cooperation of the tripod bracket and the telescopic cylinder can adjust the height of the tripod bracket to adapt to astronauts of different heights, provide optimal support and comfort, help astronauts better complete their tasks, and avoid operational inconvenience or safety hazards caused by inappropriate height. BRIEF DESCRIPTION OF THE DRAWINGS
[0017] Figure 1 Shown is a schematic diagram of a first three-dimensional structure of the computer-based space operation assistance device of the present invention; Figure 2 Shown is a second perspective structural diagram of the computer-based space operation assistance device of the present invention; Figure 3 Shown is a bottom-up perspective structural diagram of the computer-based space operation assistance device of the present invention; Figure 4 Shown is a third perspective structural diagram of the computer-based space operation assistance device of the present invention; Figure 5 Shown is a schematic diagram of a cross-sectional perspective structure of a computer-based space operation assistance device of the present invention; Figure 6 Shown is a schematic diagram of the cross-sectional three-dimensional structure of the auxiliary components of the computer-based space operation auxiliary device of the present invention.
[0018] Explanation of the accompanying reference numerals: 1. Man-carrying frame; 201. Mounting box; 202. Fixing ring; 203. Triangular bracket; 204. Slot; 205. Partition; 206. Telescopic cylinder; 207. Mounting ring; 208. Movable rod; 209. Handrail; 210. Sponge pad; 301. Groove; 302. Track; 303. Protective plate; 304. Controller; 305. Operation screen; 306. Snap-in slot; 307. Camera; 308. Lighting; 309. Fixing frame; 310. Robotic arm; 311. Display screen; 312. Drive rod. DETAILED DESCRIPTION
[0019] The present invention will be further described below with reference to the accompanying drawings and examples.
[0020] See also Figures 1-6The present invention provides an embodiment: a computer-based space operation auxiliary device, including a manned frame 1; also including a support assembly and an auxiliary assembly, the rear end of the manned frame 1 is equipped with a support assembly for auxiliary support, and the manned frame 1 is equipped with an auxiliary assembly for assisting walking, the support assembly includes an installation box 201, a fixing ring 202, a triangular bracket 203 and a slot 204, the rear end of the manned frame 1 is equipped with an installation box 201, the left and right sides of the bottom end of the installation box 201 are magnetically connected to the fixing ring 202, the outer side of the fixing ring 202 is movably connected to the triangular bracket 203, the left and right sides of the bottom end of the manned frame 1 are provided with slots 204, and the fixing ring 202 is symmetrical to the bottom end of the slot 204; the auxiliary assembly includes a groove 301, a crawler 302, a protective plate 303, a controller 304, an operation screen 305, a clamping groove 306, a camera 307, a lighting lamp 308, a fixing frame 309 and a robotic arm 310, and the bottom end of the manned frame 1 is provided with a groove 301.
[0021] See also Figure 2 、 Figure 5 In this embodiment, a partition 205 is provided inside the installation box 201, and telescopic cylinders 206 are provided on both ends of the top of the partition 205. A mounting ring 207 is symmetrically installed on the outer side of the top of the slot 204; the telescopic end of the telescopic cylinder 206 is connected to a movable rod 208, and the movable rod 208 is movably connected to the slot 204 and the triangular bracket 203. Handrails 209 are provided on both sides of the top of the installation box 201, and a sponge pad 210 is sleeved on the outer side of the handrail 209.
[0022] When the astronauts walk on the ground in space, the auxiliary device moves on the ground in space through the tracks 302. The astronauts hold the sponge pad 210 on the outside of the handrail 209 in their hands, and walk and explore on the planet with the cooperation of the auxiliary device and the magnetic auxiliary equipment of the space suit. When regional exploration is required, the telescopic cylinder 206 can be started to push the movable rod 208 downward, and slowly engage it into the tripod bracket 203, thereby pushing the tripod bracket 203 downward to support it on the ground, fixing and supporting the auxiliary device, thereby providing necessary protection and support. At the same time, when moving slightly, the tripod bracket 203 can prevent the astronauts from accidentally falling or losing balance during the spacewalk, thereby ensuring the safety of the astronauts and ensuring the smooth progress of the spacewalk mission.
[0023] See also Figure 3 、 Figure 4 、 Figure 6In this embodiment, a crawler 302 is rotatably installed inside the auxiliary groove 301, and a protective plate 303 is installed on the back side of the crawler 302, and the protective plate 303 is arranged inside the crawler 302; a controller 304 is installed on the top of the manned frame 1, and an operation screen 305 is provided on the inner wall opposite to the controller 304, and a clamping slot 306 is provided at the front end of the controller 304; a camera 307 is installed at the left end of the manned frame 1, and lighting lamps 308 are provided in the middle positions of the left and right sides of the front end of the manned frame 1; fixed frames 309 are installed at the front ends of the left and right sides of the manned frame 1, and a mechanical arm 310 is rotatably connected to the internal part of the fixed frame 309, and the fixed frame 309 and the mechanical arm 310 are connected by a connecting rod; a display screen 311 is provided on the side wall of the controller 304, and a driving rod 312 is rotatably connected on both sides of the inside of the crawler 302; a control button is provided in the middle position of the front end of the mechanical arm 310, and the material of the mechanical arm 310 is titanium alloy.
[0024] When the auxiliary device is in use, it is moved to the surface of the planet to be explored. The astronaut can fix the auxiliary device behind his back and slowly drive the auxiliary device to move when walking. The setting of the track 302 reduces the friction between the auxiliary device and the surface, which is convenient for the astronaut to use. The setting of the track 302 facilitates the movement of the auxiliary device to the surface of the planet in various environments, ensuring the normal use of the auxiliary device; the astronaut places his arm on the mechanical arm 310, and under the action of the connecting rod, adjusts the groove 301 to the appropriate angle for operation, the lighting lamp 308 is used for daily illumination, and the camera 307 shoots and records the surrounding environment for later review. The operation screen 305 facilitates the astronaut to communicate and observe.
[0025] Through the above steps, under the setting of the tripod bracket 203, the walking assist device forms a stable structure, which provides support for the astronauts when walking, ensures that the astronauts operate relatively smoothly, and helps prevent the astronauts from accidentally falling or losing balance during the spacewalk, thereby ensuring the safety of the astronauts and ensuring the smooth progress of the spacewalk mission; this solves the problem that the walking assist device is not stable during walking, cannot ensure the safety of the astronauts, and ensures the smooth progress of the spacewalk mission.
Claims
1. A computer-based space operation assisting device comprising a manned frame (1); characterized in that: The supporting assembly and the auxiliary assembly are also included. The rear end of the manned frame (1) is equipped with a supporting assembly for auxiliary support. The manned frame (1) is equipped with an auxiliary assembly for assisting walking. The supporting assembly includes an installation box (201), a fixing ring (202), a triangular bracket (203) and a slot (204). The rear end of the manned frame (1) is equipped with an installation box (201). The left and right sides of the bottom end of the installation box (201) are magnetically connected to the fixing ring (202). The outer side of the fixing ring (202) is movably connected to the triangular bracket (203). The bracket (203) is provided with slots (204) on the left and right sides of the bottom end of the manned frame (1), and the center of the fixing ring (202) is symmetrical to the bottom end of the slot (204); the auxiliary components include a slot (301), a crawler (302), a protective plate (303), a controller (304), an operating screen (305), a snap-on slot (306), a camera (307), a lighting lamp (308), a fixing frame (309) and a mechanical arm (310), and the bottom end of the manned frame (1) is provided with a slot (301).
2. The computer-based space operation assistance device according to claim 1, characterized in that: A partition (205) is provided inside the installation box (201), and telescopic cylinders (206) are provided at both left and right ends of the top of the partition (205). A mounting ring (207) is symmetrically installed on the outer side of the top of the slot (204).
3. The computer-based space operation assistance device according to claim 2, characterized in that: The telescopic end of the telescopic cylinder (206) is connected to a movable rod (208), and the movable rod (208) is movably connected to the slot (204) and the triangular bracket (203). Handrails (209) are provided on both sides of the top of the installation box (201), and a sponge pad (210) is sleeved on the outer side of the handrail (209).
4. The computer-based space operation assistance device according to claim 1, characterized in that: A crawler belt (302) is rotatably mounted inside the groove (301), and a protective plate (303) is mounted on the back side of the crawler belt (302), and the protective plate (303) is arranged inside the crawler belt (302).
5. The computer-based space operation assistance device according to claim 1, characterized in that: A controller (304) is installed at the top of the passenger carrier (1), an operation screen (305) is provided on the inner wall opposite to the controller (304), and a snap-in slot (306) is provided at the front end of the controller (304).
6. The computer-based space operation assistance device according to claim 1, characterized in that: A camera (307) is installed at the left end of the people carrier (1), and lighting lamps (308) are provided at the middle positions of the left and right sides of the front end of the people carrier (1).
7. The computer-based space operation assistance device according to claim 1, characterized in that: Fixed frames (309) are installed at the front ends of the left and right sides of the people carrier (1), and the internal rotation of the fixed frame (309) is connected to the mechanical arm (310), and the fixed frame (309) and the mechanical arm (310) are connected by a connecting rod.
8. The computer-based space operation assistance device according to claim 1, characterized in that: A display screen (311) is provided on the side wall of the controller (304), and driving rods (312) are rotatably connected to both sides of the crawler belt (302).
9. The computer-based space operation assistance device according to claim 7, characterized in that: A control button is provided at the middle position of the front end of the mechanical arm (310), and the material of the mechanical arm is titanium alloy.