CN213092562U - Stable landing device of return capsule for simulating aerospace - Google Patents
Stable landing device of return capsule for simulating aerospace Download PDFInfo
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- CN213092562U CN213092562U CN202021167936.0U CN202021167936U CN213092562U CN 213092562 U CN213092562 U CN 213092562U CN 202021167936 U CN202021167936 U CN 202021167936U CN 213092562 U CN213092562 U CN 213092562U
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- lifting rope
- resistance control
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- 239000002775 capsule Substances 0.000 title claims description 41
- 238000004088 simulation Methods 0.000 claims abstract description 43
- 239000007769 metal material Substances 0.000 claims description 2
- 230000001771 impaired effect Effects 0.000 abstract description 4
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000003550 marker Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
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Abstract
The utility model discloses a device is steadily landed to reentry module that simulation aerospace was used, including fixed table surface, fixed table surface's upper surface one side position fixed mounting has the support pole setting, fixed table surface's upper surface other side position fixed mounting has yardstick mark pole, the upper end external fixed surface who supports pole setting and yardstick mark pole installs fixed roof, fixed roof's lower fixed surface installs resistance control box, the lower surface of resistance control box is provided with connects the lifting rope, the lower extreme surface movable mounting who connects the lifting rope has the go-between, the lower fixed surface of go-between is connected with simulation reentry module. A device that steadily lands of reentry module of simulation aerospace usefulness, can be when the simulation, adjust the resistance that drops, the experiment simulation of convenient different specifications can be when the simulation reentry module drops, cushions impact force, it is impaired to have prevented that the simulation reentry module from dropping.
Description
Technical Field
The utility model relates to an aerospace simulation field, in particular to device is steadily landed to reentry module that simulation aerospace was used.
Background
The device for simulating stable landing of the recoverable capsule for aerospace is a device for performing stable landing simulation on the recoverable capsule for aerospace, can simulate the landing data of the recoverable capsule for aerospace, is widely used in aerospace experiments and teaching occasions, and can gradually improve the use demand of the device for simulating stable landing of the recoverable capsule for aerospace along with the gradual improvement of the use demand of the device for simulating stable landing of the recoverable capsule for aerospace, so that the device for simulating stable landing of the recoverable capsule for aerospace in the prior art can not meet the demand of people, and therefore, the device for simulating stable landing of the recoverable capsule for aerospace, which is more convenient to use, is needed; when the steady landing device of recoverable capsule for simulating aerospace uses, the resistance that drops can't be adjusted, the experimental simulation of inconvenient different specifications, simultaneously, can't cushion the impact force of simulation recoverable capsule, it is impaired to have led to the simulation recoverable capsule to drop easily.
SUMMERY OF THE UTILITY MODEL
The utility model discloses a main aim at provides a device is steadily landed to reentry module that simulation aerospace was used, can effectively solve the problem in the background.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
a device for simulating stable landing of a reentry module for aerospace comprises a fixed table top, wherein a supporting vertical rod is fixedly mounted at one side of the upper surface of the fixed table top, a scale marking rod is fixedly mounted at the other side of the upper surface of the fixed table top, a fixed top plate is fixedly mounted on the outer surface of the upper end of the supporting vertical rod and the scale marking rod, a resistance control box is fixedly mounted on the lower surface of the fixed top plate, a connecting lifting rope is arranged on the lower surface of the resistance control box, a connecting ring is movably mounted on the outer surface of the lower end of the connecting lifting rope, the lower surface of the connecting ring is fixedly connected with the simulated reentry module, an adjusting screw is mounted on the inner surface of the resistance control box through threads, an adjusting handle is fixedly mounted on the outer surface of one end of the adjusting screw, a connecting jacking block is movably connected on the outer, the internal surface of resistance control box is located one side position rotation of adjusting screw and installs two driven runner, the last fixed surface of fixed roof installs the location baffle, the inboard position movable mounting that the upper surface of fixed roof is located the location baffle has buffer spring, the upper end external surface fixed connection who connects the lifting rope has the stopper, the upper surface of fixed table face is located the intermediate position fixed mounting who supports pole setting and yardstick mark pole and is had the simulation mud board.
Preferably, the lower surface of the fixed table top is fixedly provided with two supporting foot stands which are symmetrically arranged and arranged in parallel.
Preferably, the supporting upright rod and the scale marking rod are the same in height, and the outer surface of the scale marking rod is provided with a marking sliding block in a sliding mode.
Preferably, the upper end of the connecting lifting rope penetrates through the resistance control box and the fixed top plate, the jacking rotating wheel and the driven rotating wheel are respectively located at two sides of the connecting lifting rope, and the adjusting handle is located at the outer side of the resistance control box.
Preferably, the buffer spring is located at the outer side position of the connecting lifting rope, and the lower surface of the limiting block is in fit connection with the upper surface of the buffer spring.
Preferably, the simulation mud plate is located below the simulation re-entry capsule, and the simulation re-entry capsule is designed to be made of metal materials.
Compared with the prior art, the utility model discloses following beneficial effect has: this device is steadily landed to reentry module that simulation aerospace was used, through the resistance control box that sets up, connect the lifting rope, adjusting screw, adjust handle, connect the kicking block, push up runner and driven runner, can be when the simulation, adjust the resistance that drops, make things convenient for the experimental simulation of different specifications, through the positioning baffle that sets up, buffering bullet and stopper, can be when the simulation reentry module drops, cushion the impact force of simulation reentry module, prevented that the simulation reentry module from dropping impaired.
Drawings
Fig. 1 is a schematic view of the overall structure of a landing device for simulating a stable landing of a re-entry capsule for aerospace use according to the present invention;
fig. 2 is an exploded view of a resistance control box of a stable landing device of a return capsule for simulating aerospace of the invention;
fig. 3 is an enlarged view of the buffer spring of the steady landing device of the re-entry capsule for simulating aerospace.
In the figure: 1. fixing the table top; 2. a supporting foot rest; 3. supporting the upright stanchion; 4. a scale marker rod; 5. marking a sliding block; 6. fixing a top plate; 7. a resistance control box; 8. connecting a lifting rope; 9. a connecting ring; 10. simulating a returning cabin; 11. adjusting the screw rod; 12. adjusting the handle; 13. connecting the top block; 14. pushing the rotating wheel; 15. a driven runner; 16. positioning a baffle plate; 17. a buffer spring; 18. a limiting block; 19. and (5) simulating a mud board.
Detailed Description
In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.
In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element to which the reference is made must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, and for example, "connected" may be either fixedly connected or detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
As shown in fig. 1-3, a steady landing device of a return capsule for simulating aerospace use comprises a fixed table top 1, a supporting upright rod 3 is fixedly installed at one side of the upper surface of the fixed table top 1, a scale marking rod 4 is fixedly installed at the other side of the upper surface of the fixed table top 1, a fixed top plate 6 is fixedly installed on the outer surfaces of the upper ends of the supporting upright rod 3 and the scale marking rod 4, a resistance control box 7 is fixedly installed on the lower surface of the fixed top plate 6, a connecting lifting rope 8 is arranged on the lower surface of the resistance control box 7, a connecting ring 9 is movably installed on the outer surface of the lower end of the connecting lifting rope 8, a simulated return capsule 10 is fixedly connected with the lower surface of the connecting ring 9, an adjusting screw 11 is installed on the inner surface of the resistance control box 7 by screw thread, an adjusting handle 12 is fixedly installed on the outer, the inner side of the connecting top block 13 is rotatably provided with a top moving rotating wheel 14, the inner surface of the resistance control box 7 is rotatably provided with two driven rotating wheels 15 at one side position of the adjusting screw rod 11, the upper surface of the fixed top plate 6 is fixedly provided with a positioning baffle 16, the upper surface of the fixed top plate 6 is movably provided with a buffer spring 17 at the inner side position of the positioning baffle 16, the outer surface of the upper end of the connecting lifting rope 8 is fixedly connected with a limiting block 18, and the upper surface of the fixed table top 1 is fixedly provided with a simulation mud plate 19 at the middle position of the supporting vertical rod 3 and the scale marking rod 4;
two supporting foot frames 2 are fixedly arranged on the lower surface of the fixed table top 1, the two supporting foot frames 2 are symmetrically arranged and arranged in parallel, and the supporting foot frames 2 are used for supporting and fixing the device; the supporting upright rod 3 and the scale marking rod 4 are the same in height, a marking sliding block 5 is slidably mounted on the outer surface of the scale marking rod 4, and the marking sliding block 5 is used for matching with the scale marking rod 4 to mark the height; the upper end of the connecting lifting rope 8 penetrates through the resistance control box 7 and the fixed top plate 6, the jacking rotating wheels 14 and the driven rotating wheels 15 are respectively positioned at two side positions of the connecting lifting rope 8, the adjusting handle 12 is positioned at the outer side position of the resistance control box 7, and the jacking rotating wheels 14 and the driven rotating wheels 15 are used for being attached to the connecting lifting rope 8 to adjust resistance; the buffer spring 17 is positioned at the outer side of the connecting lifting rope 8, and the lower surface of the limiting block 18 is in fit connection with the upper surface of the buffer spring 17; the simulated mud plate 19 is positioned below the simulated re-entry capsule 10, and the simulated re-entry capsule 10 is designed to be of a metal structure.
It should be noted that the utility model relates to a steady landing device of a return capsule for simulating aerospace, the fixed table board 1 constitutes the installation fixing part of the device, when in use, the device falls downwards above the fixed table board 1 through the simulation return capsule 10 and falls above the simulation mud plate 19, the simulation return capsule 10 and the simulation mud plate 19 simulate the return capsule and the ground, thereby the simulation experiment of steady landing of the return capsule is carried out when the simulation return capsule 10 falls on the simulation mud plate 19, the connecting lifting rope 8 is used for pulling back the simulation return capsule 10, when the simulation return capsule 10 falls downwards, the adjusting handle 12 outside the resistance control box 7 can be rotated, the adjusting handle 12 drives the adjusting screw rod 11 to rotate, the rotation of the adjusting screw rod 11 is screwed in and out through the threaded connection with the resistance control box 7, thereby the jacking runner 14 is driven to move to one side through the connecting jacking block 13, then the jacking runner 14 will connect the lifting rope 8 and push up one side at two driven runners 15, through the elasticity adjustment between jacking runner 14 and the driven runner 15, adjust the upper and lower resistance of connecting the lifting rope 8, the resistance when simulating the recoverable capsule 10 and dropping is adjusted, when simulating the recoverable capsule 10 and dropping on simulation mud slab 19, the simulation recoverable capsule 10 pulls stopper 18 through the upper end of adjusting the connection lifting rope 8 and moves downwards, make stopper 18 top at the top of buffer spring 17, then through the resilience of buffer spring 17, cushion the downward impact force of stopper 18, thereby cushion the impact force of simulating the recoverable capsule 10, prevent that simulation recoverable capsule 10 is impaired when simulating, positioning baffle 16 is used for fixing a position the sheltering from buffer spring 17.
The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (6)
1. The utility model provides a device is landed steadily to reentry module of simulation aerospace usefulness which characterized in that: including fixed table face (1), the upper surface one side position fixed mounting of fixed table face (1) has support pole setting (3), the upper surface other side position fixed mounting of fixed table face (1) has yardstick mark pole (4), the upper end external surface fixed mounting who supports pole setting (3) and yardstick mark pole (4) has fixed roof (6), the lower fixed surface of fixed roof (6) installs resistance control box (7), the lower surface of resistance control box (7) is provided with connection lifting rope (8), the lower extreme external surface movable mounting who connects lifting rope (8) has go-between (9), the lower fixed surface of go-between (9) is connected with simulation recoverable cabin (10), adjusting screw (11) are installed to the internal surface screw thread of resistance control box (7), the one end external surface fixed mounting of adjusting screw (11) has regulation handle (12), the utility model discloses a building roof, including adjusting screw (11), the inboard of connecting kicking block (13) is rotated and is installed the top and move runner (14), one side position that the internal surface of resistance control box (7) is located adjusting screw (11) is rotated and is installed two driven runner (15), the last fixed surface of fixed roof (6) installs positioning baffle (16), the inboard position movable mounting that the upper surface of fixed roof (6) is located positioning baffle (16) has buffer spring (17), the upper end outer fixed surface of connecting lifting rope (8) is connected with stopper (18), the upper surface of fixed table face (1) is located the intermediate position fixed mounting who supports pole setting (3) and yardstick mark pole (4) and has simulation mud board (19).
2. A simulated aeronautical and astronautic re-entry capsule landing apparatus as claimed in claim 1, wherein: two supporting foot stands (2) are fixedly installed on the lower surface of the fixed table top (1), and the two supporting foot stands (2) are symmetrically arranged and are arranged in parallel.
3. A simulated aeronautical and astronautic re-entry capsule landing apparatus as claimed in claim 1, wherein: the height of the supporting upright rod (3) is the same as that of the scale marking rod (4), and a marking sliding block (5) is installed on the outer surface of the scale marking rod (4) in a sliding mode.
4. A simulated aeronautical and astronautic re-entry capsule landing apparatus as claimed in claim 1, wherein: the upper end of the connecting lifting rope (8) penetrates through the resistance control box (7) and the fixed top plate (6), the jacking rotating wheels (14) and the driven rotating wheels (15) are respectively located at the positions of two sides of the connecting lifting rope (8), and the adjusting handle (12) is located at the position of the outer side of the resistance control box (7).
5. A simulated aeronautical and astronautic re-entry capsule landing apparatus as claimed in claim 1, wherein: the buffer spring (17) is located at the outer side position of the connecting lifting rope (8), and the lower surface of the limiting block (18) is connected with the upper surface of the buffer spring (17) in a fitting mode.
6. A simulated aeronautical and astronautic re-entry capsule landing apparatus as claimed in claim 1, wherein: the simulation mud plate (19) is located at the position below the simulation returning capsule (10), and the simulation returning capsule (10) is designed to be made of metal materials.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021167936.0U CN213092562U (en) | 2020-06-22 | 2020-06-22 | Stable landing device of return capsule for simulating aerospace |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021167936.0U CN213092562U (en) | 2020-06-22 | 2020-06-22 | Stable landing device of return capsule for simulating aerospace |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213092562U true CN213092562U (en) | 2021-04-30 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021167936.0U Active CN213092562U (en) | 2020-06-22 | 2020-06-22 | Stable landing device of return capsule for simulating aerospace |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213092562U (en) |
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2020
- 2020-06-22 CN CN202021167936.0U patent/CN213092562U/en active Active
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20231204 Address after: Building 2, 4th Floor, No.14 Fucheng Road, Haidian District, Beijing, 100000 Patentee after: Aerospace Engineering Consulting (Beijing) Co.,Ltd. Address before: 518000 Xinghui center, 122 Huangpu Avenue West, Tianhe District, Guangzhou City, Guangdong Province Patentee before: Zheng Yudian |
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| TR01 | Transfer of patent right |