CN115616494B - Anti-collision satellite radar used in severe environment - Google Patents
Anti-collision satellite radar used in severe environment Download PDFInfo
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- CN115616494B CN115616494B CN202211638687.2A CN202211638687A CN115616494B CN 115616494 B CN115616494 B CN 115616494B CN 202211638687 A CN202211638687 A CN 202211638687A CN 115616494 B CN115616494 B CN 115616494B
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
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Abstract
The invention discloses an anti-collision satellite radar used in a severe environment, which comprises an anti-collision machine body, wherein an anti-collision device is arranged on the outer surface of the anti-collision machine body, a tension spring is fixedly connected with the outer surface of a supporting column, an anti-shaking device is fixedly connected to the central position of the top of the anti-collision machine body, an auxiliary device is arranged on the outer surface of the anti-collision machine body and close to the bottom of the supporting column, a satellite radar main body is fixedly connected to the top of a rotary worktable, the bottom of a first protection device and the top of a second protection device are arranged on the outer surface of the anti-collision machine body and close to the edge position, and a guide plate is fixedly connected to the outer surface of the second protection device and close to the bottom position. This an anticollision type satellite radar for under adverse circumstances has reached strong adaptability's effect, can carry out the anticollision to in time reduce the focus, reduce the blowing that receives wind-force, stability is good, and safe and reliable has realized multiple functions, has improved performance.
Description
Technical Field
The invention relates to the technical field of satellite radars, in particular to an anti-collision satellite radar used in a severe environment.
Background
Radar, generally referred to as "radio detection and ranging", uses the method of radio to find objects and determine their spatial location. Therefore, radars, which are electronic devices that detect objects using electromagnetic waves, are also called "radiolocalization". The radar emits electromagnetic waves to irradiate the target and receives the echo of the target, so that information such as the distance from the target to an electromagnetic wave emission point, the distance change rate, the direction and the height can be obtained.
At present, current satellite radar adaptability is poor, can't adapt to adverse circumstances, receives the influence of strong wind weather easily to can receive the striking under adverse circumstances, make equipment overall stability poor, be unfavorable for the adjustment to satellite radar height and angle, and then influence the normal use of radar installation, reduce performance.
Disclosure of Invention
In order to realize the purpose, the invention is realized by the following technical scheme: an anti-collision satellite radar used in a severe environment comprises an anti-collision machine body, wherein an anti-collision device is arranged on the outer surface of the anti-collision machine body, a support column penetrates through the top of the anti-collision machine body, the bottom of the support column extends into the anti-collision machine body, a tension spring is fixedly connected to the outer surface of the support column, an anti-shaking device is fixedly connected to the central position of the top of the anti-collision machine body, the top end of the support column penetrates through the center of the anti-shaking device and extends to the outside, an auxiliary device is arranged on the outer surface of the anti-collision machine body and close to the bottom of the support column, a gas pipe is fixedly connected to the surface of the anti-collision machine body and communicates the anti-collision device with the anti-shaking device, a rotary workbench is fixedly connected to the top end of the support column, a satellite radar main body is fixedly connected to the top of the rotary workbench, a stabilizing barrel is fixedly connected to the inner surface of the anti-collision machine body, the stabilizing barrel is sleeved on the outer surface of the support column, and the top end of the tension spring is fixedly connected to the top of the inner wall of the stabilizing barrel, and the satellite radar main body is lifted under the tension force of the tension spring;
the anti-collision device comprises a first protection device and a second protection device, the bottom of the first protection device and the top of the second protection device are arranged on the outer surface of the anti-collision machine body and are close to the edge position, the outer surface of the anti-collision machine body and the position close to the second protection device are fixedly connected with an elastic compression body, an air port of the elastic compression body is communicated with the bottom end of the air conveying pipe, the outer surface of the first protection device and the outer surface of the second protection device are both fixedly connected with elastic reset pieces, one end of each elastic reset piece, far away from the first protection device and the second protection device, is fixedly connected with the outer surface of the anti-collision machine body, the outer surface of the second protection device and the position close to the bottom are fixedly connected with a guide plate, and when external force is applied to the anti-collision device, and utilize first protector, be connected for rotating between second protector and the anticollision organism, first protector and second protector rotate to both sides this moment, and then decompose external force, weaken the impact of external force, can also carry out the water conservancy diversion to the direction, weaken the power of blowing of wind, and along with second protector's rotation, can compress the elasticity pressurized body, and utilize the gas-supply pipe to gaseous transport, make gas enter into the anti-shake device, and then promoted the stability of support column, and along with the rotation of first protector, can exert the pressing force to auxiliary device, can promote anticollision, can also exert the pressing force to the support column bottom, make the support column drive satellite radar main part through swivel work head and move downwards, make satellite radar main part retract, and then make the device wholly shorten, the focus has been reduced.
Preferably, the bottom of the anti-collision machine body is provided with a through hole through which the bottom of the supporting column penetrates, the first protection device and the second protection device are located on the same plane when reset, and the outer surface of the elastic reset piece is provided with a curved surface.
Preferably, the first protection device comprises a protection substrate, the bottom of the protection substrate is rotationally connected with the outer surface edge position of the anti-collision machine body, the top end of the elastic reset piece is fixedly connected with the outer surface of the protection substrate, the outer surface of the protection substrate is fixedly connected with the main flexible piece, the outer surface of the protection substrate is close to the auxiliary flexible piece, when strong wind blows on the first protection device and the second protection device, the bottom of the protection substrate is rotationally connected with the outer surface edge position of the anti-collision machine body in a combined mode, the combination of the first protection device and the structure of the second protection device are the same, the first protection device rotates along a hinge point, the second protection device drives the guide plate to rotate anticlockwise along the hinge point, the elastic reset piece is compressed, the V-shaped opening is formed by the first protection device and the second protection device at the moment, the wind direction guiding can be carried out, the impact force of the wind can be decomposed, the impact force of weak wind is reduced, meanwhile, the flow guiding effect of the guide plate enables the air flow to blow downwards, downward power is applied to the machine body, the whole device is not easy to be blown, the secondary flexible piece, the impact force of the main flexible substrate is improved, the stability of the anti-collision machine body is improved, and the flexible piece, the flexible substrate is uniformly contacted with the anti-collision material, and the anti-collision material is good.
Preferably, the protective substrate is obliquely arranged, and the main flexible sheet and the auxiliary flexible sheet are uniformly distributed on the outer surface of the protective substrate.
Preferably, the anti-shaking device comprises a guide cylinder, the outer surface of the guide cylinder is fixedly connected with the top of the anti-collision machine body, the top end of the support column penetrates through the center of the guide cylinder, a limiting device is arranged on the inner surface of the guide cylinder and close to the outer surface of the support column, an elastic pressing strip is fixedly connected to the end part of the limiting device, an elastic expansion body is fixedly connected to the inner surface of the guide cylinder and close to the limiting device, and an air port of the elastic expansion body is communicated with the top end of the air conveying pipe.
Preferably, the limiting device comprises a top pressure plate, the right end of the top pressure plate is rotatably connected with the inner surface of the guide cylinder, one end, far away from the inner surface of the guide cylinder, of the top pressure plate is fixedly connected with an arc positioning plate, the right end of the elastic pressing strip is fixedly connected with the outer surface of the arc positioning plate, and one side, far away from the left end of the top pressure plate, of the outer surface of the arc positioning plate is connected with a ball in a rolling mode.
Preferably, the balls are uniformly distributed on the outer surface of the cambered surface positioning plate and far away from one side of the left end of the jacking plate, and the outer surface of the cambered surface positioning plate is provided with a rolling groove matched with the balls.
Preferably, the auxiliary device comprises an arc-shaped sleeve, the outer surface of the arc-shaped sleeve is fixedly connected with the outer surface of the anti-collision machine body, the inner portion of the arc-shaped sleeve is slidably connected with a jacking device, the outer surface of the anti-collision machine body is fixedly connected with an elastic strip close to the arc-shaped sleeve, and the top end of the elastic strip is fixedly connected with the top end of the jacking device.
Preferably, the jacking device comprises an arc jacking rod, the bottom end of the arc jacking rod penetrates through the center of the arc sleeve, the outer surface of the arc jacking rod is in sliding connection with the inner surface of the arc sleeve, a jacking ball is fixedly connected to the top end of the arc jacking rod, the top end of the elastic strip is fixedly connected with the outer surface of the jacking ball, a pressing block is fixedly connected to the bottom end of the arc jacking rod, a flexible sucker is fixedly connected to the bottom of the pressing block, when the protective substrate is blown by wind power to rotate, the jacking device on the auxiliary device can receive pressing force at the moment and is in sliding connection with the outer surface of the arc jacking rod and the inner surface of the arc sleeve, the arc jacking rod can drive the pressing block to slide downwards, the elastic strip is compressed and combines acting force and reacting force, so that the jacking ball exerts reverse thrust on the protective substrate under the reverse elastic strip, further, the collision prevention of the protective substrate is promoted again, and the pressing block sliding downwards impacts the bottom of the supporting column, so that the satellite radar main body is driven to move downwards to retract the satellite radar main body.
Preferably, the circle center of the arc-shaped jacking rod coincides with the circle center of the arc-shaped sleeve, and the flexible suckers are uniformly distributed at the bottom of the pressing block.
The invention provides an anti-collision satellite radar used in a severe environment. The method has the following beneficial effects:
1. the anti-collision satellite radar used in severe environment comprises an anti-collision body, an anti-collision device, a support column, a tension spring, an anti-shaking device, an auxiliary device, a gas pipe, a rotary workbench, a satellite radar main body, a stabilizing cylinder, a first protection device, a second protection device, an elastic pressure body, an elastic reset sheet and a guide plate, wherein the support column is used for supporting the rotary workbench, the satellite radar main body is lifted under the tension action of the tension spring, after external force is applied to the anti-collision device, the first protection device and the second protection device are rotatably connected with the anti-collision body, the first protection device and the second protection device rotate towards two sides, the external force is decomposed, the impact of the external force is weakened, the direction can be guided, and the blowing force of wind is weakened, and along with the rotation of second protector, can compress the elasticity pressurized body, and utilize the gas-supply pipe to gaseous transport, make gas enter into the anti-shaking device, and then the stability of support column has been promoted, and along with the rotation of first protector, can exert the pressing force to auxiliary device, can promote anticollision, can also exert the pressing force to the support column bottom, make the support column pass through swivel work head and drive satellite radar main part downstream, make satellite radar main part withdrawal, and then make the device wholly shorten, the focus has been reduced, reduce the impact that receives wind-force, make stability better, utilize the interact between the structure, make the integrated device can carry out anticollision, and in time reduce the holistic focus of equipment, reduce the blowing that receives wind-force, good stability, safety and reliability, multiple functions have been realized, performance has been improved.
2. The anti-collision satellite radar used in severe environment comprises a first protection device, a second protection device, an elastic pressure body, an elastic reset sheet, a guide plate, a protection substrate, a main flexible sheet and an auxiliary flexible sheet, wherein when strong wind blows on the first protection device and the second protection device, the bottom of the protection substrate is combined with the edge position of the outer surface of an anti-collision machine body to be rotationally connected, the combination of the first protection device and the second protection device have the same structure, so that the first protection device rotates along a hinge point along a needle, the second protection device drives the guide plate to rotate along the hinge point anticlockwise, the elastic reset sheet is compressed, the first protection device and the second protection device form a V-shaped opening, and the anti-collision satellite radar not only can guide the wind direction, but also can decompose the impact force of the wind, weaken the impact force of wind, simultaneously the water conservancy diversion effect of guide plate is down, make the air current blow downwards, and then exert decurrent power of blowing to the anticollision organism, and then make the whole difficult by wind blowing of device, and then holistic stability has been improved, simultaneously main flexible piece, vice flexible piece evenly distributed is at the surface of protective substrate, when making external force strike protective substrate, the material that utilizes main flexible piece and vice flexible piece all sets up to the rubber material, good flexibility, flexible contact has been played, be difficult for causing the damage to protective substrate, make the power of blowing that utilizes wind, make first protector, the second protector not only can in time be crashproof, can also change the direction of blowing of wind, make whole more stable, multiple functions have been realized, safety and reliability, service performance is improved.
3. This a crashproof type satellite radar for under adverse circumstances, through the support column, the elasticity pressurized body, the gas-supply pipe, the anti-shake device, the guide cylinder, stop device, the elastic pressing strip, the elastic expansion body, the roof pressure plate, the cambered surface locating plate, the ball, the right-hand member that combines the roof pressure plate is connected with the internal surface rotation of guide cylinder, and under the spring action of elastic pressing strip, make the cambered surface locating plate press from both sides tight support to the support column, make the surface of ball and the surface laminating of support column, when the support column reciprocates, make the ball roll, adopt rolling friction, frictional force has been reduced, help the support column to remove smoothly, and then make things convenient for the regulation to satellite radar main part overall height, and utilize along with the elasticity pressurized body to receive the compression, inside gas passes through the gas-supply pipe and carries in the elastic expansion body, along with the increase of gas pressure, make the elastic expansion body inflation, and then exert the driving force again to roof pressure plate and cambered surface locating plate, and then increased the support column of cambered surface locating plate to the clamp force, make the whole body receive after external force, the device wholly receives the external force, the mutual action between the utilization of the mutual interaction, make the gas pressure increase, and the smooth and the structure, and the whole reliable utilization of the support column of the structure of the promotion, and the mutual connection of the promotion, and the improvement of the structure, and the mutual effect of the gas, the utilization of the structure, the mutual effect of the gas.
4. This a crashproof type satellite radar for under adverse circumstances, through the support column, the protective substrate, auxiliary device, the arc sleeve, the roof pressure device, the elastic strip, arc roof pressure pole, the kickball, the briquetting, flexible suction cup, when protective substrate receives wind-force to blow and rotates, roof pressure device on the auxiliary device can receive the pressing force this moment, and sliding connection between the surface that combines arc roof pressure pole and the internal surface of arc sleeve, arc roof pressure pole can drive the briquetting lapse at this moment, and the elastic strip is compressed, and combine effort and reaction force, make the kickball under the reverse elasticity of elastic strip, exert reverse thrust to protective substrate, and then promoted protective substrate's anticollision again, the while lapse briquetting strikes the bottom of support column, make the support column drive satellite radar main part lapse, make the satellite reach the main part withdrawal, not only the height of the device is reduced wholly, make the focus lapse, stability is good, can also reduce the impact that receives wind-force, difficult the appearance rocks, and along with the pressing of briquetting to flexible suction cup, make the bottom of support column suck the bottom of support column, and then the condition of slippage is difficult to appear, help pressing the ingenious mutual connection between the structure to be put together, the realization of the safe and reliable utilization of the structure, the mutual connection has been realized.
Drawings
FIG. 1 is a schematic view of the overall structure of an anti-collision satellite radar used in a severe environment according to the present invention;
FIG. 2 is a schematic diagram of an internal structure of an anti-collision satellite radar used in a severe environment according to the present invention;
FIG. 3 is a schematic view of a bump guard of the present invention;
FIG. 4 is a schematic view of a first protective device according to the present invention;
FIG. 5 is a schematic structural view of the anti-sloshing apparatus of the present invention;
FIG. 6 is a schematic view of the structure of the position limiting device of the present invention;
FIG. 7 is a schematic view of the auxiliary device of the present invention;
fig. 8 is a schematic structural view of the pressing device of the present invention.
In the figure: 1. an anti-collision machine body; 2. a guard; 3. a support column; 4. a tension spring; 5. an anti-sloshing device; 6. an auxiliary device; 7. a gas delivery pipe; 8. rotating the working table; 9. a satellite radar main body; 10. a stabilizing cylinder; 21. a first guard; 22. a second guard; 23. an elastic compression body; 24. an elastic reset sheet; 25. a baffle; 211. a protective substrate; 212. a primary flexible sheet; 213. a secondary flexible sheet; 51. a guide cylinder; 52. a limiting device; 53. elastic pressing strips; 54. an elastic expansion body; 521. a top pressure plate; 522. a cambered surface positioning plate; 523. a ball bearing; 61. an arc-shaped sleeve; 62. an elastic strip; 63. an elastic strip; 621. an arc-shaped top pressure rod; 622. ejecting the ball; 623. pressing into blocks; 624 flexible suction cup.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings and specific embodiments. The embodiments of the present invention have been presented for purposes of illustration and description, and are not intended to be exhaustive or limited to the invention in the form disclosed. Many modifications and variations will be apparent to practitioners skilled in this art. The embodiment was chosen and described in order to best explain the principles of the invention and the practical application, and to enable others of ordinary skill in the art to understand the invention for various embodiments with various modifications as are suited to the particular use contemplated.
Example 1
Referring to fig. 1-3, the present invention provides a technical solution: an anti-collision satellite radar used in severe environment comprises an anti-collision body 1, wherein an anti-collision device 2 is arranged on the outer surface of the anti-collision body 1, a support column 3 penetrates through the top of the anti-collision body 1, the bottom of the support column 3 extends into the anti-collision body 1, a tension spring 4 is fixedly connected to the outer surface of the support column 3, an anti-shaking device 5 is fixedly connected to the center of the top of the anti-collision body 1, the top end of the support column 3 penetrates through the center of the anti-shaking device 5 and extends to the outside, an auxiliary device 6 is arranged on the outer surface of the anti-collision body 1 and close to the bottom of the support column 3, a gas pipe 7 is fixedly connected to the surface of the anti-collision body 1, the gas pipe 7 is used for communicating the anti-collision device 2 and the anti-shaking device 5, a rotary workbench 8 is fixedly connected to the top of the support column 3, a satellite radar main body 9 is fixedly connected to the top of the rotary workbench 8, a stabilizing cylinder 10 is fixedly connected to the inner surface of the anti-collision body 1, the stabilizing cylinder 10 is sleeved on the outer surface of the support column 3, and the top of the tension spring 4 is fixedly connected to the top of the stabilizing cylinder 10;
the anti-collision device 2 comprises a first protection device 21 and a second protection device 22, the bottom of the first protection device 21 and the top of the second protection device 22 are arranged on the outer surface of the anti-collision machine body 1 and are close to the edge position, the outer surface of the anti-collision machine body 1 and the position of the second protection device 22 are fixedly connected with an elastic compression body 23, an air port of the elastic compression body 23 is communicated with the bottom end of the air conveying pipe 7, the outer surface of the first protection device 21 and the outer surface of the second protection device 22 are fixedly connected with elastic reset pieces 24, the elastic reset pieces 24 are far away from one ends of the first protection device 21 and the second protection device 22 and are fixedly connected with the outer surface of the anti-collision machine body 1, and the outer surface of the second protection device 22 is fixedly connected with a guide plate 25.
The bottom of the anti-collision machine body 1 is provided with a through hole through which the bottom of the supporting column 3 passes, the first protective device 21 and the second protective device 22 are positioned on the same plane when resetting, the outer surface of the elastic resetting piece 24 is provided with a curved surface, the supporting column 3 is used for supporting the rotary worktable 8, the satellite radar main body 9 is lifted under the action of the tension spring 4, after external force is applied to the anti-collision device 2, the first protective device 21 and the second protective device 22 are rotatably connected with the anti-collision machine body 1, at the moment, the first protective device 21 and the second protective device 22 rotate towards two sides, the external force is decomposed, the impact of the external force is weakened, the direction can be guided, the blowing force of wind is weakened, and the elastic compression body 23 can be compressed along with the rotation of the second protective device 22, and utilize gas-supply pipe 7 to gaseous transport, make gas enter into in preventing shaking device 5, and then promoted the stability of support column 3, and along with first protector 21's rotation, can exert the pressing force to auxiliary device 6, can promote anticollision, can also exert the pressing force to support column 3 bottom, make support column 3 drive satellite radar main part 9 through swivel work head 8 and move down, make satellite radar main part 9 retract, and then make the device wholly turn short, the focus has been reduced, reduce the impact that receives wind-force, make stability better, utilize the interact between the structure, make the whole device can carry out anticollision, and in time reduce the holistic focus of equipment, reduce the blowing that receives wind-force, good stability, safety and reliability, multiple functions have been realized, service performance has been improved.
Example 2
Referring to fig. 4-8, the present invention provides a technical solution:
The protection substrate 211 is obliquely arranged, the main flexible sheet 212 and the auxiliary flexible sheet 213 are uniformly distributed on the outer surface of the protection substrate 211, when strong wind blows on the first protection device 21 and the second protection device 22, the bottom of the protection substrate 211 is combined to be rotationally connected with the edge position of the outer surface of the anti-collision machine body 1, the combination of the first protection device 21 is the same as the structure of the second protection device 22, so that the first protection device 21 rotates along a hinge point along a clockwise direction, the second protection device 22 drives the guide plate 25 to rotate along the hinge point anticlockwise, the elastic reset sheet 24 is compressed, the first protection device 21 and the second protection device 22 form a V-shaped opening, the wind direction can be guided, the impact force of the wind can be decomposed, the impact force of the wind is attenuated, and under the guiding effect of the guide plate 25, the feasible air current blows downwards, and then exert decurrent power that blows to anticollision organism 1, and then make the whole difficult by wind blowing of device, and then holistic stability has been improved, main flexible piece 212 simultaneously, vice flexible piece 213 evenly distributed is at the surface of protection base plate 211, when making external force strike protection base plate 211, the material that utilizes main flexible piece 212 and vice flexible piece 213 all sets up to the rubber material, flexibility is good, flexible contact has been played, be difficult for causing the damage to protection base plate 211, make the power that blows that utilizes wind, make first protector 21, second protector 22 not only can in time be crashproof, can also change the direction that blows of wind, make whole more stable, multiple functions have been realized, safety and reliability, service performance has been improved.
The anti-shaking device 5 comprises a guide cylinder 51, the outer surface of the guide cylinder 51 is fixedly connected with the top of the anti-collision machine body 1, the top end of the support column 3 penetrates through the center of the guide cylinder 51, a limiting device 52 is arranged on the inner surface of the guide cylinder 51 and close to the outer surface of the support column 3, an elastic pressing strip 53 is fixedly connected to the end part of the limiting device 52, an elastic expansion body 54 is fixedly connected to the inner surface of the guide cylinder 51 and close to the limiting device 52, and the air port of the elastic expansion body 54 is communicated with the top end of the air pipe 7.
The limiting device 52 comprises a top pressure plate 521, the right end of the top pressure plate 521 is rotatably connected with the inner surface of the guide cylinder 51, one end, far away from the inner surface of the guide cylinder 51, of the top pressure plate 521 is fixedly connected with a cambered surface positioning plate 522, the right end of the elastic pressing strip 53 is fixedly connected with the outer surface of the cambered surface positioning plate 522, and one side, far away from the left end of the top pressure plate 521, of the outer surface of the cambered surface positioning plate 522 is connected with a ball 523 in a rolling mode.
The balls 523 are uniformly distributed on the outer surface of the cambered surface positioning plate 522 and on one side far away from the left end of the top pressure plate 521, the outer surface of the cambered surface positioning plate 522 is provided with a rolling groove matched with the balls 523, the right end of the top pressure plate 521 is combined to be rotationally connected with the inner surface of the guide cylinder 51, and under the elastic action of the elastic pressing strip 53, the cambered surface positioning plate 522 clamps and supports the support column 3, so that the outer surface of the balls 523 is attached to the outer surface of the support column 3, when the support column 3 moves up and down, the balls 523 roll, rolling friction is adopted, the friction force is reduced, smooth movement of the support column 3 is facilitated, further, the overall height of the satellite radar main body 9 is conveniently adjusted, and internal gas is conveyed into the elastic expansion body 54 through the gas conveying pipe 7 along with compression of the elastic compression body 24, along with the increase of gas pressure, make the inflation body 54 inflation, and then exert the motive force again to top plate 521 and cambered surface locating plate 522, and then increased the clamp force to cambered surface locating plate 522 to support column 3, make the device wholly receive external force after, support column 3 is difficult for rocking, utilize interact between the structure, make cambered surface locating plate 522 not only can fix a position support column 3, can also utilize pressure, make ball 523 and support column 3 in close contact with, and then realize rolling friction, make support column 3 remove smoothly, and utilize the increase of gas pressure, the holistic stability of structure has further been promoted, utilize the interrelation between the structure, multiple functions have been reached, safety and reliability, service performance is improved.
The centre of a circle of arc roof pressure pole 621 and the coincidence of the centre of a circle of arc sleeve 61, flexible sucking disc 624 evenly distributed is in the bottom of briquetting 623, when protective substrate 211 receives wind-force to blow and rotates, roof pressure device 62 on auxiliary device 6 can receive the pressing force this moment, and sliding connection between the surface that combines arc roof pressure pole 621 and the internal surface of arc sleeve 61, arc roof pressure pole 621 can drive briquetting 623 gliding downwards this moment, and elastic strip 63 is compressed, and combine effort and reaction force, make the knob 622 under the reverse elasticity effect of elastic strip 63, exert reverse thrust to protective substrate 211, and then promoted the anticollision of protective substrate 211 again, gliding briquetting 623 strikes the bottom of support column 3 simultaneously, make support column 3 drive satellite radar main part 9 and move down, make satellite radar main part 9 retract, not only reduced the height of the whole device, make the focus move down, stability is good, can also can reduce the impact that receives wind-force, difficult the appearance rocks, utilize the interrelation between the structure to be in the same place ingeniously, safety and reliability, multiple functions are realized, service performance has improved.
When the anti-collision device is used, the support column 3 is used for supporting the rotary workbench 8, the satellite radar main body 9 is lifted under the action of the tension spring 4, when strong wind blows on the first protection device 21 and the second protection device 22, the bottom of the combined protection substrate 211 is rotatably connected with the edge position of the outer surface of the anti-collision machine body 1, the combination of the first protection device 21 and the second protection device 22 are the same in structure, the first protection device 21 rotates along the hinge point along the needle, the second protection device 22 drives the guide plate 25 to rotate anticlockwise along the hinge point, the elastic reset sheet 24 is compressed, the first protection device 21 and the second protection device 22 form a V-shaped opening, the wind direction can be guided, the impact force of the wind can be decomposed, the impact force of the weak wind is reduced, and the airflow is blown downwards under the guide effect of the guide plate 25, further, downward blowing power is applied to the anti-collision machine body 1, so that the whole device is not easily blown by wind, the right end of the jacking plate 521 is rotatably connected with the inner surface of the guide cylinder 51, the cambered surface positioning plate 522 is used for clamping and supporting the support column 3 under the elastic action of the elastic pressing strip 53, so that the outer surface of the ball 523 is attached to the outer surface of the support column 3, when the support column 3 moves up and down, the ball 523 rolls, rolling friction is adopted, friction force is reduced, the support column 3 can move smoothly, the overall height of the satellite radar main body 9 can be conveniently adjusted, internal gas is conveyed into the elastic expansion body 54 through the gas conveying pipe 7 by utilizing the compression of the elastic compression body 24, the elastic expansion body 54 expands along with the increase of gas pressure, and further, a pushing force is applied to the jacking plate 521 and the cambered surface positioning plate 522 again, and then increased the clamp force of arc face locating plate 522 to support column 3, make the device wholly receive external force after, support column 3 is difficult for rocking, and when protective substrate 211 receives wind-force to blow and rotates, roof pressure device 62 on auxiliary device 6 can receive the pressing force this moment, and sliding connection between the surface of combination arc roof pressure pole 621 and the internal surface of arc sleeve 61, arc roof pressure pole 621 can drive briquetting 623 gliding downwards this moment, and elastic strip 63 is compressed, and combine effort and reaction force, make the heading ball 622 under the reverse elasticity effect of elastic strip 63, exert reverse thrust to protective substrate 211, and then promoted the anticollision of protective substrate 211 again, gliding briquetting 623 strikes the bottom of support column 3 downwards simultaneously, make support column 3 drive satellite radar main part 9 and move downwards, make satellite radar main part 9 retract, utilize the interrelation between the structure, ingenious with the structure in the same place, safety and reliability, multiple functions have been realized, performance has been improved.
It is to be understood that the described embodiments are merely a few embodiments of the invention, and not all embodiments. All other embodiments, which can be derived by one of ordinary skill in the art and related arts based on the embodiments of the present invention without any creative effort, shall fall within the protection scope of the present invention. Structures, devices, and methods of operation not specifically described or illustrated herein are not specifically illustrated or described, but are instead contemplated to be practiced in the art by those skilled in the art.
Claims (10)
1. A crashproof type satellite radar for under adverse circumstances, includes crashproof organism (1), its characterized in that: the anti-collision device comprises an anti-collision machine body (1), wherein an anti-collision device (2) is arranged on the outer surface of the anti-collision machine body (1), a support column (3) penetrates through the top of the anti-collision machine body (1), the bottom of the support column (3) extends into the anti-collision machine body (1), a tension spring (4) is fixedly connected to the outer surface of the support column (3), an anti-shaking device (5) is fixedly connected to the center of the top of the anti-collision machine body (1), the top end of the support column (3) penetrates through the center of the anti-shaking device (5) and extends to the outside, an auxiliary device (6) is arranged on the outer surface of the anti-collision machine body (1) and close to the bottom of the support column (3), a gas pipe (7) is fixedly connected to the surface of the anti-collision machine body (1), the gas pipe (7) is communicated between the anti-collision device (2) and the anti-shaking device (5), a rotary workbench (8) is fixedly connected to the top end of the support column (3), a satellite radar main body (9) is fixedly connected to the top of the rotary workbench (8), a stabilizing cylinder (10) is fixedly connected to the inner surface of the anti-collision machine body (1), a stabilizing cylinder (10) is fixedly connected to the inner surface of the stabilizing cylinder (3), and a tension spring is fixedly connected to the top end of the support column (4);
the utility model discloses a safety protection device for the automobile crash-proof equipment, including buffer stop device (2) and second protector (22), the surface of buffer stop device (1) and the top setting of second protector (22) are at the surface of buffer stop body (1) and are close to border position, the surface of buffer stop body (1) and the rigidity that is close to second protector (22) are connected with elasticity pressurized body (23), the gas port of elasticity pressurized body (23) and the bottom intercommunication of gas-supply pipe (7), the surface of first protector (21) and the equal fixedly connected with elasticity of surface of second protector (22) reset piece (24), the elasticity resets piece (24) and keeps away from the one end of first protector (21) and second protector (22) and the surface fixed connection of buffer stop body (1), the surface of second protector (22) just is close to bottom rigidity and is connected with guide plate (25).
2. A collision avoidance satellite radar for use in harsh environments according to claim 1, wherein: the bottom of anticollision organism (1) is seted up the perforation that the bottom of support column (3) passed, be in the coplanar when first protector (21) and second protector (22) reset, the surface of elasticity piece (24) that resets sets up the curved surface.
3. A collision avoidance satellite radar for use in harsh environments according to claim 1, wherein: first protector (21) are including protection base plate (211), the surface border position of the bottom of protection base plate (211) and crashproof organism (1) rotates to be connected, the top of elasticity piece (24) that resets is connected with the surface fixed surface of protection base plate (211), the surface fixed surface of protection base plate (211) is connected with main flexible piece (212), the surface of protection base plate (211) just is close to the vice flexible piece (213) of position fixed connection of main flexible piece (212).
4. A collision avoidance satellite radar for use in harsh environments according to claim 3, wherein: the protective substrate (211) is obliquely arranged, and the main flexible sheet (212) and the auxiliary flexible sheet (213) are uniformly distributed on the outer surface of the protective substrate (211).
5. A collision avoidance satellite radar for use in harsh environments according to claim 1, wherein: the anti-shaking device (5) comprises a guide cylinder (51), the outer surface of the guide cylinder (51) is fixedly connected with the top of the anti-collision machine body (1), the top end of the supporting column (3) penetrates through the center of the guide cylinder (51), a limiting device (52) is arranged on the inner surface of the guide cylinder (51) and close to the outer surface of the supporting column (3), an elastic pressing strip (53) is fixedly connected to the end part of the limiting device (52), an elastic expansion body (54) is fixedly connected to the inner surface of the guide cylinder (51) and close to the limiting device (52), and an air port of the elastic expansion body (54) is communicated with the top end of the air conveying pipe (7).
6. A collision avoidance satellite radar for use in harsh environments according to claim 5, wherein: the limiting device (52) comprises a top pressure plate (521), the right end of the top pressure plate (521) is rotatably connected with the inner surface of the guide cylinder (51), one end, far away from the inner surface of the guide cylinder (51), of the top pressure plate (521) is fixedly connected with an arc positioning plate (522), the right end of the elastic pressing strip (53) is fixedly connected with the outer surface of the arc positioning plate (522), and one side, far away from the left end of the top pressure plate (521), of the outer surface of the arc positioning plate (522) is connected with a ball (523) in a rolling mode.
7. The anti-collision satellite radar for severe environments according to claim 6, wherein: the ball (523) is uniformly distributed on the outer surface of the cambered surface positioning plate (522) and is far away from one side of the left end of the top pressure plate (521), and a rolling groove matched with the ball (523) is formed in the outer surface of the cambered surface positioning plate (522).
8. A collision avoidance satellite radar for use in harsh environments according to claim 1, wherein: the auxiliary device (6) comprises an arc-shaped sleeve (61), the outer surface of the arc-shaped sleeve (61) is fixedly connected with the outer surface of the anti-collision machine body (1), the inner portion of the arc-shaped sleeve (61) is connected with a jacking device (62) in a sliding mode, the outer surface of the anti-collision machine body (1) is fixedly connected with an elastic strip (63) close to the arc-shaped sleeve (61), and the top end of the elastic strip (63) is fixedly connected with the top end of the jacking device (62).
9. The anti-collision satellite radar for severe environments according to claim 8, wherein: roof pressure device (62) include arc roof pressure pole (621), the center department of arc sleeve (61) is passed from to the bottom of arc roof pressure pole (621), sliding connection between the surface of arc roof pressure pole (621) and the internal surface of arc sleeve (61), the top fixedly connected with kickball (622) of arc roof pressure pole (621), the top of elasticity strip (63) is connected with the surface fixed connection of kickball (622), the bottom fixedly connected with briquetting (623) of arc roof pressure pole (621), the bottom fixedly connected with flexible sucking disc (624) of briquetting (623).
10. A collision avoidance satellite radar for use in harsh environments according to claim 9, wherein: the circle center of the arc-shaped top pressure rod (621) is superposed with the circle center of the arc-shaped sleeve (61), and the flexible suckers (624) are uniformly distributed at the bottom of the pressing block (623).
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| CN116551303A (en) * | 2023-07-12 | 2023-08-08 | 湖南电气职业技术学院 | Wind driven generator support overturning welding processing equipment |
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| CN107539453A (en) * | 2017-09-04 | 2018-01-05 | 陶文英 | A kind of low-latitude flying operation unmanned plane and its control system and application |
| CN108592995B (en) * | 2018-04-23 | 2020-09-29 | 黄河科技学院 | Chemical industry park environmental monitoring device protector based on loRa wide area network |
| CN209590266U (en) * | 2018-12-19 | 2019-11-05 | 江苏慧丰信息科技有限公司 | A kind of mounting bracket for Anticollision Radar |
| CN110736967B (en) * | 2019-11-05 | 2020-10-30 | 新乡岳衡电子信息技术有限公司 | Radio radar device capable of adapting to severe weather |
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