CN115833921B - S-band ground satellite data receiving equipment - Google Patents
S-band ground satellite data receiving equipment Download PDFInfo
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- CN115833921B CN115833921B CN202310116915.8A CN202310116915A CN115833921B CN 115833921 B CN115833921 B CN 115833921B CN 202310116915 A CN202310116915 A CN 202310116915A CN 115833921 B CN115833921 B CN 115833921B
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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
- Y02D—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN INFORMATION AND COMMUNICATION TECHNOLOGIES [ICT], I.E. INFORMATION AND COMMUNICATION TECHNOLOGIES AIMING AT THE REDUCTION OF THEIR OWN ENERGY USE
- Y02D30/00—Reducing energy consumption in communication networks
- Y02D30/70—Reducing energy consumption in communication networks in wireless communication networks
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Abstract
The invention discloses a data receiving device of S-band ground satellite, comprising: the supporting platform is internally provided with a rotatable self-rotating frame; the bottom end of the rotary table is erected on the self-rotating frame, and the top end of the rotary table is positioned outside the support table and used for supporting the satellite receiving equipment; the erection mechanism is positioned on the external bottom surface of the support table and comprises an outer support column and an inner support column which can be erected in a switching way; the erection of different installation base planes of the satellite receiving equipment is completed through the height switching of the outer supporting column and the inner supporting column; in application, the revolving platform is arranged on the self-rotating frame, the satellite receiving equipment rotates in the horizontal direction through the self-rotating frame, and the satellite receiving equipment is turned over on a vertical plane through the revolving platform, so that the angle of the satellite receiving equipment for receiving the signal data is adjusted, the satellite receiving equipment is applied without dead angles, and the practicability is high.
Description
Technical Field
The invention relates to the technical field of signal transmission, in particular to S-band ground satellite data receiving equipment.
Background
The satellite is applied to various regions, the environment in some regions can corrode satellite equipment and damage the equipment, the satellite equipment is easy to damage after long-term working in the environment with severe conditions, and the maintenance is complex and difficult.
In chinese utility model patent application no: CN201922186904.9 discloses a communication device with a protection device, which comprises a base, wherein three groups of support rods are arranged on the base, the upper ends of the three groups of support rods are fixedly connected with the outer wall of a satellite signal receiver, a weighting barrel is arranged in a gap surrounded by the three groups of support rods, a box body is fixed at the upper end of the satellite signal receiver, a positioning mechanism is arranged in the inner cavity of the box body, a lightning rod is fixed on the positioning mechanism, a U-shaped plate is fixed on the outer wall of the satellite signal receiver, and one end, close to the box body, of the U-shaped plate is fixedly connected with the box body; this take protector's communication equipment comes unable adjustment base through adding the weight gain piece, makes equipment be difficult for empting, installs the lightning rod and avoids receiving the thunder and lightning injury.
Still have following defect in the above-mentioned patent, satellite receiving equipment is in the installation, can not carry out effective installation based on different installation base planes, and in the use, also be convenient for make the portable direction of adjusting signal reception of equipment, in the rate of endurance, can not accomplish satellite receiving equipment rigid connection and flexible connection and combine together.
Disclosure of Invention
The invention aims to provide S-band ground satellite data receiving equipment, which realizes the switching between an outer support column and an inner support column through an erection mechanism and flexibly adjusts the installation height of the satellite receiving equipment, so that the S-band ground satellite data receiving equipment has strong installation applicability and can be installed based on different installation environments.
The purpose of the invention can be realized by the following technical scheme:
an S-band terrestrial satellite data receiving apparatus comprising:
the supporting platform is internally provided with a rotatable self-rotating frame;
the bottom end of the rotating table is erected on the self-rotating frame, and the top end of the rotating table is positioned outside the support table and used for supporting satellite receiving equipment;
the erection mechanism is positioned on the external bottom surface of the support table and comprises an outer support column and an inner support column which can be erected in a switching way;
and the erection of different installation base planes of the satellite receiving equipment is completed by switching the heights of the outer supporting columns and the inner supporting columns.
As a further scheme of the invention: the outer support column is of a cavity structure without a cover at the bottom, and the inner support column is connected inside the cavity of the outer support column in a sliding manner;
rectangular notch has been seted up to the inboard of outer support column, and the upper end of interior support column is provided with the linking arm, the linking arm slides in the rectangular notch of outer support column, and the other end of linking arm is connected on the locking dish.
As a further scheme of the invention: the connecting arms are four and are arranged on the locking disc in a crossed structure.
As a further scheme of the invention: two beams are fixedly arranged in a cavity formed by the four outer support columns, a second screw rod is arranged between the two beams, and the locking disc is in threaded connection with the second screw rod;
the upper end of the second screw rod is fixedly provided with a first bevel gear, two sides of the bottom surface of the supporting table are provided with side plates, a third screw rod is arranged between the two side plates, and the third screw rod is provided with a second bevel gear which is meshed with the first bevel gear.
As a further scheme of the invention: and knobs are arranged at two ends of the third screw rod.
As a further scheme of the invention: the rotation frame comprises an annular supporting disk arranged inside the supporting platform, a connecting sleeve is further arranged on the disk surface of the annular supporting disk, a supporting round platform is rotatably connected to the connecting sleeve, and a rotating platform is fixedly arranged on the top surface of the outside of the supporting round platform.
As a further scheme of the invention: a connecting column is arranged on the bottom surface of the inner part of the supporting circular truncated cone and is inserted into the cavity of the connecting sleeve;
the inner wall of the connecting sleeve is provided with an annular groove, an annular block matched with the annular groove is arranged on the connecting column, and the connecting column is rotatably connected in the annular groove of the connecting sleeve through the annular block.
As a further scheme of the invention: the rotary table comprises a support column, a guide cylinder and an upper bearing plate;
the support column and the guide cylinder are used for supporting the upper bearing plate, and the upper bearing plate is used for mounting the satellite receiving equipment.
As a further scheme of the invention: the supporting column is fixedly arranged on one side of the top surface of the supporting circular truncated cone, a fixed connecting block is fixedly arranged on the bottom surface of the upper bearing plate and on the same side of the supporting column, and the upper end of the supporting column is hinged to the fixed connecting block;
the fixed promotion portion that is provided with of top surface opposite side of support round platform, promotion portion are including setting up the first screw rod at support round platform top surface opposite side, and the bottom of first screw rod is connected with first bevel gear, and the upper end threaded connection of first screw rod has a guide cylinder, and the same one side that just lies in promotion portion slides and is provided with sliding connection piece on the bottom surface of accepting the board at last, and sliding connection piece can slide on accepting the board at last, and the upper end and the sliding connection piece of guide cylinder are articulated.
As a further scheme of the invention: the flexible buffer device is characterized by further comprising a bearing table, wherein the bearing table comprises two flexible bearing structures, and the two flexible bearing structures are arranged inside the supporting table and used for flexibly buffering the satellite receiving equipment.
The invention has the beneficial effects that: in the installation of the S-band ground satellite data receiving equipment, the switching between the outer supporting column and the inner supporting column is realized through the erection mechanism, and the installation height of the satellite receiving equipment is flexibly adjusted, so that the S-band ground satellite data receiving equipment has strong installation applicability and can be installed based on different installation environments;
in the aspect of the utilization rate, the two bearing mechanisms are arranged on the bearing platform, and the flexible buffering of the two bearing mechanisms enables the S-waveband ground satellite data receiving equipment to adopt a mode of combining rigid fixation and soft buffering, so that the anti-vibration effect of the satellite receiving equipment is more remarkable, and the utilization rate and the use operation resistance of the satellite receiving equipment are effectively improved;
in application, the rotary table is arranged on the self-rotating frame, the satellite receiving equipment rotates in the horizontal direction through the self-rotating frame, and the satellite receiving equipment is turned over on a vertical plane through the rotary table, so that the satellite receiving equipment can be adjusted in the angle of received signal data, the satellite receiving equipment is applied in a dead angle-free mode, and the practicability is high.
Drawings
The invention is further described below with reference to the accompanying drawings.
FIG. 1 is a front view of the present invention;
FIG. 2 is a schematic view of the structure of the turntable of the present invention;
FIG. 3 is a schematic view of the receiving platform of the present invention;
FIG. 4 is a schematic structural view of the headframe of the present invention;
FIG. 5 is a schematic structural view of the base plate of the present invention;
fig. 6 is a schematic structural view of the connection of the locking disk and the connecting arm of the present invention.
In the figure:
a support table; 101. the convex support inner ring;
an erecting mechanism; 201. an outer support column; 202. a cross beam; 203. a second screw; 204. a locking disc; 205. a connecting arm; 206. a third screw; 207. a knob; 208. an inner support column;
a receiving table; 301. a base plate; 302. a derrick; 303. a horizontal bar; 304. a supporting block; 305. a first receiving mechanism; 3051. a moving block; 3052. a first connecting plate; 3053. a second connecting plate; 3054. a strip-shaped groove; 3055. a chute; 3056. a sleeve; 3057. a spring; 3058. a columnar block; 306. a second receiving mechanism;
a swivel table; 401. a satellite receiving device; 402. an upper bearing plate; 403. a support pillar; 404. fixing a connecting block; 405. a guide cylinder; 406. a sliding connection block; 407. a first screw;
a self-rotating frame; 501. an annular support disc; 502. a supporting circular table; 503. connecting sleeves; 504. connecting columns.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments; all other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-6, the present invention is an S-band ground satellite data receiving device, including a supporting platform 1 for mounting a satellite receiving device 401, where the supporting platform 1 is a convex cavity structure, the bottom of the supporting platform 1 is provided with an erecting mechanism 2, and the supporting platform 1 is mounted on the ground through the erecting mechanism 2;
in order to solve the problems of rotation and angle adjustment of the satellite receiving device 401, in the embodiment, based on the problem of rotation of the satellite receiving device 401, a rotation frame 5 for rotating the satellite receiving device 401 is arranged in a cavity of the support table 1;
specifically, the rotation frame 5 is fixedly arranged on an annular supporting disk 501 in the cavity of the supporting platform 1, a supporting circular truncated cone 502 is rotatably connected to the disk surface of the annular supporting disk 501, wherein the supporting circular truncated cone 502 is of a cylindrical cavity structure with an uncovered bottom surface, an annular groove of a T-shaped structure is formed in the disk surface of the annular supporting disk 501, a T-shaped block which is matched with the annular groove of the T-shaped structure and is of an annular structure is arranged on the bottom surface of the supporting circular truncated cone 502, and the supporting circular truncated cone 502 is rotatably connected to the annular groove of the supporting circular truncated cone 502 through the T-shaped block on the bottom surface;
a connecting column 504 is arranged on the top surface of the inside of the supporting circular truncated cone 502, a connecting sleeve 503 is also arranged on the disc surface of the annular supporting disc 501, the connecting sleeve 503 is a hollow cylindrical structure with two uncovered ends, the connecting sleeve 503 is arranged inside the supporting circular truncated cone 502, and the connecting column 504 on the bottom surface of the inside of the supporting circular truncated cone 502 is inserted into the hollow of the connecting sleeve 503;
wherein, the inner wall of the connecting sleeve 503 is provided with an annular groove, the connecting column 504 is provided with an annular block matched with the annular groove, and the connecting column 504 is rotatably connected in the annular groove of the connecting sleeve 503 through the annular block;
further, a first motor is arranged on the disc surface of the annular supporting disc 501, the output end of the first motor is fixedly connected with the bottom surface of the connecting column 504, and the satellite receiving equipment 401 is erected on the top surface of the outer part of the supporting circular table 502;
when the satellite receiving device is used, the first motor is driven to drive the connecting column 504 to rotate through the rotation of the first motor, the connecting column 504 rotates in the annular groove of the connecting sleeve 503 through the annular block, the connecting column 504 drives the supporting circular truncated cone 502 to rotate, and the supporting circular truncated cone 502 rotates on the annular supporting plate 501, so that the whole self-rotating frame 5 drives the satellite receiving device 401 to rotate in a circling manner;
the convex supporting inner ring 101 is arranged at the upper end of the convex structure of the supporting table 1, and the outer circumferential surface of the supporting circular table 502 abuts against the circumferential surface of the convex supporting inner ring 101, so that the supporting circular table 502 is assumed to be more compact on the supporting table 1, and the satellite receiving device 401 is prevented from sliding in the rotating process, and meanwhile, the outer circumferential surface of the supporting circular table 502 abuts against the circumferential surface of the convex supporting inner ring 101, so that external dust or foreign matters can be prevented from entering the supporting table 1, and the self-rotation of the self-rotation frame 5 is prevented from being failed or abnormal.
In a specific embodiment, in order to solve the problem that the receiving angle of the satellite receiving device 401 at a fixed receiving position is not easy to adjust, in this implementation, a rotating table 4 is additionally arranged between the satellite receiving device 401 and a rotating frame 5, and the adjustment of the receiving angle of the satellite receiving device 401 is realized through the driving action of the rotating table 4;
specifically, the method comprises the following steps: the turntable 4 is arranged on a supporting circular table 502 of the self-rotating frame 5, the turntable 4 comprises a supporting column 403, a guiding cylinder 405 and an upper bearing plate 402, the supporting column 403 and the guiding cylinder 405 are used for supporting the upper bearing plate 402, and the upper bearing plate 402 is used for installing the satellite receiving equipment 401;
the supporting column 403 is fixedly arranged on one side of the top surface of the supporting circular truncated cone 502, a fixed connecting block 404 is fixedly arranged on the bottom surface of the upper bearing plate 402 and on the same side of the supporting column 403, and the upper end of the supporting column 403 is hinged to the fixed connecting block 404;
a pushing part is fixedly arranged on the other side of the top surface of the supporting circular truncated cone 502, the pushing part comprises a first screw rod 407 arranged on the other side of the top surface of the supporting circular truncated cone 502, a first bevel gear is connected to the bottom end of the first screw rod 407, a guide cylinder 405 is in threaded connection with the upper end of the first screw rod 407, a sliding connection block 406 is arranged on the bottom surface of the upper bearing plate 402 in a sliding manner and positioned on the same side of the pushing part, the sliding connection block 406 can slide on the upper bearing plate 402, and the upper end of the guide cylinder 405 is hinged to the sliding connection block 406;
further, a second motor is arranged on the top surface of the supporting circular truncated cone 502, and the output end of the second motor is connected with a second bevel gear which is in meshed connection with the first bevel gear;
when the device is used, the second bevel gear is driven to rotate by the second motor and is in meshing transmission with the first bevel gear, so that the first screw 407 is driven to rotate, the guide cylinder 405 is driven by the first screw 407 to move in the vertical direction, and the guide cylinder 405 is pushed upwards or pulled downwards to enable the upper bearing plate 402 to rotate around the supporting column 403.
In a specific embodiment, since the satellite receiving device 401 is usually installed outdoors, and most of the installation structures of the satellite receiving device 401 are rigidly connected, the satellite receiving device 401 is easily damaged and cannot be used in case of an earthquake or other vibratory disaster;
in order to solve the technical barrier, the present embodiment adds a receiving table 3 inside a support table 1, and mounts a swivel table 4 on the receiving table 3;
specifically, the method comprises the following steps: a bottom plate 301 of the receiving table 3 is fixedly arranged on the inner bottom surface of the support table 1, a well frame 302 of the receiving table 3 is positioned above the bottom plate 301 and horizontally arranged inside the support table 1, two ends of a horizontal rod 303 at two longitudinal sides of the well frame 302 are respectively and fixedly provided with a supporting block 304, and the top ends of the four supporting blocks 304 are respectively and fixedly connected with four corners of the bottom surface of the annular supporting disc 501;
a first bearing mechanism 305 and a second bearing mechanism 306 are arranged between the bottom plate 301 and the annular supporting plate 501, and the structures of the first bearing mechanism 305 and the second bearing mechanism 306 are completely consistent and are symmetrical about a central line in the vertical direction of the bottom plate 301;
specifically, the first bearing mechanism 305 comprises a moving block 3051, a first connecting plate 3052, a second connecting plate 3053, a strip-shaped groove 3054, a sliding groove 3055, a sleeve 3056, a spring 3057 and a columnar block 3058, the two ends of the horizontal rod 303 on the two longitudinal sides of the # -shaped frame 302 are both connected with the moving block 3051 in a sliding manner, the end faces of the two ends of the moving block 3051 are hinged with the first connecting plate 3052 and the second connecting plate 3053, the other ends of the first connecting plate 3052 and the second connecting plate 3053 are respectively hinged with a sliding block, and the sliding block at the end part of the first connecting plate 3052 and the sliding block at the end part of the second connecting plate 3053 are respectively connected in the hollow moving groove of the bottom plate 301 in a sliding manner;
a strip-shaped groove 3054 is formed in the middle of the first connecting plate 3052 and the second connecting plate 3053, a sliding rod is arranged in each of the strip-shaped grooves 3054 of the first connecting plate 3052 and the second connecting plate 3053 in a sliding mode and is fixedly arranged on one side of the top end of the columnar block 3058, the bottom end of the columnar block 3058 is connected to the inside of the sleeve 3056 in a sliding mode, a spring 3057 is vertically arranged inside the sleeve 3056, and the sleeve 3056 is vertically arranged on the bottom face of the bottom plate 301;
during the use, when satellite receiving equipment 401 shakes when using, annular supporting disk 501 accepts the ascending pressure in vertical direction and conveys to derrick 302 when satellite receiving equipment 401 shakes, make the movable block 3051 atress downstream of four edges of derrick 302, make movable block 3051 drive connecting plate 3052 and connecting plate two 3053 downstream on vertical direction, make connecting plate 3052 and connecting plate two 3053 drive the slider and move to both sides in spout 3055, and make spring 3057 in the sleeve 3056 play the supporting role to column piece 3058, thereby the realization is to the ascending buffering of annular supporting disk 501 in vertical direction, reduce the fault probability that satellite receiving equipment 401 shakes and cause.
That is, in this embodiment, the pure rigid connection of the conventional satellite receiving device 401 is adjusted to a parallel mode of rigid connection and flexible connection, so that the loss of the satellite receiving device 401 caused by rigid vibration is reduced, and the utilization rate of the satellite receiving device 401 is improved.
In a specific embodiment, since the satellite receiving device 401 is usually installed outdoors, the satellite receiving device 401 is very laborious in the actual following process due to the uncontrollable factors of the outdoor installation base surface;
in order to solve the problem of installation limitation of the satellite receiving equipment 401 in the prior art, in the implementation, the bottom surface of the support table 1 is provided with the erection mechanism 2, and the installation position of the erection mechanism 2 and a satellite installation base surface is adjustable, so that the satellite receiving equipment has high operability;
specifically, the erection mechanism 2 comprises outer support columns 201 fixedly arranged at four corners of the bottom surface of the support table 1, wherein the outer support columns 201 are of cavity structures with uncovered bottoms, inner support columns 208 are arranged in cavities of the outer support columns 201 in a sliding mode, guide wheels are arranged at the bottom ends of the inner support columns 208, and the satellite receiving equipment 401 can move conveniently in the installation process through the arrangement of the guide wheels;
rectangular notches are formed in the inner sides of the four outer supporting columns 201, connecting arms 205 are connected to the upper ends of the inner supporting columns 208, the connecting arms 205 slide in the rectangular notches of the outer supporting columns 201, and the other ends of the connecting arms 205 are connected to the locking disc 204;
the four connecting arms 205 are arranged on the locking disc 204 in a cross structure, two cross beams 202 are fixedly arranged inside a cavity formed by the four outer supporting columns 201, a second screw 203 is arranged between the two cross beams 202, and the locking disc 204 is in threaded connection with the second screw 203;
a first bevel gear is fixedly arranged at the upper end of the second screw 203, side plates are arranged on two sides of the bottom surface of the support table 1, a third screw 206 is arranged between the two side plates, a second bevel gear is arranged on the third screw 206, and the second bevel gear is meshed with the first bevel gear;
wherein, two ends of the third screw rod 206 are provided with knobs 207;
during the use, the third screw rod 206 is driven to rotate by rotating the knob 207, the third screw rod 206 drives the bevel gear II to be meshed with the bevel gear I for transmission, so that the second screw rod 203 is driven to rotate, the second screw rod 203 drives the locking disc 204 to move in the vertical direction, the locking disc 204 drives the connecting arm 205 to drive the inner supporting column 208 to move on the outer supporting column 201, the extending length of the inner supporting column 208 on the outer supporting column 201 is adjusted, the installation height of the satellite receiving equipment 401 is adjusted, the satellite receiving equipment 401 can be installed on installation reference surfaces with different heights, and the erection is flexible.
While one embodiment of the present invention has been described in detail, the description is only a preferred embodiment of the present invention and should not be taken as limiting the scope of the invention; all equivalent changes and modifications made within the scope of the present invention shall fall within the scope of the present invention.
Claims (5)
1. An S-band terrestrial satellite data receiving apparatus, comprising:
the device comprises a supporting table (1), wherein a rotatable self-rotating frame (5) is arranged in the supporting table (1);
the bottom end of the rotating table (4) is erected on the self-rotating frame (5), and the top end of the rotating table (4) is located outside the support table (1) and used for supporting the satellite receiving equipment (401);
the erection mechanism (2), the erection mechanism (2) is positioned on the external bottom surface of the support platform (1), and the erection mechanism (2) comprises an outer support column (201) and an inner support column (208) which can be erected in a switching way;
the erection of different installation base planes of the satellite receiving equipment (401) is completed through the height switching of the outer supporting column (201) and the inner supporting column (208);
the outer supporting column (201) is of a cavity structure without a cover at the bottom, and the inner supporting column (208) is connected inside the cavity of the outer supporting column (201) in a sliding manner;
the inner side of the outer supporting column (201) is provided with a rectangular notch, the upper end of the inner supporting column (208) is provided with a connecting arm (205), the connecting arm (205) slides in the rectangular notch of the outer supporting column (201), and the other end of the connecting arm (205) is connected to the locking disc (204);
four connecting arms (205) are arranged, and the four connecting arms (205) are arranged on the locking disc (204) in a cross structure;
two beams (202) are fixedly arranged in a cavity formed by the four outer supporting columns (201), a second screw (203) is arranged between the two beams (202), and the locking disc (204) is in threaded connection with the second screw (203);
a first bevel gear is fixedly arranged at the upper end of the second screw rod (203), side plates are arranged on two sides of the bottom surface of the support table (1), a third screw rod (206) is arranged between the two side plates, a second bevel gear is arranged on the third screw rod (206), and the second bevel gear is meshed with the first bevel gear;
the automatic rotating frame (5) comprises an annular supporting disk (501) arranged inside the supporting platform (1), a connecting sleeve (503) is further arranged on the disk surface of the annular supporting disk (501), a supporting circular table (502) is rotatably connected onto the connecting sleeve (503), and a rotating table (4) is fixedly arranged on the outer top surface of the supporting circular table (502);
a connecting column (504) is arranged on the bottom surface of the inner part of the supporting circular truncated cone (502), and the connecting column (504) is inserted into the cavity of the connecting sleeve (503);
an annular groove is formed in the inner wall of the connecting sleeve (503), an annular block matched with the annular groove is arranged on the connecting column (504), and the connecting column (504) is rotatably connected into the annular groove of the connecting sleeve (503) through the annular block.
2. An S-band terrestrial satellite data receiving apparatus according to claim 1, wherein both ends of the third screw (206) are provided with knobs (207).
3. An S-band ground satellite data reception apparatus according to claim 1, wherein said carousel (4) comprises a support column (403), a guide cylinder (405) and an upper bearing plate (402);
the supporting column (403) and the guide cylinder (405) are used for supporting the upper bearing plate (402), and the upper bearing plate (402) is used for installing the satellite receiving equipment (401).
4. An S-band ground satellite data receiving device as claimed in claim 3, wherein the supporting column (403) is fixedly arranged at one side of the top surface of the supporting circular table (502), a fixed connecting block (404) is fixedly arranged at the same side of the supporting column (403) on the bottom surface of the upper bearing plate (402), and the upper end of the supporting column (403) is hinged on the fixed connecting block (404);
the fixed promotion portion that is provided with of top surface opposite side of support round platform (502), promotion portion is including setting up first screw rod (407) at support round platform (502) top surface opposite side, the bottom of first screw rod (407) is connected with first bevel gear, the upper end threaded connection of first screw rod (407) has guide cylinder (405), on the bottom surface of last bearing plate (402) and lie in the promotion portion with one side slip be provided with sliding connection piece (406), sliding connection piece (406) can slide on last bearing plate (402), the upper end and the sliding connection piece (406) of guide cylinder (405) are articulated.
5. An S-band terrestrial satellite data receiving device according to claim 1, further comprising a receiving station (3), wherein the receiving station (3) comprises two flexible receiving structures, and the two flexible receiving structures are arranged inside the support table (1) and are used for flexibly buffering the satellite receiving device (401).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310116915.8A CN115833921B (en) | 2023-02-15 | 2023-02-15 | S-band ground satellite data receiving equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310116915.8A CN115833921B (en) | 2023-02-15 | 2023-02-15 | S-band ground satellite data receiving equipment |
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| Publication Number | Publication Date |
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| CN115833921A CN115833921A (en) | 2023-03-21 |
| CN115833921B true CN115833921B (en) | 2023-04-18 |
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| CN202310116915.8A Active CN115833921B (en) | 2023-02-15 | 2023-02-15 | S-band ground satellite data receiving equipment |
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| CN115833921A (en) | 2023-03-21 |
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