CN113482429A - Horizontal adjusting method and motor adjusting method for multi-section satellite antenna supporting tower - Google Patents
Horizontal adjusting method and motor adjusting method for multi-section satellite antenna supporting tower Download PDFInfo
- Publication number
- CN113482429A CN113482429A CN202110810696.4A CN202110810696A CN113482429A CN 113482429 A CN113482429 A CN 113482429A CN 202110810696 A CN202110810696 A CN 202110810696A CN 113482429 A CN113482429 A CN 113482429A
- Authority
- CN
- China
- Prior art keywords
- tower
- leveling
- section
- tower section
- protrusion
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000000034 method Methods 0.000 title claims abstract description 41
- 230000007704 transition Effects 0.000 claims abstract description 37
- 238000013461 design Methods 0.000 claims description 12
- 238000013459 approach Methods 0.000 claims description 11
- 230000008569 process Effects 0.000 claims description 10
- 238000003780 insertion Methods 0.000 claims description 4
- 230000037431 insertion Effects 0.000 claims description 4
- 238000009434 installation Methods 0.000 abstract description 29
- 230000003044 adaptive effect Effects 0.000 abstract description 2
- 239000011295 pitch Substances 0.000 description 12
- 230000002829 reductive effect Effects 0.000 description 6
- 230000005484 gravity Effects 0.000 description 5
- 229910000838 Al alloy Inorganic materials 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 230000006872 improvement Effects 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 230000036961 partial effect Effects 0.000 description 3
- 239000013589 supplement Substances 0.000 description 3
- 239000010963 304 stainless steel Substances 0.000 description 2
- 239000004677 Nylon Substances 0.000 description 2
- 229910000589 SAE 304 stainless steel Inorganic materials 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 238000005452 bending Methods 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 238000011900 installation process Methods 0.000 description 2
- 229920001778 nylon Polymers 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 238000003860 storage Methods 0.000 description 2
- 230000001174 ascending effect Effects 0.000 description 1
- 238000010923 batch production Methods 0.000 description 1
- 239000004568 cement Substances 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 230000000670 limiting effect Effects 0.000 description 1
- 230000009711 regulatory function Effects 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000003351 stiffener Substances 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H12/00—Towers; Masts or poles; Chimney stacks; Water-towers; Methods of erecting such structures
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
- E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
- E04B1/343—Structures characterised by movable, separable, or collapsible parts, e.g. for transport
- E04B1/34315—Structures characterised by movable, separable, or collapsible parts, e.g. for transport characterised by separable parts
- E04B1/34331—Structures characterised by movable, separable, or collapsible parts, e.g. for transport characterised by separable parts mainly constituted by three-dimensional elements
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H12/00—Towers; Masts or poles; Chimney stacks; Water-towers; Methods of erecting such structures
- E04H12/02—Structures made of specified materials
- E04H12/08—Structures made of specified materials of metal
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H12/00—Towers; Masts or poles; Chimney stacks; Water-towers; Methods of erecting such structures
- E04H12/02—Structures made of specified materials
- E04H12/08—Structures made of specified materials of metal
- E04H12/10—Truss-like structures
Landscapes
- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Wood Science & Technology (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Support Of Aerials (AREA)
Abstract
The invention relates to a horizontal adjusting method of a multi-section satellite antenna supporting tower, which at least comprises the following steps: under the condition that the first tower section (100) and the third tower section (300) are connected at two opposite ends of the second tower section (200) in a mode of forming an inclination angle (alpha) through a connecting part, at least one leveling compensation gasket (500) which is adaptive to a gap between the first tower section (100) and the second tower section (200) and can lock the connecting part is embedded between the first tower section and the second tower section, wherein the leveling compensation gasket (500) comprises an inner side surface (500c) and an outer side surface (500d), and the outer side surface (500d) is connected to the inner side surface (500c) through a transition surface (500f), a raised surface (500e) and a release opening (500g) in sequence; the inner side surface (500c) is connected to another warp protrusion (500h) opposite to the warp protrusion (500e) in a smoothly curved manner. The horizontal adjusting method of the invention is convenient for azimuth zeroing and large disc horizontal adjustment, simplifies the installation steps and has flexible adjustment.
Description
The invention relates to a satellite antenna support tower based on a self-locking structural member, which has the application number of 201911362330.4 and the application date of 2019, 12 months and 25 days, and the application type is divisional application of the invention.
Technical Field
The invention relates to the technical field of satellite technical equipment, in particular to a horizontal adjusting method and a motor adjusting method of a satellite antenna supporting tower.
Background
Antenna towers are commonly used ground station equipment for mounting antennas for signal exchange with satellites. For example, chinese patent publication No. CN201845861U discloses a wireless communication transceiver antenna tower, wherein a tower body includes a base, a lower support rod, an adjustable support rod and an upper support rod, wherein the lower support rod is connected to the base, the lower support rod is provided with a radial fixing through hole, the adjustable support rod is provided with a radial adjusting through hole, the adjustable support rod is inserted into the lower support rod and is fixed by inserting a bolt into the fixing through hole and the adjusting through hole, the total number of the fixing through hole and the adjusting through hole is at least three, and the upper support rod is connected to the adjustable support rod. But the utility model discloses a height-adjusting as required can be suitable for service environment in a flexible way. But this utility model does not have angle and levelness regulatory function, therefore can't be applicable to complicated mountain area etc. ground, can't guarantee the position and the directional precision of every single move of antenna.
The ground station of very high frequency/very high frequency small satellite mostly adopts yagi antenna to transmit and receive wireless signal, the antenna is driven by the azimuth and pitching rotating turntable to aim at the satellite target, and the rotating turntable is installed on the antenna tower. The antenna tower generally belongs to a long and narrow supporting tower and has the characteristics of heavy weight, large axial occupied space and the like. Therefore, when the satellite ground station is disposed in a remote mountain area, the antenna tower needs to be separated into a plurality of tower sections to reduce the transportation space, but when the antenna is installed, the installation error of each section needs to be reduced as much as possible to reduce the installation error when the antenna is installed on the tower, and the azimuth and pitching orientation accuracy of the antenna is ensured. Therefore, how to provide an antenna tower capable of supporting a yagi antenna is one of the technical problems to be solved by the present invention. The prior art does not disclose the self-locking structure of the leveling compensation gasket of the present invention.
Furthermore, on the one hand, due to the differences in understanding to the person skilled in the art; on the other hand, since the inventor has studied a lot of documents and patents when making the present invention, but the space is not limited to the details and contents listed in the above, however, the present invention is by no means free of the features of the prior art, but the present invention has been provided with all the features of the prior art, and the applicant reserves the right to increase the related prior art in the background.
Disclosure of Invention
Aiming at the defects of the prior art, the invention provides a satellite antenna supporting tower based on a self-locking structural part, which comprises at least three tower sections with approximately same inclination angles, wherein the tower sections can be sequentially connected through connecting parts in the axial direction, and the tower sections comprise: a first tower section comprising at least two differently sized mounting trays for mounting pitch and/or azimuth motors connected via at least three sway braces at different elevation positions, the at least two differently sized mounting trays being connectable by the at least three sway braces in a manner to form the angle of inclination; a second tower segment having opposite ends connecting the first tower segment and the third tower segment by the connecting member so as to form the tilt angle, and to which a fixing plate for mounting an azimuth motor is detachably connected so as to lower the center of gravity of the antenna tower; a third tower section for connection with an external base body for securing the support tower; at least one leveling compensation gasket which is matched with a gap between the first tower section and the second tower section and can lock the connecting part is embedded between the first tower section and the second tower section, wherein the leveling compensation gasket comprises an inner side face and an outer side face, and the outer side face is connected to the inner side face through a transition face, a tilting projection and a release port in sequence; the transition surface is connected with an embedding edge part of the tilted protrusion in a mode that the thickness of the transition surface is gradually increased to be higher than a first leveling plane in the direction extending from the outer side surface to the inner side surface, the embedding edge part is connected with a transition edge part which is gradually far away from a geometric center line of the leveling compensation gasket through a locking edge part which is gradually close to the geometric center line, the thickness of the transition edge part is gradually reduced to be approximately flush with the first leveling surface, the transition edge part is connected to the inner side surface through the release opening, and the inner side surface is connected to another tilted protrusion opposite to the tilted protrusion in a smoothly bending mode; the tilted protrusion and the another tilted protrusion are used for locking the connecting part at different positions in such a way that the tilt angle can approach a design value when the first tower section and the second tower section are connected by the connecting part.
According to a preferred embodiment, the release opening comprises a first opening edge extending from the inner side surface to the outer side surface, a second opening edge connected with the first opening edge and extending approximately in the length direction of the leveling compensation gasket, and a third opening edge connected with the second opening edge and extending from the outer side surface to the inner side surface, wherein the extension length of the second opening edge is set in a manner that the locking edge portion and another locking edge portion of another warping protrusion are in contact with the connecting part, so that the release opening can be elastically deformed, and the connecting part at different positions can be locked by the leveling compensation gasket through the elastic pre-tightening force of the release opening.
According to a preferred embodiment, the third leveling surfaces connected to the embedding edge portion and the locking edge portion are parallel to the first leveling surfaces in such a way that the inclination angle can approach the design value; the third leveling surface is connected with the outer side surface through an undulation transition surface with gradually increased thickness in the direction extending from the outer side surface to the inner side surface.
According to a preferred embodiment, the distance between the locking edge portion and the other locking edge portion of the other tilted projection is adapted to the inner diameter of the leveling shim, so that the leveling shim can be designed as a standard part according to the spatial position of the connecting part connecting the first tower section and the second tower section, thereby facilitating installation.
According to a preferred embodiment, a first end of the first tower segment is provided with a first mounting disc, and the circumferential direction of the mounting surface of the first mounting disc facing away from the support tower is provided with at least three first slot holes distributed at intervals and radially oriented along the radial direction of the first slot holes, so that the first mounting disc can be used for adaptively mounting azimuth motors and/or pitching motors with different specifications.
According to a preferred embodiment, a second mounting plate is arranged at a second end, used for connecting the second tower section, of the first tower section, and a plurality of second slotted holes which are distributed at intervals along the circumferential direction and are radially arranged along the circumferential direction are formed in the end face, facing the first mounting plate, of the second mounting plate in the circumferential direction, so that when the azimuth motor and/or the pitch motor are mounted on the first mounting plate, the azimuth motor and/or the pitch motor can perform direction fine adjustment based on friction fit between the second slotted holes and the second tower section.
According to a preferred embodiment, the first, second and third pylon segments are arranged in such a way that the third pylon segment can accommodate the second pylon segment and the second pylon segment can accommodate the first pylon segment, so that the support pylon can be arranged in such a way that the space occupied by the support pylon is reduced.
According to a preferred embodiment, the invention also discloses an antenna tower installation method based on the self-locking structure, which is used for the support tower.
According to a preferred embodiment, the invention also discloses a leveling shim for the above method and/or support tower.
The invention provides a satellite antenna support tower based on a self-locking structural part, which at least has the following advantages:
(1) the antenna tower is arranged into a multi-section type sleeve connection structure, so that the antenna tower is convenient to install and transport, and the cost is saved.
(2) By arranging the leveling compensation gasket structure, the azimuth zero adjustment and the horizontal adjustment of the large plate can be facilitated.
(3) Through setting up first slotted hole, can be applicable to the circulator installation of different fixed hole sites.
(4) Through set up position motor fixed plate in tower section middle part, can realize providing position and two kinds of mounting means of every single move circulator, adapt to the not installation needs of co-altitude.
The invention also provides a horizontal adjusting method of the multi-section satellite antenna supporting tower, which at least comprises the following steps:
under the condition that the first tower section and the third tower section are connected at two opposite ends of the second tower section in a mode of forming an inclination angle through connecting parts, at least one leveling compensation gasket which is mutually adaptive to a gap between the first tower section and the second tower section and can lock the connecting parts is embedded between the first tower section and the second tower section, wherein the leveling compensation gasket comprises an inner side surface and an outer side surface, and the outer side surface is connected to the inner side surface through a transition surface, a warping protrusion and a release opening in sequence; the inner side surface is connected to another warp protrusion opposite to the warp protrusion in a smoothly curved manner.
Preferably, the method further comprises: the first tower section, the second tower section and the third tower section are fixedly connected together through bolts, the horizontal state of the top surface of the tower sections is observed at any time in the connection process, when the relative height of any one side of the tower sections is lower than that of other sides, the bolt on the lower side is inserted into the leveling compensation gasket, and a plurality of leveling compensation gaskets are properly added according to the error distance between actual levels, so that the position of the lower side is raised to the horizontal position; when the bolt is screwed down, the warping protrusion and the other warping protrusion of the leveling compensation gasket can be flattened, and the bolt rod is clamped to realize a self-locking process.
Preferably, the method further comprises: in a case where the first tower section and the second tower section are connected by the connection member, the tilted protrusion and the other tilted protrusion lock the connection member in such a manner that a tilt angle can approach a design value, wherein the tilt angle is a tilt angle of a diagonal brace of a support tower of the satellite antenna.
Preferably, the release opening includes a first opening edge extending from the inner side surface to the outer side surface, a second opening edge connected to the first opening edge and extending substantially in a longitudinal direction of the leveling compensating shim, and a third opening edge connected to the second opening edge and extending from the outer side surface to the inner side surface.
Preferably, the transition surface is connected with the raised embedded edge part in a manner that the thickness of the transition surface is gradually increased to be higher than the first adjusting plane in the direction extending from the outer side surface to the inner side surface; the embedding edge portion is connected with a transition edge portion which is gradually far from the geometric center line through a locking edge portion which is gradually close to the geometric center line of the leveling compensation gasket, the thickness of the transition edge portion is gradually reduced to be approximately flush with the first leveling surface, and the transition edge portion is connected with the inner side surface through a release opening.
Preferably, a third leveling surface connected to the embedding edge portion and the locking edge portion is parallel to the first leveling surface in such a manner that the inclination angle can approach a design value; the third leveling surface is connected with the outer side surface through an undulation transition surface with gradually increased thickness in the direction extending from the outer side surface to the inner side surface.
Preferably, the method further comprises: under the condition that the locking edge part and the other locking edge part of the other tilting protrusion are in contact with the connecting part, the extension length of the second opening edge is set in a mode that the release opening can be elastically deformed, so that the connecting part at different positions can be locked by the leveling compensation gasket by virtue of the elastic pretightening force of the release opening.
Preferably, the method further comprises: the distance between the locking edge portion and the other locking edge portion of the other warping protrusion is set in a manner of being matched with the inner diameter of the leveling compensation gasket, so that the leveling compensation gasket can be designed as a standard part according to the spatial position of a connecting part connecting the first tower section and the second tower section.
The invention also provides a motor adjusting method of the multi-section satellite antenna supporting tower, which comprises the following steps: the first tower section, the second tower section and the third tower section are fixedly connected together through bolts, a second mounting disc is arranged at a second end, used for connecting the second tower section, of the first tower section, and a plurality of second slotted holes which are distributed at intervals along the circumferential direction and radially run along the circumferential direction are formed in the end face, facing the first mounting disc, of the second mounting disc in the circumferential direction, so that when the azimuth motor and/or the pitch motor are mounted on the first mounting disc, the azimuth motor and/or the pitch motor can perform direction fine adjustment based on friction fit between the second slotted holes and the second tower section;
the leveling compensation gasket is embedded between the first tower section and the second tower section, is matched with a gap between the first tower section and the second tower section, and can lock the connecting part, wherein the leveling compensation gasket comprises an inner side face and an outer side face, and the outer side face is connected to the inner side face through a transition face, a tilting projection and a release port in sequence; the inner side surface is connected to the other warping protrusion opposite to the warping protrusion in a smoothly bending mode, and when the bolt is screwed down, the warping protrusion and the other warping protrusion of the leveling compensation gasket can be flattened to clamp the bolt rod so as to realize a self-locking process.
Preferably, the first mounting disc is arranged at a first end of the first tower section, and at least three first slot holes distributed at intervals in the circumferential direction on a mounting surface of the first mounting disc, which faces away from the support tower, and which radially run along the radial direction of the first mounting disc are arranged on the mounting surface of the first mounting disc, so that the first mounting disc can be used for adaptively mounting azimuth motors and/or pitching motors with different specifications.
Drawings
FIG. 1 is a schematic plan view of a support tower provided by the present invention;
FIG. 2 is a preferred three-dimensional schematic view of a support tower provided by the present invention;
FIG. 3 is a preferred three-dimensional schematic view of a first tower section of a support tower provided by the present invention;
FIG. 4 is a top view modular schematic of a first tower section of a support tower provided by the present invention;
FIG. 5 is a schematic side view of a leveling shim for a support tower according to the present invention;
FIG. 6 is a second side view of a leveling shim for a support tower according to the present invention;
FIG. 7 is a schematic perspective view of a leveling shim for a support tower according to the present invention;
FIG. 8 is a third schematic side view of a leveling shim for a support tower according to the present invention;
FIG. 9 is a schematic illustration of a support tower according to the present invention in a disassembled state during transportation; and
fig. 10 is a partially enlarged schematic view of a release opening of a leveling compensation gasket of a support tower according to the present invention.
List of reference numerals
100: first tower section 500 b: second leveling surface
200: second tower section 500 c: inner side surface
300: third tower section 500 d: outer side surface
500: leveling compensation shim 500 e: warping convex
100 a: diagonal brace 500 f: transition surface
100 b: mounting plate 500 g: release port
100 b-1: first mounting plate 500 h: another raised part
100 b-2: second mounting plate 500 e-1: embedded edge part
100b-1 a: first slot 500 e-2: locking edge portion
100b-2 a: second slot 500 e-3: transition edge portion
200 a: fixing plate 500 e-4: third leveling surface
200 a-1: tube shaft hole 500 e-5: undulated transition surface
200 a-2: fixing hole 500 g-1: first edge
300 a: and the diagonal draw reinforcing rod is 500 g-2: second lip
α: inclination angle 500 g-3: third lip
500 a: first leveling surface
Detailed Description
This is described in detail below with reference to fig. 1-10.
Example 1
The antenna tower in the prior art is mainly found to have the following defects through long-time practical application:
(1) the existing antenna tower is mostly of an integral structure and is inconvenient to install, transport and hoist;
(2) the rotator is installed in a single mode, and is generally only suitable for top installation of the rotator;
(3) a rotator that is only suitable for a certain size;
(4) the azimuth zero point adjustment and the large disc horizontal adjustment are inconvenient;
(5) the height is fixed, and the height can not be flexibly changed by matching with a standard component.
Therefore, the embodiment discloses a satellite antenna support tower based on a self-locking structural part. The support tower comprises at least three tower sections. For example, as shown in fig. 1 and 2, the support tower includes a first tower section 100, a second tower section 200, and a third tower section 300. It may also comprise a fourth tower section connected to the third tower section 300, etc., if it has higher requirements in axial height. The first, second and third pylon segments 100, 200, 300 are each connected via a connecting element. According to different connection requirements, the connecting parts can be bolts with different specifications. Each pylon segment needs to have a high degree of levelness after connection, at least three pylon segments having substantially the same angle of inclination a, as shown in fig. 1. The angle of inclination alpha has a design value alpha at design time0. And after the tower sections have been mounted in sequence, the angle of inclination a approaches the design value a0So as to ensure that the installation requirements are met after the installation of the azimuth motor and the pitching motor.
The first tower section 100 includes at least three diagonal braces 100a and at least two mounting plates 100b at different height positions and with different sizes. Preferably, there are a total of two mounting plates 100b and four diagonal braces 100 a. As shown in fig. 2, 3 and 4, four diagonal braces 100a connect the mounting plates 100b to form a tower section of a stable configuration at an angle of inclination α. The mounting plate 100b is used to mount a pitch motor and/or an azimuth motor.
Second tower section 200: the opposite ends connect the first and third tower segments 100, 300 by means of connecting members in such a way that an angle of inclination α is formed. Which can be detachably attached with a fixing plate 200a for mounting an azimuth motor in such a manner as to lower the center of gravity of the antenna tower.
Third tower section 300: used for connecting with an external base body to fix the support tower.
Preferably, at least one leveling compensation shim 500 is inserted between the first tower section 100 and the second tower section 200, which is adapted to the gap between the two and can lock the connecting member. Preferably, leveling compensation shims 500 are plugged between the connecting parts of the tower body. After each tower section is installed, the height of four corners of each tower section is adjusted by additionally installing a leveling compensation gasket, so that horizontal errors generated in the installation process of the tower body can be corrected, and the rotator of the first tower section is ensured to be always kept at the horizontal position. Preferably, the leveling compensation shim is a semi-annular thin sheet structure.
Preferably, as shown in fig. 5 to 8, the leveling compensating shim 500 is U-shaped, and both ends thereof are provided with protrusions 500e protruding from the entire cross-section thereof. Preferably, the leveling shim 500 includes an inner side 500c and an outer side 500 d. The outer side surface 500d is connected to the inner side surface 500c via a transition surface 500f, a warp protrusion 500e, and a release opening 500g in this order. The transition surface 500f is connected to the insertion edge portion 500e-1 of the protrusion 500e such that the thickness thereof gradually increases from the outer surface 500d to the inner surface 500c to be higher than the first leveling surface 500 a. The insert edge portion 500e-1 is connected to a transition edge portion 500e-3 gradually spaced from the geometric centerline and gradually decreasing in thickness to be substantially flush with the first leveling plane 500a through a locking edge portion 500e-2 gradually approaching the geometric centerline of the leveling compensating pad 500, the transition edge portion 500e-3 is connected to an inner side surface 500c through a release opening 500g, and the inner side surface 500c is connected to another tilted projection 500h opposite to the tilted projection 500e in a smoothly curved manner. After each complete installation of a part of the tower,comparing the horizontal positions of the bolts at all sides, inserting the leveling compensation gaskets 500 into the bolts at the lower side, properly adding a plurality of leveling compensation gaskets 500 according to the error distance between actual levels, lifting the positions at the lower side to the horizontal positions, and when the bolts are screwed down, flattening the warping protrusion 500e and the other warping protrusion 500h of the U-shaped gasket so as to clamp the bolt rod and realize the self-locking process. The tilted projection 500e and the further tilted projection 500h are used to enable the tilt angle α to approach the design value α when the first pylon segment 100 and the second pylon segment 200 are connected by the connecting member0The connecting member is locked.
Preferably, as shown in fig. 10, the release port 500g includes a first lip 500g-1 extending from the inner side 500c to the outer side 500d, a second lip 500g-2 connected to the first lip 500g-1 and extending substantially in the lengthwise direction of the leveling compensating pad 500, and a third lip 500g-3 connected to the second lip 500g-2 and extending from the outer side 500d to the inner side 500 c. The extension length of the second lip 500g-2 is set in such a manner that the release opening 500g can be elastically deformed in the case where both the locking edge portion 500e-2 and the other locking edge portion of the other seesaw projection 500h are in contact with the connection member. Therefore, the connecting parts at different positions can be locked by the leveling compensation gasket 500 by virtue of the elastic pretightening force of the release opening 500 g.
Preferably, the third leveling plane 500e-4 connected with the embedding edge portion 500e-1 and the locking edge portion 500e-2 is formed to enable the inclination angle α to approach the design value α0In such a way that they are parallel to the first leveling plane 500 a. The third tone surface 500e-4 is connected to the outer surface 500d by a relief transition surface 500e-5 having a gradually increasing thickness in a direction extending from the outer surface 500d to the inner surface 500 c.
Preferably, the distance between the locking edge portion 500e-2 and the other locking edge portion of the other tilting protrusion 500h is set in a manner to be adapted to the inner diameter of the leveling compensating shim 500, so that the leveling compensating shim 500 can be designed as a standard part according to the spatial position of the connecting member connecting the first tower section 100 and the second tower section 200 for easy installation.
Example 2
This embodiment may be a further improvement and/or a supplement to embodiment 1 or a combination thereof, and repeated contents are not described again. This example discloses that, without causing conflict or contradiction, the whole and/or partial contents of the preferred embodiments of other examples can be supplemented by this example.
As shown in fig. 2, the present invention provides a support tower for a satellite antenna with a self-locking structural member, which includes a tower body supported by at least three sets of diagonal braces 100a, wherein the tower body is a detachable three-section split structure, and includes a first tower section 100, a second tower section 200, and a third tower section 300. A first mounting plate 100b-1 is arranged on a first end face of the first tower section 100, and a plurality of first slotted holes 100b-1a are formed in the circumferential direction of the first mounting plate 100 b-1. The second end face of the first tower section 100 is provided with a second mounting disc 100b-2, and the second mounting disc 100b-2 is circumferentially provided with a plurality of second slotted holes 100b-2 a. The first end face of the second tower section 200 is provided with a number of first bolt holes corresponding to the second slots 100b-2a on the second end face of the first tower section 100. The second end face of the second tower section 200 is provided with a number of second bolt holes. The first end face of the third tower section 300 is provided with a number of third bolt holes corresponding to the second bolt holes on the second end face of the second tower section 200. The second end face of the third tower section 300 is provided with a number of fourth bolt holes. Preferably, the first end face and the second end face of the second tower segment are formed by rectangular frame structures, and the diagonal braces are respectively and correspondingly connected to the frame corners of the second tower segment. Preferably, the inclined supporting rod is fixedly connected with the frame structure and the flange plate of the end face in a welding mode. Preferably, the material of the diagonal brace and the end face frame structure is 304 stainless steel, Q235B and/or aluminum alloy angle steel, and the material of the first mounting plate and the second mounting plate is 304 stainless steel, Q235B and/or aluminum alloy plate material.
Preferably, the tower sections are connected to each other by connecting members (e.g., bolts). During storage and transportation, the tower body can be disassembled into three tower sections, and the three tower sections can be sleeved together, so that the storage and transportation volume is reduced. The first, second and third tower sections 100, 200, 300 are arranged in such a way that the third tower section 300 can accommodate the second tower section 200, and the second tower section 200 can accommodate the first tower section 100, as shown in fig. 9.
The antenna tower is preferably directed to a typical small spinner-type G5500 spinner. The whole shape of the antenna tower is 'round top and round bottom', and the installed waterproof box does not protrude out of the outer edge of the second installation disc, so that the cable can smoothly rotate along with the antenna and is not hung by edges and corners and the waterproof box. According to the requirement of the overall height of the antenna, the lower part of the antenna tower can be connected with a standard aluminum alloy truss, the advantages of light weight and modularization of the truss are utilized, the professional characteristics of the antenna tower are exerted, and the top circular platform is suitable for the cable to rotate along with the antenna.
Preferably, as shown in fig. 1, the first and second mounting plates 100b-1 and 100b-2 of the first tower section 100 are fixedly connected by a diagonal brace 100 a. The diagonal braces 100a are arranged at equal intervals in the circumferential direction along the first mounting plate 100b-1 and/or the second mounting plate 100 b-2. The overall structure stability of the first tower section can be realized through the structure, the first mounting disc and the second mounting disc are ensured to be parallel to each other, and the reliability and the stability of the working plane of the rotator are improved. The diameter of the first mounting plate is smaller than the diameter of the second mounting plate.
Preferably, as shown in fig. 2 and 3, the first end surface of the first tower section 100 is provided with a first mounting plate 100b-1, and the mounting surface of the first mounting plate 10Ob-1 facing away from the support tower is circumferentially provided with at least three first slot holes 100b-1a distributed at intervals and radially oriented along the radial direction thereof, so that the first mounting plate 100b-1 can adaptively mount azimuth motors and/or pitching motors with different specifications. The first slots 100b-1a are circumferentially equidistantly spaced on the first mounting plate 100 b-1. The first slots 100b-1a are radially oriented along the radial direction of the first mounting plate 100 b-1. The first slot holes in radial direction are arranged, so that the installation of the azimuth motor and/or the pitching motor with different hole pitches can be adapted, and the rotating devices with other sizes can be taken into consideration. Preferably, the first slot is roughened to ensure that the azimuth motor or the pitching motor does not slide relatively after being installed, thereby ensuring the working stability of the azimuth motor or the pitching motor. Preferably, the first slot is located between adjacent diagonal braces, so as to avoid the diagonal braces from interfering with the first slot, and facilitate the installation of the rotator.
Preferably, as shown in fig. 2-4, a second mounting plate 100b-2 is disposed at a second end of the first tower section 100 for connecting to the second tower section 200, and a plurality of second slots 100b-2a arranged at intervals along the circumferential direction and radially oriented along the circumferential direction are disposed on an end surface of the second mounting plate 100b-2 facing the first mounting plate 100b-1 in the circumferential direction, so that when the azimuth motor and/or the pitch motor is mounted on the first mounting plate 100b-1, the azimuth motor and/or the pitch motor can perform fine direction adjustment based on the friction fit between the second slots 100b-2a and the second tower section 200. The second slots 100b-2a are circumferentially equidistantly spaced on the second mounting plate 100 b-2. The second slot 100b-2a extends in a circular arc shape along the circumferential direction of the second mounting plate 100 b-2. Through the second slotted hole that sets up to be circular-arc trend, can carry out the zero point fine setting of position axial to overcome the column foot position and probably have angular deviation. Preferably, the second slot is roughened to ensure that the azimuth motor does not slide relatively after being installed, thereby ensuring the working stability of the azimuth motor. Preferably, the center of the second slot hole with the arc-shaped trend is the same as the center of the second mounting disc.
Preferably, as shown in fig. 2, the first end face and the second end face of the second tower section 200 are rectangular end faces, the rectangular end faces are fixedly connected through at least four sets of diagonal braces 100a, and a detachable fixing plate 200a is arranged on the second end face of the second tower section 200. Through the structure that sets up the rectangle terminal surface, can improve the inner space of second tower section, the installation of the position motor of being convenient for. Through setting up detachable position motor fixed plate, can realize position and pitch motor's disconnect-type installation. As is known from the background art, there are two main types of mounting for the azimuth and pitch motors on the antenna tower. The first method is as follows: the azimuth motor and the pitching motor are arranged at the top of the antenna tower together; the second method comprises the following steps: in the separation mode, the azimuth motor is arranged at the lower part, and the pitching motor is arranged at the upper part and is connected with the azimuth motor and the pitching motor through an azimuth shaft. When installing with mode two, the inside nylon pipe neck that is used for laying of first mounting disc. The azimuth motor is installed on azimuth motor fixed plate, and the azimuth hollow shaft passes through anchor clamps to be fixed on the azimuth motor, and the hollow shaft passes the inside nylon pipe neck of first mounting disc, and pitching motor is fixed to the hollow shaft upper end. The installation is relatively simple through the first mode, but the center of gravity is high; when the installation is carried out through the second mode, the gravity center is low, and the zero value of the direction is convenient to adjust. The invention can realize the two installation modes, is suitable for rotators with various specifications, and enlarges the use scenes of the antenna tower; meanwhile, batch production can be carried out, and the single cost is reduced.
Preferably, as shown in fig. 2, the fixing plate 200a is provided at the middle thereof with a shaft hole 200a-1, and the outer periphery of the shaft hole 200a-1 is provided with a plurality of fixing holes 200a-2 arranged at equal intervals along the circumferential direction thereof. Through setting up the fixed orifices on the position motor fixed plate, can realize the stable installation of position motor. Preferably, the fixing holes are roughened to ensure that the azimuth motor does not slide relatively after being installed, thereby ensuring the working stability of the azimuth motor.
Preferably, as shown in fig. 2, the first end face and the second end face of the third tower section 300 are rectangular end faces, and the rectangular end faces are fixedly connected by at least four sets of diagonal braces. Through the structure that sets up the rectangle terminal surface, can form better installation cooperation relation with the second terminal surface of second tower section, ensure overall structure's stability and reliability. Preferably, the third tower segment is fastened to the cement floor, the base of the channel steel by means of screws or, for increasing the height, to an aluminum alloy truss.
Preferably, as shown in fig. 2, a plurality of diagonal tension reinforcement rods 300a are disposed between adjacent diagonal support rods of the third tower section 300. Through setting up a plurality of stiffeners that draw to one side, improved overall structure's weight on the one hand, on the other hand reduces its focus when guaranteeing that third tower section bears all members on upper portion, can improve the holistic firm degree of antenna tower.
Preferably, leveling compensation shims 500 are plugged between the connection points of the tower sections. After each tower section is installed, the height of four corners of each tower section is adjusted by additionally installing a leveling compensation gasket, so that horizontal errors generated in the installation process of the tower body can be corrected, and the rotator of the first tower section is ensured to be always kept at the horizontal position. Preferably, the leveling compensation shim is a semi-annular thin sheet structure.
Preferably, as shown in fig. 5, the leveling compensating shim 500 is U-shaped, and both ends thereof are provided with a protrusion 500e and another protrusion 500h protruding from the overall cross-section thereof. After each part of the tower body is installed, the horizontal positions of bolts on all sides are compared, the leveling compensation gaskets are inserted into the bolts on the lower side, a plurality of leveling compensation gaskets are properly added according to the error distance between actual levels, so that the positions on the lower side are lifted to the horizontal positions, and when the bolts are screwed down, the warped edges of the U-shaped gaskets are flattened, thereby clamping the bolt rods and realizing the self-locking process.
For ease of understanding, the working principle of a support tower for a satellite antenna with a self-locking structure according to the invention is illustrated.
When the supporting tower with the satellite antenna of the self-locking structural part is used, the first tower section, the second tower section and the third tower section are fixedly connected together through the bolts, the horizontal state of the top surface of the tower sections can be observed at any time in the connection process, and when the relative height of any side of the tower sections is lower than that of other sides, the height of the tower sections is adjusted through the leveling compensation gasket at the bolts, so that the leveling process of the top surface of the tower body is realized. The flange plate and the leveling compensation gasket which can be installed in the zero-adjusting direction are used, so that the antenna is more convenient to install, and the pointing accuracy of the antenna is higher. Furthermore, the segmented structure also provides a flexible way to mount the antenna and rotator. For example, the spinner and antenna may be assembled after the complete tower; the installation of second tower section + third tower section also can carry out earlier, carry out the installation of antenna + circulator + first tower section again, at last antenna + circulator + first tower section monolithic mounting is in the whole of second tower section + third tower section, in carrying out this installation, installation constructor needn't carry out the higher operation of ascending a height of dangerous degree to this danger in reducing the body of the tower installation, the work efficiency of installation has also been improved simultaneously.
Example 3
This embodiment may be a further improvement and/or a supplement to embodiments 1, 2 or a combination thereof, and repeated contents are not described again. This example discloses that, without causing conflict or contradiction, the whole and/or partial contents of the preferred embodiments of other examples can be supplemented by this example.
The embodiment discloses an antenna tower installation method based on a self-locking structure. Comprising prefabricating an antenna tower into at least three tower sections with substantially the same inclination angle alpha connected in their axial direction successively by connecting members.
The first tower segment 100 is prefabricated as follows: it includes at least two mounting plates 100b of different sizes at different height positions and connected via at least three diagonal braces 100a for mounting a pitch motor and/or an azimuth motor. At least two mounting plates 100b of different sizes can be connected by at least three diagonal braces 100a in such a way as to form an angle of inclination α.
Opposite ends of the second tower section 200 connect the first tower section 100 and the third tower section 300 by connecting members in such a manner as to form an inclination angle α, and a fixing plate 200a for mounting an azimuth motor is detachably connected in such a manner as to be able to lower the center of gravity of the antenna tower.
The third tower segment 300 is connected to an external base body for securing the support tower.
At least one leveling shim 500 is inserted between the first tower segment 100 and the second tower segment 200, which is adapted to the gap between the two and can lock the connecting member.
The leveling compensating shim 500 includes an inner side 500c and an outer side 500d, the outer side 500d being connected to the inner side 500c via a transition surface 500f, a raised protrusion 500e, and a release opening 500g in sequence.
The transition surface 500f is connected to the insertion edge portion 500e-1 of the protrusion 500e such that the thickness thereof gradually increases from the outer surface 500d to the inner surface 500c to be higher than the first leveling surface 500 a. The inset edge portion 500e-1 is connected via a locking edge portion 500e-2 that gradually approaches the geometric centerline of the leveling shim 500 to a transition edge portion 500e-3 that gradually tapers to a thickness that is substantially flush with the first leveling plane 500 a. The transitional edge portion 500e-3 is connected to the medial side 500c via a relief opening 500 g. The inner side surface 500c is connected to another warp protrusion 500h opposite to the warp protrusion 500e in a smoothly curved manner.
The tilted protrusion 500e and the other tilted protrusion 500h are used for passing through the first tower segment 100 and the second tower segment 200Can approach the design value alpha at the inclination angle alpha when the connecting parts are connected0The connecting member is locked.
Preferably, the delivery port 500g is preformed as follows: the release opening 500g includes a first lip 500g-1 extending from the inner side 500c to the outer side 500d, a second lip 500g-2 connected to the first lip 500g-1 and extending substantially in the longitudinal direction of the leveling compensating shim 500, and a third lip 500g-3 connected to the second lip 500g-2 and extending from the outer side 500d to the inner side 500 c. The extension length of the second lip 500g-2 is set in such a manner that the release opening 500g can be elastically deformed in the case where both the locking edge portion 500e-2 and the other locking edge portion of the other seesaw projection 500h are in contact with the connection member.
Example 4
This embodiment may be a further improvement and/or a supplement to embodiment 1, 2 or 3 or a combination thereof, and repeated details are not repeated. This example discloses that, without causing conflict or contradiction, the whole and/or partial contents of the preferred embodiments of other examples can be supplemented by this example.
The present embodiment discloses a leveling compensating shim, and the leveling compensating shim 500 includes an inner side surface 500c and an outer side surface 500 d. The outer side surface 500d is connected to the inner side surface 500c via a transition surface 500f, a warp protrusion 500e, and a release opening 500g in this order. The transition surface 500f is connected to the insertion edge portion 500e-1 of the protrusion 500e such that the thickness thereof gradually increases from the outer surface 500d to the inner surface 500c to be higher than the first leveling surface 500 a. The insert edge portion 500e-1 is connected to a transition edge portion 500e-3 gradually spaced from the geometric centerline and gradually decreasing in thickness to be substantially flush with the first leveling plane 500a through a locking edge portion 500e-2 gradually approaching the geometric centerline of the leveling compensating pad 500, the transition edge portion 500e-3 is connected to an inner side surface 500c through a release opening 500g, and the inner side surface 500c is connected to another tilted projection 500h opposite to the tilted projection 500e in a smoothly curved manner.
It should be noted that the above-mentioned embodiments are exemplary, and that those skilled in the art, having benefit of the present disclosure, may devise various arrangements that are within the scope of the present disclosure and that fall within the scope of the invention. It should be understood by those skilled in the art that the present specification and figures are illustrative only and are not limiting upon the claims. The scope of the invention is defined by the claims and their equivalents.
Claims (10)
1. A method for horizontally adjusting a multi-section satellite antenna support tower, the method comprising:
in the case that the first tower segment (100) and the third tower segment (300) are connected at opposite ends of the second tower segment (200) by means of a connecting member in such a way as to form an inclination angle (alpha), at least one leveling compensation shim (500) adapted to each other in a gap therebetween and capable of locking the connecting member is inserted between the first tower segment (100) and the second tower segment (200),
the leveling compensation gasket (500) comprises an inner side surface (500c) and an outer side surface (500d), and the outer side surface (500d) is connected to the inner side surface (500c) through a transition surface (500f), a raised protrusion (500e) and a release port (500g) in sequence;
the inner side surface (500c) is connected to another warp protrusion (500h) opposite to the warp protrusion (500e) in a smoothly curved manner.
2. The method of leveling a multi-section satellite antenna support tower of claim 1, further comprising:
the first tower section, the second tower section and the third tower section are fixedly connected together through bolts, the horizontal state of the top surface of the tower sections is observed at any time in the connection process,
in the case where the relative height of any one side is lower than that of the other side, the bolt on the lower side is inserted into the leveling compensation shim (500),
a plurality of leveling compensation gaskets (500) are properly added according to the error distance between the actual levels, so that the position of the lower side is raised to the horizontal position;
when the bolt is screwed down, the warping protrusion (500e) and the other warping protrusion (500h) of the leveling compensation gasket (500) can be flattened, and a bolt rod is clamped to realize a self-locking process.
3. The method of leveling a multi-section satellite antenna support tower of claim 2, further comprising:
the tilted protrusion (500e) and the further tilted protrusion (500h) can approach the design value (alpha) at a tilt angle (alpha) when the first pylon segment (100) and the second pylon segment (200) are connected by a connecting part0) The manner in which the connecting member is locked,
wherein the inclination angle (alpha) is the inclination angle of a diagonal brace of a support tower of the satellite antenna.
4. The method of claim 3, wherein the release opening (500g) comprises a first opening edge (500g-1) extending from the inner side surface (500c) to the outer side surface (500d), a second opening edge (500g-2) connected to the first opening edge (500g-1) and extending substantially in a longitudinal direction of the leveling compensation pad (500), and a third opening edge (500g-3) connected to the second opening edge (500g-2) and extending from the outer side surface (500d) to the inner side surface (500 c).
5. The method for horizontally adjusting a multi-section satellite antenna-supported tower according to claim 4, wherein the transition surface (500f) is connected to the insertion edge portion (500e-1) of the protrusion (500e) in such a manner that the thickness thereof gradually increases to be higher than the first tuning plane (500a) in a direction extending from the outer side surface (500d) to the inner side surface (500 c);
the embedded edge portion (500e-1) is connected with a transition edge portion (500e-3) which is gradually far from the geometric center line and gradually reduces in thickness to be approximately flush with the first adjusting plane (500a) through a locking edge portion (500e-2) which is gradually close to the geometric center line of the leveling compensation gasket (500), and the transition edge portion (500e-3) is connected with the inner side surface (500c) through a release opening (500 g).
6. The method of claim 5 wherein the method of horizontally adjusting a multi-section satellite antenna tower is further characterizedCharacterized in that a third leveling plane (500e-4) connected to the embedding edge portion (500e-1) and the locking edge portion (500e-2) is arranged so as to enable the inclination angle (alpha) to approach a design value (alpha)0) In such a way that they are parallel to the first levelling plane (500 a);
the third plane of adjustment (500e-4) is connected to the outer side surface (500d) by an undulating transition surface (500e-5) having a gradually increasing thickness in a direction extending from the outer side surface (500d) to the inner side surface (500 c).
7. The method for leveling a multi-section satellite antenna support tower of any one of claims 1-6, further comprising:
in the case where both the locking edge portion (500e-2) and the other locking edge portion of the other seesaw projection (500h) are in contact with the connection member,
the extension length of the second opening edge (500g-2) is set in a mode of enabling the release opening (500g) to be elastically deformed, so that connecting parts at different positions can be locked by the leveling compensation gasket (500) through the elastic pretightening force of the release opening (500 g).
8. The method of leveling a multi-section satellite antenna support tower of claim 7, further comprising:
the distance between the locking edge portion (500e-2) and another locking edge portion of the another warping protrusion (500h) is set in a manner of being adapted to the inner diameter of the leveling compensation shim (500), so that the leveling compensation shim (500) can be designed as a standard part according to the spatial position of a connection part connecting the first tower section (100) and the second tower section (200).
9. A motor adjusting method for a multi-section satellite antenna supporting tower is characterized by comprising the following steps:
the first tower section, the second tower section and the third tower section are fixedly connected together through bolts,
a second mounting disc (100b-2) is arranged at a second end, used for being connected with a second tower section (200), of the first tower section (100), and a plurality of second slotted holes (100b-2a) which are distributed at intervals along the circumferential direction and are radially arranged along the circumferential direction are formed in the end face, facing the first mounting disc (100b-1), of the second mounting disc (100b-2) in the circumferential direction, so that when the azimuth motor and/or the pitching motor are mounted on the first mounting disc (100b-1), the azimuth motor and/or the pitching motor can perform direction fine adjustment based on friction fit between the second slotted hole (100b-2a) and the second tower section (200);
wherein at least one leveling shim (500) which is adapted to the gap between the first pylon segment (100) and the second pylon segment (200) and can lock the connecting element is inserted between the two segments,
the leveling compensation gasket (500) comprises an inner side surface (500c) and an outer side surface (500d), and the outer side surface (500d) is connected to the inner side surface (500c) through a transition surface (500f), a raised protrusion (500e) and a release port (500g) in sequence;
the inner side surface (500c) is connected to another tilted protrusion (500h) opposite to the tilted protrusion (500e) in a smoothly curved manner,
when the bolt is screwed down, the warping protrusion (500e) and the other warping protrusion (500h) of the leveling compensation gasket (500) can be flattened, and a bolt rod is clamped to realize a self-locking process.
10. The method for adjusting the motors of the multi-section satellite antenna supporting tower according to claim 9, wherein the first mounting plate (100b-1) is disposed at a first end of the first tower section (100), and at least three first slots (100b-1a) radially extending along a radial direction of the first mounting plate (100b-1) are circumferentially disposed on a mounting surface of the first mounting plate (100b-1) facing away from the supporting tower, and are spaced from each other, so that the first mounting plate (100b-1) can adaptively mount azimuth motors and/or pitching motors with different specifications.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110810696.4A CN113482429B (en) | 2019-12-25 | 2019-12-25 | Horizontal adjusting method and motor adjusting method for multi-section satellite antenna supporting tower |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911362330.4A CN111021810B (en) | 2019-12-25 | 2019-12-25 | Satellite antenna's support tower based on auto-lock structure |
| CN202110810696.4A CN113482429B (en) | 2019-12-25 | 2019-12-25 | Horizontal adjusting method and motor adjusting method for multi-section satellite antenna supporting tower |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201911362330.4A Division CN111021810B (en) | 2019-12-25 | 2019-12-25 | Satellite antenna's support tower based on auto-lock structure |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN113482429A true CN113482429A (en) | 2021-10-08 |
| CN113482429B CN113482429B (en) | 2022-04-15 |
Family
ID=70213495
Family Applications (3)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110810696.4A Active CN113482429B (en) | 2019-12-25 | 2019-12-25 | Horizontal adjusting method and motor adjusting method for multi-section satellite antenna supporting tower |
| CN201911362330.4A Active CN111021810B (en) | 2019-12-25 | 2019-12-25 | Satellite antenna's support tower based on auto-lock structure |
| CN202110810698.3A Active CN113503078B (en) | 2019-12-25 | 2019-12-25 | Self-locking structural part and self-locking method |
Family Applications After (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201911362330.4A Active CN111021810B (en) | 2019-12-25 | 2019-12-25 | Satellite antenna's support tower based on auto-lock structure |
| CN202110810698.3A Active CN113503078B (en) | 2019-12-25 | 2019-12-25 | Self-locking structural part and self-locking method |
Country Status (1)
| Country | Link |
|---|---|
| CN (3) | CN113482429B (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2246212Y (en) * | 1994-06-07 | 1997-01-29 | 张玉山 | Loosen-proof bolt group |
| US6357758B1 (en) * | 1999-06-30 | 2002-03-19 | Federal-Mogul World Wide, Inc. | Metal gasket and method of manufacturing |
| CN1710297A (en) * | 2005-06-25 | 2005-12-21 | 陈通平 | Anti-theft anti-loosing fastener |
| CN2791329Y (en) * | 2005-01-11 | 2006-06-28 | 沈会清 | Screw-thread connector capable of dismounting and never loosing and droping |
| CN103225311A (en) * | 2013-03-22 | 2013-07-31 | 广东明阳风电产业集团有限公司 | Fixing and leveling structure for mounting marine fan jacket foundation |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2190673Y (en) * | 1993-12-30 | 1995-03-01 | 沈翠琴 | Matel structure component connecting device |
| ES2246119B1 (en) * | 2004-01-26 | 2007-03-16 | I.T.W. España, S.A. | NUT FASTENING FAST. |
| CN201193411Y (en) * | 2008-05-09 | 2009-02-11 | 上海同济科学技术开发有限公司 | Trilateral special joint pylon of standard steel angle pylons |
| CN110566029A (en) * | 2019-08-26 | 2019-12-13 | 常州第一建筑集团有限公司 | gradual installation and construction method for high-rise steel tower |
-
2019
- 2019-12-25 CN CN202110810696.4A patent/CN113482429B/en active Active
- 2019-12-25 CN CN201911362330.4A patent/CN111021810B/en active Active
- 2019-12-25 CN CN202110810698.3A patent/CN113503078B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2246212Y (en) * | 1994-06-07 | 1997-01-29 | 张玉山 | Loosen-proof bolt group |
| US6357758B1 (en) * | 1999-06-30 | 2002-03-19 | Federal-Mogul World Wide, Inc. | Metal gasket and method of manufacturing |
| CN2791329Y (en) * | 2005-01-11 | 2006-06-28 | 沈会清 | Screw-thread connector capable of dismounting and never loosing and droping |
| CN1710297A (en) * | 2005-06-25 | 2005-12-21 | 陈通平 | Anti-theft anti-loosing fastener |
| CN103225311A (en) * | 2013-03-22 | 2013-07-31 | 广东明阳风电产业集团有限公司 | Fixing and leveling structure for mounting marine fan jacket foundation |
Also Published As
| Publication number | Publication date |
|---|---|
| CN113503078A (en) | 2021-10-15 |
| CN111021810B (en) | 2021-09-21 |
| CN113503078B (en) | 2022-04-15 |
| CN111021810A (en) | 2020-04-17 |
| CN113482429B (en) | 2022-04-15 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US20210194109A1 (en) | Multi-antenna mounting device and multi-antenna assembly | |
| US4799642A (en) | Antenna mounting | |
| US20020196195A1 (en) | Two-axis pole mount assembly | |
| US11316244B2 (en) | Adjustable antenna mount | |
| WO2015134657A1 (en) | Solar panel mounting system with aerodynamic ballast trays | |
| US11831065B2 (en) | Antenna support system and method of installing the same | |
| AU556985B2 (en) | Bearing structure for antenna | |
| US11362502B2 (en) | Adapter for cable hanger | |
| CN113482429B (en) | Horizontal adjusting method and motor adjusting method for multi-section satellite antenna supporting tower | |
| GB2519663A (en) | Tower construction | |
| US10889957B2 (en) | Temporary support structure | |
| KR102487612B1 (en) | Electric pole bracket type 5G anatenna support apparatus for base station | |
| CN211376911U (en) | Multi-dimensional adjusting antenna tower with self-locking structure | |
| US20210376444A1 (en) | Collar mount for a cellular communications monopole | |
| CN216477155U (en) | Angle adjusting device | |
| EP3967872A1 (en) | Mounting structure for supporting a tower sector | |
| AU4312397A (en) | Universal mounting | |
| CN221272651U (en) | Base of charging pile | |
| CN212648462U (en) | Antenna presss from both sides sign indicating number | |
| JP2004200999A (en) | Antenna fixing metallic assembly | |
| US12088238B1 (en) | Solar panel tracker systems and methods | |
| CN115693085A (en) | Antenna equipment switching subassembly and support | |
| US20240235003A9 (en) | Improved antenna support system and method of installing the same | |
| JP2003105760A (en) | Built-up universal anchor pedestal | |
| CN114571171A (en) | Steel structure welding ball positioning and adjusting system and adjusting method |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |