A quick positioning mounting bracket for satellite antenna
By designing a fast positioning mount for satellite antennas including rotating rods, clamps and cleaning jet pipes, the problem of poor clamping effect caused by dust particles when the satellite antenna is installed on the carrier is solved, and the stability and signal quality of the mount are ensured in harsh environments.
Patent Information
- Application Number
- CN202411245471.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2024-09-05
- Publication Date
- 2025-03-18
- Estimated Expiration
- 2044-09-05
AI Technical Summary
In the prior art, when satellite antennas are installed on the carrier, dust particles lead to poor clamping effect, and in harsh environments, the magnetic suction cup is prone to aging and falling off, causing the mounting frame to shake and collapse, and the signal reception fails.
A quick positioning mounting frame for satellite antennas is designed, including satellite antenna support rods and artillery barrel carriers. It adopts structures such as rotary rods, ply plates, cleaning jet pipes and suction pipes. By rotating the handle, the rotary rod controls the clamps, so that the satellite antenna mounting frame and the carrier can be quickly installed, and the dust on the surface of the carrier is cleaned by cleaning the jet pipes.
It realizes that while installing between the satellite antenna mounting frame and the carrier, dust on the surface of the carrier is cleaned up, clamping effect is improved, ensuring that the satellite antenna is more stable on the carrier, exerting more stable signal transmission and reception, and at the same time protecting the carrier surface from excessive clamping.
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Figure CN118943702B_ABST
Abstract
Description
Technical Field
[0001] The invention relates to the technical field of satellite antenna mounting brackets, and in particular to a quick positioning mounting bracket for a satellite antenna. Background Art
[0002] A satellite antenna is a device used to receive signals from satellites. Military satellite antennas are a vital component of military communications and reconnaissance systems. In actual applications, there are various types of military satellite antennas, including vehicle-mounted, portable, and ship-mounted. For example, vehicle-mounted satellite antennas can be installed on military vehicles and move with the troops to maintain communications. Portable satellite antennas are convenient for special forces to use when performing missions behind enemy lines. In short, military satellite antennas play a key role in modern military operations and provide important support for military command, intelligence collection, battlefield communications, etc.
[0003] After searching, the Chinese patent authorization number CN210245701U discloses a satellite antenna mounting bracket for precise positioning of engineering machinery, which is characterized by: including a fixed support component, a movable component, a counterweight component, an elastic component and a limiting component; one end of the fixed support component is fixed to the swing arm of the engineering machinery, and the other end is connected to the movable component so that the movable component can rotate around its axis; the counterweight component is connected to the bottom of the movable component; the elastic component is connected to the top of the movable component; a satellite antenna is fixedly connected above the elastic component; the limiting component is installed on the support rod of the fixed support component to limit the rotation range of the movable component. The above patent has the following deficiencies: when installing the existing vehicle-mounted satellite antenna, a magnetic suction cup provided at the base of the satellite antenna and a threaded portion for cooperating with the satellite antenna for installation are usually used. However, under harsh environmental conditions, the magnetic suction cup is prone to aging. Although it can be installed quickly, when it is installed on a military vehicle, the road surface may be rugged at any time, and due to unequal and harsh environmental factors, the suction cup may easily fall off, causing the satellite antenna mounting frame to shake and collapse, resulting in signal reception failure, etc., and the satellite antenna mounting frame cannot be effectively positioned and installed quickly. Especially when installing the satellite antenna on the gun barrel, it is necessary to fix the satellite antenna mounting frame to the gun barrel. The prior art adopts a clamping method, but due to the long-term use of the gun barrel in harsh environments, such as high temperature, high humidity, chemical corrosion, etc., the paint surface may have been damaged, and the surface of the gun barrel may have impurities such as small dust particles on the surface due to long-term use in harsh environments. When clamped with the satellite antenna mounting frame, the surface of the gun barrel will be damaged, resulting in poor clamping effect, and the dust on the surface of the gun barrel cannot be automatically removed in advance. Summary of the invention
[0004] The purpose of the present invention is to solve the problem in the prior art that dust particles before the satellite antenna is installed on a carrier lead to poor clamping effect, and to propose a quick positioning mounting bracket for a satellite antenna.
[0005] In order to achieve the above object, the present invention adopts the following technical solutions:
[0006] A quick positioning mounting bracket for a satellite antenna comprises a satellite antenna support pole and a gun barrel carrier, wherein a mounting box is arranged at the bottom of the satellite antenna support pole, and two clamping plates are arranged on the mounting box, and further comprises: a rotating rod, which is rotatably connected to the mounting box, and driven rods are rotatably connected to the two side surfaces of the mounting box, and a synchronous belt is transmission-connected between the rotating rod and the driven rod; a protrusion, which is fixedly connected to the driven rod; a mounting plate, which is fixedly connected to the two sides of the mounting box, and a piston cylinder is fixedly connected to the surface of the mounting plate, and the internal piston of the piston cylinder is connected to a piston plate; a sliding rod, which is slidably connected in the piston cylinder; a plurality of groups of cleaning jet pipes, which are arranged between the clamping plate and the piston cylinder, and an air intake pipe is fixedly connected to the upper side of the piston cylinder, and a one-way valve is fixedly installed on the cleaning jet pipe and the air intake pipe.
[0007] Preferably, a sliding hole is provided on the top surface of the installation box, a first L-shaped plate is passed through the interior of the installation box, the first L-shaped plate is slidably connected to the sliding hole of the installation box, one end of the first L-shaped plate away from the bottom inner wall of the installation box is fixedly connected to the clamping plate, the rotating rod passes through the installation box, a bidirectional thread is provided on the surface of the rotating rod close to the interior of the installation box, a slide groove plate is fixedly connected to the bottom inner wall of the installation box, and the first L-shaped plate is slidably connected in the slide groove plate.
[0008] Preferably, the rotating rod passes through the first L-shaped plate and is threadedly connected to the first L-shaped plate, the sliding rod passes through the piston cylinder and is slidably connected to the piston cylinder, the surface of the sliding rod is sleeved with a first spring, one end of the first spring is fixedly connected to the piston cylinder, and the other end of the first spring is fixedly connected to the sliding rod.
[0009] Preferably, the cleaning jet pipe passes through the splint and is slidably connected to the splint, a circular ring passes through the surface of the cleaning jet pipe, the circular ring is fixedly connected to the cleaning jet pipe, a second spring is sleeved on the surface of the cleaning jet pipe, one end of the second spring is fixedly connected to the outer surface of the splint, and the other end of the second spring is fixedly connected to the circular ring.
[0010] Preferably, a handle is fixedly connected to the surface of the installation box, the clamping plate can be replaced according to the shape of the satellite antenna carrier, and the right end surface of the rotating rod is fixedly connected to the handle.
[0011] Preferably, a sliding groove is provided on the top surface of the splint, a second L-shaped plate is slidably connected in the top sliding groove of the splint, a third L-shaped plate passes through the surface of the first L-shaped plate, the third L-shaped plate is slidably connected to the first L-shaped plate, and a connecting plate is fixedly connected between the second L-shaped plate and the third L-shaped plate.
[0012] Preferably, a rectangular sliding hole is opened on the surface of the third L-shaped plate, a three-pronged plate is passed through the rectangular sliding hole of the third L-shaped plate, the three-pronged plate is slidably connected to the rectangular sliding hole of the third L-shaped plate, the three-pronged plate passes through the installation box and is slidably connected to the installation box, a pull rope is fixedly connected to the top surface of the three-pronged plate, and one end of the pull rope away from the three-pronged plate is fixedly connected to the third L-shaped plate.
[0013] Preferably, the bottom surface of the three-pronged plate is fixedly connected with a cross plate, and the cross plate is slidably connected to the inner walls on both sides of the installation box, a rectangular slide groove is opened on the surface of the cross plate, the first L-shaped plate is slidably connected to the rectangular slide groove of the cross plate, the top surface of the cross plate is fixedly connected with a third spring, the top of the third spring is fixedly connected to the top inner wall of the installation box, the bottom of the cross plate is hinged with a connecting rod, the bottom of the connecting rod is hinged with a push plate, the surface of the push plate is penetrated by a telescopic rod, the surface of the telescopic rod is opened with a slide groove, the push plate slides in the slide groove of the telescopic rod, a fourth spring is fixedly connected between the push plate and the slide groove of the telescopic rod, and the telescopic rod and the push plate are rotatably and slidably connected.
[0014] Preferably, the end of the telescopic rod away from the push plate is fixedly connected to a circular rod, a gear 1 is passed through the surface of the circular rod, and the gear 1 is fixedly connected to the circular rod, and a gear 2 is passed through the surface of the rotating rod close to the outside of the installation box, and the gear 2 is fixedly connected to the rotating rod, and the gear 2 is meshed with gear 1.
[0015] Preferably, the telescopic rod is hinged on the surface of one end away from the circular rod with two strip plates, and the two strip plates are hinged on the surface of one end away from the telescopic rod with friction blocks, a vertical plate is fixedly connected to the bottom inner wall of the installation box, a groove is opened on the surface of the vertical plate, a pawl is provided on the inner wall of the groove of the vertical plate, a ratchet is rotatably connected in the groove of the vertical plate, the outer surface of the ratchet is fixedly connected to a rotating drum, a rectangular frame is provided inside the rotating drum, and the friction block is slidably connected inside the rectangular frame.
[0016] Compared with the prior art, the present invention provides a quick positioning mounting bracket for a satellite antenna, which has the following beneficial effects:
[0017] The satellite antenna quick positioning mounting bracket drives the rotating rod to control the clamping plate by rotating the handle, so that the satellite antenna mounting bracket and the carrier are quickly installed, and the cleaning jet pipe cleans the dust on the surface of the carrier at the same time. The third L-shaped plate slides and controls the connecting rod to make the friction block rub against the inner wall of the rotating cylinder, and finally the handle is stuck. This realizes that when the satellite antenna mounting bracket is installed between the carrier, the surface of the carrier can be cleaned, and the fit between the clamping plate and the carrier is tighter. At the same time, the carrier surface is protected from damage by excessive clamping while the carrier is clamped, so that the satellite antenna is more stable on the carrier and more stable signal transmission and reception are achieved. BRIEF DESCRIPTION OF THE DRAWINGS
[0018] Figure 1 This is a front structural schematic diagram of a quick positioning mounting bracket for a satellite antenna proposed by the present invention;
[0019] Figure 2 A quick positioning mounting frame for a satellite antenna proposed by the present invention Figure 1 The structural diagram of part A in the figure;
[0020] Figure 3 A quick positioning mounting frame for a satellite antenna proposed by the present invention Figure 1 The structural diagram of part B;
[0021] Figure 4 A schematic diagram of the side structure of a quick positioning mounting bracket for a satellite antenna proposed by the present invention;
[0022] Figure 5 A quick positioning mounting frame for a satellite antenna proposed by the present invention Figure 4 Schematic diagram of the structure of part C;
[0023] Figure 6 This is a front cross-sectional structural schematic diagram of a rapid positioning mounting frame for a satellite antenna proposed by the present invention;
[0024] Figure 7 A quick positioning mounting frame for a satellite antenna proposed by the present invention Figure 6 The structural diagram of the D part;
[0025] Figure 8 A quick positioning mounting frame for a satellite antenna proposed by the present invention Figure 6 The structural diagram of the E part;
[0026] Fig. 9 This is a front view structural schematic diagram of a rapid positioning mounting bracket for a satellite antenna proposed by the present invention;
[0027] Fig.10This is a schematic diagram of the structure inside a mounting box in a satellite antenna rapid positioning mounting frame proposed by the present invention;
[0028] Fig.11 A quick positioning mounting frame for a satellite antenna proposed by the present invention Fig.10 Schematic diagram of the structure of part F.
[0029] In the figure: 1, satellite antenna support rod; 2, gun barrel carrier; 3, installation box; 301, slide plate; 4, clamping plate; 5, rotating rod; 501, handle; 6, driven rod; 7, synchronous belt; 8, bump; 9, installation plate; 10, piston cylinder; 11, piston plate; 12, sliding rod; 13, cleaning jet pipe; 14, suction pipe; 15, one-way valve; 16, first L-shaped plate; 17, first spring; 18, ring; 19, second spring; 20 , handle; 21. second L-shaped plate; 22. third L-shaped plate; 23. connecting plate; 24. three-pronged plate; 25. pull rope; 26. horizontal plate; 27. third spring; 28. connecting rod; 29. push plate; 30. telescopic rod; 3001. fourth spring; 31. circular rod; 32. gear one; 33. gear two; 34. strip plate; 35. friction block; 36. vertical plate; 37. pawl; 38. rotating drum; 39. rectangular frame; 40. ratchet. DETAILED DESCRIPTION
[0030] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, rather than all the embodiments.
[0031] In the description of the present invention, it is necessary to understand that the terms "upper", "lower", "front", "back", "left", "right", "top", "bottom", "inside", "outside", etc., indicating the orientation or position relationship are based on the orientation or position relationship shown in the drawings, and are only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on the present invention.
[0032] Reference Figure 1-Figure 10A quick positioning mounting frame for a satellite antenna comprises a satellite antenna support pole 1 and a gun barrel carrier 2. A mounting box 3 is arranged at the bottom of the satellite antenna support pole 1, and two clamping plates 4 are arranged on the mounting box 3. The mounting box 3 also comprises: a rotating rod 5, which is rotatably connected to the mounting box 3, and driven rods 6 are rotatably connected to the surfaces of both sides of the mounting box 3, and a synchronous belt 7 is transmission-connected between the rotating rod 5 and the driven rod 6; a convex block 8, which is fixedly connected to the driven rod 6; a mounting plate 9, which is fixedly connected to both sides of the mounting box 3, and a piston cylinder 10 is fixedly connected to the surface of the mounting plate 9, and a piston plate 11 is connected to the internal piston of the piston cylinder 10; a sliding rod 12, which is slidably connected in the piston cylinder 10; a plurality of cleaning jet pipes 13, which are arranged between the clamping plate 4 and the piston cylinder 10, and an air intake pipe 14 is fixedly connected to the upper part of the piston cylinder 10, and a one-way valve 15 is fixedly installed on both the cleaning jet pipe 13 and the air intake pipe 14.
[0033] In the present invention, when the satellite antenna and the gun barrel carrier 2 are installed, when the dust on the surface of the gun barrel carrier 2 is removed, the rotation of the rotating rod 5 cooperates with the synchronous belt 7 to drive the driven rod 6 and the surface protrusion 8 to rotate synchronously. The protrusion 8 rotates and contacts the sliding rod 12. The sliding rod 12 pushes the piston plate 11 upward to perform piston movement in the piston barrel 10 under the vertical limit of the piston cylinder 10, which causes the air in the piston cylinder 10 to spray out gas through multiple groups of cleaning jet pipes 13, forming a jet airflow to blow and remove the dust on the surface of the gun barrel carrier 2, and then the satellite antenna bracket is installed between the gun barrel carrier 2, so that before the satellite antenna is installed, the surface of the installed carrier can be cleaned of dust and other particulate impurities, which helps to make the installation effect of the satellite antenna bracket better, and can make the installation between the satellite antenna bracket and the carrier faster, reduce the labor intensity of manual labor, and simplify the operation.
[0034] In some embodiments, a sliding hole is provided on the top surface of the installation box 3, and a first L-shaped plate 16 is passed through the interior of the installation box 3. The first L-shaped plate 16 is slidably connected to the sliding hole of the installation box 3, and one end of the first L-shaped plate 16 away from the bottom inner wall of the installation box 3 is fixedly connected to the clamping plate 4. The rotating rod 5 passes through the installation box 3, and a bidirectional thread is provided on the surface of the rotating rod 5 near the interior of the installation box 3. A slide groove plate 301 is fixedly connected to the bottom inner wall of the installation box 3, and the first L-shaped plate 16 is slidably connected in the slide groove plate 301.
[0035] In the present invention, through the sliding holes on the surface of the installation box 3, the first L-shaped plate 16 will be more stable when sliding. By rotating the bidirectional threads on the surface of the rotating rod 5, the first L-shaped plate 16 will be driven to slide when the rotating rod 5 rotates, thereby driving the clamping plate 4 to slide and clamp the gun barrel carrier 2, thereby driving the satellite antenna support rod 1 and the carrier to be connected and fixed. Through the slide groove plate 301, the first L-shaped plate 16 can be limited when sliding, so that the process of driving the clamping plate 4 to slide is more stable.
[0036] The rotating rod 5 passes through the first L-shaped plate 16 and is threadedly connected to the first L-shaped plate 16. The sliding rod 12 passes through the piston cylinder 10 and is slidably connected to the piston cylinder 10. The surface of the sliding rod 12 is sleeved with a first spring 17. One end of the first spring 17 is fixedly connected to the piston cylinder 10, and the other end of the first spring 17 is fixedly connected to the sliding rod 12.
[0037] In the present invention, when the protrusion 8 rotates to make the sliding rod 12 slide upward, the first spring 17 will be compressed. When the protrusion 8 rotates to another angle, the first spring 17 will make the sliding rod 12 drive the piston plate 11 to automatically reset downward, so that the protrusion 8 can push the sliding rod 12 upward again, and repeat this process. Therefore, during the installation process between the satellite antenna bracket and the carrier, the particles, dust and impurities on the surface of the carrier can be continuously removed in advance, making the connection between the satellite antenna bracket and the carrier more stable.
[0038] The cleaning jet pipe 13 passes through the splint 4 and is slidably connected to the splint 4. A circular ring 18 passes through the surface of the cleaning jet pipe 13, and the circular ring 18 is fixedly connected to the cleaning jet pipe 13. A second spring 19 is sleeved on the surface of the cleaning jet pipe 13, and one end of the second spring 19 is fixedly connected to the outer surface of the splint 4, and the other end of the second spring 19 is fixedly connected to the circular ring 18.
[0039] In the present invention, since the cleaning jet tube 13 can slide on the clamping plate 4, when the clamping plate 4 clamps the carrier, the cleaning jet tube 13 can slide to the outside of the clamping plate 4, thereby not affecting the clamping of the clamping plate 4 on the carrier.
[0040] A grip 20 is fixedly connected to the surface of the installation box 3 , the clamping plate 4 can be replaced according to the shape of the satellite antenna carrier, and a handle 501 is fixedly connected to the right end surface of the rotating rod 5 .
[0041] In the present invention, when connecting and positioning the satellite antenna support pole 1 and the artillery barrel carrier 2, the grip 20 can be held to place the installation box 3 in a suitable position, and then the handle 501 can be turned to drive the rotating rod 5 to rotate. When it is necessary to install the satellite antenna on another carrier, the clamp 4 can be removed and replaced with a clamp of a shape matching the carrier to install the satellite antenna support pole 1.
[0042] In some embodiments, such as Figure 1-11 A slide groove is provided on the top surface of the clamping plate 4, and a second L-shaped plate 21 is slidably connected in the top slide groove of the clamping plate 4. A third L-shaped plate 22 passes through the surface of the first L-shaped plate 16, and the third L-shaped plate 22 is slidably connected to the first L-shaped plate 16. A connecting plate 23 is fixedly connected between the second L-shaped plate 21 and the third L-shaped plate 22.
[0043] In the present invention, through the sliding groove on the top surface of the clamping plate 4, after the clamping plate 4 and the carrier are in contact, the second L-shaped plate 21 can slide along the sliding groove without affecting the clamping effect between the clamping plate 4 and the carrier. When the clamping plate 4 clamps the carrier, the second L-shaped plate 21 first contacts the carrier and slides to the outside of the two clamping plates 4. Through the connecting plate 23, the third L-shaped plate 22 can be driven to slide on the first L-shaped plate 16.
[0044] A rectangular sliding hole is provided on the surface of the third L-shaped plate 22, and a three-pronged plate 24 is passed through the rectangular sliding hole of the third L-shaped plate 22. The three-pronged plate 24 is slidably connected to the rectangular sliding hole of the third L-shaped plate 22. The three-pronged plate 24 passes through the installation box 3 and is slidably connected to the installation box 3. A pull rope 25 is fixedly connected to the top surface of the three-pronged plate 24, and one end of the pull rope 25 away from the three-pronged plate 24 is fixedly connected to the third L-shaped plate 22.
[0045] In the present invention, when the third L-shaped plate 22 slides toward the edge of the installation box 3, since the three-pronged plate 24 can only slide vertically downward or upward on the installation box 3, the third L-shaped plate 22 pulls the pull rope 25, thereby causing the three-pronged plate 24 to slide downward.
[0046] A cross plate 26 is fixedly connected to the bottom surface of the tripod plate 24, and the cross plate 26 is slidably connected to the inner walls of both sides of the installation box 3. A rectangular slide groove is provided on the surface of the cross plate 26, and the first L-shaped plate 16 is slidably connected to the rectangular slide groove of the cross plate 26. A third spring 27 is fixedly connected to the top surface of the cross plate 26, and the top of the third spring 27 is fixedly connected to the top inner wall of the installation box 3. A connecting rod 28 is hinged at the bottom of the cross plate 26, and a push plate 29 is hinged at the bottom of the connecting rod 28. A telescopic rod 30 passes through the surface of the push plate 29, and a slide groove is provided on the surface of the telescopic rod 30. The push plate 29 slides in the slide groove of the telescopic rod 30, and a fourth spring 3001 is fixedly connected between the push plate 29 and the slide groove of the telescopic rod 30, and the telescopic rod 30 is rotatably and slidably connected to the push plate 29.
[0047] In the present invention, the tripod plate 24 slides downward and presses the horizontal plate 26 downward, thereby driving the connecting rod 28 at the bottom to rotate. When the connecting rod 28 rotates, it drives the push plate 29 at the bottom to compress the fourth spring 3001 on the sliding groove of the telescopic rod 30 toward the center of the installation box 3 and slide; through the fourth spring 3001, the push plate 29 can be automatically reset when the connecting rod 28 does not push the push plate 29; when the horizontal plate 26 moves downward, the third spring 27 will be stretched, and when the tripod plate 24 does not press the horizontal plate 26, the third spring 27 can make the horizontal plate 26 automatically reset upward.
[0048] One end of the telescopic rod 30 away from the push plate 29 is fixedly connected to a circular rod 31, and a gear 1 32 passes through the surface of the circular rod 31, and the gear 1 32 is fixedly connected to the circular rod 31. A gear 2 33 passes through the surface of the rotating rod 5 close to the outside of the installation box 3, and the gear 2 33 is fixedly connected to the rotating rod 5, and the gear 2 33 meshes with the gear 1 32.
[0049] The telescopic rod 30 is hinged on one end surface away from the circular rod 31 with two strip plates 34, and the two strip plates 34 are hinged on one end surface away from the telescopic rod 30 with friction blocks 35. A vertical plate 36 is fixedly connected to the inner wall of the bottom of the installation box 3, and a groove is provided on the surface of the vertical plate 36. A pawl 37 is provided on the inner wall of the groove of the vertical plate 36. A ratchet 40 is rotatably connected in the groove of the vertical plate 36. A rotating drum 38 is fixedly connected to the outer surface of the ratchet 40, and a rectangular frame 39 is provided inside the rotating drum 38. The friction block 35 is slidably connected inside the rectangular frame 39.
[0050] In the present invention, when the satellite antenna mounting frame is installed between the carrier, the first L-shaped plate 16 is driven by rotating the rotating rod 5, so that the second L-shaped plate 21 drives the three-pronged plate 24 to slide downward during the process of the clamping plate 4 clamping the carrier. At the same time, during the rotation of the rotating rod 5, the gear 2 33 is driven to rotate and mesh with the gear 1 32, so that the rotating rod 5 rotates to control the clamping plate 4 to clamp the carrier. Through the meshing of the gear 2 33 and the gear 1 32, the circular rod 31 drives the telescopic rod 30 to rotate synchronously, thereby driving the strip plate 34 and the friction block 35 and the rectangular frame 39 to rotate. After the clamping plate 4 is clamped between the carrier, the three-pronged plate 24 drives the cross plate 26 to drive the connecting rod 28 to push the push plate 29, and the push plate 29 pushes the telescopic rod 30 to drive the two strip plates 34, so that the rectangular frame 39 conflicts with the inner wall of the rotating cylinder 38, and then the two friction blocks 35 extend out of the rectangular frame 39 and The inner wall of the rotating cylinder 38 is in conflict. Since the rotating cylinder 38 can only rotate in one direction under the action of the ratchet 40 and the pawl 37, the friction block 35 can no longer drive the rotating cylinder 38 to rotate inside the rotating cylinder 38, so that the telescopic rod 30, the circular rod 31 and the gear 1 32 continue to rotate, so that the gear 2 33 is stuck, and the rotating rod 5 and the handle 501 cannot continue to rotate, and then the clamping plate 4 and the carrier cannot continue to be clamped, so that after the carrier is clamped, it can protect the carrier from excessive clamping force, prevent the carrier from being deformed due to excessive clamping, and prevent the satellite antenna from tipping over during use, so as to achieve the purpose of cleaning the dust on the surface of the carrier during the installation process between the satellite antenna mounting frame and the carrier, making the installation connection between the carrier and the satellite antenna mounting frame more stable, and protecting the carrier from damage while keeping the carrier clamped, and achieving quick installation.
[0051] The above description is only a preferred specific implementation manner of the present invention, but the protection scope of the present invention is not limited thereto. Any technician familiar with the technical field can make equivalent replacements or changes according to the technical scheme and inventive concept of the present invention within the technical scope disclosed by the present invention, which should be covered by the protection scope of the present invention.
Claims
1. A quick positioning mounting frame for a satellite antenna, comprising a satellite antenna support rod (1) and a gun barrel carrier (2), characterized in that: The bottom of the satellite antenna support pole (1) is provided with a mounting box (3), two clamping plates (4) are provided on the mounting box (3), and further comprises: A rotating rod (5) is rotatably connected to the installation box (3); two side surfaces of the installation box (3) are rotatably connected to driven rods (6); a synchronous belt (7) is transmission-connected between the rotating rod (5) and the driven rod (6); A projection (8) fixedly connected to the driven rod (6); A mounting plate (9) is fixedly connected to two sides of the mounting box (3); a piston cylinder (10) is fixedly connected to the surface of the mounting plate (9); and an internal piston of the piston cylinder (10) is connected to a piston plate (11); A sliding rod (12) slidably connected in the piston cylinder (10); A plurality of cleaning jet pipes (13) are arranged between the clamping plate (4) and the piston cylinder (10); an air suction pipe (14) is fixedly connected to the upper portion of the piston cylinder (10); and a one-way valve (15) is fixedly installed on each of the cleaning jet pipes (13) and the air suction pipe (14); The top surface of the installation box (3) is provided with a sliding hole, the interior of the installation box (3) is penetrated by a first L-shaped plate (16), the first L-shaped plate (16) is slidably connected to the sliding hole of the installation box (3), one end of the first L-shaped plate (16) away from the bottom inner wall of the installation box (3) is fixedly connected to the clamping plate (4), the rotating rod (5) penetrates the installation box (3), the surface of the rotating rod (5) close to the inside of the installation box (3) is provided with a bidirectional thread, a sliding groove plate (301) is fixedly connected to the bottom inner wall of the installation box (3), and the first L-shaped plate (16) is slidably connected inside the sliding groove plate (301); The cleaning jet pipe (13) passes through the clamping plate (4) and is slidably connected to the clamping plate (4); A sliding groove is provided on the top surface of the clamping plate (4), a second L-shaped plate (21) is slidably connected in the top sliding groove of the clamping plate (4), a third L-shaped plate (22) passes through the surface of the first L-shaped plate (16), the third L-shaped plate (22) is slidably connected to the first L-shaped plate (16), and a connecting plate (23) is fixedly connected between the second L-shaped plate (21) and the third L-shaped plate (22).
2. A satellite antenna quick positioning mounting bracket according to claim 1, characterized in that: The rotating rod (5) passes through the first L-shaped plate (16) and is threadedly connected to the first L-shaped plate (16); the sliding rod (12) passes through the piston cylinder (10) and is slidably connected to the piston cylinder (10); a first spring (17) is sleeved on the surface of the sliding rod (12); one end of the first spring (17) is fixedly connected to the piston cylinder (10), and the other end of the first spring (17) is fixedly connected to the sliding rod (12).
3. A satellite antenna quick positioning mounting bracket according to claim 1, characterized in that: A circular ring (18) passes through the surface of the cleaning jet pipe (13), and the circular ring (18) is fixedly connected to the cleaning jet pipe (13). A second spring (19) is sleeved on the surface of the cleaning jet pipe (13), and one end of the second spring (19) is fixedly connected to the outer surface of the clamping plate (4), and the other end of the second spring (19) is fixedly connected to the circular ring (18).
4. A satellite antenna rapid positioning mounting bracket according to claim 1, characterized in that: A grip (20) is fixedly connected to the surface of the installation box (3); the clamping plate (4) can be replaced according to the shape of the satellite antenna carrier; and a handle (501) is fixedly connected to the right end surface of the rotating rod (5).
5. A satellite antenna quick positioning mounting bracket according to claim 1, characterized in that: A rectangular sliding hole is provided on the surface of the third L-shaped plate (22), a three-pronged plate (24) is passed through the rectangular sliding hole of the third L-shaped plate (22), the three-pronged plate (24) is slidably connected to the rectangular sliding hole of the third L-shaped plate (22), the three-pronged plate (24) passes through the installation box (3) and is slidably connected to the installation box (3), a pull rope (25) is fixedly connected to the top surface of the three-pronged plate (24), and one end of the pull rope (25) away from the three-pronged plate (24) is fixedly connected to the third L-shaped plate (22).
6. A satellite antenna rapid positioning mounting bracket according to claim 5, characterized in that: The bottom surface of the three-pronged plate (24) is fixedly connected to a transverse plate (26), and the transverse plate (26) is slidably connected to the inner walls of both sides of the installation box (3). A rectangular slide groove is provided on the surface of the transverse plate (26), and the first L-shaped plate (16) is slidably connected to the rectangular slide groove of the transverse plate (26). The top surface of the transverse plate (26) is fixedly connected to a third spring (27), and the top of the third spring (27) is fixedly connected to the top inner wall of the installation box (3). The transverse plate (26) is provided with a plurality of springs (27) and a plurality of springs (27) are provided on the top surface of the transverse plate (26). 26) is hinged at the bottom with a connecting rod (28), and the bottom of the connecting rod (28) is hinged with a push plate (29), and a telescopic rod (30) passes through the surface of the push plate (29), and a sliding groove is opened on the surface of the telescopic rod (30), and the push plate (29) slides in the sliding groove of the telescopic rod (30), and a fourth spring (3001) is fixedly connected between the push plate (29) and the sliding groove of the telescopic rod (30), and the telescopic rod (30) and the push plate (29) are rotatably and slidably connected.
7. A satellite antenna rapid positioning mounting bracket according to claim 6, characterized in that: One end of the telescopic rod (30) away from the push plate (29) is fixedly connected to a circular rod (31), a surface of the circular rod (31) is penetrated by a gear 1 (32), the gear 1 (32) is fixedly connected to the circular rod (31), and a surface of the rotating rod (5) close to the outside of the installation box (3) is penetrated by a gear 2 (33), the gear 2 (33) is fixedly connected to the rotating rod (5), and the gear 2 (33) is meshed with the gear 1 (32).
8. A satellite antenna rapid positioning mounting bracket according to claim 7, characterized in that: The telescopic rod (30) is hingedly connected to the surface of one end away from the circular rod (31) with two strip plates (34), and the surfaces of the two strip plates (34) are hingedly connected to the surfaces of the ends away from the telescopic rod (30) with friction blocks (35). A vertical plate (36) is fixedly connected to the inner wall of the bottom of the installation box (3), and a groove is provided on the surface of the vertical plate (36). A ratchet (37) is provided on the inner wall of the groove of the vertical plate (36). A ratchet (40) is rotatably connected in the groove of the vertical plate (36). A rotating drum (38) is fixedly connected to the outer surface of the ratchet (40), and a rectangular frame (39) is provided inside the rotating drum (38). The friction block (35) is slidably connected inside the rectangular frame (39).
Citation Information
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