A satellite antenna with automatic fault detection function

Abstract

The present invention discloses a satellite antenna with an automatic fault detection function, belonging to the technical field of satellite antennas. A satellite antenna with an automatic fault detection function comprises a satellite dish body for reflecting and focusing electromagnetic wave signals and a high-frequency head body for receiving signals, and also comprises a mounting frame as a mounting carrier of the satellite dish body, the mounting frame is fixedly connected with a fixing frame, the fixing frame is provided with two, a connecting plate is rotatably connected with the fixing frame, and the other end of the connecting plate is fixedly connected to the back of the satellite dish body; the present invention can automatically calibrate the rotation angle of the satellite antenna, and in complex situations, the rotation angle of the antenna can be double-detected, and in the case of inaccurate rotation mechanism, the angle rotation can be self-adjusted to meet the emergency communication in a short time.

Description

Technical Field

[0001] The present invention relates to the technical field of satellite antennas, and in particular to a satellite antenna with an automatic fault detection function. Background Art

[0002] If the mechanism that controls the rotation of the satellite antenna (such as a gyroscope) is damaged or worn, it may cause inaccurate adjustment angles. For example, when trying to adjust the antenna to 90 degrees, the antenna may only rotate 60 degrees due to damage or wear of the rotation mechanism. This situation may be caused by a variety of reasons, such as circuit failure, mechanical failure, magnetic field interference, etc. In addition, friction, load and poor lubrication are also common causes of wear and failure of the antenna rotation mechanism.

[0003] Based on the above problems, the present invention proposes a method that can be automatically calibrated and can dual-detect the antenna rotation angle in complex situations. When the rotation mechanism is inaccurate, the angle rotation can be self-adjusted to meet emergency communication needs in a short time (the travel time for staff to be dispatched for maintenance). Summary of the invention

[0004] The purpose of the present invention is to solve the problems in the prior art and to propose a satellite antenna with an automatic fault detection function.

[0005] In order to achieve the above object, the present invention adopts the following technical solutions:

[0006] The invention comprises a satellite dish body for reflecting and focusing electromagnetic wave signals and a high-frequency head body for receiving signals, and also comprises: a mounting frame as a mounting carrier of the satellite dish body; a fixing frame is fixedly connected to the mounting frame, and two fixing frames are provided. A connecting plate is rotatably connected to the fixing frame, and the other end of the connecting plate is fixedly connected to the back of the satellite dish body; a connecting main rod is provided between the two fixing frames, and a connecting rod 1 and a connecting rod 2 are rotatably connected in the connecting main rod, and the side end of the connecting rod 1 is fixedly connected to the connecting plate, and the connecting rod 1 and the connecting rod 2 are sleeved together, and the connecting rod 1 and the connecting rod 2 are sleeved together. The connection is wrapped in a magnetic ring, a magnetic block is slidably connected inside the magnetic ring, an insertion rod is provided below the magnetic block, and a socket matching the insertion rod is provided on the second connecting rod; a receiving groove is provided in the fixed frame, a turntable is rotatably connected in the receiving groove, and a receiving block is fixedly connected to the turntable; a driven gear 1 rotates synchronously with the turntable, and an angle sensor is provided below the driven gear 1; arc grooves are provided in both of the two fixed frames, and the arc grooves extend into the connecting plate, and the two arc grooves are respectively provided with a distance measuring sensor 1 and a distance measuring sensor 2 matching the receiving block.

[0007] Preferably, the connecting plate and the fixing frame are both provided with a through sliding groove, a sliding rod is provided in the sliding groove, and two ends of the sliding rod are fixed to the two connecting plates by nuts.

[0008] Preferably, a driving motor 1 is provided on the mounting frame, and the output end of the driving motor 1 extends to the inside of the connecting main rod. The inside of the connecting main rod is hollow, and the output end of the driving motor 1 is placed in the end of the connecting main rod and is fixedly connected to a bevel gear 2. The bevel gear 2 is meshed with a bevel gear 1, and the bevel gear 1 is fixedly connected to the connecting rod 2.

[0009] Preferably, a second driving motor is disposed in the fixing frame, and an output end of the second driving motor is fixedly connected to a driving gear.

[0010] Furthermore, the rotating disk is a hollow ring, and a driven gear 2 is fixedly connected to the rotating disk, and the driven gear 2 is meshed and connected with the driving gear.

[0011] Furthermore, the driven gear 1 is meshed and connected with the driven gear 2.

[0012] Preferably, a double-headed motor is provided in the connecting main rod, and both output ends of the double-headed motor are fixedly connected to a driving gear, and a driven gear three is meshedly connected to the driving gear, and the driven gear three is fixedly connected to the connecting rod one.

[0013] Preferably, a built-in groove is provided in the magnetic ring, and the magnetic ring is an electromagnet.

[0014] Furthermore, a retreat groove is provided on the connecting rod, and a hole for the insertion rod to pass through is provided at the bottom of the retreat groove.

[0015] Furthermore, a magnetic block is slidably connected in the built-in groove, the insertion rod is fixedly connected to the bottom of the magnetic block, and the magnetic block cooperates with the retreat groove.

[0016] Compared with the prior art, the present invention provides a satellite antenna with automatic fault detection function, which has the following beneficial effects:

[0017] 1. The satellite antenna with automatic fault detection function detects the distance to the receiving block through the first and second ranging sensors respectively or simultaneously, and cooperates with the data measured by the angle sensor alone to double detect the rotation angle of the antenna.

[0018] 2. The satellite antenna with automatic fault detection function can control the rotation of the connecting rod through a double-headed motor, and can self-adjust the angle rotation in combination with the data measured by the angle sensor to meet the emergency communication needs in a short time.

[0019] The parts not involved in the satellite antenna with automatic fault detection function are the same as the prior art or can be implemented by using the prior art. The present invention can automatically calibrate the rotation angle of the satellite antenna. In complex situations, the rotation angle of the antenna can be doubly detected. When the rotation mechanism is not accurate, the angle rotation can be self-adjusted to meet the emergency communication needs in a short time. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] Figure 1 The overall structure of a satellite antenna with automatic fault detection function proposed by the present invention is shown in FIG. Figure 1 ;

[0021] Figure 2 The overall structure of a satellite antenna with automatic fault detection function proposed by the present invention is shown in FIG. Figure 2 ;

[0022] Figure 3 The overall structure of a satellite antenna with automatic fault detection function proposed by the present invention is shown in FIG. Figure 3 ;

[0023] Figure 4 A cross-sectional view of a satellite antenna with automatic fault detection function connected to a main pole proposed by the present invention;

[0024] Figure 5 A satellite antenna with automatic fault detection function proposed by the present invention Figure 4 The structural diagram of the enlarged part A in the middle;

[0025] Figure 6 A schematic diagram of the structure of a satellite antenna connecting plate with automatic fault detection function proposed by the present invention Figure 1 ;

[0026] Figure 7 A schematic diagram of the structure of a satellite antenna connecting plate with automatic fault detection function proposed by the present invention Figure 2 ;

[0027] Figure 8 A cross-sectional view of a magnetic ring portion of a satellite antenna with an automatic fault detection function proposed by the present invention;

[0028] Fig. 9 This is an exploded view of the magnetic ring part of a satellite antenna with automatic fault detection function proposed by the present invention.

[0029] In the figure: 1. Satellite dish body; 2. High-frequency head body; 3. Mounting frame; 4. Fixed frame; 5. Sliding groove; 6. Sliding rod; 7. Connecting plate; 8. Arc groove; 9. Distance sensor 1; 10. Connecting main rod; 11. Distance sensor 2; 12. Receiving block; 13. Driving motor 1; 14. Connecting rod 1; 15. Driving motor 2; 16. Driving gear; 17. Driven gear 1; 18. Turntable; 19. Driven gear 2; 20. Arc mounting plate; 21. Angle sensor; 22. Double-headed motor; 23. Driving gear; 24. Driven gear 3; 25. Bevel gear 1; 26. Bevel gear 2; 27. Connecting rod 2; 28. Magnetic ring; 29. ​​Built-in groove; 30. Magnetic block; 31. Insert rod; 32. Socket; 33. Recess groove; 34. Accommodating groove. 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 9, including a satellite dish body 1 for reflecting and focusing electromagnetic wave signals and a high-frequency head body 2 for receiving signals, and also including: a mounting frame 3 as a mounting carrier of the satellite dish body 1; a fixing frame 4 is fixedly connected to the mounting frame 3, and two fixing frames 4 are provided. A connecting plate 7 is rotatably connected to the fixing frame 4, and the other end of the connecting plate 7 is fixedly connected to the back of the satellite dish body 1; a connecting main rod 10 is provided between the two fixing frames 4, and a connecting rod 14 and a connecting rod 27 are rotatably connected in the connecting main rod 10, and the side end of the connecting rod 14 is fixedly connected to the connecting plate 7, and the connecting rod 14 and the connecting rod 27 are mutually sleeved together, and the connection part thereof is wrapped in a magnetic A magnetic block 30 is slidably connected inside the magnetic ring 28, a plug rod 31 is provided below the magnetic block 30, and a socket 32 ​​matching with the plug rod 31 is provided on the connecting rod 27; a receiving groove 34 is provided in the fixing frame 4, a turntable 18 is rotatably connected in the receiving groove 34, and a receiving block 12 is fixedly connected to the turntable 18; a driven gear 17 that rotates synchronously with the turntable 18, and an angle sensor 21 is provided below the driven gear 17; arc grooves 8 are provided in both fixing frames 4, and the arc grooves 8 extend into the connecting plate 7, and the two arc grooves 8 are respectively provided with a distance sensor 1 9 and a distance sensor 2 11 matching with the receiving block 12.

[0033] In the present invention, the high-frequency head body 2 is fixed in front of the focus of the satellite dish body 1 by a plurality of fixed support rods arranged on the satellite dish body 1, so that the high-frequency head body 2 can receive the strongest signal, thereby improving the signal receiving efficiency. The high-frequency head body 2 is located at the focus, which can ensure the stability of the received signal quality and reduce the image deformation and interference caused by signal fluctuations.

[0034] When controlling the satellite dish body 1 to rotate and adjust the angle, the plug rod 31 is inserted into the socket 32 ​​on the second connecting rod 27, so that the connecting rod 1 14 and the second connecting rod 27 form a whole rod and rotate synchronously. In the initial state, the plug rod 31 is inserted into the socket 32, the connecting rod 1 14 and the second connecting rod 27 rotate, the connecting rod 1 14 drives the connecting plate 7 to rotate, and the connecting plate 7 drives the satellite dish body 1 to adjust its angle;

[0035] The distance sensor 1 9 and the distance sensor 2 11 are respectively located in the two arc grooves 8, and the arc grooves 8 extend into the connecting plate 7. The depth of the arc grooves 8 extending inward in the connecting plate 7 covers the installation height of the distance sensor 1 9 and the distance sensor 2 11, so that when the connecting plate 7 rotates on the fixing frame 4, the distance sensor 1 9 and the distance sensor 2 11 will not collide with the fixing frame 4. In normal operation, the rotation angle of the satellite dish body 1 is the range of motion of the arc grooves 8;

[0036] The receiving block 12, the distance sensor 1 9 and the distance sensor 2 11 move on three planes respectively, and the three planes are parallel to each other, so the distance between the receiving block 12, the distance sensor 1 9 and the distance sensor 2 11 is a constant value;

[0037] The angles that the connecting rod 14 and the connecting rod 27 need to rotate are uniformly adjusted by the control center. When the driving device controls the connecting rod 14 and the connecting rod 27 to rotate to the required angle, the connecting plate 7 synchronously drives the ranging sensor 1 9 and the ranging sensor 2 11 to move. Similarly, the driving device controls the turntable 18 to rotate, so that the receiving block 12 also rotates to the corresponding position angle. After the rotation is completed, the ranging sensor 1 9 and the ranging sensor 2 11 detect the distance from the receiving block 12 separately or simultaneously. If the values ​​detected by the ranging sensor 1 9 and the ranging sensor 2 11 are the same as the initial state, and are consistent with the angle measured by the angle sensor 21, it means that the rotation angle of the satellite dish body 1 is accurate; if the ranging sensor 1 9 and the ranging sensor 2 11 are consistent with the initial state, the angle of the satellite dish body 1 is accurate. If the values ​​detected by the distance sensor 11 are the same as the initial state, but are inconsistent with the angle measured by the angle sensor 21, it means that the angle sensor 21 fails. In this case, the rotation angle of the satellite dish body 1 is also accurate; if the values ​​detected by the distance sensor 1 9 and the distance sensor 2 11 are different from one or two of the initial state, and the angle values ​​measured by the angle sensor 21 are compared, it can be determined that a certain distance sensor is damaged and failed. In this case, the rotation angle of the satellite dish body 1 is also accurate; if the values ​​detected by the distance sensor 1 9 and the distance sensor 2 11 are different from the initial state, and the angle values ​​measured by the angle sensor 21 are compared, it can be determined that the rotation angle of the satellite dish body 1 is not accurate;

[0038] When it is determined that the rotation angle of the satellite dish body 1 is not accurate, the insertion rod 31 disengages from the socket 32, and the connecting rod 14 and the connecting rod 2 27 are no longer connected as a whole. Since the connecting rod 14 is disengaged from the connecting rod 2 27, the satellite dish body 1 automatically resets under the action of gravity. Through the angle value of the angle sensor 21, the control center controls the connecting rod 14 to rotate to the corresponding position by independently controlling the connecting rod 14. At this time, the ranging sensor 1 9 and the ranging sensor 2 11 continue to detect with the receiving block 12. If the detected values ​​are the same as the initial state, it means that after self-adjustment, the satellite dish body 1 rotates to the corresponding angle to meet temporary emergency communication.

[0039] Reference Figure 1-Figure 9 A through sliding groove 5 is provided on the connecting plate 7 and the fixing frame 4. A sliding rod 6 is provided in the sliding groove 5. Both ends of the sliding rod 6 are fixed to the two connecting plates 7 by nuts.

[0040] In the present invention, when the connecting plate 7 rotates, the sliding groove 5 cooperates with the sliding rod 6, so that the connecting plate 7 can rotate more smoothly on the fixing frame 4.

[0041] Reference Figure 1-Figure 9 A driving motor 13 is provided on the mounting frame 3, and the output end of the driving motor 13 extends to the inside of the connecting main rod 10. The inside of the connecting main rod 10 is hollow. The output end 13 of the driving motor 1 is placed at the end inside the connecting main rod 10 and is fixedly connected with a bevel gear 26. The bevel gear 26 is meshed with a bevel gear 25, and the bevel gear 25 is fixedly connected to the connecting rod 27.

[0042] In the present invention, the driving motor 13 drives the bevel gear 26 to rotate, and the bevel gear 26 drives the bevel gear 1 25 to rotate, so that the connecting rod 27 rotates, thereby controlling the satellite dish body 1 to adjust the angle.

[0043] Reference Figure 1-Figure 9 A driving motor 2 15 is arranged in the fixed frame 4, and a driving gear 16 is fixedly connected to the output end of the driving motor 2 15; a turntable 18 is a hollow ring, and a driven gear 2 19 is fixedly connected to the turntable 18, and the driven gear 2 19 is meshed and connected with the driving gear 16; a driven gear 1 17 is meshed and connected with the driven gear 2 19.

[0044] In the present invention, the driving motor 2 15 is used to control the rotation of the driving gear 16, the driving gear 16 drives the driven gear 2 19 to rotate, the driven gear 2 19 drives the driven gear 1 17 to rotate, the angle sensor 21 below the driven gear 17 detects the rotation angle of the driven gear 17, and the rotation angle of the receiving block 12 can be calculated by calculation. The turntable 18 is a hollow ring, which is convenient for the connecting rod 14 to drive the connecting plate 7 to rotate, and the part of the connecting rod 14 close to the connecting plate 7 is solid;

[0045] An arc-shaped mounting plate 20 is disposed in the accommodating groove 34 , and the angle sensor 21 is mounted on the arc-shaped mounting plate 20 , and the arc-shaped mounting plate 20 serves as a side end limit support of the driving gear 16 .

[0046] Reference Figure 1-Figure 9 A double-headed motor 22 is provided in the connecting main rod 10, and the two output ends of the double-headed motor 22 are fixedly connected to a driving gear 23, and a driven gear three 24 is meshedly connected to the driving gear 23, and the driven gear three 24 is fixedly connected to the connecting rod one 14.

[0047] In the present invention, when the driving motor 13 rotates inaccurately, the double-headed motor 22 independently controls the connecting rod 14 to rotate through the driving gear 23 and the driven gear 3 24, so that the satellite dish body 1 rotates to the required angle to achieve temporary emergency communication.

[0048] Reference Figure 1-Figure 9A built-in groove 29 is provided in the magnetic ring 28, and the magnetic ring 28 is an electromagnet; a retreat groove 33 is provided on the connecting rod 14, and a hole for the insertion rod 31 to pass through is provided at the bottom of the retreat groove 33; a magnetic block 30 is slidably connected in the built-in groove 29, and the insertion rod 31 is fixedly connected to the bottom of the magnetic block 30, and the magnetic block 30 cooperates with the retreat groove 33.

[0049] In the present invention, the magnetic ring 28 is an electromagnet. When the insertion rod 31 needs to be inserted into the insertion hole 32, the magnetic poles of the magnetic ring 28 are controlled so that the magnetic ring 28 and the magnetic block 30 repel each other, and the magnetic block 30 is repelled into the retreat groove 33, and the insertion rod 31 is inserted into the insertion hole 32, and the connecting rod 1 14 and the connecting rod 2 27 are connected as a whole; when the insertion rod 31 needs to be separated from the insertion hole 32, the magnetic poles of the magnetic ring 28 are controlled so that the magnetic ring 28 and the magnetic block 30 are attracted to each other, the magnetic ring 28 absorbs the magnetic block 30, and the magnetic block 30 drives the insertion rod 31 to separate from the insertion hole 32. At this time, the double-headed motor 22 controls the rotation of the connecting rod 1 14 alone through the driving gear 23 and the driven gear three 24.

[0050] 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 satellite antenna with an automatic fault detection function, comprising a satellite dish body (1) for reflecting and focusing electromagnetic wave signals and a high-frequency head body (2) for receiving signals, characterized in that: Also includes: A mounting frame (3) serving as a mounting carrier for the satellite dish; The mounting frame is fixedly connected to a fixing frame (4), two fixing frames are provided, and a connecting plate (7) is rotatably connected to the fixing frame, the other end of the connecting plate being fixedly connected to the back of the satellite dish body; A connecting main rod (10) is provided between the two fixing frames, and a connecting rod 1 (14) and a connecting rod 2 (27) are rotatably connected in the connecting main rod, and the side end of the connecting rod 1 is fixedly connected to the connecting plate, and the connecting rod 1 and the connecting rod 2 are sleeved together, and the connection part thereof is wrapped in a magnetic ring (28), and a magnetic block (30) is slidably connected in the magnetic ring, and an insertion rod (31) is provided below the magnetic block, and a socket (32) matching with the insertion rod is provided on the connecting rod 2, and a double-headed motor (22) for controlling the independent rotation of the connecting rod 1 is provided in the connecting main rod; A receiving groove (34) is provided in the fixed frame, a rotating disk (18) is rotatably connected in the receiving groove, and a receiving block (12) is fixedly connected to the rotating disk; A driven gear (17) that rotates synchronously with the rotating disk, an angle sensor (21) being provided below the driven gear (17); The two fixing frames are each provided with an arc-shaped groove (8), the arc-shaped groove extending into the connecting plate, and the two arc-shaped grooves are respectively provided with a distance measuring sensor 1 (9) and a distance measuring sensor 2 (11) which cooperate with the receiving block.

2. A satellite antenna with automatic fault detection function according to claim 1, characterized in that: The connecting plate and the fixing frame are both provided with a through-type sliding groove (5), a sliding rod (6) is provided in the sliding groove, and two ends of the sliding rod are fixed to the two connecting plates by nuts.

3. A satellite antenna with automatic fault detection function according to claim 1, characterized in that: The mounting frame is provided with a driving motor 1 (13), the output end of the driving motor 1 extending into the interior of the connecting main rod, the interior of the connecting main rod being hollow, the output end of the driving motor 1 being arranged at the end inside the connecting main rod and being fixedly connected with a bevel gear 2 (26), the bevel gear 2 being meshingly connected with a bevel gear 1 (25), and the bevel gear 1 being fixedly connected to the connecting rod 2.

4. The satellite antenna with automatic fault detection function according to claim 1, characterized in that: A second driving motor (15) is arranged in the fixing frame, and a driving gear (16) is fixedly connected to the output end of the second driving motor.

5. A satellite antenna with automatic fault detection function according to claim 4, characterized in that: The rotating disk is a hollow ring, and a driven gear 2 (19) is fixedly connected to the rotating disk, and the driven gear 2 is meshed and connected with the driving gear.

6. A satellite antenna with automatic fault detection function according to claim 5, characterized in that: The driven gear 1 is meshed and connected with the driven gear 2.

7. The satellite antenna with automatic fault detection function according to claim 1, characterized in that: Both output ends of the double-headed motor are fixedly connected to a driving gear (23), the driving gear is meshingly connected to a driven gear three (24), and the driven gear three is fixedly connected to a connecting rod one.

8. The satellite antenna with automatic fault detection function according to claim 1, characterized in that: A built-in groove (29) is provided in the magnetic ring, and the magnetic ring is an electromagnet.

9. A satellite antenna with automatic fault detection function according to claim 8, characterized in that: A retreat groove (33) is provided on the connecting rod, and a hole for the insertion rod to pass through is provided at the bottom of the retreat groove.

10. A satellite antenna with automatic fault detection function according to claim 9, characterized in that: A magnetic block is slidably connected in the built-in groove, the insertion rod is fixedly connected to the bottom of the magnetic block, and the magnetic block matches the retreat groove.

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