Ship signal receiving device and use method thereof

Abstract

The invention discloses a ship signal receiving device and a use method thereof, and relates to the technical field of ship communication, the ship signal receiving device comprises a base, a U-shaped plate is fixedly arranged on the base, a lifting plate is arranged above the U-shaped plate, a fixed plate is arranged above the lifting plate, and the lifting plate is connected with the U-shaped plate and the fixed plate through a hinge mechanism; a fixed pin shaft is arranged above the fixed plate and is connected with the fixed plate through a limiting mechanism; a cross-shaped bottom plate is fixedly arranged at the top end part of the fixed pin shaft, and a cross-shaped top plate is arranged above the cross-shaped bottom plate; a satellite receiver is arranged above the cross-shaped top plate, and the hemispherical antenna and the cross-shaped top plate are connected with the satellite receiver through a clamping mechanism. According to the invention, the azimuth and angle of signal receiving can be flexibly adjusted according to different navigation environments and requirements, diversified signal requirements in changeable navigation environments can be met, the signal receiving direction and range can be adaptively adjusted in different navigation stages and sea conditions, and the important requirements of improving the navigation efficiency and safety are met.

Description

Technical Field

[0001] The present invention relates to the field of ship communication technology, and in particular to a ship signal receiving device and a use method thereof. Background Art

[0002] As the global requirements for environmental protection and energy conservation and emission reduction continue to increase, new energy ships, as a clean energy carrier, are gradually gaining attention in the shipping industry. Ship signal receiving devices are an indispensable component, which not only help ships understand the dynamic situation on the waterway, but also respond to emergency signals in time to ensure navigation safety.

[0003] Currently, the ship signal receiving devices on the market mainly adopt a fixed installation method. Once the installation position is determined, it is difficult to adjust it again. This is not possible for large ships to flexibly change the signal receiving direction during different navigation phases or when encountering different sea conditions, thus affecting the timeliness and accuracy of information transmission. Summary of the invention

[0004] The purpose of the present invention is to solve the shortcomings of the prior art and to propose a ship signal receiving device and a method of using the same.

[0005] In order to solve the problems existing in the prior art, the present invention adopts the following technical solutions:

[0006] A ship signal receiving device comprises a base, a U-shaped plate with an opening facing downward is fixedly arranged in the middle of the top surface of the base, a lifting plate suspended in the air is arranged above the U-shaped plate, a fixed plate distributed in parallel is arranged above the lifting plate, and the lifting plate is connected to the U-shaped plate and the fixed plate through a hinge mechanism;

[0007] A pair of first ear seats are fixedly provided on the front and rear sides of the top surface of the fixing plate, a first semicircular bracket with an opening facing downward is hingedly provided between the pair of first ear seats, and a first flat pin hole is provided on the first semicircular bracket;

[0008] A pair of second ear seats are fixedly provided on the left and right sides of the top surface of the fixing plate, a second semicircular bracket with an opening facing downward is hingedly provided between the pair of second ear seats, and a second flat pin hole is provided on the second semicircular bracket;

[0009] The second semicircular bracket is located in the opening of the first semicircular bracket, and a fixed pin shaft is slidably inserted at the overlap between the first flat pin hole and the second flat pin hole, and the bottom end of the fixed pin shaft is connected to the fixed plate through a limiting mechanism;

[0010] A cross bottom plate is fixedly arranged at the top end of the fixed pin shaft, a second electric telescopic cylinder with its telescopic end facing upward is installed at the middle of the top surface of the cross bottom plate, and a cross top plate is fixedly arranged at the end of the telescopic rod of the second electric telescopic cylinder;

[0011] A suspended satellite receiver is arranged above the cross top plate, the cross top plate is connected with the satellite receiver through a clamping mechanism, and a hemispherical antenna with an opening facing upward is fixedly arranged in the middle of the top surface of the satellite receiver.

[0012] Preferably, the hinge mechanism comprises a fixed connecting plate, a first swing arm, and a second swing arm, and the front and rear side surfaces of the lifting plate are hingedly provided with two pairs of hinged connecting rods cross-distributed in an "X" shape, and a pair of fixed connecting plates are fixedly provided on the front and rear sides of the bottom surface of the fixed plate;

[0013] Each of the fixed connecting plates is hingedly provided with a first swing arm at both corners, and the bottom end of each of the first swing arms is movably hinged to the top end of the hinged connecting rod on the adjacent side; two pairs of second swing arms are hingedly provided on the front and rear side surfaces of the U-shaped plate, and the top end of each of the second swing arms is movably hinged to the bottom end of the hinged connecting rod on the adjacent side.

[0014] Preferably, a first electric telescopic cylinder with its telescopic end facing upward is installed in the middle of the inner top wall of the U-shaped plate, and the end of the telescopic rod of the first electric telescopic cylinder slides through the U-shaped plate and is fixedly connected to the middle of the lifting plate;

[0015] The four corners of the lifting plate are all provided with fixed sliding holes, each of the fixed sliding holes is inserted with a fixed sliding rod that slides through, and the top end of each fixed sliding rod is fixedly connected to the bottom surface of the fixed plate.

[0016] Preferably, the limiting mechanism comprises a second trapezoidal slider and a first trapezoidal slider, a spherical block suspended in the opening of the second semicircular bracket is provided, four through-distributed limiting slide grooves are provided on the outer surface of the spherical block, a second trapezoidal slider is fixed at the bottom end of the fixed pin shaft, and the second trapezoidal slider slides left and right to engage in the adjacent limiting slide grooves;

[0017] A positioning seat is fixedly arranged in the middle of the top surface of the fixing plate, and a first trapezoidal sliding block is fixedly arranged in the middle of the top surface of the positioning seat. The first trapezoidal sliding block is slidably engaged in the adjacent limiting sliding groove.

[0018] Preferably, a pair of first pins are fixedly disposed at both ends of the first semicircular bracket, and the outer end of each of the first pins is rotatably inserted into the corresponding first ear seat;

[0019] A first side plate is fixedly disposed on the front side of the fixing plate, a first through hole is formed on the top of the first side plate, a first motor is installed inside the first through hole, and a motor shaft end of the first motor is fixedly connected to a first pin shaft on an adjacent side.

[0020] Preferably, a pair of second pins are fixedly disposed at both ends of the second semicircular bracket, and the outer end of each second pin is rotatably inserted into the corresponding second ear seat;

[0021] A second side plate is fixedly disposed on the right side of the fixing plate, a second through hole is formed on the top of the second side plate, a second motor is installed inside the second through hole, and a motor shaft end of the second motor is fixedly connected to a second pin shaft on an adjacent side.

[0022] Preferably, four evenly distributed I-shaped slide rails are fixed on the top surface of the cross top plate, a U-shaped slider is slidably engaged in the middle of each I-shaped slide rail, and an L-shaped slide plate with an opening facing downward is fixed on the top surface of each U-shaped slider.

[0023] Preferably, the clamping mechanism includes an L-shaped connecting plate and a limit pin shaft. A pair of limit pin holes are opened in the middle of the four sides of the satellite receiver. An L-shaped connecting plate with an opening facing upward is fixed on the top surface of each L-shaped slide plate. A pair of limit pin shafts are fixed on the top of the inner side surface of each L-shaped connecting plate. The outer end portion of each limit pin shaft is slidably inserted in the corresponding limit pin hole.

[0024] Preferably, U-shaped ear seats are fixed at the four corners of the top surface of the cross bottom plate, a U-shaped notch is opened at the bottom of each L-shaped slide plate, a hinged connecting plate is hingedly provided inside each U-shaped notch, and the bottom end portion of each hinged connecting plate is hingedly engaged in the opening of the U-shaped ear seat on the adjacent side.

[0025] The present invention also proposes a method for using a ship signal receiving device, comprising the following steps:

[0026] Step 1: When installing the hemispherical antenna, place the satellite receiver in the center on the top surface of the four L-shaped connecting plates. Under the driving action of the second electric telescopic cylinder, the cross top plate is driven to rise. Under the hinged action of the hinged connecting plate, the U-shaped ear seat and the U-shaped notch, the L-shaped slide plate and the U-shaped slide block are driven to slide inward along the I-shaped slide rail, and the limit pin shaft is driven to be inserted into the corresponding limit pin hole, so as to form a fixed installation of the satellite receiver and the hemispherical antenna;

[0027] Step 2: When the hemispherical antenna is raised and adjusted, the lifting plate is driven to rise under the driving action of the first electric telescopic cylinder, and a multi-link telescopic frame is formed under the articulation action of the articulated connecting rod and the first swing arm and the second swing arm, which drives the fixed plate, the cross bottom plate, the cross top plate, the satellite receiver, and the hemispherical antenna to further rise, and simultaneously drives the fixed slide bar to slide upward along the fixed slide hole, so that the satellite receiver and the hemispherical antenna are raised to a suitable position;

[0028] Step 3: When the hemispherical antenna swings left and right, under the driving action of the first motor, the motor shaft of the first motor drives the first pin shaft and the first semicircular bracket to rotate along the first ear seat, and drives the second trapezoidal slider to slide along the limiting slide groove, and simultaneously drives the fixed pin shaft to slide along the second flat pin hole, thereby driving the cross bottom plate, the cross top plate, the satellite receiver, and the hemispherical antenna to swing left and right;

[0029] Step four, when the hemispherical antenna swings back and forth, under the driving action of the second motor, the motor shaft of the second motor drives the second pin shaft and the second semicircular bracket to rotate along the second ear seat, and drives the second trapezoidal slider and the spherical block to slide along the first trapezoidal slider, and simultaneously drives the fixed pin shaft to slide along the first flat pin hole, thereby driving the cross bottom plate, the cross top plate, the satellite receiver, and the hemispherical antenna to swing back and forth for adjustment.

[0030] Compared with the prior art, the present invention has the following beneficial effects:

[0031] 1. In the present invention, when installing a satellite receiver and a hemispherical antenna, the installation process can be simplified. The installer only needs to place the device in a suitable position and then fix it through a clamping mechanism, without the need for complicated welding or drilling operations;

[0032] Satellite receivers and hemispherical antennas of different models and sizes can be fixed by a suitable clamping mechanism. There are many precise electronic components inside the satellite receivers and hemispherical antennas. A stable installation environment can prevent these components from loosening and being damaged due to vibration.

[0033] 2. In the present invention, different satellites are located at different orbital heights and angles, and the lifting antenna can conveniently adjust the antenna to point to satellites in different orbits; by lifting the antenna to a suitable height, the signals of satellites in different orbits can be flexibly switched to be received according to actual needs, thereby improving the adaptability of the device to different satellite systems; when the satellite receiver and the hemispherical antenna are lifted to a suitable height, a certain space will be formed below them, which is convenient for maintenance personnel to operate;

[0034] 3. In the present invention, after the satellite receiver and the hemispherical antenna are installed on the ship, shaking, tilting, etc. may occur during movement or operation. The multi-directional swing adjustment of the limit mechanism can compensate for these changes, so that the antenna always remains in a suitable signal receiving position; the satellite antenna installed on the ship can continuously adjust the antenna position through the limit mechanism as the ship shakes in the waves, thereby ensuring stable signal reception during the navigation of the ship. BRIEF DESCRIPTION OF THE DRAWINGS

[0035] The drawings described herein are used to provide a further understanding of the present invention and constitute a part of this application. The exemplary embodiments of the present invention and their descriptions are used to explain the present invention and do not constitute an improper limitation of the present invention. In the drawings:

[0036] Figure 1 It is a schematic diagram of the overall structure of the present invention;

[0037] Figure 2 It is a schematic diagram of the structure of the base, U-shaped plate, lifting plate and fixed plate of the present invention;

[0038] Figure 3 It is an exploded schematic diagram of the base, U-shaped plate, lifting plate and fixed plate structure of the present invention;

[0039] Figure 4 It is a schematic diagram of the structure of the fixed plate, spherical block and cross bottom plate of the present invention;

[0040] Figure 5 It is an exploded schematic diagram of the fixed plate, spherical block and cross bottom plate structure of the present invention;

[0041] Figure 6 It is a schematic diagram of the structure of the cross bottom plate and the cross top plate of the present invention;

[0042] Figure 7 It is an exploded schematic diagram of the cross bottom plate and cross top plate structure of the present invention;

[0043] Figure 8 It is a schematic diagram of the structure of a satellite receiver and a hemispherical antenna of the present invention;

[0044] The serial numbers in the figure are: 1, base; 11, U-shaped plate; 12, lifting plate; 13, hinged connecting rod; 14, fixed connecting plate; 15, first swing arm; 16, second swing arm; 17, first electric telescopic cylinder; 18, fixed slide bar; 2, fixed plate; 21, first ear seat; 22, first semicircular bracket; 23, second ear seat; 24, second semicircular bracket; 25, first side plate; 26, first motor; 27, second side plate; 28, first Two motors; 3. Spherical block; 31. Positioning seat; 32. First trapezoidal slider; 33. Second trapezoidal slider; 34. Fixed pin; 35. Cross bottom plate; 36. Second electric telescopic cylinder; 37. U-shaped ear seat; 38. Articulated connecting plate; 4. Cross top plate; 41. I-shaped slide rail; 42. U-shaped slider; 43. L-shaped slide plate; 44. L-shaped connecting plate; 45. Limit pin; 46. Satellite receiver; 47. Hemispherical antenna. DETAILED DESCRIPTION

[0045] 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.

[0046] Embodiment 1: This embodiment provides a ship signal receiving device, see Figure 1-8 Specifically, it comprises a base 1, a U-shaped plate 11 with an opening facing downward is fixedly arranged in the middle of the top surface of the base 1, a lifting plate 12 suspended in the air is arranged above the U-shaped plate 11, and a fixed plate 2 distributed in parallel is arranged above the lifting plate 12, and the lifting plate 12 is connected to the U-shaped plate 11 and the fixed plate 2 through a hinge mechanism;

[0047] A pair of first ear seats 21 are fixedly provided on the front and rear sides of the top surface of the fixing plate 2, a first semicircular bracket 22 with its opening facing downward is hingedly provided between the pair of first ear seats 21, and a first flat pin hole is provided on the first semicircular bracket 22;

[0048] A pair of second ear seats 23 are fixedly provided on the left and right sides of the top surface of the fixing plate 2, a second semicircular bracket 24 with an opening facing downward is hingedly provided between the pair of second ear seats 23, and a second flat pin hole is provided on the second semicircular bracket 24;

[0049] The second semicircular bracket 24 is located in the opening of the first semicircular bracket 22, and a fixed pin shaft 34 is slidably inserted at the overlap between the first flat pin hole and the second flat pin hole, and the bottom end of the fixed pin shaft 34 is connected to the fixed plate 2 through a limiting mechanism;

[0050] A cross bottom plate 35 is fixedly provided at the top end of the fixed pin shaft 34, and a second electric telescopic cylinder 36 with its telescopic end facing upward is installed in the middle of the top surface of the cross bottom plate 35. A cross top plate 4 is fixedly provided at the end of the telescopic rod of the second electric telescopic cylinder 36. Under the driving action of the second electric telescopic cylinder 36, the cross top plate 4 is driven to rise.

[0051] A suspended satellite receiver 46 is provided above the cross top plate 4. The cross top plate 4 is connected to the satellite receiver 46 through a clamping mechanism, and a hemispherical antenna 47 with an opening facing upward is fixed in the middle of the top surface of the satellite receiver 46.

[0052] It can flexibly adjust the direction and angle of signal reception according to different navigation environments and needs, adapt to the diverse signal needs in a changing navigation environment, and adaptively adjust the direction and range of signal reception under different navigation stages and sea conditions to improve navigation efficiency and safety, which is an important requirement.

[0053] Embodiment 2: Based on Embodiment 1, this embodiment further includes:

[0054] In the specific implementation process, Figure 2 and Figure 3As shown, the hinge mechanism includes a fixed connecting plate 14, a first swing arm 15, and a second swing arm 16. The front and rear sides of the lifting plate 12 are hinged with two pairs of hinged connecting rods 13 that are cross-distributed in an "X" shape, and a pair of fixed connecting plates 14 are fixed on the front and rear sides of the bottom of the fixed plate 2.

[0055] First swing arms 15 are hingedly provided at the two corners of each fixed connecting plate 14, and the bottom end of each first swing arm 15 is movably hinged to the top end of the hinged connecting rod 13 on the adjacent side; two pairs of second swing arms 16 are hingedly provided on the front and rear sides of the U-shaped plate 11, and the top end of each second swing arm 16 is movably hinged to the bottom end of the hinged connecting rod 13 on the adjacent side. Under the hinged action of the hinged connecting rod 13 and the first swing arms 15 and the second swing arms 16, a multi-link telescopic frame is formed, which drives the fixed plate 2, the cross bottom plate 35, the cross top plate 4, the satellite receiver 46, and the hemispherical antenna 47 to further rise;

[0056] A first electric telescopic cylinder 17 with its telescopic end facing upward is installed in the middle of the top wall of the U-shaped plate 11. The end of the telescopic rod of the first electric telescopic cylinder 17 slides through the U-shaped plate 11 and is fixed to the middle of the lifting plate 12. Under the driving action of the first electric telescopic cylinder 17, the lifting plate 12 is driven to rise.

[0057] The four corners of the lifting plate 12 are provided with fixed sliding holes, each of which is inserted with a fixed sliding rod 18 that slides through it, and the top end of each fixed sliding rod 18 is fixedly connected to the bottom surface of the fixed plate 2. The fixed sliding rod 18 slides upward along the fixed sliding hole, so that the satellite receiver 46 and the hemispherical antenna 47 are raised to a suitable position;

[0058] The satellite receiver 46 and the hemispherical antenna 47 are raised to a suitable position by the double lifting effect of the articulated mechanism, so as to avoid being blocked by ship obstacles, optimize the receiving angle of the satellite signal, significantly improve the signal strength and quality, and effectively reduce the signal blind area;

[0059] When the satellite receiver 46 and the hemispherical antenna 47 are in a higher position, they can reduce contact with these interference sources, making the signal received by the antenna purer. The height of the satellite receiver 46 and the hemispherical antenna 47 can be flexibly adjusted by lifting the articulated mechanism to adapt to different changes.

[0060] Embodiment 3: Based on Embodiment 2, this embodiment further includes:

[0061] In the specific implementation process, Figure 4 and Figure 5As shown, the limiting mechanism includes a second trapezoidal slider 33 and a first trapezoidal slider 32. A suspended spherical block 3 is provided in the opening of the second semicircular bracket 24. Four through-distributed limiting slots are provided on the outer surface of the spherical block 3. A second trapezoidal slider 33 is fixed at the bottom end of the fixed pin shaft 34. The second trapezoidal slider 33 is slidably engaged in the adjacent limiting slots. The second trapezoidal slider 33 slides along the limiting slots, and synchronously drives the fixed pin shaft 34 to slide along the second flat pin hole, thereby driving the cross bottom plate 35, the cross top plate 4, the satellite receiver 46, and the hemispherical antenna 47 to swing left and right.

[0062] A positioning seat 31 is fixedly provided in the middle of the top surface of the fixing plate 2, and a first trapezoidal slider 32 is fixedly provided in the middle of the top surface of the positioning seat 31. The first trapezoidal slider 32 is slidably engaged in the adjacent limiting slide groove, and the second trapezoidal slider 33 and the spherical block 3 slide along the first trapezoidal slider 32, synchronously driving the fixed pin shaft 34 to slide along the first flat pin hole, thereby driving the cross bottom plate 35, the cross top plate 4, the satellite receiver 46, and the hemispherical antenna 47 to swing forward and backward for adjustment;

[0063] A pair of first pins are fixedly provided at both ends of the first semicircular bracket 22, and the outer end of each first pin is rotatably inserted into the corresponding first ear seat 21; a first side plate 25 is fixedly provided at the front side of the fixed plate 2, and a first through hole is provided at the top of the first side plate 25, and a first motor 26 is installed inside the first through hole, and the motor shaft end of the first motor 26 is fixedly connected to the first pin on the adjacent side, and the motor shaft of the first motor 26 drives the first pin and the first semicircular bracket 22 to rotate along the first ear seat 21;

[0064] A pair of second pins are fixedly provided at both ends of the second semicircular bracket 24, and the outer end of each second pin is rotatably inserted into the corresponding second ear seat 23; a second side plate 27 is fixedly provided on the right side of the fixed plate 2, and a second through hole is provided on the top of the second side plate 27, and a second motor 28 is installed inside the second through hole, and the motor shaft end of the second motor 28 is fixedly connected to the second pin on the adjacent side, and the motor shaft of the second motor 28 drives the second pin and the second semicircular bracket 24 to rotate along the second ear seat 23;

[0065] The reception of satellite signals requires extremely high pointing accuracy of the antenna. The satellite receiver 46 and the hemispherical antenna 47 can be swung forward, backward, left, and right in multiple directions by the limit mechanism, so that the pointing of the antenna can be finely adjusted so that it can be accurately aimed at the satellite.

[0066] Through this multi-directional adjustment, the azimuth and elevation of the antenna can be accurately adjusted to the strongest receiving angle of the target satellite signal, thereby obtaining the clearest and most stable satellite signal. When it is necessary to switch to receive signals from different satellites, the multi-directional swing adjustment function of the limit mechanism becomes particularly important.

[0067] Embodiment 4: Based on Embodiment 3, this embodiment further includes:

[0068] In the specific implementation process, Figure 6 and Figure 7 As shown, four evenly distributed I-shaped slide rails 41 are fixed on the top surface of the cross top plate 4, and a U-shaped slider 42 is slidably engaged in the middle of each I-shaped slide rail 41, and an L-shaped slider 43 with an opening facing downward is fixed on the top surface of each U-shaped slider 42;

[0069] The clamping mechanism includes an L-shaped connecting plate 44 and a limiting pin 45. A pair of limiting pin holes are opened in the middle of the four sides of the satellite receiver 46. An L-shaped connecting plate 44 with an opening facing upward is fixed on the top surface of each L-shaped slide plate 43. A pair of limiting pins 45 are fixed on the top of the inner side of each L-shaped connecting plate 44. The outer end of each limiting pin 45 is slidably inserted into the corresponding limiting pin hole, and the limiting pin 45 is inserted into the corresponding limiting pin hole, so as to form a fixed installation of the satellite receiver 46 and the hemispherical antenna 47.

[0070] U-shaped ear seats 37 are fixedly provided at the four corners of the top surface of the cross bottom plate 35, and a U-shaped notch is provided at the bottom of each L-shaped slide plate 43. A hinged connecting plate 38 is hingedly provided inside each U-shaped notch. The bottom end of each hinged connecting plate 38 is hingedly engaged in the opening of the U-shaped ear seat 37 on the adjacent side. Under the hinged action of the hinged connecting plate 38, the U-shaped ear seat 37 and the U-shaped notch, the L-shaped slide plate 43 and the U-shaped slide block 42 are driven to slide inward along the I-shaped slide rail 41.

[0071] The satellite receiver 46 and the hemispherical antenna 47 need to be precisely aligned with the satellite signal source. Factors such as wind and vibration in the external environment may interfere with their normal operation. Through the use of the clamping mechanism, they can be firmly fixed; in a strong wind environment, the clamping mechanism can prevent the satellite receiver 46 and the hemispherical antenna 47 from shaking. This stability helps to maintain the continuity and accuracy of signal reception and reduce signal interruptions or quality degradation.

[0072] Specifically, the working principle and operation method of the present invention are as follows:

[0073] Step 1: When installing the hemispherical antenna 47, place the satellite receiver 46 in the center on the top surface of the four L-shaped connecting plates 44. Under the driving action of the second electric telescopic cylinder 36, the cross top plate 4 is driven to rise. Under the hinged action of the hinged connecting plate 38, the U-shaped ear seat 37 and the U-shaped notch, the L-shaped slide plate 43 and the U-shaped slide block 42 are driven to slide inward along the I-shaped slide rail 41, and the limit pin shaft 45 is driven to be inserted into the corresponding limit pin hole, so as to form a fixed installation of the satellite receiver 46 and the hemispherical antenna 47.

[0074] Step 2: When the hemispherical antenna 47 is raised and adjusted, the lifting plate 12 is driven to rise under the driving action of the first electric telescopic cylinder 17, and a multi-link telescopic frame is formed under the hinged action of the hinged connecting rod 13 and the first swing arm 15 and the second swing arm 16, which drives the fixed plate 2, the cross bottom plate 35, the cross top plate 4, the satellite receiver 46, and the hemispherical antenna 47 to further rise, and simultaneously drives the fixed slide rod 18 to slide upward along the fixed slide hole, so that the satellite receiver 46 and the hemispherical antenna 47 are raised to a suitable position;

[0075] Step 3: When the hemispherical antenna 47 swings left and right, under the driving action of the first motor 26, the motor shaft of the first motor 26 drives the first pin shaft and the first semicircular bracket 22 to rotate along the first ear seat 21, and drives the second trapezoidal slider 33 to slide along the limiting slide groove, and simultaneously drives the fixed pin shaft 34 to slide along the second flat pin hole, thereby driving the cross bottom plate 35, the cross top plate 4, the satellite receiver 46, and the hemispherical antenna 47 to swing left and right;

[0076] Step 4, when the hemispherical antenna 47 swings back and forth, under the driving action of the second motor 28, the motor shaft of the second motor 28 drives the second pin shaft and the second semicircular bracket 24 to rotate along the second ear seat 23, and drives the second trapezoidal slider 33 and the spherical block 3 to slide along the first trapezoidal slider 32, and simultaneously drives the fixed pin shaft 34 to slide along the first flat pin hole, thereby driving the cross bottom plate 35, the cross top plate 4, the satellite receiver 46, and the hemispherical antenna 47 to swing back and forth for adjustment.

[0077] 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 ship signal receiving device, comprising a base (1), characterized in that: A U-shaped plate (11) with an opening facing downward is fixedly provided in the middle of the top surface of the base (1); a lifting plate (12) suspended in the air is provided above the U-shaped plate (11); a fixed plate (2) arranged in parallel is provided above the lifting plate (12); the lifting plate (12) is connected to the U-shaped plate (11) and the fixed plate (2) via a hinge mechanism; A pair of first ear seats (21) are fixedly provided on the front and rear sides of the top surface of the fixing plate (2), a first semicircular bracket (22) with an opening facing downward is hingedly provided between the pair of first ear seats (21), and a first flat pin hole is provided on the first semicircular bracket (22); A pair of second ear seats (23) are fixedly provided on the left and right sides of the top surface of the fixing plate (2), a second semicircular bracket (24) with an opening facing downward is hingedly provided between the pair of second ear seats (23), and a second flat pin hole is provided on the second semicircular bracket (24); The second semicircular bracket (24) is located in the opening of the first semicircular bracket (22), and a fixed pin shaft (34) is slidably inserted at the overlap between the first flat pin hole and the second flat pin hole, and the bottom end of the fixed pin shaft (34) is connected to the fixed plate (2) through a limiting mechanism; A cross bottom plate (35) is fixedly provided at the top end of the fixed pin shaft (34), a second electric telescopic cylinder (36) with the telescopic end facing upward is installed at the middle of the top surface of the cross bottom plate (35), and a cross top plate (4) is fixedly provided at the end of the telescopic rod of the second electric telescopic cylinder (36); A suspended satellite receiver (46) is provided above the cross top plate (4), the cross top plate (4) is connected to the satellite receiver (46) via a clamping mechanism, and a hemispherical antenna (47) with an opening facing upward is fixedly provided in the middle of the top surface of the satellite receiver (46).

2. A ship signal receiving device according to claim 1, characterized in that: The hinge mechanism comprises a fixed connecting plate (14), a first swing arm (15), and a second swing arm (16); the front and rear side surfaces of the lifting plate (12) are hingedly provided with two pairs of hinged connecting rods (13) cross-distributed in an "X" shape; and a pair of fixed connecting plates (14) are fixedly provided on the front and rear sides of the bottom surface of the fixed plate (2); Each of the fixed connecting plates (14) is hingedly provided with a first swing arm (15) at both corners, and the bottom end of each of the first swing arms (15) is movably hinged to the top end of the hinged connecting rod (13) on the adjacent side; and two pairs of second swing arms (16) are hingedly provided on the front and rear side surfaces of the U-shaped plate (11), and the top end of each of the second swing arms (16) is movably hinged to the bottom end of the hinged connecting rod (13) on the adjacent side.

3. A ship signal receiving device according to claim 2, characterized in that: A first electric telescopic cylinder (17) with its telescopic end facing upward is installed in the middle of the top wall of the U-shaped plate (11); the end of the telescopic rod of the first electric telescopic cylinder (17) slides through the U-shaped plate (11) and is fixedly connected to the middle of the lifting plate (12); The four corners of the lifting plate (12) are provided with fixed sliding holes, each of which is provided with a fixed sliding rod (18) that slides through it, and the top end of each fixed sliding rod (18) is fixedly connected to the bottom surface of the fixed plate (2).

4. A ship signal receiving device according to claim 3, characterized in that: The limiting mechanism comprises a second trapezoidal slider (33) and a first trapezoidal slider (32); a spherical block (3) suspended in the opening of the second semicircular bracket (24); four through-distributed limiting sliding grooves are provided on the outer surface of the spherical block (3); a second trapezoidal slider (33) is fixed at the bottom end of the fixed pin shaft (34); the second trapezoidal slider (33) is slidably engaged in adjacent limiting sliding grooves; A positioning seat (31) is fixedly provided in the middle of the top surface of the fixing plate (2), and a first trapezoidal sliding block (32) is fixedly provided in the middle of the top surface of the positioning seat (31). The first trapezoidal sliding block (32) is slidably engaged in an adjacent limiting sliding groove.

5. A ship signal receiving device according to claim 4, characterized in that: A pair of first pins are fixedly disposed at the two ends of the first semicircular bracket (22), and the outer end of each of the first pins is rotatably inserted into the corresponding first ear seat (21); A first side plate (25) is fixedly provided on the front side of the fixing plate (2), a first through hole is provided on the top of the first side plate (25), a first motor (26) is installed inside the first through hole, and the motor shaft end of the first motor (26) is fixedly connected to the first pin shaft on the adjacent side.

6. A ship signal receiving device according to claim 5, characterized in that: A pair of second pin shafts are fixedly disposed at the two ends of the second semicircular bracket (24), and the outer end of each second pin shaft is rotatably inserted into the corresponding second ear seat (23); A second side plate (27) is fixedly provided on the right side of the fixing plate (2), a second through hole is provided on the top of the second side plate (27), a second motor (28) is installed inside the second through hole, and the motor shaft end of the second motor (28) is fixedly connected to the second pin shaft on the adjacent side.

7. A ship signal receiving device according to claim 6, characterized in that: Four evenly distributed I-shaped slide rails (41) are fixedly arranged on the top surface of the cross top plate (4), a U-shaped slide block (42) is slidably engaged in the middle of each I-shaped slide rail (41), and an L-shaped slide block (43) with an opening facing downward is fixedly arranged on the top surface of each U-shaped slide block (42).

8. A ship signal receiving device according to claim 7, characterized in that: The clamping mechanism comprises an L-shaped connecting plate (44) and a limiting pin shaft (45). A pair of limiting pin holes are provided in the middle of the four side surfaces of the satellite receiver (46). An L-shaped connecting plate (44) with an opening facing upward is fixed on the top surface of each L-shaped sliding plate (43). A pair of limiting pin shafts (45) are fixed on the top of the inner side surface of each L-shaped connecting plate (44). The outer end of each limiting pin shaft (45) is slidably inserted into the corresponding limiting pin hole.

9. A ship signal receiving device according to claim 8, characterized in that: U-shaped ear seats (37) are fixedly arranged at the four corners of the top surface of the cross bottom plate (35), a U-shaped notch is opened at the bottom of each L-shaped slide plate (43), a hinged connecting plate (38) is hingedly arranged inside each U-shaped notch, and the bottom end of each hinged connecting plate (38) is hingedly engaged in the opening of the U-shaped ear seat (37) on the adjacent side.

10. The method for using a ship signal receiving device according to claim 9, characterized in that: The following steps are involved: Step 1: When installing the hemispherical antenna (47), the satellite receiver (46) is placed centrally on the top surface of the four L-shaped connecting plates (44). Under the driving action of the second electric telescopic cylinder (36), the cross top plate (4) is driven to rise. Under the hinged action of the hinged connecting plate (38) and the U-shaped ear seat (37) and the U-shaped notch, the L-shaped slide plate (43) and the U-shaped slide block (42) are driven to slide inward along the I-shaped slide rail (41), and the limit pin shaft (45) is driven to be inserted into the corresponding limit pin hole, so as to form a fixed installation of the satellite receiver (46) and the hemispherical antenna (47); Step 2: When the hemispherical antenna (47) is raised and adjusted, the lifting plate (12) is driven to rise under the driving action of the first electric telescopic cylinder (17), and a multi-link telescopic frame is formed under the hinged action of the hinged connecting rod (13) and the first swing arm (15) and the second swing arm (16), so as to further raise the fixed plate (2), the cross bottom plate (35), the cross top plate (4), the satellite receiver (46), and the hemispherical antenna (47), and synchronously drive the fixed slide rod (18) to slide upward along the fixed slide hole, so that the satellite receiver (46) and the hemispherical antenna (47) are raised to a suitable position; Step 3, when the hemispherical antenna (47) swings left and right, under the driving action of the first motor (26), the motor shaft of the first motor (26) drives the first pin shaft and the first semicircular bracket (22) to rotate along the first ear seat (21), and drives the second trapezoidal slider (33) to slide along the limiting slide groove, and simultaneously drives the fixed pin shaft (34) to slide along the second flat pin hole, thereby driving the cross bottom plate (35), the cross top plate (4), the satellite receiver (46), and the hemispherical antenna (47) to swing left and right; Step 4: When the hemispherical antenna (47) swings back and forth, under the driving action of the second motor (28), the motor shaft of the second motor (28) drives the second pin shaft and the second semicircular bracket (24) to rotate along the second ear seat (23), and drives the second trapezoidal slider (33) and the spherical block (3) to slide along the first trapezoidal slider (32), and simultaneously drives the fixed pin shaft (34) to slide along the first flat pin hole, thereby driving the cross bottom plate (35), the cross top plate (4), the satellite receiver (46), and the hemispherical antenna (47) to swing back and forth for adjustment.

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