Energy-saving rotary air duct mechanism for ship
By designing the driving, vibration damping and stabilizing mechanism in the rotating air duct mechanism for ships, the vibration and wear problems caused by lateral force differentiation of the air duct are solved, and higher rotational stability and efficiency are achieved.
Patent Information
- Application Number
- CN202510069258.5
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-01-16
- Publication Date
- 2025-02-18
- Estimated Expiration
- Not applicable · inactive patent
AI Technical Summary
The existing energy-saving rotary air duct mechanism for ships will cause lateral force differentiation when the rotation angle between the air and the air duct is inconsistent, resulting in vibration and wear of the air duct, which will affect stability and efficiency.
A rotating air duct mechanism including a driving mechanism, a vibration damping mechanism and a stabilizing mechanism are designed. The vibration damping mechanism consumes the energy of the air cylinder vibration through the scrubbing disc. The stabilizing mechanism enhances the rotational stability of the air cylinder through the reinforcement and magnet system, and enhances the stability of the support base through the sliding rod and double inclined plate.
It effectively reduces vibration and wear of the air tube, improves the rotation stability and efficiency of the air tube, and extends the service life of the equipment.
Smart Images

Figure CN119460040A_ABST
Abstract
Description
Technical Field
[0001] The invention relates to the technical field of rotary sails, in particular to an energy-saving rotary wind cylinder mechanism for ships. Background Art
[0002] The rotor sail is a new type of wind-assisted propulsion device installed on ships. It mainly uses wind energy to provide additional propulsion power for ships and is an efficient, environmentally friendly ship energy-saving device.
[0003] The existing energy-saving rotating wind tube mechanism for ships has the following problems: 1. When the angle of rotation of the wind and the wind tube is not in the same direction but at an angle, the lateral force will be differentiated. One part of the force will push the ship forward, while another part of the force will move outward and be lost, while another part will act on the wind tube. At this time, the wind tube under force will produce certain vibrations; 2. When the wind tube vibrates or shakes, the connection point between the rotating wind tube and the deck will be worn, as well as vibrate and shake accordingly. Summary of the invention
[0004] The present invention provides an energy-saving rotating wind tube mechanism for ships to solve the problems raised in the above-mentioned background technology.
[0005] To achieve the above-mentioned object, the present invention provides the following technical solutions: An energy-saving rotating wind tube mechanism for a ship comprises a driving mechanism, which is used for operating the device and maintaining its stable operation; A vibration reduction mechanism, which is used for vibration reduction of a rotating wind cylinder; A stabilizing mechanism, which is used to reinforce the stability between the splint and the device; The vibration reduction mechanism is arranged inside the driving mechanism, the outer side of the driving mechanism is fixedly connected with an inner plate, the outer side of the inner plate is fixedly connected with a support seat, the top of the inner plate and the inner side of the support seat are fixedly connected with a rib plate, and the stabilizing mechanism is fixedly installed on the outer side of the support seat; The driving mechanism includes a servo motor, which is fixedly installed on the bottom of the inner board. The top of the inner board is fixedly connected to a pillar. The outer side of the pillar is fixedly connected to the rib plate. The inner side of the pillar is extruded with a No. 1 bearing. The side of the No. 1 bearing away from the pillar is extruded with a wind tube, and a reinforcement component is arranged inside the wind tube.
[0006] Preferably, the reinforcement assembly includes a connecting plate, which is fixedly installed inside the wind tube, and the side of the connecting plate away from the wind tube is connected to the output end of the servo motor, the outer side of the output end of the servo motor is fixedly connected with an adapter sleeve, the outer side of the adapter sleeve is fixedly connected with a reinforcement rod, the top of the adapter sleeve is fixedly installed with a hydraulic rod, and the top of the hydraulic rod is fixedly connected with a curved bending rod.
[0007] Preferably, the outer side of the curved bending rod is extruded and adapted with a reinforcement piece, the outer side of the reinforcement piece is sleeved with a suspension plate, the bottom of the suspension plate is fixedly connected with a frame rod, the bottom end of the frame rod is fixedly connected to the top of the adapter sleeve, the interior of the suspension plate is fixedly connected with a No. 1 magnet, a No. 2 magnet is provided at the end of the No. 1 magnet away from the suspension plate, the end of the No. 2 magnet away from the No. 1 magnet is fixedly connected to the reinforcement piece, the upper and lower sides of the suspension plate are provided with top grooves, the internal sliding adaptation of the top groove is provided with a resistance rod, and the end of the resistance rod away from the top groove is fixedly connected to the reinforcement piece.
[0008] Preferably, the interior of the curved bending rod is connected to an electric push rod through a No. 2 bearing, the top of the electric push rod is fixedly connected to a hole block, the interior of the hole block is fixedly connected to a No. 1 magnetic block, slots are provided at the top and inside of the hole block, a magnetic blocking plate is provided above the slot, the top of the magnetic blocking plate is fixedly connected to a top sheet, the center of the bottom of the top sheet is fixedly connected to a reset spring, and the bottom end of the reset spring is fixedly connected to the top of the hole block.
[0009] Preferably, the vibration reduction mechanism includes a rotating sleeve, which is rotatably installed on the top of the wind tube, and the bottom of the rotating sleeve is respectively fixedly connected with a fixed head and an elastic telescopic rod, the bottom end of the elastic telescopic rod is fixedly connected with a stabilizing plate, and the inside of the stabilizing plate is fixedly connected with a sleeve rod.
[0010] Preferably, a spring is fixedly connected to the inside of the sleeve rod, an end of the spring away from the sleeve rod is fixedly connected to an insertion rod, the insertion rod is slidably adapted inside the sleeve rod, an end of the insertion rod away from the spring is fixedly connected to a No. 2 magnetic block, side grooves are provided on the upper and lower sides of the insertion rod, a limit rod is slidably adapted inside the side groove, and an end of the limit rod away from the side groove is fixedly connected to the stabilizing plate.
[0011] Preferably, the stabilizing mechanism includes a straight slot hole, which is opened on the outer side of the support seat, and the inner sliding adapter of the straight slot hole is equipped with a sliding rod, the outer end of the sliding rod is fixedly connected with a double inclined plate, the top of the double inclined plate is fixedly connected with a double-headed fillet strip, and the end of the double-headed fillet strip away from the double inclined plate is embedded with the rib plate.
[0012] Preferably, a stabilizing platform is provided directly below the double inclined plates, and the stabilizing platform is fixedly installed on the outer side of the support seat. Reinforcement platforms are inserted at both ends of the stabilizing platform, and the top of the reinforcement platform is squeezed and adapted to the bottom of the double inclined plates. A perforation is opened on the outer side of the reinforcement platform, and a compensation plate is fixedly connected to the end of the reinforcement platform away from the double inclined plates.
[0013] Preferably, the inner side of the compensation plate is extruded and adapted to be equipped with an inner connecting rod, which is inserted through the outer side of the support seat and extends into the interior thereof, and the top and bottom of the inner connecting rod are both inserted with receiving and attachment plates, and a No. 3 magnetic block is fixedly connected to the side of the receiving and attachment plate away from the inner connecting rod, and a blocking plate is provided at one end of the No. 3 magnetic block away from the receiving and attachment plate, and a ring support is rotatably installed on the top of the blocking plate, and the ring support is fixedly connected to the inside of the support seat.
[0014] Preferably, one end of the inner connecting rod away from the compensation plate is fixedly connected to the end panel, and the inner side of the end panel is respectively fixedly connected to a compression spring and a short rod, one end of the compression spring away from the end panel is fixedly connected to the inner side of the support seat, and one end of the short rod away from the end panel is fixedly connected to a No. 4 magnetic block.
[0015] Compared with the prior art, the present invention has the following beneficial effects: 1. Move the reinforcement piece outward along the inner wall of the suspended plate until it is in close contact with the inner wall of the wind tube. The reinforcement piece is arranged at the center of the inner cavity of the wind tube, so it can balance the force of the overall rotation of the wind tube, and at the same time increase the force that keeps the wind tube connected to the bottom during the rotation process, thereby increasing the rotation stability of the wind tube.
[0016] 2. When the air duct vibrates, the stabilizing plate repeatedly moves up and down inside it, which can change the vibration characteristics of the air duct to a certain extent. From an energy perspective, the movement of the stabilizing plate can consume the energy of the air duct vibration. When the air duct vibrates, the air inside it will vibrate with the air duct, generating fluctuations. The up and down movement of the stabilizing plate will interact with these fluctuations and consume the vibration energy through damping.
[0017] 3. Move the sliding rod downward along the straight slot hole so that the double inclined plate connected to the outer end of the sliding rod will be inserted from the top of the stabilizing platform, wherein the top of the double inclined plate is connected to the double-headed molding, so the other end of the double-headed molding will be embedded and squeezed with the rib plate, thereby increasing the connection between the stabilizing platform and the rib plate, and strengthening the stabilizing effect on the support seat.
[0018] 4. By extending the attached sheet outward from the inner connecting rod and clinging to the outer side of the reinforcement platform, the connection between the reinforcement platform and the support seat will be greatly improved, thereby increasing the contact area between the stabilization platform and the support seat and strengthening the stability of the support seat. BRIEF DESCRIPTION OF THE DRAWINGS
[0019] Figure 1 The figure is a schematic diagram of the external structure of the energy-saving rotating wind tube mechanism for ships of the present invention.
[0020] Figure 2 It is a schematic diagram of the overall cross-sectional structure of the present invention.
[0021] Figure 3 It is a schematic cross-sectional structural diagram of the driving mechanism of the present invention.
[0022] Figure 4 It is a schematic diagram of the full cross-section structure of the reinforcement component of the present invention.
[0023] Figure 5 It is a schematic cross-sectional structural diagram of some components of the reinforcement assembly of the present invention.
[0024] Figure 6 For the present invention Figure 5 Schematic diagram of the enlarged structure at point A in the middle.
[0025] Figure 7 For the present invention Figure 5 Schematic diagram of the enlarged structure at point B in the middle.
[0026] Figure 8 It is a schematic diagram of the full cross-section structure of the vibration reduction mechanism of the present invention.
[0027] Fig. 9 For the present invention Figure 8 Schematic diagram of the enlarged structure at point C in the middle.
[0028] Fig.10 It is a structural schematic diagram of the stabilizing mechanism of the present invention.
[0029] Fig.11 It is a schematic diagram of the full cross-section structure of the stabilizing mechanism of the present invention.
[0030] Fig.12 It is a schematic diagram of the vertical section structure of some components of the stabilizing mechanism of the present invention.
[0031] Fig.13 It is a schematic cross-sectional structural diagram of some components of the stabilizing mechanism of the present invention.
[0032] Fig.14 For the present invention Fig.13 Schematic diagram of the enlarged structure at D in the middle.
[0033] In the figure: 1, support seat; 2, inner plate; 3, rib plate; 4, driving mechanism; 5, vibration reduction mechanism; 6, stabilizing mechanism; 41, servo motor; 42, pillar; 43, bearing No. 1; 44, air duct; 45, reinforcement assembly; 451, connecting plate; 452, adapter sleeve; 453, reinforcement rod; 454, hydraulic rod; 455, curved bending rod; 456, reinforcement member; 457, suspended plate; 458, frame rod; 459, magnet No. 1; 450, magnet No. 2; 4501, top slot; 4502, resistance rod; 4503, electric push rod; 4504, hole block; 4505, magnet No. 1; 4506, slot; 4507 , magnetic blocking plate; 4508, top plate; 4509, return spring; 51, fixed head; 52, elastic telescopic rod; 53, stabilizing plate; 54, sleeve rod; 55, spring; 56, plug rod; 57, side groove; 58, limit rod; 59, No. 2 magnetic block; 50, rotating sleeve; 61, straight slot hole; 62, sliding rod; 63, double inclined plate; 64, double-headed insert; 65, stabilizing table; 66, reinforcement table; 67, perforation; 68, compensation plate; 69, inner connecting rod; 60, receiving and attaching plate; 601, No. 3 magnetic block; 602, compression spring; 603, end panel; 604, short rod; 605, No. 4 magnetic block; 606, ring support; 607, blocking plate. DETAILED DESCRIPTION
[0034] The present invention is further described below in conjunction with the accompanying drawings and specific implementation methods. It should be noted that, under the premise of no conflict, the various embodiments or technical features described below can be arbitrarily combined to form a new embodiment. It should be noted that the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative work are within the scope of protection of the present invention.
[0035] See also Figures 1 to 14 The present invention provides a technical solution: Figure 1 , Figure 2 , Figure 3 , Figure 4 , Figure 5 , Figure 6 and Figure 7 As shown, it includes a driving mechanism 4, which is used for the operation of the device and maintaining its stable operation; A vibration reduction mechanism 5, which is used for vibration reduction of the rotating wind tube; A stabilizing mechanism 6, which is used to reinforce the stability between the splint and the device; The vibration reduction mechanism 5 is arranged inside the driving mechanism 4, the outer side of the driving mechanism 4 is fixedly connected with the inner plate 2, the outer side of the inner plate 2 is fixedly connected with the support seat 1, the top of the inner plate 2 and the inner side of the support seat 1 are fixedly connected with the rib plate 3, and the stabilizing mechanism 6 is fixedly installed on the outer side of the support seat 1.
[0036] The driving mechanism 4 includes a servo motor 41, which is fixedly mounted on the bottom of the inner saddle board 2, and a pillar 42 is fixedly connected to the top of the inner saddle board 2. The outer side of the pillar 42 is fixedly connected to the rib plate 3, and the inner side of the pillar 42 is extruded and adapted with a No. 1 bearing 43, and the side of the No. 1 bearing 43 away from the pillar 42 is extruded and adapted with a wind tube 44, and a reinforcement component 45 is arranged inside the wind tube 44. By starting the servo motor 41, the connecting plate 451 connected to the outer side of the output end thereof will drive the wind tube 44 to rotate, wherein the outer side of the wind tube 44 is extruded and adapted with the No. 1 bearing 43, and the other side of the No. 1 bearing 43 is extruded and adapted with the pillar 42, so the wind tube 44 will rotate in the pillar 42, and the wind tube 44 will produce a Magnus effect during the rotation process. When the wind tube 44 moves in the flowing air, wherein the flowing air is referred to as fluid, the fluid velocity distribution on the surface of the wind tube 44 is uneven. Due to the rotation of the wind tube 44, the air flow speed on one side is consistent with and adds to the rotation speed of the rotor, while the air flow speed on the other side is opposite and subtracts, resulting in different pressures on both sides. This pressure difference will generate a lateral force perpendicular to the incoming flow direction and the rotation axis direction of the wind tube 44. In addition, in ship applications, a component of this lateral force can be converted into power to propel the ship forward.
[0037] The reinforcement component 45 includes a connecting plate 451, which is fixedly installed inside the wind tube 44. The side of the connecting plate 451 away from the wind tube 44 is connected to the output end of the servo motor 41. The outer side of the output end of the servo motor 41 is fixedly connected with an adapter sleeve 452, and the outer side of the adapter sleeve 452 is fixedly connected with a reinforcement rod 453. The top of the adapter sleeve 452 is fixedly installed with a hydraulic rod 454, and the top of the hydraulic rod 454 is fixedly connected with a curved curved rod 455. The outer side of the curved curved rod 455 is extruded and adapted with a reinforcement piece 456, and the outer side of the reinforcement piece 456 is sleeved with a suspended plate 457. By starting the hydraulic rod 454, the curved curved rod 455 connected to the top thereof will move upward and squeeze the reinforcement piece 456 outward, wherein the contact surfaces between the curved curved rod 455 and the reinforcement piece 456 are both inclined surfaces. At this time, the reinforcement piece 456 will move outward along the inner wall of the suspended plate 457 until it is in contact with the wind tube. The inner walls of the cylinder 44 are tightly attached, and the reinforcement 456 is arranged at the central part of the inner cavity of the wind cylinder 44, so it will play a role in balancing the overall rotation of the wind cylinder 44, and at the same time increase a force that keeps the wind cylinder 44 connected to the bottom during rotation, thereby increasing the rotation stability of the wind cylinder 44, the bottom of the suspension plate 457 is fixedly connected with a frame rod 458, the bottom end of the frame rod 458 is fixedly connected to the top of the adapter sleeve 452, the interior of the suspension plate 457 is fixedly connected with a No. 1 magnet 459, the end of the No. 1 magnet 459 away from the suspension plate 457 is provided with a No. 2 magnet 450, and the end of the No. 2 magnet 450 away from the No. 1 magnet 459 is fixedly connected to the reinforcement 456, and the upper and lower sides of the suspension plate 457 are provided with top grooves 4501, the internal sliding adapter of the top groove 4501 is equipped with a resistance rod 4502, and the end of the resistance rod 4502 away from the top groove 4501 is fixedly connected to the reinforcement 456. The interior of the reinforcement 456 is fixedly connected with the second magnet 450, and the interior of the suspension plate 457 is fixedly connected with the first magnet 459, and the two magnets maintain an attractive relationship, so the two magnets play a role in resetting the reinforcement 456. In addition, as the reinforcement 456 moves outward, the resistance rod 4502 connected thereto will move outward along the top groove 4501, and a triangle-like state is formed between the resistance rod 4502 and the reinforcement 456, thereby increasing the stability between the reinforcement 456 and the wind tube 44.
[0038] The interior of the curved bending rod 455 is connected to an electric push rod 4503 through a No. 2 bearing, the top of the electric push rod 4503 is fixedly connected to a hole block 4504, the interior of the hole block 4504 is fixedly connected to a No. 1 magnetic block 4505, slots 4506 are provided on the top and inside of the hole block 4504, a magnetic blocking plate 4507 is provided above the slot 4506, the top of the magnetic blocking plate 4507 is fixedly connected to a top plate 4508, the center of the bottom of the top plate 4508 is fixedly connected to a return spring 4509, and the bottom end of the return spring 4509 is fixedly connected to the top of the hole block 4504. By extending the electric push rod 4503 to the longest distance, the top plate 4508 will be squeezed downward by the fixed head 51, and the fixed head 51 will compress the return spring 4509, wherein the return spring 4509 has a slow recovery speed and plays a role in resetting the fixed head 51, and then the magnetic blocking plate 4507 connected to the bottom of the fixed head 51 will be inserted into the opening block 4504 along the slot 4506, and then the magnetic blocking plate 4507 will separate the first magnetic block 4505 from the second magnetic block 59 and block the magnetism. At this time, under the compression force of the spring 55, the insertion rod 56 will be retracted into the sleeve rod 54, and then the electric push rod 4503 will be retracted to return the device to its original position.
[0039] like Figure 8 and Fig. 9As shown, the vibration reduction mechanism 5 includes a rotating sleeve 50, which is rotatably mounted on the top of the air duct 44, and the bottom of the rotating sleeve 50 is fixedly connected to a fixed head 51 and an elastic telescopic rod 52, respectively, and the bottom end of the elastic telescopic rod 52 is fixedly connected to a stabilizing plate 53. When the air duct 44 is affected by wind and vibrates, the electric push rod 4503 is started, and the hole block 4504 connected to the top of the electric push rod 4503 will move upward until the hole block 4504 moves to a position flush with the insertion rod 56, wherein the inside of the hole block 4504 is fixedly connected to the first magnetic block 4505, and the outer end of the insertion rod 56 is connected to the second magnetic block 59. , and the two magnetic blocks are mutually attracted, so the insertion rod 56 will move outward along the inner wall of the sleeve rod 54 and stretch the spring 55, wherein the spring 55 plays a role in resetting the insertion rod 56 until it is inserted into the inside of the opening block 4504, and finally the electric push rod 4503 will be indirectly connected with the stabilizing plate 53. Therefore, when the electric push rod 4503 is extended and retracted up and down, the stabilizing plate 53 will periodically move up and down along the inner wall of the wind tube 44, and compress and stretch the elastic telescopic rod 52. When the wind tube 44 vibrates, the stabilizing plate 53 moves up and down repeatedly inside it, which can change the vibration characteristics of the wind tube 44 to a certain extent. From the perspective of energy, the movement of the stabilizing plate 53 can consume the energy of the vibration of the wind tube 44. When the wind tube 44 vibrates, the air inside it will vibrate with the wind tube 44, generating fluctuations. The up and down movement of the stabilizing plate 53 will interact with these fluctuations and consume the vibration energy through damping. The stabilizing plate 53 is fixedly connected to a sleeve rod 54 inside, and a spring 55 is fixedly connected to the sleeve rod 54. The end of the spring 55 away from the sleeve rod 54 is fixedly connected to an insertion rod 56. The insertion rod 56 is slidably adapted inside the sleeve rod 54, and the end of the insertion rod 56 away from the spring 55 is fixedly connected to a No. 2 magnetic block 59. Side grooves 57 are provided on the upper and lower sides of the insertion rod 56. The inside of the side groove 57 is slidably adapted to a limit rod 58, and the end of the limit rod 58 away from the side groove 57 is fixedly connected to the stabilizing plate 53.
[0040] like Fig.10 , Fig.11 , Fig.12 , Fig.13 and Fig.14As shown, the stabilizing mechanism 6 includes a straight slot hole 61, which is opened on the outer side of the support seat 1. The inner sliding adapter of the straight slot hole 61 is equipped with a sliding rod 62. The outer end of the sliding rod 62 is fixedly connected to a double inclined plate 63. The top of the double inclined plate 63 is fixedly connected to a double-headed fillet 64. The end of the double-headed fillet 64 away from the double inclined plate 63 is engaged with the rib plate 3. A stabilizing platform 65 is arranged directly below the double inclined plate 63. During the operation of the wind tube 44, the No. 1 bearing 43 connected to the bottom end thereof and the indirectly connected pillar 42 will both shake or vibrate. The outer side of the pillar 42 is fixedly connected to the support seat 1 through the rib plate 3. Therefore, the part where the support seat 1 is connected to the deck will tear and vibrate. When the sliding rod 62 is moved downward along the straight groove hole 61, the double inclined plate 63 connected to the outer end of the sliding rod 62 will be inserted from the top of the stabilizing platform 65, wherein the top of the double inclined plate 63 is connected to the double-headed fillet 64, so the other end of the double-headed fillet 64 will be embedded and squeezed to fit with the rib plate 3, thereby increasing the connection between the stabilizing platform 65 and the rib plate 3, and strengthening the stabilizing effect on the support seat 1. The stabilizing platform 65 is fixedly installed on the outer side of the support seat 1, and both ends of the stabilizing platform 65 are inserted with reinforcement platforms 66. The top of the reinforcement platform 66 is squeezed and fit with the bottom of the double inclined plate 63, and the outer side of the reinforcement platform 66 is provided with a through hole 67. The end of the reinforcement platform 66 away from the double inclined plate 63 is fixedly connected with a compensation plate 68. In addition, as the double inclined plate 63 is inserted into the interior of the stabilizing platform 65, it will squeeze the reinforcement platform 66 arranged inside the stabilizing platform 65 outward, wherein the contact surfaces between the double inclined plate 63 and the stabilizing platform 65 are both inclined surfaces, and then the reinforcement platform 66 will extend from both ends of the stabilizing platform 65 respectively, and at the same time, the through hole 67 opened on the surface of the reinforcement platform 66 will move to a position overlapping with the inner connecting rod 69, and then the inner connecting rod 69 will pass through the support seat 1 and the through hole 67 in sequence under the compression force of the compression spring 602 until it passes through the other side of the reinforcement platform 66, wherein the inner connecting rod 69 is initially squeezed against the inner side of the compensation plate 68 under the compression force of the compression spring 602.
[0041] The inner side of the compensation plate 68 is extruded and adapted with an inner connecting rod 69, which is inserted into the outer side of the support seat 1 and extends into the interior thereof, and the top and bottom of the inner connecting rod 69 are both inserted with a receiving and attaching sheet 60, and the side of the receiving and attaching sheet 60 away from the inner connecting rod 69 is fixedly connected with a No. 3 magnetic block 601, and the end of the No. 3 magnetic block 601 away from the receiving and attaching sheet 60 is provided with a blocking plate 607, and the top of the blocking plate 607 is rotatably installed with a ring support 606, and the ring support 606 is fixedly connected to the inside of the support seat 1, and the end of the inner connecting rod 69 away from the compensation plate 68 is fixedly connected to the end panel 603, and the inner side of the end panel 603 is respectively fixedly connected with a compression spring 602 and a short rod 604, and the end of the compression spring 602 away from the end panel 603 is fixedly connected to the inner side of the support seat 1, and the end of the short rod 604 away from the end panel 603 is fixedly connected to the No. 4 magnetic block 605. In addition, the inner end of the inner connecting rod 69 is connected to the end panel 603, and the outer side of the end panel 603 is connected to the short rod 604. Therefore, after the inner connecting rod 69 passes outward, the short rod 604 will move outward immediately thereafter. At this time, the short rod 604 will first hit the blocking plate 607 outward, and the blocked plate 607 hit will deflect upward with the ring support 606 as the fulcrum, and then the short rod 604 will pass over the blocking plate 607 and extend outward from the support seat 1, wherein the outer end of the short rod 604 is connected to the fourth magnetic block 605. The inner connecting rod 69 is connected, and the upper and lower sides of the inner connecting rod 69 are both inserted with the collecting and attaching pieces 60, and the side of the collecting and attaching piece 60 away from the inner connecting rod 69 is fixedly connected with the third magnetic block 601, wherein the third magnetic block 601 and the fourth magnetic block 605 are mutually attracted, so the collecting and attaching piece 60 will extend outward from the inner connecting rod 69 and closely adhere to the outer side of the reinforcing platform 66. At this time, the connection relationship between the reinforcing platform 66 and the support seat 1 will be greatly improved, thereby increasing the contact area between the stabilizing platform 65 and the support seat 1, and strengthening the stability of the support seat 1.
[0042] When the present invention is used: first, the servo motor 41 is started, so that the connecting plate 451 connected to the outer side of the output end thereof will drive the wind tube 44 to rotate, wherein the outer side of the wind tube 44 is squeezed and adapted with the No. 1 bearing 43, and the other side of the No. 1 bearing 43 is squeezed and adapted with the pillar 42, so the wind tube 44 will rotate inside the pillar 42, and the wind tube 44 will produce a Magnus effect during the rotation process. When the wind tube 44 moves in the flowing air, wherein the flowing air is referred to as the fluid, the fluid velocity distribution on the surface of the wind tube 44 is uneven. Due to the rotation of the wind tube 44, the air flow velocity on one side is consistent with the rotation velocity of the rotor and is added, while the other side is opposite and subtracted, resulting in different pressures on both sides. This pressure difference will generate a lateral force perpendicular to the incoming flow direction and the direction of the rotation axis of the wind tube 44. In ship applications, through reasonable design and installation angles, a component of this lateral force is converted into a driving force to propel the ship forward.
[0043] By starting the hydraulic rod 454, the curved bent rod 455 connected to the top thereof will move upward and squeeze the reinforcement 456 outward, and the reinforcement 456 will move outward along the inner wall of the suspension disk 457 until it is tightly attached to the inner wall of the wind tube 44. At this time, the reinforcement 456 will reinforce the wind tube 44 as a whole, wherein the interior of the reinforcement 456 is fixedly connected with the second magnet 450, and the interior of the suspension disk 457 is fixedly connected with the first magnet 459, and the two magnets maintain an attractive relationship. In addition, as the reinforcement 456 moves outward, the resistance rod 4502 connected thereto will move outward along the top groove 4501. When the air duct 44 is affected by the wind and vibrates, the electric push rod 4503 is started, and the hole block 4504 connected to the top of the electric push rod 4503 will move upward until the hole block 4504 moves to a position level with the insertion rod 56, wherein the interior of the hole block 4504 is fixedly connected with the No. 1 magnetic block 4505, and the outer end of the insertion rod 56 is connected to the No. 2 magnetic block 59, and the two magnetic blocks are attracted to each other, so the insertion rod 56 will move outward along the inner wall of the sleeve rod 54 and stretch the spring 55 until it is inserted into the interior of the hole block 4504, and finally the electric push rod 4503 will be indirectly connected to the stabilizing plate 53. Therefore, when the electric push rod 4503 is extended and retracted up and down, the stabilizing plate 53 will periodically move up and down along the inner wall of the air duct 44 and compress and stretch the elastic telescopic rod 52.
[0044] During the operation of the air duct 44, the No. 1 bearing 43 connected to its bottom end and the indirectly connected pillar 42 will shake or vibrate, wherein the outer side of the pillar 42 is fixedly connected to the support seat 1 through the rib plate 3, so the part where the support seat 1 is connected to the deck will tear and vibrate, and then the sliding rod 62 is moved downward along the straight slot hole 61, so that the double inclined plate 63 connected to the outer end of the sliding rod 62 will be inserted from the top of the stabilizing platform 65, wherein the top of the double inclined plate 63 is connected to the double-headed insert 64, so the other end of the double-headed insert 64 will be embedded and squeezed to fit with the rib plate 3. In addition, as the double inclined plate 63 is inserted into the interior of the stabilizing platform 65, the reinforcing platform 66 arranged inside the stabilizing platform 65 is squeezed outward, and the reinforcing platform 66 will extend from both ends of the stabilizing platform 65 respectively, and at the same time, the through hole 67 provided on the surface of the reinforcing platform 66 will move to a position overlapping with the inner connecting rod 69. At this time, the inner connecting rod 69 will pass through the support seat 1 and the through hole 67 in sequence under the compression force of the compression spring 602 until it passes through the other side of the reinforcing platform 66. In addition, the inner end of the inner connecting rod 69 is connected to the end panel 603, and the outer side of the end panel 603 is connected to the short rod 604. Therefore, after the inner connecting rod 69 passes outward, the short rod 604 It will move outwards immediately thereafter, and at this time the short rod 604 will first hit the blocking plate 607 outwards, and the blocked plate 607 that has been hit will deflect upwards with the ring support 606 as the fulcrum, and then the short rod 604 will pass over the blocking plate 607 and extend outwards from the support seat 1, wherein the outer end of the short rod 604 is connected to the fourth magnetic block 605, and the upper and lower sides of the inner connecting rod 69 that passes through are both plugged with the receiving and attaching sheet 60, and the side of the receiving and attaching sheet 60 away from the inner connecting rod 69 is fixedly connected with the third magnetic block 601, wherein the third magnetic block 601 and the fourth magnetic block 605 are attracted to each other, so the receiving and attaching sheet 60 will extend outwards from the inner connecting rod 69.
[0045] The above-mentioned embodiments are only preferred embodiments of the present invention, and cannot be used to limit the scope of protection of the present invention. Various changes made by ordinary technicians in this field based on the above-mentioned concepts without creative work all fall within the scope of protection of the present invention.
Claims
1. An energy-saving rotating wind tube mechanism for ships, characterized in that: include: A driving mechanism (4), the driving mechanism (4) is used to operate the device and maintain its stable operation; A vibration reduction mechanism (5), the vibration reduction mechanism (5) being used for vibration reduction treatment of a rotating wind cylinder; A stabilizing mechanism (6), the stabilizing mechanism (6) being used to reinforce the stability between the splint and the device; The vibration reduction mechanism (5) is arranged inside the driving mechanism (4); the outer side of the driving mechanism (4) is fixedly connected to an inner plate (2); the outer side of the inner plate (2) is fixedly connected to a support seat (1); the top of the inner plate (2) and the inner side of the support seat (1) are both fixedly connected to a rib plate (3); and the stabilizing mechanism (6) is fixedly mounted on the outer side of the support seat (1); The driving mechanism (4) comprises a servo motor (41), the servo motor (41) being fixedly mounted on the bottom of the inner slab (2), the top of the inner slab (2) being fixedly connected to a support column (42), the outer side of the support column (42) being fixedly connected to the rib plate (3), the inner side of the support column (42) being extruded with a No. 1 bearing (43), the side of the No. 1 bearing (43) away from the support column (42) being extruded with a wind tube (44), the wind tube (44) being provided with a reinforcement component (45) inside.
2. The energy-saving rotating wind tube mechanism for ships according to claim 1, characterized in that: The reinforcement component (45) comprises a connection plate (451), the connection plate (451) being fixedly mounted inside the wind tube (44), the side of the connection plate (451) away from the wind tube (44) being connected to the output end of the servo motor (41), an adapter sleeve (452) being fixedly connected to the outside of the output end of the servo motor (41), a reinforcement rod (453) being fixedly connected to the outside of the adapter sleeve (452), a hydraulic rod (454) being fixedly mounted on the top of the adapter sleeve (452), and a curved curved rod (455) being fixedly connected to the top of the hydraulic rod (454).
3. The energy-saving rotating wind tube mechanism for ships according to claim 2, characterized in that: The outer side of the curved curved rod (455) is extruded and adapted with a reinforcement piece (456), the outer side of the reinforcement piece (456) is sleeved with a suspended disk (457), the bottom of the suspended disk (457) is fixedly connected to a frame rod (458), the bottom end of the frame rod (458) is fixedly connected to the top of the adapter sleeve (452), the interior of the suspended disk (457) is fixedly connected to a first magnet (459), and the first magnet (459) is away from the suspended disk ( A second magnet (450) is provided at one end of the suspension plate (457), and an end of the second magnet (450) away from the first magnet (459) is fixedly connected to the reinforcement (456), and top grooves (4501) are provided on the upper and lower sides of the suspension plate (457), and a resistance rod (4502) is adapted to slide inside the top groove (4501), and an end of the resistance rod (4502) away from the top groove (4501) is fixedly connected to the reinforcement (456).
4. The energy-saving rotating wind tube mechanism for ships according to claim 2, characterized in that: The interior of the curved bending rod (455) is connected to an electric push rod (4503) via a No. 2 bearing, the top of the electric push rod (4503) is fixedly connected to a hole block (4504), the interior of the hole block (4504) is fixedly connected to a No. 1 magnetic block (4505), a slot (4506) is provided at the top and inside of the hole block (4504), a magnetic blocking plate (4507) is provided above the slot (4506), the top of the magnetic blocking plate (4507) is fixedly connected to a top plate (4508), the center of the bottom of the top plate (4508) is fixedly connected to a return spring (4509), and the bottom end of the return spring (4509) is fixedly connected to the top of the hole block (4504).
5. The energy-saving rotating wind tube mechanism for ships according to claim 1, characterized in that: The vibration reduction mechanism (5) comprises a rotating sleeve (50), the rotating sleeve (50) being rotatably mounted on the top of the air cylinder (44), the bottom of the rotating sleeve (50) being fixedly connected to a fixed head (51) and an elastic telescopic rod (52), the bottom end of the elastic telescopic rod (52) being fixedly connected to a stabilizing plate (53), and the interior of the stabilizing plate (53) being fixedly connected to a sleeve rod (54).
6. The energy-saving rotating wind tube mechanism for ships according to claim 5, characterized in that: A spring (55) is fixedly connected to the interior of the sleeve rod (54); an end of the spring (55) away from the sleeve rod (54) is fixedly connected to an insertion rod (56); the insertion rod (56) is slidably fitted inside the sleeve rod (54); an end of the insertion rod (56) away from the spring (55) is fixedly connected to a second magnetic block (59); side grooves (57) are provided on both upper and lower sides of the insertion rod (56); a limiting rod (58) is slidably fitted inside the side groove (57); and an end of the limiting rod (58) away from the side groove (57) is fixedly connected to the stabilizing plate (53).
7. The energy-saving rotating wind tube mechanism for ships according to claim 1, characterized in that: The stabilizing mechanism (6) comprises a straight slot hole (61), wherein the straight slot hole (61) is provided on the outer side of the supporting seat (1), wherein the inner side of the straight slot hole (61) is slidably adapted to be provided with a sliding rod (62), wherein the outer end of the sliding rod (62) is fixedly connected to a double inclined plate (63), wherein the top of the double inclined plate (63) is fixedly connected to a double-headed fillet strip (64), wherein one end of the double-headed fillet strip (64) away from the double inclined plate (63) is engaged with the rib plate (3).
8. The energy-saving rotating wind tube mechanism for ships according to claim 7, characterized in that: A stabilizing platform (65) is arranged directly below the double inclined plate (63). The stabilizing platform (65) is fixedly mounted on the outer side of the support seat (1). Both ends of the stabilizing platform (65) are plugged with reinforcing platforms (66). The top of the reinforcing platform (66) is squeezed and adapted to the bottom of the double inclined plate (63). A through hole (67) is provided on the outer side of the reinforcing platform (66). One end of the reinforcing platform (66) away from the double inclined plate (63) is fixedly connected to a compensation plate (68).
9. The energy-saving rotating wind tube mechanism for ships according to claim 8, characterized in that: An inner connecting rod (69) is extruded and adapted on the inner side of the compensation plate (68), the inner connecting rod (69) is inserted through the outer side of the support seat (1) and extends into the interior thereof, the top and bottom of the inner connecting rod (69) are both plugged with a receiving and attaching sheet (60), a side of the receiving and attaching sheet (60) away from the inner connecting rod (69) is fixedly connected to a third magnetic block (601), an end of the third magnetic block (601) away from the receiving and attaching sheet (60) is provided with a blocking plate (607), a ring support (606) is rotatably mounted on the top of the blocking plate (607), and the ring support (606) is fixedly connected to the interior of the support seat (1).
10. The energy-saving rotating wind tube mechanism for ships according to claim 9, characterized in that: One end of the inner connecting rod (69) away from the compensation plate (68) is fixedly connected to the end panel (603), and the inner side of the end panel (603) is respectively fixedly connected to a compression spring (602) and a short rod (604), one end of the compression spring (602) away from the end panel (603) is fixedly connected to the inner side of the support seat (1), and one end of the short rod (604) away from the end panel (603) is fixedly connected to a No. 4 magnetic block (605).
Citation Information
Patent Citations
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