Pod propeller motor propulsion shafting structure suitable for ice region ship

By adopting a combination of segmented structure and arc-shaped fixing plates in the pod propulsion shaft system, the problem of inconvenience in fixing the bearing is solved. Through the combined structure of the air cooler and the heat dissipation hole, the heat dissipation effect of the bearing is improved, the rapid fixation and efficient heat dissipation of the equipment are achieved, and the convenience and stability of the equipment are improved.

CN120080985AInactive Publication Date: 2025-06-03JIANGSU UNIV OF SCI & TECH
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Patent Information

Application Number
CN202510383458.8
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2025-03-28
Publication Date
2025-06-03
Estimated Expiration
Not applicable · inactive patent

AI Technical Summary

Technical Problem

In the prior art, in the pod propulsion shaft system structure, it is difficult to quickly fix the bearings and effectively dissipate heat, resulting in inconvenient use of the equipment and may affect normal operation due to excessive temperatures.

Method used

The motor propulsion shaft system with a segmented structure is adopted to achieve rapid fixation of the bearing through arc-shaped fixing plates and drive components, and the heat dissipation effect of the bearing is improved through the combined structure of the air cooler and the heat dissipation hole.

Benefits of technology

It realizes rapid fixation and efficient heat dissipation of bearings, improves the convenience and stability of the equipment, and prevents equipment failures caused by excessive temperatures.

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Abstract

The invention discloses a pod propeller motor propulsion shafting structure suitable for a ship in an ice area, and belongs to the technical field of motor propulsion shafting structures.The pod propeller motor propulsion shafting structure comprises a first motor and a mounting base, a rotating shaft is fixedly mounted at the output end of the first motor, a propeller side shaft is mounted at one end of the rotating shaft through a coupler, and a propeller is fixedly mounted at one end of the propeller side shaft; a bearing is inserted into the mounting groove, the rotating shaft and the paddle side shaft are both mounted on the inner side of the bearing, movable arc-shaped fixing plates are mounted at the two ends of the mounting seat through driving assemblies, one ends of the arc-shaped fixing plates are tightly attached to the bearing, a supporting plate is fixedly mounted on one side of the mounting seat, and a heat dissipation assembly is mounted at the upper end of the supporting plate; by manually rotating the threaded rod, the arc-shaped fixing plate fixes the bearing, convenience and rapidness are achieved, time and labor are saved, cold air can be conveyed into the heat dissipation holes to dissipate heat of the bearing, the bearing is rapidly cooled, the heat dissipation effect is improved, and normal use of the bearing is prevented from being affected by too high temperature in the bearing.
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Description

Technical Field

[0001] The present invention belongs to the technical field of ship propulsion, and particularly relates to a motor propulsion shafting structure of a podded propeller applicable to ice area ships. Background Art

[0002] A ship propeller is an important component in the power equipment of ice area ships. The motor propulsion shafting structure is the core component of the power transmission system of the podded propeller, and its design directly affects the power transmission efficiency and equipment stability.

[0003] For example, the publication number is: CN218431703, which discloses a motor propulsion shafting structure and a podded propeller for a podded propeller. The motor propulsion shafting structure includes a motor assembly, a thrust end assembly, and a propeller side end assembly. The motor assembly includes a rotor part and a stator part, and the stator part is configured to drive the rotor part to rotate; the thrust end assembly includes a thrust side shaft, and one end of the thrust side shaft is detachably connected to one end of the rotor part; the propeller side end assembly includes a propeller side shaft, and one end of the propeller side shaft is connected to the end of the rotor part away from the thrust side shaft; the rotor part, the thrust side shaft, and the propeller side shaft are coaxially arranged. The motor propulsion shafting structure of the podded propeller of the present invention adopts a segmented structure, divides the overall shafting into three independent axial connecting parts, namely the rotor part, the thrust side shaft, and the propeller side shaft, which is easy to disassemble, install and repair, avoids vibrations, noises and other situations caused by shafting deformation, and ensures the safety performance of the podded propeller.

[0004] When the motor propulsion shafting structure of the podded propeller is in use, although it adopts a segmented structure and is easy to disassemble, install and repair, it is inconvenient to manually fix the bearing through the bearing end cover, which is time-consuming and laborious. Moreover, after long-term operation, the bearings at one end of the motor rotating shaft and the propeller side shaft have too high temperatures. If heat dissipation is not carried out, it will affect its normal use. The prior art generally dissipates heat through heat dissipation holes, and the heat dissipation effect is poor. Summary of the Invention

[0005] In order to overcome the deficiencies of the prior art, the purpose of the present invention is to solve the above problems in the prior art, and provide a motor propulsion shafting structure of a podded propeller applicable to ice area ships, so as to achieve the purpose of quickly fixing the bearing and improving the heat dissipation effect of the bearing.

[0006] The present invention adopts the following technical solutions to achieve:

[0007] Pod propeller motor propulsion shafting structure applicable to ice area ships, including a first motor and a mounting seat. A rotating shaft is fixedly installed at the output end of the first motor. One end of the rotating shaft is installed with a propeller side shaft through a coupling. One end of the propeller side shaft is fixedly installed with a propeller. An installation groove is opened at one end of the mounting seat. A bearing is inserted into the installation groove. The rotating shaft and the propeller side shaft are both installed inside the bearing. Both ends of the mounting seat are installed with movable arc-shaped fixing plates through a driving component. One end of the arc-shaped fixing plate is in close contact with the bearing. A support plate is fixedly installed on one side of the mounting seat. A heat dissipation component for dissipating heat from the bearing is installed at the upper end of the support plate. When in use, the arc-shaped fixing plate is used to fix the bearing, and the driving component is used to move the arc-shaped fixing plate. The coupling is a conventional structure for connecting the rotating shaft and the propeller side shaft.

[0008] To optimize the above technical solution, the specific measures taken also include:

[0009] Further, in order to make the arc-shaped fixing plate move smoothly, sliding grooves are opened at both ends inside the installation groove. The arc-shaped fixing plate is slidably installed in the sliding grooves, and the arc-shaped fixing plate can move in the sliding grooves.

[0010] Further, in order to increase the friction between the arc-shaped fixing plate and the bearing, an anti-slip pad is fixedly installed at one end of the arc-shaped fixing plate. The anti-slip pad is made of rubber material.

[0011] Further, in order to enable the arc-shaped fixing plate to move, the driving component includes a threaded rod. The threaded rod is threadedly connected to both ends of the mounting seat. One end of the threaded rod is rotatably connected to the arc-shaped fixing plate. The threaded rod is used to change the position of the arc-shaped fixing plate.

[0012] Further, in order to facilitate the rotation of the threaded rod, a handwheel is fixedly installed at one end of the threaded rod.

[0013] Further, in order to dissipate heat from the bearing, a ring plate is fixedly installed at one end of the bearing. A plurality of heat dissipation holes are arranged in a circumferential array at one end of the ring plate.

[0014] Further, in order to convey cold air into the bearing, the heat dissipation component includes a cold air blower and an air outlet cover. The air outlet cover is fixedly installed on one side of the mounting seat. One end of the air outlet cover is communicated with the heat dissipation holes.

[0015] Furthermore, in order to convey cold air into the air outlet hood, the air cooler is fixedly installed on the support plate. An air delivery pipe is fixedly installed at the output end of the air cooler. An L-shaped pipe is fixedly installed at one end of the air outlet hood. One end of the L-shaped pipe is communicated with the air delivery pipe. The air cooler is used to convey cold air, and the control end of the air cooler is electrically connected to the control module of the pod thruster.

[0016] Advantages of the present invention:

[0017] When the present invention is in use, by manually rotating the threaded rod, the arc-shaped fixing plate fixes the bearing, which is convenient, fast, time-saving and labor-saving. It is also possible to dissipate heat from the bearing by conveying cold air into the heat dissipation holes, quickly cool down the bearing, improve the heat dissipation effect, and prevent the internal temperature of the bearing from being too high to affect its normal use. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 is a schematic diagram of the overall structure of the present invention;

[0019] Figure 2 is a schematic diagram of the connection structure of the mounting seat of the present invention;

[0020] Figure 3 is a schematic diagram of the bearing connection structure of the present invention;

[0021] Figure 4 is a partially sectional schematic diagram of the mounting seat of the present invention;

[0022] Figure 5 is a schematic diagram of the drive assembly structure of the present invention;

[0023] Figure 6 is a schematic diagram of the heat dissipation assembly structure of the present invention.

[0024] Reference numerals are: first motor 1, mounting seat 2, mounting groove 3, bearing 4, drive assembly 5, threaded rod 501, handwheel 502, arc-shaped fixing plate 6, support plate 7, heat dissipation assembly 8, air cooler 801, air outlet hood 802, air delivery pipe 803, L-shaped pipe 804, rotating shaft 9, propeller side shaft 10, propeller 11, sliding groove 12, anti-slip pad 13, annular plate 14, heat dissipation hole 15. DETAILED DESCRIPTION OF THE EMBODIMENTS

[0025] In order to clarify the technical solution and working principle of the present invention, the present invention will be further described in detail below with reference to the accompanying drawings and specific embodiments. It should be noted that many specific details are set forth in the following description in order to fully understand the present invention. However, the present invention can also be implemented in other ways different from those described herein. Those skilled in the art can make similar generalizations without departing from the connotation of the present invention. Therefore, the present invention is not limited by the specific embodiments disclosed below.

[0026] Please refer to Figures 1-6 As shown, the podded propeller motor propulsion shafting structure applicable to ice area ships includes a first motor 1 and a mounting seat 2. A rotating shaft 9 is fixedly installed at the output end of the first motor 1. One end of the rotating shaft 9 is installed with a propeller side shaft 10 through a coupling. One end of the propeller side shaft 10 is fixedly installed with a propeller 11. An installation groove 3 is opened at one end of the mounting seat 2. A bearing 4 is inserted into the installation groove 3. Both the rotating shaft 9 and the propeller side shaft 10 are installed inside the bearing 4. Both ends of the mounting seat 2 are installed with movable arc-shaped fixing plates 6 through a driving component 5. One end of the arc-shaped fixing plate 6 is in close contact with the bearing 4. A support plate 7 is fixedly installed on one side of the mounting seat 2. A heat dissipation component 8 for dissipating heat from the bearing 4 is installed at the upper end of the support plate 7. Sliding grooves 12 are opened at both ends inside the installation groove 3. The arc-shaped fixing plate 6 is slidably installed in the sliding grooves 12. An anti-slip pad 13 is fixedly installed at one end of the arc-shaped fixing plate 6. The anti-slip pad 13 is made of rubber. A circular plate 14 is fixedly installed at one end of the bearing 4. Heat dissipation holes 15 are arranged in a circumferential array at one end of the circular plate 14. When in use, first fixedly install the mounting seat 2 at the corresponding position, then respectively fixedly install the rotating shaft 9 and the propeller side shaft 10 inside the bearing 4, then connect the rotating shaft 9 and the propeller side shaft 10 together through a coupling, then install the bearing 4 into the installation groove 3 at one end of the mounting seat 2, and then manually move the arc-shaped fixing plate 6 through the driving component 5 to fix the bearing 4, which is convenient, fast, time-saving and labor-saving. At this time, the arc-shaped fixing plate 6 moves in the sliding grooves 12, so that the arc-shaped fixing plate 6 can move smoothly without deviation. At the same time, the anti-slip pad 13 at one end of the arc-shaped fixing plate 6 can increase the friction between the arc-shaped fixing plate 6 and the bearing 4 to prevent slipping. After fixing the bearing 4, start the first motor 1 to drive the rotating shaft 9 to rotate, and the propeller side shaft 10 rotates accordingly, so that the propeller 11 rotates circumferentially to propel the ship to move. After working for a period of time, start the heat dissipation component 8 to dissipate heat from the bearing 4. By delivering cold air into the heat dissipation holes 15 at one end of the circular plate 14, the inside of the bearing 4 can be quickly cooled, and the heat dissipation effect is good, preventing the internal temperature of the bearing 4 from being too high and affecting its normal use.

[0027] The driving component 5 includes a threaded rod 501. The threaded rod 501 is threadedly connected to both ends of the mounting seat 2. One end of the threaded rod 501 is rotatably connected to the arc-shaped fixing plate 6. A handwheel 502 is fixedly installed at one end of the threaded rod 501. When in use, manually rotate the handwheel 502 to drive the threaded rod 501 to rotate, so that the arc-shaped fixing plate 6 moves to one side in the sliding grooves 12 to fix the bearing 4, which is convenient, fast, time-saving and labor-saving. When the bearing 4 needs to be replaced, rotate the handwheel 502 in the reverse direction, and the threaded rod 501 rotates in the reverse direction accordingly, so that the arc-shaped fixing plate 6 resets to release the fixing effect on the bearing 4, and then the bearing 4 can be taken out.

[0028] The heat dissipation component 8 includes a cooling fan 801 and an air outlet cover 802. The air outlet cover 802 is fixedly installed on one side of the mounting base 2. One end of the air outlet cover 802 is communicated with the heat dissipation hole 15. The cooling fan 801 is fixedly installed on the support plate 7. A duct 803 is fixedly installed at the output end of the cooling fan 801. An L-shaped pipe 804 is fixedly installed at one end of the air outlet cover 802. One end of the L-shaped pipe 804 is communicated with the duct 803. When in use, when it is necessary to dissipate heat from the bearing 4, manually start the cooling fan 801. The cold air generated by the cooling fan 801 is transported to the L-shaped pipe 804 through the duct 803, and then transported to the air outlet cover 802 through the L-shaped pipe 804, and then transported to the inside of the bearing 4 through the heat dissipation hole 15 at one end of the annular plate 14 for cooling, and the hot air inside the bearing 4 is quickly discharged through the heat dissipation hole 15 at the other end, preventing the temperature inside the bearing 4 from being too high and affecting its normal use.

[0029] For those skilled in the art, it is obvious that the present invention is not limited to the details of the above exemplary embodiments, and can be implemented in other specific forms without departing from the spirit or basic characteristics of the present invention. Therefore, from any point of view, the embodiments should be regarded as exemplary and non-limiting. The scope of the present invention is defined by the appended claims rather than the above description. Therefore, all changes falling within the meaning and scope of the equivalent elements of the claims are intended to be included in the present invention. Any reference signs in the claims should not be regarded as limiting the claimed rights.

[0030] The above is only the preferred embodiment of the present invention, and the protection scope of the present invention is not limited to the above embodiments. All technical solutions falling within the idea of the present invention belong to the protection scope of this application. It should be noted that for those of ordinary skill in the art, several improvements and refinements made without departing from the principle of this application should be regarded as the protection scope of this application.

Claims

1. A pod thruster motor propulsion shaft system structure suitable for ice-covered ships, comprising a first motor and a mounting seat, wherein a rotating shaft is fixedly mounted on the output end of the first motor, a propeller side shaft is mounted on one end of the rotating shaft through a coupling, and a propeller is fixedly mounted on one end of the propeller side shaft, characterized in that: A mounting groove is provided at one end of the mounting seat, a bearing is inserted in the mounting groove, the rotating shaft and the propeller side shaft are both installed on the inner side of the bearing, and movable arc-shaped fixing plates are installed at both ends of the mounting seat through a driving component, one end of the arc-shaped fixing plate is tightly attached to the bearing, a support plate is fixedly installed on one side of the mounting seat, and a heat dissipation component for dissipating the heat of the bearing is installed on the upper end of the support plate.

2. The pod propulsion motor propulsion shaft system structure suitable for ice-covered ships according to claim 1 is characterized in that: Sliding grooves are provided at both ends of the installation groove, and the arc-shaped fixing plate is slidably installed in the sliding grooves.

3. The pod propulsion motor propulsion shaft system structure suitable for ice-covered ships according to claim 2 is characterized in that: An anti-skid pad is fixedly installed at one end of the arc-shaped fixing plate, and the anti-skid pad is made of rubber material.

4. The pod propulsion motor propulsion shaft system structure suitable for ice-covered ships according to claim 1 is characterized in that: The driving assembly comprises a threaded rod, the threaded rod is threadedly connected to two ends of the mounting seat, and one end of the threaded rod is rotatably connected to the arc-shaped fixing plate.

5. The pod propulsion motor propulsion shaft system structure suitable for ice-covered ships according to claim 4 is characterized in that: A hand wheel is fixedly mounted on one end of the threaded rod.

6. The pod propulsion motor propulsion shaft system structure suitable for ice-covered ships according to claim 1 is characterized by: An annular plate is fixedly mounted on one end of the bearing, and heat dissipation holes are arranged in a circumferential array on one end of the annular plate.

7. The pod propulsion motor propulsion shaft system structure suitable for ice-covered ships according to claim 6 is characterized by: The heat dissipation assembly comprises an air cooler and an air outlet cover. The air outlet cover is fixedly mounted on one side of the mounting seat, and one end of the air outlet cover is connected to the heat dissipation hole.

8. The pod propulsion motor propulsion shaft system structure suitable for ice-covered ships according to claim 7 is characterized by: The air cooler is fixedly mounted on the support plate, an air supply pipe is fixedly mounted on the output end of the air cooler, an L-shaped pipe is fixedly mounted on one end of the air outlet cover, and one end of the L-shaped pipe is connected to the air supply pipe.