A rotor threading tool for a marine motor and a processing method thereof
By designing a rotor insertion tooling for marine motors and utilizing a base and a variety of drive components to securely fix the rotor, the problem of inconvenient on-site assembly is solved, assembly efficiency is improved, and labor costs are saved.
Patent Information
- Application Number
- CN202211247596.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2022-10-12
- Publication Date
- 2025-09-05
- Estimated Expiration
- 2042-10-12
AI Technical Summary
When existing marine motors are installed through the rotor, on-site assembly is inconvenient, time-consuming and labor-intensive.
A rotor insertion tooling for a marine motor is designed, which includes a base, a pressure block seat and multiple drive components. The rotor is firmly fixed on the base through multiple fixing structures, and the rotor is fixed in all directions by combining motor drive and manual operation.
It improves the convenience of on-site assembly, saves labor, and simplifies the process of the diesel engine main shaft passing through the motor rotor.
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Figure CN115498833B_ABST
Abstract
Description
Technical Field
[0001] The present invention particularly relates to a rotor threading tool for a marine motor and a processing method thereof. Background Art
[0002] A motor is an electromagnetic device that converts or transmits electrical energy based on the law of electromagnetic induction. The motor is represented by the letter M (D in the old standard) in the circuit. Its main function is to generate driving torque and serve as a power source for electrical appliances or various machines. A generator is represented by the letter G in the circuit. Its main function is to convert mechanical energy into electrical energy. The propulsion device of a boat includes an engine and a transmission. The driving force of the engine is decelerated by the transmission and then drives the propeller connected to the transmission. The generator equipment is arranged between the engine and the transmission. The power output of the engine drives the generator equipment while driving the propeller, and the electricity output by the generator equipment is transmitted to the equipment in the cabin.
[0003] Currently, when marine motors are installed on-site through rotors, after the diesel engine main shaft passes through the motor rotor, the flange on the main shaft is docked and fixed to the annular flange bracket in the middle of the rotor yoke cylindrical cavity. The annular flange bracket is located in the center of the motor rotor cavity. This fixing structure is inconvenient for on-site assembly and is time-consuming and labor-intensive. Summary of the Invention
[0004] The object of the present invention is to provide a rotor threading tool and a processing method for a marine motor to solve the problems raised in the above background technology.
[0005] To achieve the above-mentioned objectives, the present invention provides the following technical solutions: A rotor threading tooling for a marine motor, comprising a base, a base for placing a rotor is provided on the base, a pressure block seat for fixing the rotor on the base is provided vertically above the base, a first drive component for driving the pressure block seat to rise and fall in a power-off state is provided on the pressure block seat, a connecting rod is provided on the outside of the pressure block seat, and the connecting rod is connected to a shell for abutting and fixing one end of the rotor at one end away from the pressure block seat, a second drive component for driving the pressure block seat to rise and fall in a power-on state is provided in the shell, and a third drive component for changing the axial position of the shell on the base according to the length of the rotor is also provided in the base.
[0006] Preferably, a support frame is provided on the upper surface of the base, the first driving assembly includes a clamping bolt installed on the support frame, a pressure handle for rotating the clamping bolt is connected to the upper surface of the clamping bolt, and the lower surface of the clamping bolt is connected to the pressure block seat.
[0007] Preferably, a second sliding groove is provided on both sides of the support frame, a first connecting rod slides in the second sliding groove, and the first connecting rod is connected to the pressure block seat at one end away from the second sliding groove.
[0008] Preferably, the second drive assembly includes a second screw installed in the shell, a first bearing sleeve is provided on the second screw, the first bearing sleeve is connected to the telescopic rod, a second motor is also provided in the shell, the power output end of the second motor is connected to the first gear, the outer side of the first gear is meshed with a second gear, the second gear is installed on the rotating shaft, the upper surface of the rotating shaft is connected to the second screw, and the lower surface of the rotating shaft is installed on the lower surface of the shell.
[0009] Preferably, a third sliding groove is provided on both sides of the shell, a second connecting rod slides in the third sliding groove, and the second connecting rod is connected to the first bearing sleeve at one end away from the third sliding groove.
[0010] Preferably, the third driving component includes a strip groove opened on the upper surface of the base, a first screw is arranged in the strip groove, a second bearing sleeve is arranged on the outside of the first screw, two third connecting rods are symmetrically arranged on the outside of the second bearing sleeve, and first sliding grooves are opened on both sides of the strip groove, and the third connecting rod extends away from one end of the second bearing sleeve into the first sliding groove.
[0011] Preferably, the upper surface of the second bearing sleeve is connected to the lower surface of the shell, and the first screw rod passes through the strip groove and extends to the outside of the base and is connected to the first motor.
[0012] Preferably, the upper surface of the pressure block seat is provided with reinforcing ribs, and the lower surface of the pressure block seat is provided with a pressure block for pressing the rotor. Preferably, there are four bases, which are symmetrically arranged in pairs, and the opposite surfaces of each two symmetrical bases are provided with inclined portions.
[0013] A method for using a rotor threading tool for a marine motor comprises the following steps:
[0014] In step A, the rotor is first placed on the inclined portion between the bases. The first motor is started according to the axial length of the rotor. The power output end of the first motor drives the first screw to rotate, causing the second bearing sleeve to rotate accordingly. As the third connecting rod slides in the first slide groove, the second bearing sleeve is rotationally limited, allowing the second bearing sleeve to move on the first screw, driving the movement of the housing, so that the housing abuts against one end of the rotor.
[0015] In step B, when power is supplied, the second motor is started, and the power output end of the second motor drives the first gear to rotate, and the first gear is meshed with the second gear, thereby driving the second gear to rotate, causing the second screw to rotate, and driving the first bearing sleeve to rotate. As the second connecting rod slides in the third sliding groove, the first bearing sleeve is rotationally limited, causing the first bearing sleeve to descend on the second screw, driving the telescopic rod to descend, thereby lowering the pressure block seat, and allowing the pressure block to abut against the rotor;
[0016] Step C: When there is no power, insert a rod into the pressure handle and rotate the rod to drive the clamping bolt to rotate. As the first connecting rod slides in the second slide groove, the pressure block seat is rotationally limited, causing the pressure block seat to descend, and the pressure block can also be abutted against the rotor to be fixed;
[0017] Step D: Finally, after fixing the rotor between the pressing block and the base, the flange on the main shaft is docked and fixed with the annular flange bracket in the middle of the inner cavity of the rotor yoke cylinder to complete the rotor insertion.
[0018] The technical effects and advantages of the present invention are as follows: a rotor threading tooling and processing method for a marine motor of the present invention drives the first screw to rotate through the power output end of the first motor, so that the second bearing sleeve moves on the first screw, drives the movement of the housing, makes the housing abut against one end of the rotor, and starts the second motor. The power output end of the second motor drives the first gear to rotate, drives the second gear to rotate, and rotates the second screw, so that the first bearing sleeve descends on the second screw, drives the telescopic rod to descend, thereby lowering the pressure block seat, and making the pressure block abut against the rotor. A rod-shaped object is inserted into the pressure handle, and the rod-shaped object is rotated to lower the pressure block seat. The pressure block can also be abutted against the rotor for fixing. The rotor can be fixed in all directions by various fixing structures, which makes it easier to pass the diesel engine main shaft through the motor rotor on site. The on-site assembly is convenient, time-saving, and labor-saving. BRIEF DESCRIPTION OF THE DRAWINGS
[0019] Figure 1 It is a schematic diagram of the overall structure of the present invention;
[0020] Figure 2 It is a schematic structural diagram of the reinforcing rib of the present invention;
[0021] Figure 3 It is a structural schematic diagram of the base of the present invention;
[0022] Figure 4 It is a structural schematic diagram of the strip groove of the present invention;
[0023] Figure 5 is a schematic structural diagram of the second drive assembly of the present invention;
[0024] Figure 6 It is a schematic structural diagram of the second bearing sleeve of the present invention.
[0025] In the figure: 1. base; 2. pressure block seat; 3. support frame; 4. tightening bolt; 5. pressure handle; 6. inclined portion; 7. first motor; 8. strip groove; 9. first slide; 10. first screw; 11. reinforcing rib; 12. telescopic rod; 13. base; 14. pressure block; 15. first connecting rod; 16. second slide; 17. housing; 18. second screw; 19. second connecting rod; 20. third connecting rod; 21. third slide; 22. first gear; 23. second motor; 24. second gear; 25. first bearing sleeve; 26. second bearing sleeve. DETAILED DESCRIPTION
[0026] The technical solutions in the embodiments of the present invention will be described clearly and completely below with reference to the accompanying drawings in the embodiments of the present invention.
[0027] In order to facilitate the full fixation of the rotor, refer to Figure 1 、 Figure 2 、 Figure 3 and Figure 4 As shown, it includes a base 1, on which is provided a base 13 for placing the rotor. There are four bases 13, and they are arranged symmetrically in pairs. The opposite sides of each two symmetrical bases 13 are provided with inclined portions 6, and a gap is reserved between the two symmetrical bases 13, forming a V-shaped placement groove between the inclined portions 6, which facilitates subsequent operation of the rotor. A pressure block seat 2 for fixing the rotor to the base 13 is provided vertically above the base 13. The pressure block seat 2 is provided with a first driving component for driving the pressure block seat 2 to rise and fall in the absence of power. A rod is inserted into the pressure handle 5, and the rod is rotated to make the pressure block seat 2 descend, and the pressure block 14 can also be abutted against the rotor for fixing. A connecting rod is provided on the outside of the pressure block seat 2. The connecting rod is connected to a housing 17 at one end away from the pressure block seat 2 for abutting and fixing one end of the rotor. A second driving component is provided in the housing 17 for driving the pressure block seat 2 to rise and fall when the power is on. The second motor 23 is started, and the power output end of the second motor 23 drives the first gear 22 to rotate, driving the second gear 24 to rotate, causing the second screw 18 to rotate, causing the first bearing sleeve 25 to descend on the second screw 18, driving the telescopic rod 12 to descend, thereby lowering the pressure block seat 2 and allowing the pressure block 14 to abut against the rotor. A third driving component is also provided in the base 1 for changing the axial position of the housing 17 on the base 1 according to the length of the rotor. The first screw 10 is driven to rotate by the power output end of the first motor 7, causing the second bearing sleeve 26 to move on the first screw 10, driving the movement of the housing 17, and causing the housing 17 to abut against one end of the rotor.
[0028] In order to improve the stability when wearing the rotor, refer to Figure 1 、 Figure 2 、 Figure 3 、 Figure 4 、 Figure 5 and Figure 6 As shown, a support frame 3 is provided on the upper surface of the base 1, and the first driving assembly includes a clamping bolt 4 mounted on the support frame 3. The clamping bolt 4 passes through the support frame 3, and a threaded hole is provided on the support frame 3 to match the clamping bolt 4. A pressure handle 5 for rotating the clamping bolt 4 is connected to the upper surface of the clamping bolt 4, and the lower surface of the clamping bolt 4 is connected to the pressure block seat 2. A second slide groove 16 is provided on both sides of the support frame 3, and a first connecting rod 15 slides in the second slide groove 16. The end of the first connecting rod 15 away from the second slide groove 16 is connected to the pressure block seat 2. The first connecting rod 15 slides axially in the second slide groove 16, so that the pressure block seat 2 can be rotationally limited, thereby ensuring that the pressure block seat 2 can be raised or lowered. The second drive assembly includes a second screw 18 installed in the housing 17, and a first bearing sleeve 25 is provided on the second screw 18. The first bearing sleeve 25 is connected to the telescopic rod 12. A second motor 23 is also provided in the housing 17. The second motor 23 is existing technology and will not be described here. The power output end of the second motor 23 is connected to the first gear 22, and the outer side of the first gear 22 is meshed with the second gear 24. The second gear 24 is installed on the rotating shaft, the upper surface of the rotating shaft is connected to the second screw 18, and the lower surface of the rotating shaft is installed on the lower surface of the shell 17. Third slide grooves 21 are opened on both sides of the shell 17, and a second connecting rod 19 slides in the third slide groove 21. The second connecting rod 19 is connected to the first bearing sleeve 25 at one end away from the third slide groove 21. The second connecting rod 19 slides in the third slide groove 21 to limit the rotation of the first bearing sleeve 25 so that the first bearing sleeve 25 can move on the second screw 18 to realize the displacement of the shell 17. When the shell 17 approaches the pressure block seat 2, the telescopic rod 12 will be squeezed and the telescopic rod 12 will contract. When the shell 17 is away from the pressure block seat 2, the telescopic rod 12 is stretched.
[0029] Furthermore, the third drive assembly includes a strip groove 8 formed on the upper surface of the base 1. A first screw 10 is provided in the strip groove 8. A second bearing sleeve 26 is provided on the outer side of the first screw 10. Two third connecting rods 20 are symmetrically provided on the outer side of the second bearing sleeve 26. First sliding grooves 9 are provided on both sides of the strip groove 8. The third connecting rod 20 extends into the first sliding groove 9 away from one end of the second bearing sleeve 26. The upper surface of the second bearing sleeve 26 is connected to the lower surface of the housing 17. When the first screw 10 rotates, the third connecting rod 20 slides in the first sliding groove 9, limiting the rotation of the second bearing sleeve 26 so that the second bearing sleeve 26 can move on the first screw 10. The first screw 10 extends through the strip groove 8 to the outside of the base 1 and is connected to the first motor 7. The upper surface of the pressure block seat 2 is provided with a reinforcing rib 11. The reinforcing rib 11 increases the self-stress resistance of the pressure block seat 2 and improves the stability after the rotor is fixed. A pressing block 14 for pressing the rotor is provided on the lower surface of the pressing block seat 2. The contact surface between the pressing block 14 and the rotor is arc-shaped, so as to better fit the rotor and fix the rotor.
[0030] A method for using a rotor threading tool for a marine motor comprises the following steps:
[0031] In step A, the rotor is first placed on the inclined portion 6 between the bases 13. The first motor 7 is started according to the axial length of the rotor. The power output end of the first motor 7 drives the first screw 10 to rotate, causing the second bearing sleeve 26 to rotate accordingly. As the third connecting rod 20 slides in the first chute 9, the second bearing sleeve 26 is rotationally limited, allowing the second bearing sleeve 26 to move on the first screw 10, driving the movement of the housing 17, so that the housing 17 abuts against one end of the rotor.
[0032] Step B, when there is power, start the second motor 23, the power output end of the second motor 23 drives the first gear 22 to rotate, and the first gear 22 is engaged with the second gear 24, driving the second gear 24 to rotate, so that the second screw 18 rotates, driving the first bearing sleeve 25 to rotate, as the second connecting rod 19 slides in the third slide groove 21, the first bearing sleeve 25 is rotationally limited, so that the first bearing sleeve 25 descends on the second screw 18, driving the telescopic rod 12 to descend, thereby lowering the pressure block seat 2, allowing the pressure block 14 to abut against the rotor;
[0033] Step C: When there is no power, insert a rod into the pressure handle 5 and rotate the rod to drive the clamping bolt 4 to rotate. As the first connecting rod 15 slides in the second slide groove 16, the pressure block seat 2 is rotationally limited, causing the pressure block seat 2 to descend. The pressure block 14 can also be fixed against the rotor;
[0034] Step D: Finally, after fixing the rotor between the pressing block 14 and the base 13, the flange on the main shaft is docked and fixed with the annular flange bracket in the middle of the inner cavity of the rotor yoke cylinder to complete the rotor insertion.
[0035] The basic principles, main features, and advantages of the present invention are shown and described above. Those skilled in the art should understand that the present invention is not limited to the foregoing embodiments. The foregoing embodiments and descriptions are merely illustrative of the principles of the present invention. Various changes and modifications may be made to the present invention without departing from the spirit and scope of the present invention. Such changes and modifications are intended to fall within the scope of the present invention. The scope of protection claimed in the present invention is defined by the appended claims and their equivalents.
Claims
1. A rotor threading tool for a marine motor, characterized in that: The invention comprises a base (1), wherein a base (13) for placing a rotor is provided on the base (1), a pressure block seat (2) for fixing the rotor on the base (13) is provided vertically above the base (13), a first driving component for driving the pressure block seat (2) to rise and fall in a power-off state is provided on the pressure block seat (2), a connecting rod is provided on the outside of the pressure block seat (2), and the end of the connecting rod away from the pressure block seat (2) is connected to a shell (17) for abutting and fixing one end of the rotor, a second driving component for driving the pressure block seat (2) to rise and fall in a power-on state is provided in the shell (17), and a third driving component for changing the axial position of the shell (17) on the base (1) according to the length of the rotor is further provided in the base (1), the second driving component comprises a second screw (18) installed in the shell (17), a first bearing sleeve (25) is provided on the second screw (18), and the first bearing sleeve (25) is connected to the telescopic rod (12), and a second motor (23) is also provided in the housing (17), and the power output end of the second motor (23) is connected to the first gear (22), and the outer side of the first gear (22) is meshed with a second gear (24), and the second gear (24) is installed on the rotating shaft, the upper surface of the rotating shaft is connected to the second screw (18), and the lower surface of the rotating shaft is installed on the lower surface of the housing (17), and the third driving component includes a strip groove (8) opened on the upper surface of the base (1), a first screw (10) is provided in the strip groove (8), a second bearing sleeve (26) is provided on the outer side of the first screw (10), and two third connecting rods (20) are symmetrically provided on the outer side of the second bearing sleeve (26), and a first slide groove (9) is provided on both sides of the strip groove (8), and the third connecting rod (20) extends from one end away from the second bearing sleeve (26) to the first slide groove (9).
2. The rotor inserting tool for a marine motor according to claim 1, characterized in that: A support frame (3) is provided on the upper surface of the base (1), and the first driving assembly includes a clamping bolt (4) mounted on the support frame (3), a pressure handle (5) for rotating the clamping bolt (4) is connected to the upper surface of the clamping bolt (4), and the lower surface of the clamping bolt (4) is connected to the pressure block seat (2).
3. The rotor inserting tool for a marine motor according to claim 2, characterized in that: Second sliding grooves (16) are provided on both sides of the support frame (3), a first connecting rod (15) slides in the second sliding groove (16), and the end of the first connecting rod (15) away from the second sliding groove (16) is connected to the pressure block seat (2).
4. The rotor inserting tool for a marine motor according to claim 1, characterized in that: A third sliding groove (21) is provided on both sides of the housing (17), a second connecting rod (19) slides in the third sliding groove (21), and the end of the second connecting rod (19) away from the third sliding groove (21) is connected to the first bearing sleeve (25).
5. The rotor inserting tool for a marine motor according to claim 1, characterized in that: The upper surface of the second bearing sleeve (26) is connected to the lower surface of the housing (17), and the first screw (10) passes through the strip groove (8) and extends to the outside of the base (1) and is connected to the first motor (7).
6. The rotor inserting tool for a marine motor according to claim 1, characterized in that: The upper surface of the pressing block seat (2) is provided with a reinforcing rib (11), and the lower surface of the pressing block seat (2) is provided with a pressing block (14) for pressing the rotor.
7. The rotor inserting tool for a marine motor according to claim 1, characterized in that: There are four bases (13) arranged symmetrically in pairs, and the opposite surfaces of each two symmetrical bases (13) are provided with inclined portions (6).
8. A method for using a rotor threading tool for a marine motor according to any one of claims 1 to 7, characterized in that: The following steps are included: Step (A): first, the rotor is placed on the inclined portion (6) between the bases (13), and the first motor (7) is started according to the axial length of the rotor. The power output end of the first motor (7) drives the first screw (10) to rotate, so that the second bearing sleeve (26) rotates accordingly. As the third connecting rod (20) slides in the first slide groove (9), the second bearing sleeve (26) is rotationally limited, so that the second bearing sleeve (26) moves on the first screw (10), driving the movement of the housing (17), so that the housing (17) abuts against one end of the rotor. Step (B), when there is power, start the second motor (23), the power output end of the second motor (23) drives the first gear (22) to rotate, and the first gear (22) is engaged with the second gear (24), driving the second gear (24) to rotate, so that the second screw (18) rotates, driving the first bearing sleeve (25) to rotate, and as the second connecting rod (19) slides in the third slide groove (21), the first bearing sleeve (25) is rotationally limited, so that the first bearing sleeve (25) descends on the second screw (18), driving the telescopic rod (12) to descend, thereby descending the pressure block seat (2), allowing the pressure block (14) to abut against the rotor; Step (C), when there is no power supply, use a rod-shaped object to be inserted into the pressure handle (5), and rotate the rod-shaped object to drive the clamping bolt (4) to rotate, and as the first connecting rod (15) slides in the second sliding groove (16), the pressure block seat (2) is rotationally limited, so that the pressure block seat (2) is lowered, and the pressure block (14) can also be fixed by contacting with the rotor; Step (D): After the rotor is finally fixed between the pressing block (14) and the base (13), the flange on the main shaft is docked and fixed with the annular flange bracket in the middle of the inner cavity of the rotor yoke cylinder to complete the rotor insertion.
Citation Information
Patent Citations
Method for electric motor with stationary rotor to on site penetrate rotor
CN101257238A
Motor assembling machine
CN201369646Y