Detachable turbine rotor assembly

Abstract

The utility model relates to the technical field of turbine rotors, and discloses a detachable turbine rotor assembly which comprises an input shaft, a differential mechanism is arranged at one end of the input shaft, an output shaft is fixedly connected to the output end of the differential mechanism, a turbine is arranged at the end, away from the differential mechanism, of the output shaft, and a second connecting assembly is arranged between the turbine and the output shaft. A rotor is inserted into the end, away from the differential mechanism, of the input shaft, a first connecting assembly is arranged between the rotor and the input shaft, the second connecting assembly comprises a limiting strip, the limiting strip is fixedly connected to the outer side of the rotor, a limiting groove matched with the limiting strip is formed in the inner side of the input shaft, and the limiting strip is slidably connected with the limiting groove. The outer side of the input shaft is in threaded connection with a first positioning bolt, and the threaded section of the first positioning bolt is in threaded connection with the rotor. According to the utility model, the rotor can be quickly disassembled and assembled, and the maintenance cost of the rotor is greatly reduced.

Description

Technical Field

[0001] The utility model relates to the technical field of turbine rotors, and more specifically, to a detachable turbine rotor assembly. Background Art

[0002] The rotor of a brushed claw-pole generator is composed of a rotating shaft, two claw-poles, an exciting winding, front and rear fan blades, slip rings, etc. The exciting winding is sleeved in the cavities of the two claw-poles and pressed onto the rotating shaft. The exciting winding is wound with high-strength enameled wire. The slip rings are composed of two insulated copper rings, which are generally pressed into one body with phenolic fiber plastic and then pressed onto the rotating shaft.

[0003] After retrieval, the Chinese patent publication number CN221103138U discloses "a rotor assembly of a generator, including a rotor connecting shaft rod, a differential mechanism is arranged at the end of the rotor connecting shaft rod, and a turbine blade is connected to the other side of the differential mechanism through a connecting shaft; the differential mechanism includes a housing, the cross-section of the housing is in a "C" shape and a circle of teeth is arranged on the inner wall, and a plurality of driving gears limited between the two inner walls of the housing are arranged inside the housing, and the driving gears are meshed with the teeth".

[0004] The above generator rotor drives the rotating shaft to rotate through an external force to drive the motor to generate electricity. Among them, the connection between the rotor and the input shaft adopts an integral fixed structure, and the generator rotor will be worn during the working process. Once the generator rotor is damaged, it needs to be replaced as a whole, greatly increasing the maintenance cost. Content of the Utility Model

[0005] In order to overcome the deficiencies of the prior art, the utility model provides a detachable turbine rotor assembly, which has the advantage of being able to disassemble and replace the rotor to reduce the maintenance cost.

[0006] To achieve the above object, the utility model provides the following technical solution: a detachable turbine rotor assembly. As a preferred technical solution of the utility model, a screw hole matching with the first positioning bolt is opened at one end of the rotor, and the first positioning bolt is in threaded connection with the screw hole.

[0007] As a preferred technical solution of the utility model, the second connection assembly includes a docking block, the docking block is fixedly connected to the end of the output shaft, clamping heads are fixedly connected to both ends of the docking block, a docking seat rotatably matched with the docking block is fixedly connected to one side of the turbine, and a positioning member for fixing the clamping head and the docking seat is arranged inside the docking seat.

[0008] As a preferred technical solution of the utility model, clamping grooves matching with the clamping heads are opened at both ends of the docking seat, and the clamping heads are slidably matched with the clamping grooves.

[0009] As a preferred technical solution of the present utility model, the positioning member includes two stoppers, the two stoppers are respectively fixedly connected to both ends inside the docking seat, the two chucks can be rotated to abut against the corresponding stoppers, and positioning bolts II are threadedly connected to both ends outside the docking seat, and the threaded sections of the two positioning bolts II are threadedly connected to the corresponding chucks.

[0010] As a preferred technical solution of the present utility model, the differential mechanism includes an installation box, one end inside the installation box is rotatably connected with a first gear, one end of the input shaft is fixedly connected to the first gear, the other end inside the installation box is rotatably connected with a second gear, one end of the output shaft is fixedly connected to the second gear, a coaxially fixed third gear and a fourth gear are rotatably connected to the outer edge shaft inside the installation box, the third gear meshes with the first gear, and the fourth gear meshes with the second gear.

[0011] As a preferred technical solution of the present utility model, the number of teeth of the first gear is greater than that of the second gear, and the number of teeth of the third gear is less than that of the fourth gear.

[0012] Compared with the prior art, the beneficial effects of the present utility model are as follows: The limiting strip can make the rotor and the input shaft always rotate synchronously, which realizes the stable transmission of power. By loosening the positioning bolt I, the rotor can be removed from the input shaft, which is convenient for replacing the rotor when it is damaged. At the same time, the positioning bolt I can realize the quick installation of the rotor, and the whole process can realize the quick disassembly and assembly of the rotor, greatly reducing the maintenance cost of the rotor. Description of the Drawings

[0013] Figure 1 It is a schematic structural diagram of a detachable turbine rotor assembly of the present utility model;

[0014] Figure 2 It is a schematic structural diagram of the first connection assembly of the present utility model;

[0015] Figure 3 It is a schematic structural diagram of the second connection assembly of the present utility model;

[0016] Figure 4 It is a schematic structural diagram of the positioning member of the present utility model;

[0017] Figure 5 It is a schematic structural diagram of the differential mechanism of the present utility model.

[0018] In the figure: input shaft 1, differential mechanism 2, mounting box 21, first gear 22, second gear 23, third gear 24, fourth gear 25, rotor 3, first connection assembly 4, limit strip 41, limit groove 42, first positioning bolt 43, screw hole 44, output shaft 5, second connection assembly 6, docking block 61, chuck 62, docking seat 63, card slot 64, positioning member 65, stop block 651, second positioning bolt 652, turbine 7. Specific embodiments

[0019] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present invention without creative efforts shall fall within the protection scope of the present invention.

[0020] As Figures 1 to 5 As shown, the present invention provides a detachable turbine rotor assembly, including an input shaft 1. One end of the input shaft 1 is provided with a differential mechanism 2. The output end of the differential mechanism 2 is fixedly connected to an output shaft 5. One end of the output shaft 5 away from the differential mechanism 2 is provided with a turbine 7. A second connection assembly 6 is arranged between the turbine 7 and the output shaft 5. One end of the input shaft 1 away from the differential mechanism 2 is inserted with a rotor 3. A first connection assembly 4 is arranged between the rotor 3 and the input shaft 1. The second connection assembly 6 includes a limit strip 41. The limit strip 41 is fixedly connected to the outer side of the rotor 3. A limit groove 42 matching the limit strip 41 is formed in the inner side of the input shaft 1. The limit strip 41 is slidably connected to the limit groove 42. A first positioning bolt 43 is threadedly connected to the outer side of the input shaft 1. The threaded section of the first positioning bolt 43 is threadedly connected to the rotor 3. A screw hole 44 matching the first positioning bolt 43 is formed at one end of the rotor 3. The first positioning bolt 43 is threadedly connected to the screw hole 44.

[0021] The limit strip 41 can make the rotor 3 and the input shaft 1 always rotate synchronously, thus realizing the stable transmission of power. By loosening the first positioning bolt 43, the rotor 3 can be removed from the input shaft 1, which is convenient for replacing the rotor 3 when it is damaged. At the same time, the first positioning bolt 43 can realize the rapid installation of the rotor 3. The whole process can realize the rapid disassembly and assembly of the rotor 3, greatly reducing the maintenance cost of the rotor 3.

[0022] Among them, the second connection component 6 includes a docking block 61, the docking block 61 is fixedly connected to the end of the output shaft 5, both ends of the docking block 61 are fixedly connected with a chuck 62, one side of the turbine 7 is fixedly connected with a docking seat 63 that rotates in cooperation with the docking block 61, a positioning member 65 for fixing the chuck 62 and the docking seat 63 is arranged inside the docking seat 63, clamping grooves 64 matching the chucks 62 are formed at both ends of the docking seat 63, and the chucks 62 are slidably matched with the clamping grooves 64. By quickly docking the docking seat 63 with the docking block 61 and then using the positioning member 65 to fix the chuck 62 and the docking seat 63, the installation of the turbine 7 is realized, and at the same time, the disassembly of the turbine 7 can also be realized, so that the replacement of the turbine 7 can be realized to reduce the maintenance cost.

[0023] Among them, the positioning member 65 includes two stoppers 651, the two stoppers 651 are respectively fixedly connected to both ends inside the docking seat 63, the two chucks 62 can be rotated to abut against the corresponding stoppers 651, and positioning bolts II 652 are threadedly connected to both ends outside the docking seat 63, and the threaded sections of the two positioning bolts II 652 are threadedly connected to the corresponding chucks 62.

[0024] Among them, the differential mechanism 2 includes an installation box 21, a first gear 22 is rotatably connected to one end inside the installation box 21, one end of the input shaft 1 is fixedly connected to the first gear 22, a second gear 23 is rotatably connected to the other end inside the installation box 21, one end of the output shaft 5 is fixedly connected to the second gear 23, a coaxially fixed third gear 24 and fourth gear 25 are rotatably connected to the outer edge shaft inside the installation box 21, the third gear 24 meshes with the first gear 22, the fourth gear 25 meshes with the second gear 23, the number of teeth of the first gear 22 is greater than that of the second gear 23, and the number of teeth of the third gear 24 is less than that of the fourth gear 25.

[0025] The first gear 22 is driven to rotate by the input shaft 1, and then the third gear 24 and the fourth gear 25 are driven to rotate synchronously, which causes the second gear 23 to rotate. Since the number of teeth of the first gear 22 is greater than that of the second gear 23, the rotation speed of the first gear 22 is less than that of the second gear 23, so that the rotation speed of the input shaft 1 is less than that of the output shaft 5, and thus the differential process is realized.

[0026] It should be noted that in this article, relational terms such as first and second are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any actual relationship or order between these entities or operations. Moreover, the term "comprising", "including" or any other variation thereof is intended to cover non-exclusive inclusion, so that a process, method, article or device comprising a series of elements not only includes those elements, but also includes other elements not expressly listed, or elements inherent to such process, method, article or device.

[0027] Although embodiments of the present utility model have been shown and described, those of ordinary skill in the art can understand that various changes, modifications, substitutions, and variations can be made to these embodiments without departing from the principle and spirit of the present utility model. The scope of the present utility model is defined by the appended claims and their equivalents.

Claims

1. A detachable turbine rotor assembly, comprising an input shaft (1), one end of the input shaft (1) being provided with a differential mechanism (2), an output end of the differential mechanism (2) being fixedly connected with an output shaft (5), and an end of the output shaft (5) being away from the differential mechanism (2) being provided with a turbine (7), characterized in that: A second connecting assembly (6) is arranged between the turbine (7) and the output shaft (5); a rotor (3) is inserted into the end of the input shaft (1) away from the differential mechanism (2); a first connecting assembly (4) is arranged between the rotor (3) and the input shaft (1); the second connecting assembly (6) comprises a limit bar (41); the limit bar (41) is fixedly connected to the outer side of the rotor (3); a limit groove (42) matching the limit bar (41) is provided on the inner side of the input shaft (1); the limit bar (41) is slidably connected to the limit groove (42); a positioning bolt (43) is threadedly connected to the outer side of the input shaft (1); and a threaded section of the positioning bolt (43) is threadedly connected to the rotor (3).

2. A detachable turbine rotor assembly according to claim 1, characterized in that: One end of the rotor (3) is provided with a screw hole (44) matching with a positioning bolt (43), and the positioning bolt (43) is threadedly connected to the screw hole (44).

3. A detachable turbine rotor assembly according to claim 1, characterized in that: The second connection assembly (6) comprises a docking block (61), the docking block (61) being fixedly connected to the end of the output shaft (5), both ends of the docking block (61) being fixedly connected to a clamping head (62), one side of the turbine (7) being fixedly connected to a docking seat (63) rotatably matched with the docking block (61), and a positioning piece (65) for fixing the clamping head (62) to the docking seat (63) is provided on the inner side of the docking seat (63).

4. A detachable turbine rotor assembly according to claim 3, characterized in that: Both ends of the docking seat (63) are provided with a clamping groove (64) matching with the clamping head (62), and the clamping head (62) and the clamping groove (64) are slidably matched.

5. A detachable turbine rotor assembly according to claim 3, characterized in that: The positioning member (65) comprises two stoppers (651), the two stoppers (651) are respectively fixedly connected to the two ends of the inner side of the docking seat (63), the two clamping heads (62) can contact the corresponding stoppers (651) by rotating, and the two ends of the outer side of the docking seat (63) are both threadedly connected with positioning bolts (652), and the threaded sections of the two positioning bolts (652) are threadedly connected to the corresponding clamping heads (62).

6. A detachable turbine rotor assembly according to claim 1, characterized in that: The differential mechanism (2) comprises a mounting box (21), one end of the inner side of the mounting box (21) is rotatably connected to a gear one (22), one end of the input shaft (1) is fixedly connected to the gear one (22), the other end of the inner side of the mounting box (21) is rotatably connected to a gear two (23), one end of the output shaft (5) is fixedly connected to the gear two (23), and the outer shaft inside the mounting box (21) is rotatably connected to a coaxially fixed gear three (24) and a gear four (25), the gear three (24) is meshed with the gear one (22), and the gear four (25) is meshed with the gear two (23).

7. A detachable turbine rotor assembly according to claim 6, characterized in that: The number of teeth of gear one (22) is greater than that of gear two (23), and the number of teeth of gear three (24) is less than that of gear four (25).

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