Method of tuning bending and torsion stiffness of ducted rotor core of an induction motor
View Patent ↗Electrodymamic machine rotating mass, including for example induction motor rotors, stiffness tuning methods include selective orientation and compression of modular tie rod assemblies into through bores formed in the rotor lamination core outboard of the rotor shaft during motor manufacture, repair or refurbishment. Stiffness tuning enables a motor manufacturer to tune a rotor's rotordynamic stability, and hence the assembled motor's critical vibration speed. Electrodynamic machine rotating mass tuning can be adjusted in response to machine physical design, operational application and manufacturing variation attributes that impact the assembled machine's critical vibration frequency. Thus the present invention offers a systematic, holistic approach to motor vibration refinement through use of a simple kit of modular tie rod assemblies oriented and tightened in a selected array. Rotor stiffness tuning can be tested virtually on computer work stations. Additional actual rotor stiffness tuning can be performed during manufacture.
1. A method for tuning the structural stiffness of the rotor of an induction motor for achieving rotordynamic stability objectives, comprising:
providing a rotor having: a rotatable shaft, a rotor core of stacked rotor laminas radially projecting from the shaft and defining a generally cylindrical outer circumference that is generally concentrically aligned with the shaft and axial ends, and a plurality of bores defined in the rotor core through both ends thereof that are radially symmetrical with and generally parallel to the shaft;
inserting a dynamically balanced array pattern of tie rods into at least a portion of the rotor core bores;
compressing the rotor core axially by selectively tensioning the tie rods to create a first rotor stiffness characteristic;
determining whether the first rotor stiffness characteristic resulting from the tie rod insertion and compressing steps achieves motor rotordynamic stability objectives; and
adjusting at least one tie rod in the array pattern of tie rods in order to selectively tune a second rotor stiffness characteristic for achieving the rotordynamic stability objectives, if the first rotor stiffness characteristic does not achieve rotordynamic stability objectives.
2. The method of claim 1 , wherein the adjusting step comprises repositioning the tie rods.
3. The method of claim 1 , wherein the compressing step further comprises providing a biasing element on at least one end of one tie rod and adjusting the biasing element tension as part of the tensioning steps.
4. The method of claim 3 , wherein the biasing element is selected from a group consisting of wavy washers, mechanical springs and resilient elastomers.
5. The method of claim 4 , wherein the biasing element includes a tuned damper for damping rotor vibrations.
6. The method of claim 1 , wherein the plurality of rotor bores is arrayed in a standard design pattern in a plurality of different rotors, and subsets of the array are designated for tie rod insertion and tensioning for different tuning applications.
7. The method of claim 1 , wherein the adjusting step comprises retensioning the tie rods.
8. A method for manufacturing an induction motor rotor and tuning the structural stiffness thereof for achieving rotordynamic stability objectives, comprising:
stacking plurality of rotor laminas into a rotor core defining a generally cylindrical outer circumference and axial ends, the rotor laminas having holes therein that collectively define: a central bore generally concentrically aligned with the outer circumference, and a plurality of bores defined in the rotor core through both ends thereof that are radially symmetrical with and generally parallel to the central bore;
inserting a dynamically balanced array pattern of tie rods into at least a portion of the rotor core bores;
compressing the rotor core axially by selectively tensioning the tie rods to create a first rotor stiffness characteristic;
inserting a rotatable shaft into the central bore;
determining whether the first rotor stiffness characteristic resulting from the tie rod insertion and compressing steps achieves motor rotordynamic stability objectives; and
adjusting the array pattern of tie rods in a second dynamically balanced array pattern in order to selectively tune a second rotor stiffness characteristic for achieving the rotordynamic stability objectives, if the first rotor stiffness characteristic does not achieve rotordynamic stability objectives.
9. The method of claim 8 , wherein the adjusting step comprises repositioning the tie rods.
10. The method of claim 8 , wherein the compressing step further comprises providing a biasing element on at least one end of one tie rod and adjusting the biasing element tension as part of the tensioning steps.
11. The method of claim 10 , wherein the biasing element is selected from a group consisting of wavy washers, mechanical springs and resilient elastomers.
12. The method of claim 8 , wherein the plurality of rotor bores is arrayed in a standard design pattern in a plurality of different rotors, and subsets of the array are designated for tie rod insertion for different tuning applications.
13. The method of claim 8 , wherein the adjusting step comprises retensioning the tie rods.
14. An induction motor rotor comprising:
a rotatable shaft;
a rotor core formed from stacked rotor laminas radially projecting from the shaft and defining a generally cylindrical outer circumference that is generally concentrically aligned with the shaft and axial ends, and a plurality of bores defined in the rotor core through both ends thereof that are radially symmetrical with and generally parallel to the shaft; and
at least two tie rods coupled within respective rotor core bores by the process of:
inserting a dynamically balanced array pattern of tie rods into at least a portion of the rotor core bores;
compressing the rotor core axially by selectively tensioning the tie rods;
determining whether rotor stiffness resulting from the tie rod insertion and tensioning steps achieves motor rotordynamic stability objectives; and
the tie rods further adapted to be removed, reinserted and re-tensioned in a second dynamically balanced array pattern in order to tune selectively a second rotor stiffness characteristic for achieving the rotordynamic stability objectives.
15. The rotor of claim 14 , wherein at least one end of one of the tie rods has a biasing element, the tension of which is adjusted as part of the tensioning steps.
16. The rotor of claim 14 , wherein the biasing element is selected from a group consisting of wavy washers, mechanical springs and resilient elastomers.
17. The rotor of claim 16 , wherein the biasing element includes a tuned damper for damping rotor vibrations.
18. The rotor of claim 14 , wherein the plurality of rotor bores is arrayed in a standard design pattern in a plurality of different rotors, and subsets of the array are designated for tie rod insertion for different tuning applications.
19. The rotor of claim 14 , wherein the core bores are oriented in concentric inner and outer rings.
20. A kit having component parts capable of being assembled to tune structural stiffness of an induction motor rotor for achieving rotordynamic stability objectives, comprising:
a rotatable shaft;
a rotor core formed from stacked rotor laminas radially projecting from the shaft, and defining both a generally cylindrical outer circumference that is generally concentrically aligned with the shaft and axial ends, and a pluralty of bores defined in the rotor or through both ends thereof that are radially symmetrical with and generally parallel to the shaft; and
a plurality of tie rods adapted to be inserted and tensioned selectively into the into at least a portion of the rotor core bores in a first dynamically balanced array pattern, so as to tune selectively a first rotor stiffness characteristic resulting from the tie rod insertion and tensioning, the tie rods further adapted to be removed, reinserted and re-tensioned in a second dynamically balanced array pattern in order to tune selectively a second rotor stiffness characteristic for achieving the rotordynamic stability objectives if the first rotor stiffness characteristic does not achieve the rotordynamic stabiliy objectives.
21. The kit of claim 20 , wherein at least one end of one of the tie rods has a biasing element, the tension of which is adjusted as part of the tensioning steps.
22. The kit of claim 21 , wherein the biasing element is selected from a group consisting of wavy washers, mechanical springs and resilient elastomers.
23. The kit of claim 22 , wherein the biasing element includes a tuned damper for damping rotor vibrations.
24. The kit of claim 20 , wherein the plurality of rotor bores is arrayed in a standard design pattern in a plurality of different rotors, and subsets of the array are designated for tie rod insertion for different tuning applications.
25. A method for tuning the structural stiffness of a plurality of induction motor rotors for achieving rotordynamic stability objectives, comprising:
providing a first rotor having: a rotatable shaft, a rotor core of stacked rotor laminas radially projecting from the shaft and defining a generally cylindrical outer circumference that is generally concentrically aligned with the shaft and axial ends, and a plurality of bores defined in the rotor core through both ends thereof that are radially symmetrical with and generally parallel to the shaft;
inserting into the first rotor a dynamically balanced array pattern of tie rods into at least a portion of the rotor core bores;
compressing the rotor core of the first rotor axially by selectively tensioning the tie rods to create a first stiffness characteristic;
determining whether the first rotor first stiffness characteristic resulting from the tie rod insertion and compressing steps achieves motor rotordynamic stability objectives;
adjusting at least one tie rod in the array pattern of the tie rods in the first rotor in order to selectively tune a second stiffness characteristic for achieving the rotordynamic stability objectives, if the first stiffness characteristic does not achieve rotordynamic stability objectives; and
assembling a plurality of rotors to match the stiffness characteristic of the first rotor that achieves the rotordynamic stability objectives.