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Heat treatment device and method for high-speed rotor core of dual-performance reluctance motor

A technology of heat treatment device and heat treatment method, which is applied in the direction of electromechanical devices, manufacturing motor generators, electrical components, etc., can solve the problems of lack of high-speed motor rotor cores, etc., to prevent oxidation reactions, ensure adjustability and accuracy, and ensure The effect of mechanical strength

Active Publication Date: 2021-06-22
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In summary, there is a lack of high-speed motor rotor cores with good magnetic properties and mechanical stress in the prior art

Method used

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  • Heat treatment device and method for high-speed rotor core of dual-performance reluctance motor
  • Heat treatment device and method for high-speed rotor core of dual-performance reluctance motor
  • Heat treatment device and method for high-speed rotor core of dual-performance reluctance motor

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Embodiment Construction

[0030] In order to enable those skilled in the art to better understand the technical solutions of the present invention, the present invention will be further described in detail below in conjunction with specific embodiments.

[0031] An embodiment of the present invention provides a dual-performance reluctance motor rotor core heat treatment device, such as Figure 4 As shown, it includes: heater 2, cooling pipe 3, adapter 4, sealing box interface 5, shielding gas 6, sealing box 7, drive pump 8, radiator 9, pipeline 10, coolant tank 11, heater signal line 12. A first temperature sensor 13 , a sealing ring 14 , a temperature controller 15 , and a second temperature sensor 16 .

[0032] Iron core to be processed 1 such as figure 1 As shown, the iron-cobalt soft magnetic material is used, and it is arranged in the sealed box 7. The cooling pipe 3 passes through the iron core 1, and the heater 2 is arranged on the circumference of the iron core 1.

[0033] The two ends of the...

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Abstract

The invention discloses a heat treatment device and method for a high-speed rotor core of a dual-performance reluctance motor, and relates to the field of heat treatment of a reluctance motor rotor core. Optimal magnetic properties for optimal mechanical strength at the bore. The device of the invention comprises: a heater, a cooling pipe, a sealed box, a driving pump, a pipeline, a first temperature sensor, a second temperature sensor and a temperature controller. The method of the invention comprises: a gradient heat treatment method for the rotor iron core of the reluctance motor, heating or cooling the rotor iron core of the reluctance motor, and at the same time ensuring a safe and reliable heat treatment environment. The invention can realize dual-performance heat treatment on the rotor iron core of the reluctance motor, and has high practicability.

Description

technical field [0001] The invention relates to the field of heat treatment of rotor cores of reluctance motors, in particular to a heat treatment device and method for high-speed rotor cores of dual-performance reluctance motors. Background technique [0002] The increase of the speed of the aircraft motor can effectively increase the power density of the motor. The rotor core of a high-speed motor rotates at high speed and will bear huge centrifugal force, which requires the material of the rotor core to have high yield strength. Iron-cobalt-vanadium soft magnetic alloy has the characteristics of high saturation flux density and is widely used in aerospace motors. At present, the saturation flux density of iron-cobalt-vanadium soft-magnetic alloy is 2.4T, the coercivity is below 125A / m, and the yield strength is 360Mpa. , its mechanical strength is difficult to meet the development of high-speed motors. Iron-cobalt-vanadium soft magnetic alloy can effectively increase th...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H02K15/12
CPCH02K15/12
Inventor 张卓然张健李涵琪于立
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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