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Full-superconducting claw-pole motor adopting liquid hydrogen spray cooling

A technology of spray cooling and claw pole motors, which is applied in household refrigeration devices, cooling/ventilation devices, applications, etc. It can solve the problems of power performance attenuation, large size, and discount of high power density gain effects of full superconducting motors, so as to reduce the size and quality, improved power density, and compact motor structure

Active Publication Date: 2021-03-26
BEIHANG UNIV +1
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  • Application Information

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Problems solved by technology

[0003] Most of the traditional full superconducting motors use rotor superconducting excitation, and the superconducting power supply is powered by slip rings. At the same time, the superconducting motor is affected by the centrifugal force, and the power performance will be attenuated, which will affect the performance of the full superconducting motor, resulting in the failure of the full superconducting motor. Work at high speed, unable to meet the needs of aviation motors working at high speed
Moreover, the cooling of full superconducting motors generally adopts low-temperature immersion cooling or low-temperature conduction cooling, but the auxiliary structure of immersion cooling and conduction cooling is too large for the motor, which greatly reduces the high power density gain effect of full superconducting motors

Method used

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  • Full-superconducting claw-pole motor adopting liquid hydrogen spray cooling
  • Full-superconducting claw-pole motor adopting liquid hydrogen spray cooling
  • Full-superconducting claw-pole motor adopting liquid hydrogen spray cooling

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Embodiment Construction

[0019] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention. In addition, the technical features involved in the various embodiments of the present invention described below can be combined with each other as long as they do not constitute a conflict with each other.

[0020] figure 1 and figure 2 They are respectively a longitudinal sectional view and a transverse sectional view of a fully superconducting claw pole motor structure provided by the embodiment provided by liquid hydrogen spray cooling, including a rotor structure (100), a stator structure (200), a vacuum heat insulation structure (300), a superconducting Conductive armature winding (400), sup...

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Abstract

The invention belongs to the technical field of motors, and relates to a full-superconducting claw-pole motor adopting liquid hydrogen spray cooling, the motor comprises a rotor structure (100), a stator structure (200), a vacuum heat insulation structure (300), a superconducting armature winding (400), a superconducting excitation winding (500), a liquid hydrogen spray cooling structure (600) andan axial dual-channel flux loop (700), the superconducting cooling difficulty is reduced by the aid of the static superconducting excitation winding and the superconducting armature winding, the airgap flux density is increased by the aid of superconducting electric excitation of the axial double-channel flux loop, a rotor claw pole magnetic conduction structure is suitable for high-rotating-speed operation, the latent heat of vaporization of liquid hydrogen is brought into full play by liquid hydrogen spray cooling, and accordingly the full-superconducting motor is compact in cooling structure, and the power density of the motor is improved.

Description

Technical field: [0001] The invention belongs to the technical field of motors, and more specifically relates to a fully superconducting claw-pole motor cooled by spraying liquid hydrogen. Background technique: [0002] Multi-electric aircraft and all-electric aircraft are the trend of aviation development in the future, and motors are the key guarantee for realizing electric flight. Fully superconducting motors have the advantages of high reliability, high power density, and high efficiency, and are the preferred solution for realizing electric aviation. [0003] Most of the traditional full superconducting motors use rotor superconducting excitation, and the superconducting power supply is powered by slip rings. At the same time, the superconducting motor is affected by the centrifugal force, and the power performance will be attenuated, which will affect the performance of the full superconducting motor, resulting in the failure of the full superconducting motor. It work...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H02K55/02H02K9/193F25D3/10
CPCF25D3/10H02K9/193H02K55/02
Inventor 宋东彬姚轩宇杨文将王长辉刘宇王少鹏
Owner BEIHANG UNIV
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