Novel magnetic-resistance-type electromagnetic clutch

An electromagnetic clutch, reluctance technology, applied in electric brake/clutch, asynchronous induction clutch/brake, electrical components, etc., can solve the problems of reduced service life, large volume torque, degraded magnetic performance, etc., to achieve service life length, increase the amount of magnetoresistance change, and improve the effect of bonding torque

Pending Publication Date: 2017-10-24
李亚涛
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] At present, in the flight control systems of some aircrafts in Russia and my country, small magnetic powder clutches are usually used. Because the magnetic powder of the magnetic powder clutch enters the running bearing, the bearing will be stuck, and the magnetic powder will rub against each other in the clutch. can deteriorate, lead to coagulation, agglomeration, cause failure, and greatly reduce the service life; and (ZL201210078990.1) patent, the reluctance eddy current electromagnetic clutch is a special micro-motor in essence, and the reluctance eddy current electromagnetic clutch is a single breath Reluctance, low motor coefficient, large volume and small torque, in order to improve flight reliability and safety, therefore, it is necessary to improve

Method used

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  • Novel magnetic-resistance-type electromagnetic clutch
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  • Novel magnetic-resistance-type electromagnetic clutch

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Embodiment Construction

[0021] Attached below Figure 1-7 An embodiment of the present invention is described.

[0022] The new reluctance electromagnetic clutch has a stator 1, a winding 2 and a rotor. The rotor includes a driving rotor 3 and a driven rotor 4. The stator 1 is supported on the output shaft 6 of the driven rotor 4 through a bearing I5 and driven The rotor disk 9 on the rotor 4 is inserted into the annular space 10 on the active rotor disk 3, the active rotor 3 is supported on the outer circumference of the stator 1 through the bearing II7 and the bearing III8 and the winding 2 sleeved on the stator 1 is placed on the stator 1 and the driving rotor 3, specifically, the stator 1 is composed of a left stator 17 and a right stator 18, and the left stator 17 and the right stator 18 are connected and supported on the output shaft 6 through a bearing I5, The left side and the right side of the active rotor 3 are respectively supported on the outer circumference of the left stator 17 and the...

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Abstract

A new type of reluctance electromagnetic clutch is provided, which has a stator, a winding and a rotor. The rotor includes a driving rotor and a driven rotor. The stator is supported on the output shaft of the driven rotor through a bearing I and the rotor on the driven rotor is The disc is inserted into the annular space on the active rotor disc. The active rotor is supported on the outer circumference of the stator through bearings II and III, and the windings sleeved on the stator are placed between the stator and the active rotor. The annular space is formed by the upper jaw Teeth and mandibular teeth are formed, and the maxillary teeth and mandibular teeth are provided with the same number of teeth corresponding to each other. The rotor disk is embedded with teeth corresponding to the maxillary teeth and mandibular teeth and inserted into the annular space. The invention solves the problems of the magnetic powder clutches due to mutual friction and aging, which lead to deterioration of magnetic properties, resulting in condensation, agglomeration, or magnetic powder leakage, causing the bearing to be stuck, etc., has a simple structure, long service life, and improves the reliability and safety of flight. , The combined torque and combined speed are greatly improved.

Description

technical field [0001] The invention belongs to the technical field of aircraft automatic control, and in particular relates to a novel reluctance type electromagnetic clutch, which is used in an executive mechanism of an airborne aircraft automatic control system. Background technique [0002] At present, in the flight control systems of some aircrafts in Russia and my country, small magnetic powder clutches are usually used. Because the magnetic powder of the magnetic powder clutch enters the running bearing, the bearing will be stuck, and the magnetic powder will rub against each other in the clutch. can deteriorate, lead to coagulation, agglomeration, cause failure, and greatly reduce the service life; and (ZL201210078990.1) patent, the reluctance eddy current electromagnetic clutch is a special micro-motor in essence, and the reluctance eddy current electromagnetic clutch is a single breath Reluctance, low motor coefficient, large volume and small torque, in order to impr...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H02K49/04
CPCH02K49/043
Inventor 李亚涛
Owner 李亚涛
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