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Aeromagnetic motor rotor

A magnetic motor and rotor technology, applied in the direction of magnetic circuit rotating parts, electric components, electrical components, etc., can solve the problems of weak current, low positioning accuracy of parts, poor stability, etc., to avoid false touches, ensure safety, and ensure The effect of stability

Inactive Publication Date: 2020-03-06
芜湖市努尔航空信息科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The existing magneto produces an alternating magnetic field in the transformer core, which has a complex structure, heavy weight, and low positioning accuracy of parts. At the same time, the current generated by a single rotor in the working process of the magneto is relatively weak, and the stability of the output is poor at the same time.

Method used

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Embodiment Construction

[0027] The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with 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. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative work shall fall within the protection scope of the present invention.

[0028] In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. The indicated orientation or positional relationship is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention and simplifying the description, rather than indicating or impl...

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PUM

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Abstract

The invention discloses an aeromagnetic motor rotor, which includes a motor mounting plate and a rotor core shaft. The distance between the axis of the rotor core shaft and the top of the motor mounting plate is twenty centimeters. A thrust cushion block is fitted in the middle of the motor mounting plate. A diagonal brace plate is disposed on one side of the thrust cushion block. The tail end ofthe diagonal brace plate is hinged to a supporting arc plate. Motor standing plates are bolted to the two side edges of the motor mounting plate. The bottoms of the motor standing plates are providedwith fixing bolt holes. Load bearing bolts are fitted in the top surfaces of the motor standing plates. An end shaft cover is fixedly installed on the inner sides of the motor standing plates throughload bolts. A bottom sealing plate is bolted to the bottoms of the motor standing plates. An auxiliary roller is fitted in the middle of the bottom sealing plate. In the aeromagnetic motor rotor, thenew structure is used, and double rotation cores are connected in series so as to to ensure a good current output of the entire equipment. In addition, a non-magnetic sealing plate is used for isolation to ensure the operational stability of the entire equipment.

Description

Technical field [0001] The invention relates to the technical field of aviation electrical equipment, in particular to an aviation magneto rotor. Background technique [0002] The magneto rotor is the magnetic energy source of the magneto, which is used to generate an alternating magnetic field in the transformer core, so that the magneto can work normally. The aviation magneto rotor is the magnetic energy source of the aviation magneto, which is used to generate the magnetic energy in the transformer core. The alternating magnetic field enables the magneto to work normally, which mainly includes permanent magnets, magnetic poles, rotor shafts, and other connecting parts. [0003] The existing magneto generates an alternating magnetic field in the transformer core, has a complex structure, heavy weight, and low parts positioning accuracy. At the same time, the current generated by a single rotor during the operation of the magneto is weak, and the output stability is poor. Summary...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H02K1/27H02K1/28H02K3/46H02K3/51H02K16/00
CPCH02K1/27H02K1/28H02K3/46H02K3/51H02K16/00
Inventor 胡家斌
Owner 芜湖市努尔航空信息科技有限公司