CN204168070U - A kind of anti-electric motor with superheat automatic protector - Google Patents

A kind of anti-electric motor with superheat automatic protector Download PDF

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Publication number
CN204168070U
CN204168070U CN201420507690.5U CN201420507690U CN204168070U CN 204168070 U CN204168070 U CN 204168070U CN 201420507690 U CN201420507690 U CN 201420507690U CN 204168070 U CN204168070 U CN 204168070U
Authority
CN
China
Prior art keywords
fuselage
stator
temperature controlling
end cap
pin
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201420507690.5U
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Chinese (zh)
Inventor
邹兆林
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
JIANGSU YINENG MOTOR Co Ltd
Original Assignee
JIANGSU YINENG MOTOR Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by JIANGSU YINENG MOTOR Co Ltd filed Critical JIANGSU YINENG MOTOR Co Ltd
Priority to CN201420507690.5U priority Critical patent/CN204168070U/en
Application granted granted Critical
Publication of CN204168070U publication Critical patent/CN204168070U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

A kind of anti-electric motor with superheat automatic protector, comprise fuselage, body upper is provided with terminal box; terminal box has connector, and connector is connected with stator, is provided with rotor outside stator; front fuselage is provided with screens end cap, is provided with control module in fuselage, is provided with Temperature Controlling Chip in control module; Temperature Controlling Chip is connected with warming infrared module; Temperature Controlling Chip is provided with pin, and pin connects power input, and power input is connected with terminal box; be provided with fan after rear end cap, protective device is fine-structure mesh fan housing.In fuselage, establish attemperating unit, motor can be allowed to play a protective role when in use, can lower the temperature when temperature is too high time, do not need those operations artificial, improve the operational effect of motor.

Description

A kind of anti-electric motor with superheat automatic protector
Technical field
The utility model relates to a kind of motor, is specifically related to a kind of anti-electric motor with superheat automatic protector.
Background technology
Along with industrial development, the use of motor is very general, motor provides a large amount of stable power in the industrial production, the normal operation of machinery can be ensured, the manpower of at substantial is not needed to manufacture, save human cost, a lot of motor often produces a large amount of heats when in use at present, these heats can not well emit, the normal operation of motor can be affected, too increase the heat in workshop, can not well produce, heat also can cause motor to form condensed water, condensed water can not discharge for a long time, the corrosion of motor parts can be caused, have impact on the normal use of motor.
Summary of the invention
It is simple that the purpose of this utility model is to provide a kind of structure, and heat distributes the anti-electric motor with superheat automatic protector of fast one.
The technical solution of the utility model is: a kind of anti-electric motor with superheat automatic protector, comprise fuselage, described body upper is provided with terminal box, described terminal box has connector, described connector is connected with stator, rotor is provided with outside described stator, described stator adopts cylindrical stator, described front fuselage is provided with screens end cap, described screens end cap is connected with fuselage by bolt, control module is provided with in described fuselage, Temperature Controlling Chip is provided with in described control module, described Temperature Controlling Chip is connected with warming infrared module, described warming infrared module is positioned at the upper end of stator, described Temperature Controlling Chip is provided with pin, described pin connects power input, described power input is connected with terminal box, rear end cap is provided with on rear side of described fuselage, fan is provided with after described rear end cap, protective device is provided with outside described fan, described protective device is fine-structure mesh fan housing.
Water circle device is provided with outside described fuselage, corrugation is provided with outside described fuselage, pore is provided with in described corrugation, described pore is connected with water circle device, described water circle device is made up of water pump and tube connector, described water circle device is connected by cable with Temperature Controlling Chip, and described water circle device can carry out cooling water circulation automatically.
Described fuselage adopts thin iron casting, and described fuselage bottom is provided with center rest, and described center rest is provided with concave groove, and described concave groove is provided with and is fixedly connected with pin, and the described pin that is fixedly connected with adopts round end connecting pin.
The utility model has the advantages that: in fuselage, establish attemperating unit; motor can be allowed to play a protective role when in use; can lower the temperature when temperature is too high time; do not need those operations artificial, improve the operational effect of motor, outside fuselage, be provided with water circle device; can be lowered the temperature by water-cooled; taken away by the heat of water circulation by motor, protect motor, the useful life of motor can be extended.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Fig. 2 is left view of the present utility model.
In figure, 1 is fuselage, and 2 is terminal box, and 3 is stator, and 4 is rotor, and 5 is screens end cap, and 6 is control module, and 7 is rear end cap, and 8 is protective device, and 9 is water circle device, and 10 is corrugation, and 11 is Temperature Controlling Chip, and 12 is center rest.
Embodiment
Below in conjunction with accompanying drawing, the utility model is further illustrated.
A kind of anti-electric motor with superheat automatic protector, comprise fuselage 1, terminal box 2 is provided with above fuselage 1, terminal box 2 has connector, connector is connected with stator 3, rotor 4 is provided with outside stator 3, stator 3 adopts cylindrical stator, fuselage 1 front end is provided with screens end cap 5, screens end cap 5 is connected with fuselage by bolt, control module 6 is provided with in fuselage 1, Temperature Controlling Chip is provided with in control module 6, Temperature Controlling Chip is connected with warming infrared module, warming infrared module is positioned at the upper end of stator 3, Temperature Controlling Chip is provided with pin, pin connects power input, power input is connected with terminal box 2, rear end cap 7 is provided with on rear side of fuselage 1, fan is provided with after rear end cap 7, protective device 8 is provided with outside fan, protective device 8 is fine-structure mesh fan housing, water circle device 9 is provided with outside fuselage 1, corrugation 10 is provided with outside fuselage 1, pore is provided with in corrugation 10, pore is connected with water circle device 9, water circle device 9 is made up of water pump and tube connector, water circle device 9 is connected by cable with Temperature Controlling Chip 11, water circle device 9 can carry out cooling water circulation automatically, fuselage 1 adopts thin iron casting, center rest 12 is provided with bottom fuselage 1, center rest 12 is provided with concave groove, concave groove is provided with and is fixedly connected with pin, be fixedly connected with pin and adopt round end connecting pin.

Claims (3)

1. an anti-electric motor with superheat automatic protector, comprise fuselage, it is characterized in that: described body upper is provided with terminal box, described terminal box has connector, described connector is connected with stator, rotor is provided with outside described stator, described stator adopts cylindrical stator, described front fuselage is provided with screens end cap, described screens end cap is connected with fuselage by bolt, control module is provided with in described fuselage, Temperature Controlling Chip is provided with in described control module, described Temperature Controlling Chip is connected with warming infrared module, described warming infrared module is positioned at the upper end of stator, described Temperature Controlling Chip is provided with pin, described pin connects power input, described power input is connected with terminal box, rear end cap is provided with on rear side of described fuselage, fan is provided with after described rear end cap, protective device is provided with outside described fan, described protective device is fine-structure mesh fan housing.
2. the anti-electric motor with superheat automatic protector of one according to claim 1; it is characterized in that: outside described fuselage, be provided with water circle device; corrugation is provided with outside described fuselage; pore is provided with in described corrugation; described pore is connected with water circle device; described water circle device is made up of water pump and tube connector, and described water circle device is connected by cable with Temperature Controlling Chip, and described water circle device can carry out cooling water circulation automatically.
3. the anti-electric motor with superheat automatic protector of one according to claim 1; it is characterized in that: described fuselage adopts thin iron casting; described fuselage bottom is provided with center rest; described center rest is provided with concave groove; described concave groove is provided with and is fixedly connected with pin, and the described pin that is fixedly connected with adopts round end connecting pin.
CN201420507690.5U 2014-09-04 2014-09-04 A kind of anti-electric motor with superheat automatic protector Expired - Fee Related CN204168070U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420507690.5U CN204168070U (en) 2014-09-04 2014-09-04 A kind of anti-electric motor with superheat automatic protector

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420507690.5U CN204168070U (en) 2014-09-04 2014-09-04 A kind of anti-electric motor with superheat automatic protector

Publications (1)

Publication Number Publication Date
CN204168070U true CN204168070U (en) 2015-02-18

Family

ID=52541719

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420507690.5U Expired - Fee Related CN204168070U (en) 2014-09-04 2014-09-04 A kind of anti-electric motor with superheat automatic protector

Country Status (1)

Country Link
CN (1) CN204168070U (en)

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20150218

Termination date: 20170904

CF01 Termination of patent right due to non-payment of annual fee