CN202340173U - Double-frequency hysteresis synchronous motor - Google Patents

Double-frequency hysteresis synchronous motor Download PDF

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Publication number
CN202340173U
CN202340173U CN2011205080042U CN201120508004U CN202340173U CN 202340173 U CN202340173 U CN 202340173U CN 2011205080042 U CN2011205080042 U CN 2011205080042U CN 201120508004 U CN201120508004 U CN 201120508004U CN 202340173 U CN202340173 U CN 202340173U
Authority
CN
China
Prior art keywords
bearing
synchronous motor
bifrequency
casing
enclosure
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
CN2011205080042U
Other languages
Chinese (zh)
Inventor
朱志能
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.)
Guizhou Aerospace Linquan Motor Co Ltd
Original Assignee
Guizhou Aerospace Linquan 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 Guizhou Aerospace Linquan Motor Co Ltd filed Critical Guizhou Aerospace Linquan Motor Co Ltd
Priority to CN2011205080042U priority Critical patent/CN202340173U/en
Application granted granted Critical
Publication of CN202340173U publication Critical patent/CN202340173U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model discloses a double-frequency hysteresis synchronous motor, which comprises an enclosure. A stator core (6) and an armature winding (7) are arranged in the enclosure (4). A front bearing (3) and a front bearing cap (2) are arranged at the front end of the enclosure (4). A rear end cover (9) is arranged at the rear end of the enclosure (4). A rear bearing (8) is arranged in a bearing hole of the end cover (9). A rear bearing cap (10) fixedly presses the end cover (9) on the enclosure (4) through a bolt. A rotor shaft (1) with a non-magnetic conducting material structure is arranged on the front bearing (3) and the rear bearing (8). A rotor core (5) with a hysteresis material structure is fixed on the rotor shaft (1). The double-frequency hysteresis synchronous motor has the advantage of capability of normally working under two different power frequencies, simple structure, wide application range and low manufacture cost and use cost.

Description

A kind of bifrequency hysteresis synchronous motor
Technical field
the utility model relates to a kind of bifrequency hysteresis synchronous motor, belongs to the motor manufacture technology field.
Background technology
are present, and synchronous machine of the prior art generally can only be worked under the power drives under single, the specific frequency, can not be used for the power drives of two kinds of different frequencies.When adopting this motor that is applicable to the single-frequency power supply in running, to have defective because of control or system, can't guarantee motor under its basic frequency during operate as normal, this motor is out of service, thereby system is affected.So the motor of existing this single-frequency work still can not satisfy the needs of use.
Summary of the invention
The purpose of the utility model is, provide a kind of simple in structure, and can be under two kinds of different electrical power frequencies the bifrequency hysteresis synchronous motor of operate as normal, to overcome the deficiency of prior art.
The technical scheme of the utility model is to constitute like this: a kind of bifrequency hysteresis synchronous motor of the utility model; Comprise casing; Stator core and armature winding are housed in casing, fore bearing and front bearing retainer are installed, end cap is installed in the rear end of casing at the front end of casing; Rear bearing is installed in the dead eye of end cap; Rear bearing cover presses solidly end cap on casing through bolt, and the armature spindle of non-magnet material structure is installed on fore bearing and rear bearing, and on armature spindle, is fixed with the rotor core of hysteresis material structure.
are provided with the input power connector end that is connected with bifrequency AC power driving governor on above-mentioned armature winding.
The supply frequency of above-mentioned bifrequency AC power driving governor output that is connected with the input power connector end of armature winding is 120Hz or 80Hz.
Owing to adopted technique scheme, the utility model can be worked under the input power supply of two kinds of different frequencies .Adopt same the motor of the utility model under the mode of operation of two frequencies, to switch, when this motor operates in main operating frequency (120Hz) process, it is big that the load of system becomes; Step-out appears in motor; When making system's cisco unity malfunction,, make machine operation under task frequency (80Hz) mode of operation through the frequency of Switching power; Reaching increases synchronous torque and locked-rotor torque, makes system works under slow-speed of revolution synchronous operation pattern.Adopt the technical scheme of the utility model, motor can be worked down in two frequencies (rotating speed), the utility model is not changing under motor size, the weight situation, makes motor performance index reach backup, has increased reliability.So, the utility model compared with prior art, the utility model not only have can be under two kinds of different electrical power frequencies the advantage of operate as normal, but also have simple in structure, range of application is wide, cost of manufacture and all low advantage of use cost.
Description of drawings
Fig. 1 is the structural representation of the utility model.
Being labeled as in accompanying drawing: 1-armature spindle, 2-front bearing retainer, 3-fore bearing, 4-casing, 5-rotor core, 6-stator core, 7-armature winding, 7.1-power connector end, 8-rear bearing, 9-end cap, 10-rear bearing cover.
Embodiment
are further described the utility model below in conjunction with accompanying drawing and embodiment, but not as the foundation to the utility model restriction.
The embodiment of the utility model: the structural representation of a kind of bifrequency hysteresis synchronous motor of the utility model is as shown in Figure 1; This motor comprises casing 4; Traditional stator core 6 and armature winding 7 are housed in casing 4, at the front end of casing 4 fore bearing 3 and front bearing retainer 2 are installed, during making; An end cap 9 is installed in rear end at casing 4; Rear bearing 8 is installed in the dead eye of end cap 9, and rear bearing cover 10 is pressed solidly end cap 9 on casing 4 through bolt, on fore bearing 3 and rear bearing 8, install the armature spindle 1 of a non-magnet material structure; Make the employing of armature spindle 1 and can adopt the higher non-magnet material of intensity of the prior art; Like materials such as stainless steel, alloy aluminum, and at the rotor core 5 of fixing the hysteresis material structure on the armature spindle 1, it is the magnetic hysteresis alloy rod making of 2J25 that rotor core 5 preferably adopts model; On armature winding 7, produce the input power connector end 7.1 that can be connected simultaneously with the bifrequency AC power; And when using the utility model, the supply frequency of the bifrequency AC power that will be connected with the input power connector end 7.1 of armature winding 7 is chosen as the bifrequency AC power of 120Hz or 80Hz.

Claims (3)

1. bifrequency hysteresis synchronous motor; Comprise casing (4), stator core (6) and armature winding (7) are housed in casing (4), fore bearing (3) and front bearing retainer (2) are installed at the front end of casing (4); It is characterized in that; In the rear end of casing (4) end cap (9) is installed, rear bearing (8) is installed in the dead eye of end cap (9), and rear bearing cover (10) presses solidly end cap (9) on casing (4) through bolt; The armature spindle (1) of non-magnet material structure is installed on fore bearing (3) and rear bearing (8), and on armature spindle (1), is fixed with the rotor core (5) of hysteresis material structure.
2. bifrequency hysteresis synchronous motor according to claim 1 is characterized in that: on armature winding (7), be provided with the input power connector end (7.1) that is connected with bifrequency AC power driving governor.
3. bifrequency hysteresis synchronous motor according to claim 2 is characterized in that: the supply frequency of the bifrequency AC power driving governor output that is connected with the input power connector end (7.1) of armature winding (7) is 120Hz or 80Hz.
CN2011205080042U 2011-12-08 2011-12-08 Double-frequency hysteresis synchronous motor Expired - Fee Related CN202340173U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2011205080042U CN202340173U (en) 2011-12-08 2011-12-08 Double-frequency hysteresis synchronous motor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2011205080042U CN202340173U (en) 2011-12-08 2011-12-08 Double-frequency hysteresis synchronous motor

Publications (1)

Publication Number Publication Date
CN202340173U true CN202340173U (en) 2012-07-18

Family

ID=46488860

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2011205080042U Expired - Fee Related CN202340173U (en) 2011-12-08 2011-12-08 Double-frequency hysteresis synchronous motor

Country Status (1)

Country Link
CN (1) CN202340173U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109462309A (en) * 2018-10-30 2019-03-12 中国船舶重工集团公司第七0七研究所 The miniature hysteresis synchronous motor of aircraft inertia platform

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109462309A (en) * 2018-10-30 2019-03-12 中国船舶重工集团公司第七0七研究所 The miniature hysteresis synchronous motor of aircraft inertia platform

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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: 20120718

Termination date: 20171208

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