CN203608000U - Motor structure with aviation plug - Google Patents

Motor structure with aviation plug Download PDF

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Publication number
CN203608000U
CN203608000U CN201320794447.1U CN201320794447U CN203608000U CN 203608000 U CN203608000 U CN 203608000U CN 201320794447 U CN201320794447 U CN 201320794447U CN 203608000 U CN203608000 U CN 203608000U
Authority
CN
China
Prior art keywords
aviation plug
rivet
hexagonal
screw
motor structure
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
CN201320794447.1U
Other languages
Chinese (zh)
Inventor
刘岸
黄国辉
王庆威
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.)
KUNSHAN SENLIMA ELECTRIC MOTOR CO Ltd
Original Assignee
KUNSHAN SENLIMA ELECTRIC 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 KUNSHAN SENLIMA ELECTRIC MOTOR CO Ltd filed Critical KUNSHAN SENLIMA ELECTRIC MOTOR CO Ltd
Priority to CN201320794447.1U priority Critical patent/CN203608000U/en
Application granted granted Critical
Publication of CN203608000U publication Critical patent/CN203608000U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model discloses a motor structure with an aviation plug, which comprises an aviation plug (1), a fan cover (4) and a plurality of screws (2). The motor structure with the aviation plug is characterized by further comprising hexagonal rivets (3) whose number is identical to that of the screws, wherein the rivets are punched on the fan cover (4), a threaded hole (31) is knocked out in the hexagonal rivet (3) after the rivet is punched, the screw (2) and the threaded hole (31) in the hexagonal rivet (3) realize threaded fastening so as to fix the aviation plug (1) on the fan cover (4). The motor structure disclosed by the utility model enables installation and later-period maintenance and disassembling of the aviation plug to be more convenient and simpler, thereby greatly saving time and cost, and improving the production efficiency.

Description

With the electric machine structure of aviation plug
Technical field
The utility model relates to a kind of electric machine structure with aviation plug.
Background technology
The mode that the common electric machine structure with aviation plug of existing market is installed as shown in Figure 3, aviation plug (1) is fixed on fan housing (4) above by screw (2), then uses nut (5) by fastening aviation plug (1).The electric machine structure form that this kind installed aviation plug manufacture and application process in there are a lot of defects: if aviation plug damages or air plug bonding wire comes off in the process using, need to change aviation plug or again first whole fan housing will be dismantled when bonding wire, whole process is also with the dismounting of blower fan lead-in wire or brake lead-in wire, specialty and complicated relatively, waste time and energy, safeguard more difficult, greatly increase maintenance cost; With in the nut process that aviation plug is fastening, because nut is smaller, and also invisible in fan housing the inside in the process of operation, this just brings certain difficulty to assembling, causes inefficiency.
Utility model content
Safeguard and change difficult problem in order to solve aviation plug, the utility model provides a kind of electric machine structure with aviation plug.The technical solution of the utility model is: include an aviation plug, fan housing, several screw, also include the hexagonal rivet identical with screw number; Its rivet punching press, on fan housing, is got screwed hole again after rivet punching press completes on hexagonal rivet, and the screwed hole on screw and hexagonal rivet is realized screw threads for fastening aviation plug is fixed on fan housing.
The utility model adopts the beneficial effect of above technical scheme to be:. aviation plug can directly be fixed on above the hexagonal rivet that is threaded hole by screw, as long as turn on screw in the time of dismounting aviation plug, so just whole fan housing is not dismantled, there is no the dismounting of blower fan lead-in wire or brake lead-in wire yet, thereby make the installation of aviation plug and later maintenance dismounting convenient simple, greatly save time and cost; The hexagonal rivet simultaneously adopting is standard component, can on market, buy easily and relative low price, also can enhance productivity and reduce production costs.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the cross-sectional view of hexagonal rivet described in the utility model;
Fig. 3 is existing electric machine structure schematic diagram.
In figure, 1 aviation plug, 2 screws, 3 hexagonal rivets, 31 screwed holes, 4 fan housings, 5 nuts.
Embodiment
As shown in Figure 1, the utility model includes an aviation plug 1, fan housing 4, several screw 2, also includes the hexagonal rivet 3 identical with screw number; Its rivet punching press, on fan housing 4, as shown in Figure 2, is got screwed hole 31 after rivet punching press completes on hexagonal rivet 3 again, and screw 2 is realized screw threads for fastening with the screwed hole on hexagonal rivet 3 aviation plug 1 is fixed on fan housing 4; As long as turn on screw in the time of dismounting aviation plug, so just whole fan housing is not dismantled, there is no the dismounting of blower fan lead-in wire or brake lead-in wire, thereby make the installation of aviation plug and later maintenance dismounting convenient simply, and greatly save time and cost yet; Described hexagonal rivet is standard component, on market, can buy easily.
Above-mentioned embodiment is exemplary, is to be the restriction that this patent is comprised to scope in order better to make those skilled in the art can understand this patent, can not to be interpreted as; As long as the technology contents essence made according to the disclosed technical scheme of this patent is identical or be equal to any change or modification, all fall into the scope that this patent comprises.

Claims (1)

1. with an electric machine structure for aviation plug, include an aviation plug (1), a fan housing (4), several screw (2), it is characterized in that: also include the hexagonal rivet (3) identical with screw number; Its rivet punching press is upper at fan housing (4), gets screwed hole (31) after rivet punching press completes on hexagonal rivet (3) again, and screw (2) is realized screw threads for fastening with the screwed hole on hexagonal rivet (3) aviation plug (1) is fixed on fan housing (4).
CN201320794447.1U 2013-12-06 2013-12-06 Motor structure with aviation plug Expired - Fee Related CN203608000U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201320794447.1U CN203608000U (en) 2013-12-06 2013-12-06 Motor structure with aviation plug

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201320794447.1U CN203608000U (en) 2013-12-06 2013-12-06 Motor structure with aviation plug

Publications (1)

Publication Number Publication Date
CN203608000U true CN203608000U (en) 2014-05-21

Family

ID=50720658

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201320794447.1U Expired - Fee Related CN203608000U (en) 2013-12-06 2013-12-06 Motor structure with aviation plug

Country Status (1)

Country Link
CN (1) CN203608000U (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
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20140521

Termination date: 20181206