CN203091959U - Multifunctional butt welding mold for motor frame - Google Patents
Multifunctional butt welding mold for motor frame Download PDFInfo
- Publication number
- CN203091959U CN203091959U CN 201220660574 CN201220660574U CN203091959U CN 203091959 U CN203091959 U CN 203091959U CN 201220660574 CN201220660574 CN 201220660574 CN 201220660574 U CN201220660574 U CN 201220660574U CN 203091959 U CN203091959 U CN 203091959U
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- CN
- China
- Prior art keywords
- annular matrix
- positioning disk
- slidable adjustment
- adjustment plate
- multiple purpose
- 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 - Lifetime
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- Moulds For Moulding Plastics Or The Like (AREA)
Abstract
The utility model discloses a multifunctional butt welding mold for a motor frame. The multifunctional butt welding mold comprises an annular base body, a positioning disk, sliding adjustment plates, enclosure angle plate fixing blocks and an enclosure positioning block, wherein the positioning disk is arranged in the annular base body, is in threaded connection with the annular base body and can vertically move; three sliding adjustment plates are respectively connected with the upper end surface of the annular base body and can make adjusting movement in the circumferential direction along the upper end surface of the annular base body; three enclosure angle plate fixing blocks are respectively connected onto the three sliding adjustment plates and can move along with the sliding adjustment plates; and the enclosure positioning block is connected onto the upper end of the positioning disk. According to the multifunctional butt welding mold disclosed by the utility model, operation steps are simple and convenient; the butt welding of the motor frames of various products can be met; and in the process of replacing the motor frames with different model numbers, the three enclosure angle plate fixing blocks are moved to adjust the angle and the positioning disk is rotated to adjust the height of the enclosure positioning block.
Description
Technical field
The utility model relates to a kind of mould, relates in particular to a kind of multiple purpose aeroplane seat butt-joint mould.
Background technology
For the workshop of a production motor new product, the sample characteristics of manufacturing are that product is new, and model is many, and are little in batches, and the time of delivery is short.Because product shape is various, when the support butt-joint of new product motor, run into situations such as the height of stand corner plate and angle and Standard Module do not match through regular meeting.Subject matter is: the product stand corner plate height dimensional requirement of different model is inconsistent, and the angle disunity.In order to guarantee support butt-joint quality, or manual splicing mould, speed is fast but shortcoming is a unstable product quality; Make new die on request, steady quality but shortcoming is that the manufacturing cycle is long causes the lot of manpower and material resources waste.
Summary of the invention
The purpose of this utility model in order to solve the problem that above-mentioned prior art exists, provides a kind of multiple purpose aeroplane seat butt-joint mould exactly.
In order to achieve the above object, the utility model has adopted following technical scheme: a kind of multiple purpose aeroplane seat butt-joint mould, and it comprises:
The annular matrix;
Positioning disk, it is arranged in the annular matrix and with the annular matrix and is threaded and can moves up and down;
The slidable adjustment plate, totally three, the adjusting that also can make circumferencial direction along the upper surface of annular matrix that links to each other with the upper surface of annular matrix is respectively moved;
Casing gusset fixed block, is connected on three slidable adjustment plates and can moves with the slidable adjustment plate by totally three;
The casing locating piece is connected the upper end of positioning disk.
The upper end of described annular matrix is provided with flange, evenly be interval with three arc-shaped slots that axially connect on the flange, the bottom of described slidable adjustment plate is provided with the circular arc projection, realizes linking to each other with the upper surface of annular matrix and can doing moving of circumferencial direction along the upper surface of annular matrix in the arc-shaped slot of slidable adjustment plate by its circular arc projection insertion annular matrix.
The top of described positioning disk is provided with one section undergauge section that is formed by reduced diameter, and the undergauge section is provided with one section slotted eye that radially connects, described casing locating piece by this slotted eye be connected positioning disk the upper end and can left and right adjusting.
Described slidable adjustment plate is connected with the annular matrix is detachable, and described casing gusset fixed block is connected with the slidable adjustment plate is detachable.
The threaded connection relation of described positioning disk and annular matrix adopts the pitch of M100 * 0.75.
Utility model multiple purpose aeroplane seat butt-joint mould has following advantage and characteristics owing to adopted above technical scheme:
(1) existing support butt-joint mould only is applicable to single product, can not finish two or more different products simultaneously, and interchangeability is relatively poor, and the utility model multiple purpose aeroplane seat butt-joint mould is applicable to the product of different size.
(2) three casing gusset fixed blocks can move with the slidable adjustment plate, help regulating the angle position of three casing gusset fixed blocks, are fit to the various angle supports of processing.
(3) positioning disk in the middle of the mould is designed to be threaded with the annular matrix, can change its high and low position by the rotation positioning disk, and use the pitch of M100 * 0.75, can accurately regulate the product height, through measuring every half-twist, the height variation has only 0.18mm.
Description of drawings
Fig. 1 is the structural representation of facing of the utility model multiple purpose aeroplane seat butt-joint mould;
Fig. 2 is the plan structure schematic diagram;
Fig. 3 is the D-D sectional structure schematic diagram of Fig. 2;
Fig. 4 is the perspective view of the annular matrix in the utility model;
Fig. 5 is the perspective view of the positioning disk in the utility model;
Fig. 6 is the perspective view of the slidable adjustment plate in the utility model;
Fig. 7 is the perspective view of the casing gusset fixed block in the utility model;
Fig. 8 is the perspective view of the casing locating piece in the utility model.
The specific embodiment
Referring to Fig. 1, cooperate referring to Fig. 2, Fig. 3, the utility model multiple purpose aeroplane seat butt-joint mould comprises annular matrix 1, positioning disk 2, slidable adjustment plate 3, casing gusset fixed block 4 and casing locating piece 5.
Cooperation is referring to Fig. 4, and the upper end of the annular matrix 1 in the utility model is provided with flange, evenly is interval with three arc-shaped slots 11 that axially connect on the flange.
Cooperation is referring to Fig. 5, positioning disk 2 in the utility model is arranged in the annular matrix 1 and with the annular matrix and is threaded and can moves up and down, be provided with one section undergauge section that forms by reduced diameter on the top of positioning disk 2, the undergauge section is provided with one section slotted eye 21 that radially connects, casing locating piece 5 by this slotted eye be connected positioning disk the upper end and can left and right adjusting.Positioning disk 2 adopts the pitch of M100 * 0.75 with the threaded connection relation of annular matrix 1.
Cooperation is referring to Fig. 6, and the adjusting of totally three circumferencial directions that link to each other with the upper surface of annular matrix 1 respectively and can do along the upper surface of annular matrix of the slidable adjustment plate 3 in the utility model moves; Be provided with circular arc projection 31 in the bottom of slidable adjustment plate 3, slidable adjustment plate 3 links to each other with the upper surface of annular matrix and can do moving of circumferencial direction along the upper surface of annular matrix by arc-shaped slot 11 interior realizations that its circular arc projection 31 inserts annular matrix 1.
Cooperation is referring to Fig. 7, the casing gusset fixed block 4 in the utility model totally three be connected on three slidable adjustment plates 3 and can move with the slidable adjustment plate.
Cooperation is referring to Fig. 8, and the casing locating piece 5 in the utility model is connected the upper end of positioning disk.
Slidable adjustment plate in the utility model is connected with the annular matrix is detachable, and casing gusset fixed block is connected with the slidable adjustment plate is detachable.
The utility model multiple purpose aeroplane seat butt-joint Mould operation step is simple and convenient, in the process of changing the different model motor case, adjust angle as long as move three casing gusset fixed blocks, rotating positioning disk again, to adjust the high low dimensional of casing gusset fixed block just passable, do not need other odd parts of demolition, installation.The advantage that embodies is that applicability is strong, can satisfy the support butt-joint of various products, manipulates very conveniently, and it is very fast to regulate various different product speed, the average per adjusting that just can finish a product in 20 minutes.The mould of present this structure has also guaranteed the uniformity of new product support butt-joint quality when improving the replacing product type, provide assurance for accelerating exploitation new product speed.
Claims (5)
1. multiple purpose aeroplane seat butt-joint mould is characterized in that comprising:
The annular matrix;
Positioning disk, it is arranged in the annular matrix and with the annular matrix and is threaded and can moves up and down;
The slidable adjustment plate, totally three, the adjusting that also can make circumferencial direction along the upper surface of annular matrix that links to each other with the upper surface of annular matrix is respectively moved;
Casing gusset fixed block, is connected on three slidable adjustment plates and can moves with the slidable adjustment plate by totally three;
The casing locating piece is connected the upper end of positioning disk.
2. multiple purpose aeroplane seat butt-joint mould according to claim 1, it is characterized in that: the upper end of described annular matrix is provided with flange, evenly be interval with three arc-shaped slots that axially connect on the flange, the bottom of described slidable adjustment plate is provided with the circular arc projection, realizes linking to each other with the upper surface of annular matrix and can doing moving of circumferencial direction along the upper surface of annular matrix in the arc-shaped slot of slidable adjustment plate by its circular arc projection insertion annular matrix.
3. multiple purpose aeroplane seat butt-joint mould according to claim 1, it is characterized in that: the top of described positioning disk is provided with one section undergauge section that is formed by reduced diameter, the undergauge section is provided with one section slotted eye that radially connects, described casing locating piece by this slotted eye be connected positioning disk the upper end and can left and right adjusting.
4. multiple purpose aeroplane seat butt-joint mould according to claim 1, it is characterized in that: described slidable adjustment plate is connected with the annular matrix is detachable, and described casing gusset fixed block is connected with the slidable adjustment plate is detachable.
5. multiple purpose aeroplane seat butt-joint mould according to claim 1 is characterized in that: the threaded connection relation of described positioning disk and annular matrix adopts the pitch of M100 * 0.75.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220660574 CN203091959U (en) | 2012-12-04 | 2012-12-04 | Multifunctional butt welding mold for motor frame |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220660574 CN203091959U (en) | 2012-12-04 | 2012-12-04 | Multifunctional butt welding mold for motor frame |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203091959U true CN203091959U (en) | 2013-07-31 |
Family
ID=48843403
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220660574 Expired - Lifetime CN203091959U (en) | 2012-12-04 | 2012-12-04 | Multifunctional butt welding mold for motor frame |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203091959U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102962575A (en) * | 2012-12-04 | 2013-03-13 | 上海日用-友捷汽车电气有限公司 | Multi-purpose frame butt-welding die |
| CN104858339A (en) * | 2015-04-24 | 2015-08-26 | 深圳市源明杰科技有限公司 | Line-winding and butt-welding integrated equipment and method |
-
2012
- 2012-12-04 CN CN 201220660574 patent/CN203091959U/en not_active Expired - Lifetime
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102962575A (en) * | 2012-12-04 | 2013-03-13 | 上海日用-友捷汽车电气有限公司 | Multi-purpose frame butt-welding die |
| CN104858339A (en) * | 2015-04-24 | 2015-08-26 | 深圳市源明杰科技有限公司 | Line-winding and butt-welding integrated equipment and method |
| CN104858339B (en) * | 2015-04-24 | 2017-02-01 | 深圳源明杰科技股份有限公司 | Line-winding and butt-welding integrated equipment and method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20130731 |