CN205130445U - Rotor cuts hydraulic press - Google Patents
Rotor cuts hydraulic press Download PDFInfo
- Publication number
- CN205130445U CN205130445U CN201520975464.4U CN201520975464U CN205130445U CN 205130445 U CN205130445 U CN 205130445U CN 201520975464 U CN201520975464 U CN 201520975464U CN 205130445 U CN205130445 U CN 205130445U
- Authority
- CN
- China
- Prior art keywords
- rotor
- bed die
- hydraulic press
- hydraulic cylinder
- utility
- 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
Links
Abstract
The utility model relates to a hydraulic press especially relates to a rotor cuts hydraulic press. The utility model provides a rotor cuts hydraulic press includes fuselage, support frame, oil hydraulic cylinder, power supply, goes up mould and bed die, on oil hydraulic cylinder fixed mounting and the support frame, it fixes at the piston of oil hydraulic cylinder epaxially to go up the mould, the bed die sets up on the board of fuselage, be equipped with a plurality of draw -in grooves that are used for blocking the rotor on the bed die, go up the punching pin of the hole one -to -one that is equipped with a plurality of and rotor on the mould, the both sides of bed die are equipped with the locating lever, and the position that upward corresponds the locating lever on the mould is equipped with the locating hole. The utility model has the advantages that: the utility model discloses a rotor cuts hydraulic press, it is rational in infrastructure, can improve work efficiency, reduce staff's intensity of labour, excellent in use effect, the practicality is strong.
Description
Technical field
The utility model relates to a kind of hydraulic press, particularly relates to a kind of rotor and cuts hydraulic press.
Background technology
Motor rotor or engine rotor are through casting formation, general is all that several casting together forms, have casting liquid adhesion between rotor and rotor, need the part of adhesion to cut, to be all that staff is hand-held cut instrument to traditional mode that cuts, manually cut, not only waste time and energy, inefficiency, and also job security is low, therefore, a kind of new technical scheme should be provided to solve the problem.
Summary of the invention
The purpose of this utility model is: for above-mentioned deficiency, and provide a kind of rational in infrastructure, the rotor that result of use is good cuts hydraulic press.
For achieving the above object, the technical solution adopted in the utility model is:
Rotor cuts hydraulic press, comprise fuselage, bracing frame, oil hydraulic cylinder, power source, mold and bed die, described oil hydraulic cylinder fixed installation is with on bracing frame, described mold is fixed on the piston axle of oil hydraulic cylinder, described bed die is arranged on the board of fuselage, described bed die is provided with multiple draw-in groove for blocking rotor, described mold is provided with endoporus punching pin one to one that is multiple and rotor, the both sides of described bed die are provided with backstay, and on mold, the position of corresponding backstay is provided with locating hole.
The bottom bilateral symmetry of described bed die is provided with the back-up block that a group supports bed die, and the bottom of described back-up block contacts with board.
Also comprise a blow device, described blow device comprises a gas blow pipe, and the end of described gas blow pipe is provided with blow head, and the other end of gas blow pipe is connected with high-pressure air source.
Container cavity is provided with between described back-up block.
Described gas blow pipe is resilientiy stretchable flexible pipe.
Due to the application of technique scheme, the utility model compared with prior art tool has the following advantages:
Rotor of the present utility model cuts hydraulic press, rational in infrastructure, can increase work efficiency, and reduce the labour intensity of staff, result of use is good, practical.
Accompanying drawing explanation
Accompanying drawing 1 is the utility model structural representation.
In above accompanying drawing: 1, fuselage, 2, bracing frame, 3, oil hydraulic cylinder, 4, power source, 5, bed die, 6, piston axle, 7, board, 8, draw-in groove, 9, punching pin, 10, backstay, 11, locating hole, 12, mold, 13, back-up block, 14, container cavity, 15, gas blow pipe, 16, blow head, 17, high-pressure air source.
Detailed description of the invention
Below in conjunction with drawings and Examples, the utility model is further described:
Embodiment one:
As shown in Figure 1, the utility model rotor cuts hydraulic press, comprise fuselage 1, bracing frame 2, oil hydraulic cylinder 3, power source 4, mold 12 and bed die 5, described oil hydraulic cylinder 3 fixedly mounts with on bracing frame 2, described mold 12 is fixed on the piston axle 6 of oil hydraulic cylinder 3, described bed die 5 is arranged on the board 7 of fuselage 1, described bed die 5 is provided with multiple draw-in groove 8 for blocking rotor, described mold 12 is provided with endoporus punching pin 9 one to one that is multiple and rotor, the both sides of described bed die 5 are provided with backstay 10, on mold 12, the position of corresponding backstay 10 is provided with locating hole 11.
Preferably, as an embodiment, the bottom bilateral symmetry of described bed die 5 is provided with the back-up block 13 that a group supports bed die 5, and the bottom of described back-up block 13 contacts with board 7.
Preferably, as another embodiment, the hydraulic press that cuts of the present utility model also comprises a blow device, described blow device comprises a gas blow pipe 15, the end of described gas blow pipe 15 is provided with blow head 16, the other end of gas blow pipe 15 is connected with high-pressure air source 17, and described gas blow pipe 15 is Telescopic flexible pipe.
Rotor of the present utility model cuts hydraulic press, in use, rotor is placed in the draw-in groove 8 of bed die 5, mold 12 moves downward under the drive of the piston axle 6 of oil hydraulic cylinder 3, punching pin 9 on mold 12 is inserted in the centre bore of rotor, under gravity, rotor drops in container cavity 14, has cut.The edge of the foundry goods that cutting on mould can be got off by blow device purges clean, to ensure follow-up to cut work.
The above is preferred embodiment of the present utility model; should be understood that; for those skilled in the art; under the prerequisite not departing from principle described in the utility model; can also make some improvement or replacement, these improve or replace and also should be considered as protection domain of the present utility model.
Claims (5)
1. a rotor cuts hydraulic press, it is characterized in that: comprise fuselage (1), bracing frame (2), oil hydraulic cylinder (3), power source (4), mold (12) and bed die (5), described oil hydraulic cylinder (3) is fixedly installed on bracing frame (2), described mold (12) is fixed on the piston axle (6) of oil hydraulic cylinder (3), described bed die (5) is arranged on the board (7) of fuselage (1), described bed die (5) is provided with multiple draw-in groove (8) for blocking rotor, described mold (12) is provided with endoporus punching pin (9) one to one that is multiple and rotor, the both sides of described bed die (5) are provided with backstay (10), the position of the upper corresponding backstay (10) of mold (12) is provided with locating hole (11).
2. a kind of rotor according to claim 1 cuts hydraulic press, it is characterized in that: the bottom bilateral symmetry of described bed die (5) is provided with the back-up block (13) that a group supports bed die (5), and the bottom of described back-up block (13) contacts with board (7).
3. a kind of rotor according to claim 1 cuts hydraulic press, it is characterized in that: also comprise a blow device, described blow device comprises a gas blow pipe (15), the end of described gas blow pipe (15) is provided with blow head (16), and the other end of gas blow pipe (15) is connected with high-pressure air source (17).
4. a kind of rotor according to claim 2 cuts hydraulic press, it is characterized in that: be provided with container cavity (14) between described back-up block (13).
5. a kind of rotor according to claim 3 cuts hydraulic press, it is characterized in that: described gas blow pipe (15) is resilientiy stretchable flexible pipe.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201520975464.4U CN205130445U (en) | 2015-11-27 | 2015-11-27 | Rotor cuts hydraulic press |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201520975464.4U CN205130445U (en) | 2015-11-27 | 2015-11-27 | Rotor cuts hydraulic press |
Publications (1)
Publication Number | Publication Date |
---|---|
CN205130445U true CN205130445U (en) | 2016-04-06 |
Family
ID=55616266
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201520975464.4U Expired - Fee Related CN205130445U (en) | 2015-11-27 | 2015-11-27 | Rotor cuts hydraulic press |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN205130445U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109290423A (en) * | 2018-10-17 | 2019-02-01 | 毛建国 | A kind of road vehicle component stamping device |
-
2015
- 2015-11-27 CN CN201520975464.4U patent/CN205130445U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109290423A (en) * | 2018-10-17 | 2019-02-01 | 毛建国 | A kind of road vehicle component stamping device |
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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: 20160406 Termination date: 20181127 |
|
CF01 | Termination of patent right due to non-payment of annual fee |