CN203695836U - Inclining press - Google Patents

Inclining press Download PDF

Info

Publication number
CN203695836U
CN203695836U CN201420090538.1U CN201420090538U CN203695836U CN 203695836 U CN203695836 U CN 203695836U CN 201420090538 U CN201420090538 U CN 201420090538U CN 203695836 U CN203695836 U CN 203695836U
Authority
CN
China
Prior art keywords
fuselage
base
press
inclining
adjusting nut
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
CN201420090538.1U
Other languages
Chinese (zh)
Inventor
张天行
吴健浩
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.)
SHENGZHOU KANGLI MACHINERY CO Ltd
Original Assignee
SHENGZHOU KANGLI MACHINERY 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 SHENGZHOU KANGLI MACHINERY CO Ltd filed Critical SHENGZHOU KANGLI MACHINERY CO Ltd
Priority to CN201420090538.1U priority Critical patent/CN203695836U/en
Application granted granted Critical
Publication of CN203695836U publication Critical patent/CN203695836U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Landscapes

  • Press Drives And Press Lines (AREA)

Abstract

The utility model discloses an inclining press. The inclining press comprises a press body, a base and a supporting unit. Locking nuts, adjusting nuts and adjusting grooves are formed in the base, the adjusting nuts are mounted in the adjusting grooves, the press body is connected with the base through the locking nuts and the adjusting nuts, and the supporting unit is connected with the press body and is arranged at the front end of the base. By means of the inclining press, the inclination of the press can be adjusted as required, the machining requirement of special work-pieces is met, and waste produced by machining can slip down automatically along the inclination surface of a working table.

Description

A kind of tilting-type pressure fuselage
Technical field
The utility model relates to metal forming machinery field, relates in particular to forcing press.
Background technology
In machining; often can run into side punching to workpiece, turn over riveting; common horizontal punch press of the prior art is because workbench is a horizontal plane; cannot meet the processing of special workpiece; and the waste material producing in the time of punching press can be deposited on workbench; workpiece of every processing needs workbench to clear up, and wastes time and energy.
Utility model content
For overcoming above-mentioned deficiency, the utility model provides a kind of tilting-type press frame, meets the processing of special workpiece, and machining produces waste material can be with the automatic landing in the inclined plane of workbench.
The technical solution adopted in the utility model is: a kind of tilting-type pressure fuselage, comprise fuselage, base and bracing or strutting arrangement, described base is provided with locking nut, adjusting nut and regulating tank, adjusting nut is arranged on regulating tank, described fuselage is connected with base with adjusting nut by locking nut, and described bracing or strutting arrangement connects fuselage and is arranged on the front end of base.
Described bracing or strutting arrangement comprises support backing plate and two atmospheric pressure poles, and two atmospheric pressure poles are flexibly connected respectively fuselage and support backing plate.
Described regulating tank is deep-slotted chip breaker.
Effective effect of the present utility model is: when forcing press is adjusted, unclamp locking nut and adjusting nut, regulate the gradient of fuselage, the length of two atmospheric pressure poles and gradient are carried out corresponding adjustment with fuselage, locking nut and adjusting nut again, can complete the setting of fuselage gradient, meet the process requirements of special workpiece, machining produces waste material can be with the automatic landing in the inclined plane of workbench.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model;
Fig. 2 is left view of the present utility model.
In figure: fuselage 1, base 2, bracing or strutting arrangement 3, locking nut 4, adjusting nut 5, regulating tank 6, support backing plate 7, atmospheric pressure pole 8.
Detailed description of the invention
Below in conjunction with drawings and Examples, the utility model is described further.
Shown in Fig. 1 and Fig. 2, a kind of tilting-type pressure fuselage, comprise fuselage 1, base 2 and bracing or strutting arrangement 3, described base 1 is provided with locking nut 4, adjusting nut 5 and regulating tank 6, adjusting nut 5 is arranged on regulating tank 6, described fuselage 1 is connected with base 2 with adjusting nut 5 by locking nut 4, described bracing or strutting arrangement 3 connects fuselage 1 and is arranged on the front end of base 2, described bracing or strutting arrangement 3 comprises support backing plate 7 and two atmospheric pressure poles 8, two atmospheric pressure poles 8 are flexibly connected respectively fuselage 1 and support backing plate 7, and described regulating tank 6 is deep-slotted chip breaker; When forcing press is adjusted, unclamp locking nut 4 and adjusting nut 5, regulate the gradient of fuselage 1, the length of two atmospheric pressure poles 8 and gradient are carried out corresponding adjustment with fuselage 1, locking nut 4 and adjusting nut 5, can complete the setting of fuselage gradient again, convenient and simple.

Claims (3)

1. a tilting-type pressure fuselage, it is characterized in that: comprise fuselage (1), base (2) and bracing or strutting arrangement (3), described base (1) is provided with locking nut (4), adjusting nut (5) and regulating tank (6), adjusting nut (5) is arranged on regulating tank (6), described fuselage (1) is connected with base (2) with adjusting nut (5) by locking nut (4), and described bracing or strutting arrangement (3) connects fuselage (1) and is arranged on the front end of base (2).
2. a kind of tilting-type pressure fuselage according to claim 1, it is characterized in that: described bracing or strutting arrangement (3) comprises support backing plate (7) and two atmospheric pressure poles (8), two atmospheric pressure poles (8) are flexibly connected respectively fuselage (1) and support backing plate (7).
3. a kind of tilting-type pressure fuselage according to claim 1, is characterized in that: described regulating tank (6) is deep-slotted chip breaker.
CN201420090538.1U 2014-02-21 2014-02-21 Inclining press Expired - Fee Related CN203695836U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420090538.1U CN203695836U (en) 2014-02-21 2014-02-21 Inclining press

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420090538.1U CN203695836U (en) 2014-02-21 2014-02-21 Inclining press

Publications (1)

Publication Number Publication Date
CN203695836U true CN203695836U (en) 2014-07-09

Family

ID=51046335

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420090538.1U Expired - Fee Related CN203695836U (en) 2014-02-21 2014-02-21 Inclining press

Country Status (1)

Country Link
CN (1) CN203695836U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107138663A (en) * 2017-06-21 2017-09-08 杨朴 One kind forging belt drop hammer may move polished stake
WO2024057309A1 (en) * 2022-09-12 2024-03-21 Criaterra Innovations Ltd A mold for producing an article of manufacture

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107138663A (en) * 2017-06-21 2017-09-08 杨朴 One kind forging belt drop hammer may move polished stake
WO2024057309A1 (en) * 2022-09-12 2024-03-21 Criaterra Innovations Ltd A mold for producing an article of manufacture

Similar Documents

Publication Publication Date Title
CN104474968B (en) A kind of compound traction forming machine with simple and easy trimming cutter sweep
CN204545123U (en) A kind of diel
CN203695836U (en) Inclining press
CN204747185U (en) Automobile rear drive shell body blanking die
CN104369015A (en) Clamping device
CN201760501U (en) Face frame die
CN104525744A (en) Continuous production die for automobile brake support parts
CN203726208U (en) Auxiliary machining tool for gear pump front cover inclined holes
CN104525743A (en) Continuous production die for automobile activated carbon canister support parts
CN205289407U (en) Mould is cut off to female arranging
CN204221070U (en) The special milling groove craft equipment of a kind of cable Contra wire frame
CN204275916U (en) Compound traction forming machine with simple and easy trimming cutter sweep
CN204975015U (en) Rolling machine mould of adjustable indent width
CN205628978U (en) Simple and easy flattening device
CN202572562U (en) Rattan mat frame rattan-pulling machine for furniture
CN206373236U (en) A kind of quick adjustment clutch damping disk(-isc) part window shaping dies
CN204449454U (en) The plate shearing machine of efficient location
CN104014683B (en) A kind of automatic fetching device
CN204365813U (en) A kind of modified angle bar punching die
CN204109401U (en) A kind of foot-operated press of improvement
CN203917577U (en) A kind of mould of processing groove
CN203817826U (en) Special part processing equipment
CN204108082U (en) A kind of diel of machining gap on thin-walled tubular part
CN203917628U (en) A kind of automobile hand brake bearing mould
CN210188191U (en) Porous stamping die for hardware processing

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: 20140709

Termination date: 20180221