CN2630832Y - Nonmetal plate rupture modulus testing machine - Google Patents
Nonmetal plate rupture modulus testing machine Download PDFInfo
- Publication number
- CN2630832Y CN2630832Y CN 03207586 CN03207586U CN2630832Y CN 2630832 Y CN2630832 Y CN 2630832Y CN 03207586 CN03207586 CN 03207586 CN 03207586 U CN03207586 U CN 03207586U CN 2630832 Y CN2630832 Y CN 2630832Y
- Authority
- CN
- China
- Prior art keywords
- belt
- worktable
- guide rail
- column
- testing machine
- 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
Images
Landscapes
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
Abstract
The utility model relates to a nonmetallic material test machine. The test machine consists of a stand (1), a worktable (3), a frame (4), an upper cantilever beam (5), a force-measuring device (6), an upper pressure head (7), a column (13) and a driving device. The worktable (3) is fixed with the frame (4) to be integral. The driving device consists of a belt (10), an adjustable speed motor (11), a belt pulley (12) and a lead screw (15), the lead screw (15) is arranged on the belt pulley (12), and is connected with the adjustable speed motor (11) by the belt (10). The column is provided with a guide rail (14), the upper cantilever beam (5) which matches and is connected with the lead screw is provided on the guide rail (14). The utility model has a unique frame structure, can test large, severe nonmetallic plates, can satisfy the requirements of equal displacement, equal load loading modes and various test standards.
Description
Technical field
The utility model belongs to the mechanical hook-up field, particularly relates to a kind of nonmetallic material testing machine, tool.
Background technology
Existing nonmetal plate adopts C type open type fuselage or two column fuselage as anti-reflecting bending strength test machines such as Ceramic Tiles, device for measuring force and seaming chuck are fixed on the top or entablature of fuselage, and worktable and the push-down head that is placed on it place on following of fuselage or the base.Tested sheet material is placed on the push-down head.During test, by being contained in the driving mechanism-gas-liquid conversion cylinder in the base or the oil cylinder push work platform is up, load, up to surface of the work contact seaming chuck, the device for measuring force open type dynamometry that links to each other with seaming chuck is up to the test of finishing the modulus of rupture.Because this testing machine structure and afterburning mode have certain limitation, are difficult to large-scale, heavy test specimen is tested.Special needs to be pointed out is: such testing machine can not satisfy stipulate in the new test method wait the displacement load mode, etc. the requirement of load load mode.
Summary of the invention
The purpose of this utility model is at existing nonmetallic material testing machine, above shortcomings part, a kind of model structure uniqueness is provided, can test big, heavy nonmetal plate, and can satisfy etc. displacement, etc. the novel metalloid sheet material modulus of rupture testing machine of load load mode requirement.
The technical solution of the utility model is such.This testing machine comprises frame, worktable, support, upper cantilever beam, device for measuring force, seaming chuck, column and drive unit.The utility model has been abandoned traditional C type fuselage form, and worktable and support are fixed as one.Drive unit comprises belt, buncher, belt pulley and leading screw, and leading screw is installed on the belt pulley, and is connected with buncher by belt.The column that is fixed on the base is equipped with guide rail, is connected the upper cantilever beam that cooperates with leading screw and is installed on the guide rail.
The utlity model has following remarkable result: 1, worktable and base are one, and device for measuring force is descending under the driving mechanism effect, and it is motionless that test specimen keeps, and can guarantee measuring accuracy effectively; But 2 testing larges, heavy nonmetal plate; 3, can satisfy etc. displacement, etc. load load mode and various test standard requirement; 4 airframe structure uniquenesses, modern design.
Brief Description Of Drawings
Fig. 1 is a structural representation of the present utility model.
Fig. 2 is that the A of the utility model Fig. 1 is to synoptic diagram.
Each parts of the present utility model are: 1-frame 2-fixed head 3-worktable 4-support 5-upper cantilever beam 6-device for measuring force 7-seaming chuck 8-sample 9-free beam 10-belt 11-buncher 12-belt pulley 13-column 14-guide rail 15-leading screw 16-balance bob 17-test specimen fulcrum
As shown in the figure, the utility model worktable (3) and support (4) are fixed as one, and leading screw (15) is installed on the belt pulley (12), and are connected with buncher (11) by belt (10).Guide rail (14) is housed on the column (13), is connected with leading screw and cooperates to such an extent that upper cantilever beam (5) is installed on the guide rail (14).
Embodiment
Embodiment is in conjunction with Fig. 1, Fig. 2 explanation.
The utility model column (13) is fixed on the support (4), and worktable (3) is fixed as one with support (4), and the size of worktable can be extended to both sides according to the size of test specimen.Guide rail (14) is housed on the column (13), and the big I of column and guide rail is according to the situation design of maximum test force.Driving mechanism comprises belt (10), buncher (11), belt pulley (12) and leading screw (15).Upper cantilever beam (5) moves at driving mechanism effect lower edge guide rail.Device for measuring force (6) is installed in the front end bottom of upper cantilever beam (5), and seaming chuck (7) is fixed on the bottom of device for measuring force (6).During work, it is descending that drive unit drags upper cantilever beam (5), lead the test specimen (8) on the push-down head of the free beam (9) that is placed on worktable until seaming chuck (7) contact, load beginning, rupture up to test specimen (8), measured the maximum, force value and handled by device for measuring force, the up return of upper cantilever beam (5) is waited for on-test next time afterwards.
Load mode can be according to the test standard requirement of test specimen, the selection displacement load mode of Denging or etc. the load load mode.
Drive unit of the present utility model can be a leading screw screw mechanism, also can be mechanism forms such as rack-and-pinion, hydraulic jack, gas-liquid conversion cylinder.
Claims (2)
1, a kind of novel metalloid sheet material modulus of rupture testing machine, comprise frame (1), worktable (3), support (4), upper cantilever beam (5), device for measuring force (6), seaming chuck (7), column (13) and drive unit, it is characterized in that: worktable (3) and support (4) are fixed as one, drive unit comprises belt (10), buncher (11), belt pulley (12) and leading screw (15), leading screw (15) is installed on the belt pulley (12), and be connected with buncher (11) by belt (10), guide rail (14) is housed on the column (13), is connected the upper cantilever beam (5) that cooperates with leading screw and is installed on the guide rail (14).
2, a kind of novel metalloid sheet material modulus of rupture testing machine according to claim 1 is characterized in that drive unit can be a leading screw screw mechanism, also can be rack-and-pinion, hydraulic jack, gas-liquid conversion cylinder mechanism form.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 03207586 CN2630832Y (en) | 2003-08-14 | 2003-08-14 | Nonmetal plate rupture modulus testing machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 03207586 CN2630832Y (en) | 2003-08-14 | 2003-08-14 | Nonmetal plate rupture modulus testing machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2630832Y true CN2630832Y (en) | 2004-08-04 |
Family
ID=34288446
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 03207586 Expired - Fee Related CN2630832Y (en) | 2003-08-14 | 2003-08-14 | Nonmetal plate rupture modulus testing machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2630832Y (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101829709A (en) * | 2010-05-14 | 2010-09-15 | 威海市宝威渔具有限公司 | Rod winder |
| CN101233402B (en) * | 2005-07-26 | 2011-08-31 | 空中客车法国公司 | Apparatus for testing a fuselage structure having a longitudinal and circumferential curvature |
| WO2021017185A1 (en) * | 2019-07-27 | 2021-02-04 | 南京昱晟机器人科技有限公司 | Intelligent machining device and strength detection mechanism for sheet materials |
| CN112557018A (en) * | 2020-12-24 | 2021-03-26 | 苏州拓博机械设备有限公司 | Cantilever type rack bearing test machine |
-
2003
- 2003-08-14 CN CN 03207586 patent/CN2630832Y/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101233402B (en) * | 2005-07-26 | 2011-08-31 | 空中客车法国公司 | Apparatus for testing a fuselage structure having a longitudinal and circumferential curvature |
| CN101829709A (en) * | 2010-05-14 | 2010-09-15 | 威海市宝威渔具有限公司 | Rod winder |
| CN101829709B (en) * | 2010-05-14 | 2012-09-05 | 威海市宝威渔具有限公司 | Rod winder |
| WO2021017185A1 (en) * | 2019-07-27 | 2021-02-04 | 南京昱晟机器人科技有限公司 | Intelligent machining device and strength detection mechanism for sheet materials |
| CN112557018A (en) * | 2020-12-24 | 2021-03-26 | 苏州拓博机械设备有限公司 | Cantilever type rack bearing test machine |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN2630832Y (en) | Nonmetal plate rupture modulus testing machine | |
| CN200950102Y (en) | 300 ton rubber bearing pressing-shear-transfer full-automatic test machine | |
| CN213091418U (en) | Reciprocating push-pull workpiece detection tool | |
| CN213986762U (en) | Jacking positioning transfer mechanism of square battery cell module | |
| CN201287220Y (en) | Charpy key hole specimen break broaching machine | |
| CN201193978Y (en) | Lifting device for falling experiment bench | |
| CN212621487U (en) | Wheel shaft clamping and fixing device | |
| CN205483243U (en) | At last pneumatic testing arrangement who measures two column type weighing sensor of force standard machine | |
| CN216728308U (en) | Automatic sampling and detecting equipment for pole piece | |
| JP2983922B2 (en) | Perforator | |
| CN215034091U (en) | Multifunctional numerical control material cutting saw | |
| CN111077015A (en) | Dead weight type force standard machine | |
| CN101318293A (en) | Workbench of hydraulic drawing press for sheet | |
| CN2840006Y (en) | Frequency conversion type double-oil cylinder universal material testing machine | |
| CN201195402Y (en) | Balance, pre-tightening type large-scale high-accuracy single-arm hydraulic press | |
| CN206230283U (en) | A kind of vertical machining centre air clamper | |
| CN2820505Y (en) | Guide pole type high precision computer mould closing machine | |
| CN201659427U (en) | Long-length work bench | |
| CN214373955U (en) | Compression testing machine for concrete sample | |
| CN217775366U (en) | Auxiliary tool for clamping and shaping aluminum alloy thin-wall structural part | |
| CN220398432U (en) | Workpiece aperture gauge | |
| CN215551197U (en) | Four-column hydraulic machine for automobile machining | |
| CN220279858U (en) | Stamping die is used in circuit board production | |
| CN217474596U (en) | Laminating device for preventing rigid collision and abrasion | |
| CN221707185U (en) | Fixed-height and energy drop hammer testing machine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |