CN202947853U - Falling weight impact testing stand - Google Patents

Falling weight impact testing stand Download PDF

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Publication number
CN202947853U
CN202947853U CN 201220671341 CN201220671341U CN202947853U CN 202947853 U CN202947853 U CN 202947853U CN 201220671341 CN201220671341 CN 201220671341 CN 201220671341 U CN201220671341 U CN 201220671341U CN 202947853 U CN202947853 U CN 202947853U
Authority
CN
China
Prior art keywords
testing stand
falling weight
tests
impact
impact testing
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
Application number
CN 201220671341
Other languages
Chinese (zh)
Inventor
裴明尧
赵永红
任套牢
张忠国
石农铭
侯林
魏鹏飞
杜会峰
王义猛
程玉斌
杨晋
王云超
李仁杰
李红梅
马靖
贾炎
陈宁
闫来清
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.)
Taiyuan Institute of China Coal Technology and Engineering Group
Shanxi Tiandi Coal Mining Machinery Co Ltd
Original Assignee
Taiyuan Institute of China Coal Technology and Engineering Group
Shanxi Tiandi Coal Mining 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 Taiyuan Institute of China Coal Technology and Engineering Group, Shanxi Tiandi Coal Mining Machinery Co Ltd filed Critical Taiyuan Institute of China Coal Technology and Engineering Group
Priority to CN 201220671341 priority Critical patent/CN202947853U/en
Application granted granted Critical
Publication of CN202947853U publication Critical patent/CN202947853U/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Abstract

The utility model belongs to the technical field of coal mine product test apparatuses and specifically relates to a falling weight impact testing stand, solving the problem that conventional test stands for impact tests are incapable of meeting the needs of the impact tests for coal mine products. The falling weight impact testing stand comprises a body, a base, an upper platform, and a lower platform. The base is mounted on the upper platform and comprises a cabinet form frame, a drive stepping motor, two screw rods, and two polished rods. The body comprises two parallel guide pipes fixedly connected with the bottom of a mounting seat, an impact height adjusting transmission device, a weight body, and a secondary impact preventing device. The beneficial effects of the falling weight impact testing stand are that: the falling weight impact testing stand is applicable to tests of test samples in various sizes and does not affect the transportation due to space problems, and the tests can be conducted after simply placing the test samples onto the lower platform through a forklift.

Description

Drop hammer type shock test bench
Technical field
The utility model belongs to the technical field of colliery product testing device, is specifically related to a kind of drop hammer type shock test bench.
Background technology
Not of uniform size, different because of the colliery series products, testing table requires that various test products are had general adaptability.According to investigation, at present domestic such shock table is all falling weight impact tests of carrying out for tubing, but the pipe-type test specimen is less, so the narrow space of testing table installation test sample can not satisfy the needs of coal mine explosion-proof electric product.
Summary of the invention
The utility model can not satisfy the problem of the needs of colliery product impulse test for the testing table that solves existing impulse test, and a kind of drop hammer type shock test bench is provided.
The utility model adopts following technical scheme to realize:
Drop hammer type shock test bench comprises fuselage, support, upper platform and lower floor's platform of placing test specimen,
Described support is installed on upper platform, support comprises casing shape framework, Driving Stepping Motor and two leading screws, two polished rods, the output shaft of Driving Stepping Motor connects respectively two leading screws by the chain transmission, all supporting on two leading screws have a nut, two nuts connect by mount pad, also be provided with two pilot holes on mount pad, two pilot holes are placed in respectively to consist of on polished rod and are slidably matched;
Described fuselage comprises two parallel guide pipes, shock height adjustment gearing, hammer body and the anti-secondary pulse device that is fixedly connected with bottom mount pad, guide pipe top arranges shock height and adjusts gearing, hammer body is set, the anti-secondary pulse device of guide pipe exit installation in guide pipe.
The relative prior art of the utility model has following beneficial effect: this device is broad because of its riding position, and interfere without miscellaneous part the installation site, and the test specimen that can be applicable to all size is tested.Need the test specimen of forklift transport also more to have superiority for the colliery with heavier test specimen in addition, because its test specimen installation site is broad, can because space problem affects transportation, only not need the test specimen fork is put on platform and can tests.
Description of drawings
Fig. 1 is structural representation of the present utility model,
In figure: the 1-support, 2-fuselage hoisting gear, 3-leading screw group, the 4-shock height is adjusted gearing, 5-upper platform, 6-fuselage, 7-guide pipe, 8-hammer body, 9-test specimen, 10-lower floor platform.
Embodiment
By reference to the accompanying drawings embodiment of the present utility model is described further.
Drop hammer type shock test bench comprises fuselage 6, support 1, upper platform 5 and lower floor's platform 10 of placing test specimen 9, as shown in Figure 1.
Support 1 is installed on upper platform 5, support 1 comprises casing shape framework, Driving Stepping Motor and two leading screws, two polished rods, the output shaft of Driving Stepping Motor connects respectively two leading screws by the chain transmission, all supporting on two leading screws have a nut, two nuts connect by mount pad, also be provided with two pilot holes on mount pad, two pilot holes are placed in respectively to consist of on polished rod and are slidably matched; Two rhizoid thick sticks drive fuselage and move up and down, and two feed rods play the guiding role, and are used for keeping the balance of fuselage, and Driving Stepping Motor drives two rhizoid thick sticks by the chain transmission and synchronously rotates.Support is installed on upper platform, and fuselage hangs on support from upper platform below, and fuselage hoisting gear (leading screw, feed rod and Driving Stepping Motor) can be adjusted the terrain clearance of fuselage, tests with the test products that adapt to different sizes.
Fuselage 6 comprises two parallel guide pipes 7, shock height adjustment gearing, hammer body and the anti-secondary pulse device that is fixedly connected with bottom mount pad, guide pipe 7 tops arrange shock height and adjust gearing 4, the interior hammer body 8 that arranges of guide pipe 7, the guide pipe 7 anti-secondary pulse devices of exits installation.It is the mechanism that promotes hammer body that shock height is adjusted gearing, is mainly caught by stepper motor, driving chain, electromagnetism and puts hammer mechanism, scrambler and electric control box and form, and can rise to the height that needs to tup exactly; Guide pipe shields, and prevents that hammer body from falling to having an accident outward; Hammer body is impact part; Anti-secondary pulse device is mounted in fuselage foot guide pipe exit position, adopts optoelectronic switch to start cylinder and catches the hammer body of being upspring.Shock height is adjusted gearing and anti-secondary pulse device can obtain from prior art.
Lower floor's platform fixedly is placed on ground, is used for the installation test sample.
At the trial, first fuselage is risen, then will test sample and be placed on lower floor's platform, then fuselage is dropped to suitable position, then promote hammer body and test.

Claims (1)

1. a drop hammer type shock test bench, is characterized in that comprising fuselage (6), support (1), upper platform (5) and lower floor's platform (10) of placing test specimen (9),
Described support (1) is installed on upper platform (5), support (1) comprises casing shape framework, Driving Stepping Motor and two leading screws, two polished rods, the output shaft of Driving Stepping Motor connects respectively two leading screws by the chain transmission, all supporting on two leading screws have a nut, two nuts connect by mount pad, also be provided with two pilot holes on mount pad, two pilot holes are placed in respectively to consist of on polished rod and are slidably matched;
Described fuselage (6) comprises two parallel guide pipes (7), shock height adjustment gearing, hammer body and the anti-secondary pulse device that is fixedly connected with bottom mount pad, guide pipe (7) top arranges shock height and adjusts gearing (4), hammer body (8) is set, the anti-secondary pulse device of guide pipe (7) exit installation in guide pipe (7).
CN 201220671341 2012-12-09 2012-12-09 Falling weight impact testing stand Expired - Lifetime CN202947853U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201220671341 CN202947853U (en) 2012-12-09 2012-12-09 Falling weight impact testing stand

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201220671341 CN202947853U (en) 2012-12-09 2012-12-09 Falling weight impact testing stand

Publications (1)

Publication Number Publication Date
CN202947853U true CN202947853U (en) 2013-05-22

Family

ID=48423549

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201220671341 Expired - Lifetime CN202947853U (en) 2012-12-09 2012-12-09 Falling weight impact testing stand

Country Status (1)

Country Link
CN (1) CN202947853U (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103926045A (en) * 2014-04-17 2014-07-16 合肥安达数控技术有限责任公司 Automobile transmission shaft impact performance test rig
CN109238619A (en) * 2018-10-22 2019-01-18 杨佳魏 The multi-axial Impact testing machine examined for auto parts and components
CN110017996A (en) * 2018-10-24 2019-07-16 广州行安德达科技有限公司 A kind of vehicle hub collision stress test equipment
CN111595702A (en) * 2020-07-22 2020-08-28 佛山市公路桥梁工程监测站有限公司 Secondary-strike-prevention galvanized layer adhesion performance testing device

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103926045A (en) * 2014-04-17 2014-07-16 合肥安达数控技术有限责任公司 Automobile transmission shaft impact performance test rig
CN109238619A (en) * 2018-10-22 2019-01-18 杨佳魏 The multi-axial Impact testing machine examined for auto parts and components
CN109238619B (en) * 2018-10-22 2020-04-24 郑州卓达汽车零部件制造有限公司 Multi-axis impact testing machine for automobile part inspection
CN110017996A (en) * 2018-10-24 2019-07-16 广州行安德达科技有限公司 A kind of vehicle hub collision stress test equipment
CN111595702A (en) * 2020-07-22 2020-08-28 佛山市公路桥梁工程监测站有限公司 Secondary-strike-prevention galvanized layer adhesion performance testing device

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C14 Grant of patent or utility model
GR01 Patent grant
CX01 Expiry of patent term

Granted publication date: 20130522

CX01 Expiry of patent term