CN102879160A - Multifunctional fixed table for loading machine test - Google Patents

Multifunctional fixed table for loading machine test Download PDF

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Publication number
CN102879160A
CN102879160A CN2012103480730A CN201210348073A CN102879160A CN 102879160 A CN102879160 A CN 102879160A CN 2012103480730 A CN2012103480730 A CN 2012103480730A CN 201210348073 A CN201210348073 A CN 201210348073A CN 102879160 A CN102879160 A CN 102879160A
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CN
China
Prior art keywords
stand
base
fixed station
stationary platform
bracing frame
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.)
Pending
Application number
CN2012103480730A
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Chinese (zh)
Inventor
王青春
陈忠加
陈福军
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.)
Beijing Forestry University
Original Assignee
Beijing Forestry University
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 Beijing Forestry University filed Critical Beijing Forestry University
Priority to CN2012103480730A priority Critical patent/CN102879160A/en
Publication of CN102879160A publication Critical patent/CN102879160A/en
Pending legal-status Critical Current

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Abstract

A multifunctional fixed table for loading machine test comprises a base, an I-shaped fixed platform, and two I-shaped horizontal cross arms, wherein the horizontal cross arms are distributed on both sides of the fixed platform, and can adjust the positions on the base along the length direction of the fixed platform; four vertical stands are respectively mounted on the adjusting holes of the fixed platform and the horizontal cross arms, and the distance from the vertical stands to the base center can be adjusted independently by selecting different adjusting holes; a plurality of rows of adjusting holes are formed on the front side of the vertical stands in the vertical direction; each vertical stand is connected with a support frame through the adjusting holes via bolts; the position of the support frame can be adjusted along the vertical direction of the vertical stand; a plurality of rows of adjusting holes are formed on the upper side of the support frame; and a position-adjustable semi-columnar support is mounted on the adjusting holes. Accordingly, the fixed table provided by the invention can adjust the positions of the horizontal cross arms, the vertical stands, the support frame and the semi-columnar support independently according to the shape of a test piece so as to meet the requirement for loading tests of different complicated parts.

Description

The multi-functional carrier aircraft test fixed station that adds
Technical field
The invention belongs to mechanical engineering field, is a kind of multi-functional carrier aircraft test fixed station that adds.
Background technology
When doing mechanics or vibratory test, test specimen need to be fixed on the test fixed station.Existing test fixed station is regulated inconvenience, but and regulating degree lower.
Summary of the invention
A kind of multi-functional carrier aircraft test fixed station that adds, have stationary platform and horizontal crossbearer, be connected to the stand on the two, the bracing frame and the semicolumn that are connected in the stand support, can be along with the difference of Specimen Shape, regulate the position that single horizontal crossbearer, stand, bracing frame and semicolumn support, thereby adapt to the load test of different complex parts.
The described multi-functional carrier aircraft test fixed station that adds has base, and it act as fixing and supports whole test fixed station, and a plurality of adjustment holes are set on the base; Base is fixedly connected with an I shape stationary platform and two horizontal crossbearers of I shape by the adjustment hole of its top, and horizontal crossbearer is distributed in the stationary platform both sides, and can be on base along the length direction adjusting position of stationary platform.
The described multi-functional carrier aircraft test fixed station that adds, stationary platform and horizontal crossbearer upside have teases and ridicule knothole more, and four stands are installed on the adjustment hole respectively, and stand can select different adjustment holes, therefore can regulate separately the distance that it arrives the base center.
The described multi-functional carrier aircraft test fixed station that adds has on the vertical direction of stand front and teases and ridicule knothole more, and each stand is connected with bolt with a bracing frame respectively by adjustment hole; Bracing frame can be along stand vertical direction adjusting position.
The described multi-functional carrier aircraft test fixed station that adds, the bracing frame upside has teases and ridicule knothole more, and semicolumn supports and is installed on the adjustment hole, and the position can be regulated.
Description of drawings
Accompanying drawing 1 is axonometric drawing of the present invention
The figure number explanation
1-base, 2-stationary platform, the horizontal crossbearer of 3-, 4-stand, 5-bracing frame, 6-semicolumn support.
Embodiment
Accompanying drawing 1 has provided the specific embodiment of the present invention.Below in conjunction with accompanying drawing it is described as follows.
This multi-functional carrier aircraft test fixed station that adds has base (1), and it act as fixing and supports whole test fixed station, and base arranges a plurality of adjustment holes on (1).Base (1) top is fixedly connected with an I shape stationary platform (2) and two horizontal crossbearers of I shape (3), horizontal crossbearer (3) is distributed in stationary platform (2) both sides, and can be at the upper length direction adjusting position along stationary platform (2) of base (1).
Stationary platform (2) and horizontal crossbearer (3) upside have teases and ridicule knothole more, four stands (4) are installed in respectively on the adjustment hole, and stand (4) can be selected different adjustment holes, therefore can regulate separately it to the distance at base (1) center.
Have on the vertical direction of stand (4) front and tease and ridicule knothole more, each stand (4) is connected with bolt with a bracing frame (5) respectively by adjustment hole.Bracing frame (5) can be along stand (4) vertical direction adjusting position.
Bracing frame (5) upside has teases and ridicule knothole more, and semicolumn supports (6) and is installed on the adjustment hole, and the position can be regulated.
Therefore, this test fixed station can be regulated the position that single horizontal crossbearer (3), stand (4), bracing frame (5) and semicolumn support (6) along with the difference of Specimen Shape, thereby adapts to the load test of different complex parts.

Claims (5)

1. the multi-functional carrier aircraft that adds is tested fixed station, have stationary platform and horizontal crossbearer, be connected to the stand on the two, the bracing frame and the semicolumn that are connected in the stand support, above-mentioned part all has adjustment hole, can regulate separately the position that horizontal crossbearer, stand, bracing frame and semicolumn support along with the difference of Specimen Shape, thereby adapt to the load test of different complex parts.
2. the multi-functional carrier aircraft test fixed station that adds as claimed in claim 1 has base, and it act as fixing and supports whole test fixed station, and a plurality of adjustment holes are set on the base; Base is fixedly connected with a stationary platform and two horizontal crossbearers by the adjustment hole of its top, and described stationary platform and horizontal crossbearer are I shape; Horizontal crossbearer is distributed in the stationary platform both sides, and can be on base along the length direction adjusting position of stationary platform.
3. the multi-functional carrier aircraft that adds as claimed in claim 1 is tested fixed station, stationary platform and horizontal crossbearer upside have teases and ridicule knothole more, four stands are fixedly connected on the adjustment hole respectively, and stand can select different adjustment holes, therefore can regulate separately it to the distance at base center.
4. the multi-functional carrier aircraft test fixed station that adds as claimed in claim 1 has on the vertical direction of stand front and teases and ridicule knothole more, and each stand is connected with bolt with a bracing frame respectively by adjustment hole; Bracing frame can be regulated its position along the stand vertical direction.
5. the multi-functional carrier aircraft that adds as claimed in claim 1 is tested fixed station, and the bracing frame upside has teases and ridicule knothole more, and semicolumn supports and is installed on the adjustment hole, and the position can be regulated.
CN2012103480730A 2012-09-19 2012-09-19 Multifunctional fixed table for loading machine test Pending CN102879160A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2012103480730A CN102879160A (en) 2012-09-19 2012-09-19 Multifunctional fixed table for loading machine test

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2012103480730A CN102879160A (en) 2012-09-19 2012-09-19 Multifunctional fixed table for loading machine test

Publications (1)

Publication Number Publication Date
CN102879160A true CN102879160A (en) 2013-01-16

Family

ID=47480571

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2012103480730A Pending CN102879160A (en) 2012-09-19 2012-09-19 Multifunctional fixed table for loading machine test

Country Status (1)

Country Link
CN (1) CN102879160A (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2078663A (en) * 1980-06-24 1982-01-13 Squires Michael Loading and unloading platform for a road trailer
CN201583235U (en) * 2009-11-27 2010-09-15 中国航天科工集团第三研究院第八三五七研究所 Shape and position error contact-type detection measurement bracket device
CN201756808U (en) * 2010-05-31 2011-03-09 中建钢构有限公司 Elevation regulator for installing steel members
CN201899199U (en) * 2010-12-23 2011-07-20 厦门谊和商业道具有限公司 Liftable commodity support frame
CN201945500U (en) * 2010-11-29 2011-08-24 常州亿晶光电科技有限公司 Movable hanger assembly fixing device
CN202433268U (en) * 2012-01-13 2012-09-12 西北工业大学 Broadband measuring device for dynamic mechanical properties of viscous-elastic materials

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2078663A (en) * 1980-06-24 1982-01-13 Squires Michael Loading and unloading platform for a road trailer
CN201583235U (en) * 2009-11-27 2010-09-15 中国航天科工集团第三研究院第八三五七研究所 Shape and position error contact-type detection measurement bracket device
CN201756808U (en) * 2010-05-31 2011-03-09 中建钢构有限公司 Elevation regulator for installing steel members
CN201945500U (en) * 2010-11-29 2011-08-24 常州亿晶光电科技有限公司 Movable hanger assembly fixing device
CN201899199U (en) * 2010-12-23 2011-07-20 厦门谊和商业道具有限公司 Liftable commodity support frame
CN202433268U (en) * 2012-01-13 2012-09-12 西北工业大学 Broadband measuring device for dynamic mechanical properties of viscous-elastic materials

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
王志明: "用于童车测试的加载试验机的研制", 《机械设计与制造》 *

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Application publication date: 20130116