CN201210116Y - Initiative and follow-up loading structure experiment system - Google Patents
Initiative and follow-up loading structure experiment system Download PDFInfo
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- CN201210116Y CN201210116Y CNU2008200880745U CN200820088074U CN201210116Y CN 201210116 Y CN201210116 Y CN 201210116Y CN U2008200880745 U CNU2008200880745 U CN U2008200880745U CN 200820088074 U CN200820088074 U CN 200820088074U CN 201210116 Y CN201210116 Y CN 201210116Y
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Abstract
The utility model relates to a testing system with an active and tracking loading structure, which comprises a bearing framework, a horizontal loading actuator and a vertical loading actuator. A sample is respectively connected with a vertical micro detecting device and a horizontal micro detecting device; a vertical servo tracking actuator is arranged at the side of the horizontal loading actuator; a horizontal servo tracking actuator is positioned at the side of the vertical loading actuator; and the vertical micro detecting device, the vertical servo tracking actuator, the horizontal micro detecting device and the horizontal servo tracking actuator are respectively connected with a computer control system. The utility model can ensure that the vertical testing force can maintain in the vertical state in the testing process all the time and can not be influenced by the horizontal deformation of the tested sample; and the utility model can ensure that the horizontal testing force can maintain in the horizontal state in the testing process all the time and can not be influenced by the vertical deformation of the tested sample.
Description
(1) technical field
The utility model relates to a kind of structural test system of initiatively following moving value-added tax function that has.
(2) background technology
The large-sized structure experiment system is a kind of large-scale instrument that is used for the test structure mechanical property, its development and development, to the infrastructure that must build in the modernization of the country process of construction such as: the design check of super-high buildings, subway, airport, office building, auditoriums, hotels, Longspan Bridge, airliner, space shuttle, jumbo ship, ocean platform, atomic power station etc., optimize, checking has landmark meaning.
In national economy extensive developing period, above-mentioned all kinds of structure Design are based on analogy method, be design precisely or rationality is not the emphasis of considering.Such method for designing is mainly being to use in the design of conventional material and conventional structure, although heuristic methods has bigger design error, because forefathers' experience and relatively advanced computer Simulation calculation technology, final result or acceptable are arranged.
Enter 21st century, the develop rapidly that modernization of the country is built, various new constructions, new material emerge in an endless stream, all kinds of contradictions that product and engineering maximization, integration and complicated developing direction and shortage of resources cause, the analogy design has run into increasing challenge, the application of new construction and new material causes not having the successful experience that similarly can use for reference, and the risk of ultra-large engineering design and the general requirement that reduces cost that economizes on resources also become even more important and essential to the verification experimental verification of heavy construction in the design phase.And the research of the structure that must consider in design and use process problem such as technical indicator such as the distortion of (load, vibration, high low temperature, burn into weathering) and fracture strength and various structural entity serviceability, reinforced concrete structure non-linear behaviour under complicated external condition need also become increasingly conspicuous.
Because application standard sample or small-scale model are inferred the complete reliable data that are difficult to obtain the one-piece construction performance, in order to satisfy the above-mentioned requirements of outwardness, modern structural experiment must be finished by the single component test in past and test and the full size cun conversion of testing to one-piece construction.And the structure of forming for compound substance, even carry out multi parameter analysis with computing machine and also be difficult to infer, must carry out for guaranteeing safety near practical structures or full-scale test.Simultaneously, the science and technology development particularly develop rapidly of computer technology, electronic technology, automatic control technology and hydraulic servo technology provides solid foundation for the development of structural test and monitoring technology, for design, test and the monitoring of various labyrinths provides sound assurance, promoted the development of structural design theory.Therefore, in the world each state all in the development research of being devoted to the large-sized structure experiment instrument.
Existing large scale structure experimental system generally includes bearing frame, level loads actuator, vertical loading actuator, and level loading actuator and vertical loading actuator are installed on the loading frame respectively and act on sample.In the process of the test, load the hydraulic test power that actuator applies if tested sample is subjected to level, the distortion that will produce horizontal direction can not guarantee that hydraulic test power remains horizontality in process of the test; Equally,, will produce vertical distortion, can not guarantee that vertical test power remains at plumbness in process of the test, will produce than mistake like this when structural experiment if tested sample is subjected to the vertical test power that vertical loading actuator applies.
(3) utility model content
Technical problem to be solved in the utility model is to provide a kind of and has active with moving value-added tax function, can make tested sample not be subjected to the structural test system of level and vertical deformation effect.
Described active is with moving loading structure pilot system, comprise that bearing frame, level load actuator, vertical loading actuator, level loading actuator and vertical loading actuator are installed on the loading frame respectively and act on sample, described sample connects vertical jiggle detecting device and horizontal jiggle detecting device respectively, vertical jiggle detecting device is provided with vertical micro-displacement sensor, and horizontal jiggle detecting device is provided with horizontal micro-displacement sensor; Described level loads the actuator side and is provided with the level that acts on and loads actuator and make the vertical servo with moving actuator of its vertical deviation, vertical servo be provided with moving actuator vertical with moving displacement transducer; Described vertical loading actuator side is provided with the horizontal servo that acts on vertical loading actuator and make its horizontal shift and follows moving actuator, and horizontal servo is provided with level with moving displacement transducer with moving actuator; Described vertical jiggle detecting device, vertical servo moving actuator, horizontal jiggle detecting device, the horizontal servo of following connect computer control system respectively with moving actuator.
Further, described horizontal jiggle detecting device is positioned at the effect end of vertical loading actuator and sample, and horizontal jiggle detecting device is connected with sample by vertical ball pivot; Described vertical jiggle detecting device is positioned at the effect end that level loads actuator and sample, and vertical jiggle detecting device is connected with sample by horizontal ball pivot.
Further, describedly vertically servoly be provided with vertically with moving displacement transducer with moving actuator, described horizontal servo is provided with level with moving displacement transducer with moving actuator.Vertical effect with moving displacement transducer is to guarantee vertically to be in the closed-loop control state all the time with moving control, and the level that prevents loads the passive of actuator and moves.Level is that the assurance level is in the closed-loop control state all the time with moving control with the effect of moving displacement transducer, prevents that the passive of vertical loading actuator from moving.
Further, the link of described vertical loading actuator and bearing frame is provided with the horizontal linear guide rail, and bearing frame is fixedlyed connected with the horizontal linear guide rail, and vertical loading actuator and horizontal linear guide rail are slidingly connected; The link that described level loads actuator and bearing frame is provided with vertical line slideway, and bearing frame is fixedlyed connected with vertical line slideway, and level loads actuator and vertical line slideway is slidingly connected.
The effect of above-mentioned horizontal linear guide rail is to guarantee that the friction force between vertical loading actuator and the bearing frame is very little when being subjected to being up to the vertical test power of 10000kN, horizontal servo with moving actuator still can be freely with moving and can not produce creeping phenomenon.
The effect of above-mentioned vertical line slideway is to guarantee that the friction force that level loads between actuator and the bearing frame is very little when being subjected to being up to the vertical test power of 3000kN, vertical servo with moving actuator still can be freely with moving and can not produce creeping phenomenon.
The utility model can guarantee that the vertical test power that vertical loading actuator is applied on the tested sample remains at plumbness in process of the test, thereby is not subjected to level to load the influence that actuator is applied to the tested sample horizontal distortion that the hydraulic test power on the sample causes; And the assurance level loads the hydraulic test power that actuator is applied on the tested sample remain horizontality in process of the test, thereby is not subjected to vertical loading actuator to be applied to the influence of the vertical distortion of tested sample that the vertical test power on the sample causes.
(4) description of drawings
Fig. 1 is the structural representation of the described active of embodiment with moving loading structure pilot system.
(5) embodiment
Below by embodiment the utility model is made preferably specific description, but protection domain of the present utility model is not limited to this.
With reference to Fig. 1, a kind of active is with moving loading structure pilot system, comprise that bearing frame 1, level load actuator 2, vertical loading actuator 3, level loading actuator 2 and vertical loading actuator 3 are installed on the loading frame 1 respectively and act on sample 4, described sample 4 connects vertical jiggle detecting device 5 and horizontal jiggle detecting device 6 respectively, vertical jiggle detecting device 5 is provided with vertical micro-displacement sensor 7, and horizontal jiggle detecting device 6 is provided with horizontal micro-displacement sensor 8; Described level loads actuator 2 sides and is provided with the level that acts on and loads actuator 2 and make the vertical servo with moving actuator 9 of its vertical deviation, and described vertical loading actuator 3 sides are provided with the horizontal servo that acts on vertical loading actuator 3 and make its horizontal shift with moving actuator 11; Described vertical jiggle detecting device 5, vertical servo moving actuator 9, horizontal jiggle detecting device 6, the horizontal servo of following connect computer control system 13 respectively with moving actuator 11.
Described horizontal jiggle detecting device 6 is positioned at the effect end of vertical loading actuator 3 and sample 4, and horizontal jiggle detecting device 6 is connected with sample 4 by vertical ball pivot 14; Described vertical jiggle detecting device 5 is positioned at the effect end that level loads actuator 2 and sample 4, and vertical jiggle detecting device 5 is connected with sample 4 by horizontal ball pivot 15.
Describedly vertically servoly be provided with vertically with moving displacement transducer 10 with moving actuator 9, described horizontal servo is provided with level with moving displacement transducer 12 with moving actuator 11.
Described vertical loading actuator 3 is provided with horizontal linear guide rail 16 with the link of bearing frame 1, and bearing frame 1 is fixedlyed connected with horizontal linear guide rail 16, and vertical loading actuator 3 is slidingly connected with horizontal linear guide rail 16; The link that described level loads actuator 2 and bearing frame 1 is provided with vertical line slideway 17, and bearing frame 1 is fixedlyed connected with vertical line slideway 17, and level loads actuator 2 and is slidingly connected with vertical line slideway 17.
In the process of the test, if tested sample is subjected to level and loads the hydraulic test power FH that actuator 2 applies, produce the distortion S2 of horizontal direction, horizontal micro-displacement sensor 8 on the horizontal jiggle detecting device 6 detects sample and has produced horizontal shift S3 (because have joint gap between level loading actuator and the sample, so, S2〉S3) and transfer to computer control system 13, computer control system 13 is sent instruction and is given level servo with moving actuator 11, promote vertical loading actuator 3 along continuous straight runs with moving, when horizontal micro-displacement sensor 8 detected horizontal shift S3 were reduced to target value set, computer control system was sent instruction and is failed with moving actuator 11 to level is servo.
If tested sample is subjected to the vertical test power F that vertical loading actuator 3 applies
VAnd the distortion S1 of generation vertical direction, vertical micro-displacement sensor 7 on the vertical jiggle detecting device 5 detects sample and has produced vertical deviation S4 (because have joint gap between level loading actuator 2 and the sample 4, so, S1〉S4) and transfer to computer control system 13, computer control system 13 is sent instruction and is given vertical servo with moving actuator 9, the promotion level loads actuator 2 vertically with moving, when vertical micro-displacement sensor 7 detected horizontal shift S4 were reduced to target value set, computer control system 11 was sent instruction and is given vertical servoly fail with moving actuator 9.
Claims (5)
1, a kind of active is with moving loading structure pilot system, comprise that bearing frame, level load actuator, vertical loading actuator, level loading actuator and vertical loading actuator are installed on the loading frame respectively and act on sample, it is characterized in that: described sample connects vertical jiggle detecting device and horizontal jiggle detecting device respectively, vertical jiggle detecting device is provided with vertical micro-displacement sensor, and horizontal jiggle detecting device is provided with horizontal micro-displacement sensor; Described level loads the actuator side and is provided with the level that acts on and loads actuator and make the vertical servo with moving actuator of its vertical deviation, and described vertical loading actuator side is provided with the horizontal servo that acts on vertical loading actuator and make its horizontal shift with moving actuator; Described vertical jiggle detecting device, vertical servo moving actuator, horizontal jiggle detecting device, the horizontal servo of following connect computer control system respectively with moving actuator.
2, active according to claim 1 is characterized in that with moving loading structure pilot system described horizontal jiggle detecting device is positioned at the effect end of vertical loading actuator and sample, and horizontal jiggle detecting device is connected with sample by vertical ball pivot; Described vertical jiggle detecting device is positioned at the effect end that level loads actuator and sample, and vertical jiggle detecting device is connected with sample by horizontal ball pivot.
3, active according to claim 1 and 2 is with moving loading structure pilot system, it is characterized in that describedly vertically servoly being provided with vertically with moving displacement transducer with moving actuator, and described horizontal servo is provided with level with moving displacement transducer with moving actuator.
4, active according to claim 1 and 2 is with moving loading structure pilot system, the link that it is characterized in that described vertical loading actuator and bearing frame is provided with the horizontal linear guide rail, bearing frame is fixedlyed connected with the horizontal linear guide rail, and vertical loading actuator and horizontal linear guide rail are slidingly connected; The link that described level loads actuator and bearing frame is provided with vertical line slideway, and bearing frame is fixedlyed connected with vertical line slideway, and level loads actuator and vertical line slideway is slidingly connected.
5, active according to claim 3 is with moving loading structure pilot system, the link that it is characterized in that described vertical loading actuator and bearing frame is provided with the horizontal linear guide rail, bearing frame is fixedlyed connected with the horizontal linear guide rail, and vertical loading actuator and horizontal linear guide rail are slidingly connected; The link that described level loads actuator and bearing frame is provided with vertical line slideway, and bearing frame is fixedlyed connected with vertical line slideway, and level loads actuator and vertical line slideway is slidingly connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008200880745U CN201210116Y (en) | 2008-05-30 | 2008-05-30 | Initiative and follow-up loading structure experiment system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008200880745U CN201210116Y (en) | 2008-05-30 | 2008-05-30 | Initiative and follow-up loading structure experiment system |
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| Publication Number | Publication Date |
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| CN201210116Y true CN201210116Y (en) | 2009-03-18 |
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| Application Number | Title | Priority Date | Filing Date |
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| CNU2008200880745U Expired - Lifetime CN201210116Y (en) | 2008-05-30 | 2008-05-30 | Initiative and follow-up loading structure experiment system |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101290269B (en) * | 2008-05-30 | 2010-10-13 | 杭州邦威机电控制工程有限公司 | Initiative and follow-up loading structure experiment system |
| CN103940627A (en) * | 2014-04-11 | 2014-07-23 | 同济大学 | Bidirectional sliding device suitable for civil engineering space loading test |
| CN104102229A (en) * | 2014-07-09 | 2014-10-15 | 苏州筑邦测控科技有限公司 | Active actuator tracing system |
| CN106706284A (en) * | 2016-11-23 | 2017-05-24 | 上海宇航系统工程研究所 | Simplified verification method for bearing capacity of support type multi-sphere storage box |
-
2008
- 2008-05-30 CN CNU2008200880745U patent/CN201210116Y/en not_active Expired - Lifetime
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101290269B (en) * | 2008-05-30 | 2010-10-13 | 杭州邦威机电控制工程有限公司 | Initiative and follow-up loading structure experiment system |
| CN103940627A (en) * | 2014-04-11 | 2014-07-23 | 同济大学 | Bidirectional sliding device suitable for civil engineering space loading test |
| CN104102229A (en) * | 2014-07-09 | 2014-10-15 | 苏州筑邦测控科技有限公司 | Active actuator tracing system |
| CN104102229B (en) * | 2014-07-09 | 2017-02-01 | 苏州筑邦测控科技有限公司 | Active actuator tracing system |
| CN106706284A (en) * | 2016-11-23 | 2017-05-24 | 上海宇航系统工程研究所 | Simplified verification method for bearing capacity of support type multi-sphere storage box |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20090318 Effective date of abandoning: 20080530 |