CN203849277U - Outdoor actual measurement apparatus for quickly and freely switching signals with limited data acquisition systems - Google Patents

Outdoor actual measurement apparatus for quickly and freely switching signals with limited data acquisition systems Download PDF

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Publication number
CN203849277U
CN203849277U CN201420282061.7U CN201420282061U CN203849277U CN 203849277 U CN203849277 U CN 203849277U CN 201420282061 U CN201420282061 U CN 201420282061U CN 203849277 U CN203849277 U CN 203849277U
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CN
China
Prior art keywords
signal
aviation plug
data acquisition
boxcar
actual measurement
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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
CN201420282061.7U
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Chinese (zh)
Inventor
戴益民
高阳
刘也
吕卫华
雷静敏
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Hunan University of Science and Technology
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Hunan University of Science and Technology
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Priority to CN201420282061.7U priority Critical patent/CN203849277U/en
Application granted granted Critical
Publication of CN203849277U publication Critical patent/CN203849277U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model discloses an outdoor actual measurement apparatus for quickly and freely switching signals with limited data acquisition systems. A wind speed sensor and a wind pressure sensor are connected with fixed double-row binding post terminal slots through data acquisition wires and then are correspondingly connected with aviation plugs on a signal switching box. According to actually-measured change in the wind direction of a wind field, measuring points required to be monitored are selected by quickly plugging the aviation plugs in order to switch signals connected with data acquisition systems in limited amount. According to actually-measured environmental wind direction, the outdoor actual measurement apparatus emphatically monitors and researches surface wind pressure of a need area as required by using limited data acquisition systems, and provides convenience for outdoor structural wind engineering actual measurement. The outdoor actual measurement apparatus is simple in structure, low in cost, easy to control, and high in precision.

Description

The limited fieldwork device of realizing the conversion of fast reserve signal of data collecting instrument
Technical field
The utility model belongs to civil building field, be specifically related to be a kind ofly mainly used in allly building, structures or the structure data acquisition in the wild such as Loads of Long-span Bridges, ocean platform count in limited situation, carry out the actual measurement device of wind resistance research, by fixed double post groove and signal boxcar etc., can realize the actual measurement device that the wind characteristic parameter changes such as wind direction is carried out to the motor-driven conversion of signal for required emphasis monitored area.
Background technology
The fieldwork device that data collecting instrument is limited realizes the conversion of fast reserve signal is that a class is utilized during signal boxcar surveys in the wild, and data acquisition system (DAS) collection is counted when inadequate, realizes the device that gathers on demand the motor-driven adjustment signal of representative area measuring point.For accurately grasping the effect of typhoon to structure, the full chi actual measurement of general structure need to be arranged large gauge point, and the each measuring point of data acquisition system (DAS) needs more than at least 5000 yuan, want synchronously to survey the data of all measuring points, general R&D institution is difficult to drop into so large financial support, so, can be according to wind vector rule, in finite data acquisition system situation, select representative measuring point to monitor, and almost blank to this research device both at home and abroad, so exploitation this invention has important and real meaning.
Summary of the invention
When the purpose of this utility model is to provide one to be applicable to data acquisition system (DAS) limited amount, carry out monitoring representative area by the semi-automatic actual measurement device of the motor-driven adjustment signals collecting of wind direction, i.e. the limited fieldwork device of realizing the conversion of fast reserve signal of data collecting instrument.It utilizes aviation plug can connect fast and can not change the advantage of sensor signal progress, select representative body structure surface blast region to carry out motor-driven monitoring by change of the wind rule, realize finite data collection measuring point and reach accurately the effectively needed emphasis measured data object of collection, energy implementation structure is simple, cost is low, be easy to control and the high feature of precision.
The purpose of this utility model realizes by the following technical solutions: the limited fieldwork device of realizing the conversion of fast reserve signal of this data collecting instrument, and it comprises fixed double post groove, signal boxcar, aviation plug and signal wire; Aviation plug comprises housing and joint, and the joint of some aviation plugs is movably arranged on first signal boxcar panel, and the housing of corresponding some aviation plugs is installed on secondary signal boxcar panel with it; After wind speed and wind pressure sensor are connected with the first fixed double post groove by signal wire, then need to by signal wire, the first fixed double post groove be connected with the joint of the aviation plug on first signal boxcar according to measuring in batches; The housing of the aviation plug on secondary signal boxcar is connected with the second fixed double post groove by signal wire, and the second fixed double post groove is connected with data acquisition system (DAS) by signal wire; The joint of the aviation plug on first signal boxcar can be extracted from first signal boxcar together with signal wire as required, is connected, thereby realizes the motor-driven connection at aviation plug two ends with the housing of corresponding aviation plug on secondary signal boxcar.
Further, the section of described signal boxcar is groove type, and on panel, housing and the joint of aviation plug installed in perforate, corresponding aviation plug position perforate respectively on biside plate.
Principle of work of the present invention is, by utilizing the motor-driven plug of aviation plug not affect data-signal distortion and quick switching signal advantage, according to actual measurement on-the-spot wind direction and measurement research emphasis monitored area target thereof, monitor under a limited number of prerequisites at data collecting instrument, realize the object of fast reserve conversion collection signal.
When actual coming into operation, also can select according to specific needs the material of signal boxcar, and offer according to aviation plug position the hole that interts signal wire and aviation plug top connection and housing are installed at signal boxcar correspondence position.
As known from the above, the utility model is that one is applicable in a limited number of situations of data acquisition system (DAS), according to the main target of measurement research, according to change of the wind rule, representative measuring point is carried out to the device of field measurement, in conjunction with aviation plug quick-speed plug advantage, this device uses tool and has the following advantages:
(1) actual measurement device of the present utility model is said on the whole, with minimum economic input, obtain the needed measuring point measured data of research, and apparatus structure is simple, and institute takes up space also little, and cost is low, and principle of work is clear, and measured result is good;
(2) actual measurement device of the present invention has utilized aviation plug quick-speed plug advantage, and signal simple and easy and that solve easily under the undistorted prerequisite of collection signal is changed fast.
Brief description of the drawings
Fig. 1 is the structural representation of the utility model embodiment.
Fig. 2 is the view profile of signal boxcar in Fig. 1.
Embodiment
Below in conjunction with drawings and Examples, the utility model will be further described.
Referring to Fig. 1, the present embodiment comprises the first fixed double post groove 1, the second fixed double post groove 2, first signal boxcar 3, secondary signal boxcar 4, aviation plug (comprising joint 5 and housing 6), signal wire 7; The joint 5 of some aviation plugs is movably arranged on the panel of first signal boxcar 3, and the housing 6 of corresponding some aviation plugs is installed on the panel of secondary signal boxcar 4 with it; After air velocity transducer 8 and wind pressure sensor 9 are connected with the first fixed double post groove 1 by signal wire 7, then need to by signal wire, the first fixed double post groove 1 be connected with the joint 5 of the aviation plug on first signal boxcar 3 according to measuring in batches; The housing 6 of the aviation plug on secondary signal boxcar 4 is connected with the second fixed double post groove 2 by signal wire, and the second fixed double post groove 2 is connected with data acquisition system (DAS) 10 by signal wire; The joint 5 of the aviation plug on first signal boxcar 3 can be extracted from first signal boxcar 3 together with signal wire as required, is connected, thereby realizes the motor-driven connection at aviation plug two ends with the housing 6 of corresponding aviation plug on secondary signal boxcar 4.The utility model is pressed actual measurement emphasis monitored area according to wind direction, with signal wire, aviation plug two ends are realized after motor-driven connection, finally with signal wire, the housing of aviation plug 6 is connected and data-signal is passed to data acquisition system (DAS) 10 with the second fixed double post groove 2 and carry out Real-time Collection.
Referring to Fig. 2, the section of signal boxcar is groove type, and on panel, housing and the joint of aviation plug installed in perforate, corresponding aviation plug position perforate respectively on biside plate.Signal boxcar upper surface perforate size determines according to joint and the housing installation site sectional dimension of aviation plug, and lateral opening hole position and size are determined by aviation plug spacing and signal line dimensions.

Claims (2)

1. the limited fieldwork device of realizing the conversion of fast reserve signal of data collecting instrument, is characterized in that: it comprises fixed double post groove, signal boxcar, aviation plug and signal wire; Aviation plug comprises housing and joint, and the joint of some aviation plugs is movably arranged on first signal boxcar panel, and the housing of corresponding some aviation plugs is installed on secondary signal boxcar panel with it; After wind speed and wind pressure sensor are connected with the first fixed double post groove by signal wire, then need to by signal wire, the first fixed double post groove be connected with the joint of the aviation plug on first signal boxcar according to measuring in batches; The housing of the aviation plug on secondary signal boxcar is connected with the second fixed double post groove by signal wire, and the second fixed double post groove is connected with data acquisition system (DAS) by signal wire; The joint of the aviation plug on first signal boxcar can be extracted from first signal boxcar together with signal wire as required, is connected, thereby realizes the motor-driven connection at aviation plug two ends with the housing of corresponding aviation plug on secondary signal boxcar.
2. the limited fieldwork device of realizing fast reserve signal conversion of data collecting instrument according to claim 1, it is characterized in that: the section of described signal boxcar is groove type, on panel, housing and the joint of aviation plug installed in perforate, corresponding aviation plug position perforate respectively on biside plate.
CN201420282061.7U 2014-05-29 2014-05-29 Outdoor actual measurement apparatus for quickly and freely switching signals with limited data acquisition systems Expired - Fee Related CN203849277U (en)

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CN201420282061.7U CN203849277U (en) 2014-05-29 2014-05-29 Outdoor actual measurement apparatus for quickly and freely switching signals with limited data acquisition systems

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420282061.7U CN203849277U (en) 2014-05-29 2014-05-29 Outdoor actual measurement apparatus for quickly and freely switching signals with limited data acquisition systems

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CN203849277U true CN203849277U (en) 2014-09-24

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104407191A (en) * 2014-12-01 2015-03-11 江西洪都航空工业集团有限责任公司 Conversion device of data acquisition system
CN104880293A (en) * 2015-04-02 2015-09-02 苏州中州安勃起重有限公司 Crane wind load modeling method
CN106546374A (en) * 2016-11-24 2017-03-29 中国核动力研究设计院 Static pressure measurement device and flow velocity measuring method in a kind of complex flowfield

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104407191A (en) * 2014-12-01 2015-03-11 江西洪都航空工业集团有限责任公司 Conversion device of data acquisition system
CN104407191B (en) * 2014-12-01 2017-05-17 江西洪都航空工业集团有限责任公司 Conversion device of data acquisition system
CN104880293A (en) * 2015-04-02 2015-09-02 苏州中州安勃起重有限公司 Crane wind load modeling method
CN106546374A (en) * 2016-11-24 2017-03-29 中国核动力研究设计院 Static pressure measurement device and flow velocity measuring method in a kind of complex flowfield
CN106546374B (en) * 2016-11-24 2019-01-22 中国核动力研究设计院 Static pressure measurement device and flow velocity measuring method in a kind of complex flowfield

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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: 20140924

Termination date: 20170529