IEC TS 62727-2012 Photovoltaic systems - Specifications for solar trackers《光伏系统.太阳追踪器规格》.pdf
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1、 IEC/TS 62727 Edition 1.0 2012-05 TECHNICAL SPECIFICATION Photovoltaic systems Specifications for solar trackers IEC/TS 62727:2012(E) colour inside THIS PUBLICATION IS COPYRIGHT PROTECTED Copyright 2012 IEC, Geneva, Switzerland All rights reserved. Unless otherwise specified, no part of this publica
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8、ervice Centre - webstore.iec.ch/csc If you wish to give us your feedback on this publication or need further assistance, please contact the Customer Service Centre: csciec.ch. IEC/TS 62727 Edition 1.0 2012-05 TECHNICAL SPECIFICATION Photovoltaic systems Specifications for solar trackers INTERNATIONA
9、L ELECTROTECHNICAL COMMISSION U ICS 27.160 PRICE CODE ISBN 978-2-83220-122-0 Registered trademark of the International Electrotechnical Commission Warning! Make sure that you obtained this publication from an authorized distributor. colour inside 2 TS 62727 IEC:2012(E) CONTENTS FOREWORD . 5 1 Scope
10、and object 7 2 Terms and definitions . 7 2.1 Photovoltaics (PV) . 7 2.2 Concentrating photovoltaics (CPV) 7 2.3 Concentrator module (CPV module) 7 2.4 Concentrator assembly 8 3 Specifications for solar trackers for PV applications 8 3.1 Specification template . 8 4 Tracker definitions and taxonomy .
11、 10 4.1 General . 10 4.2 Payload types 10 4.2.1 Standard photovoltaic (PV) module trackers 10 4.2.2 Concentrated photovoltaic (CPV) module trackers . 11 4.3 Rotational axes . 11 4.3.1 Single axis trackers . 11 4.3.2 Dual axis trackers 12 4.4 Actuation and control . 14 4.4.1 Architecture . 14 4.4.2 D
12、rive types 14 4.5 Types of tracker control . 15 4.5.1 Passive control 15 4.5.2 Active control. 15 4.5.3 Backtracking 15 4.6 Structural characteristics . 16 4.6.1 Vertical supports 16 4.6.2 Foundation types . 16 4.6.3 Tracker positions . 17 4.6.4 Stow time 17 4.7 Energy consumption 17 4.7.1 Daily ene
13、rgy consumption 17 4.7.2 Stow energy consumption 18 4.8 External elements and interfaces . 18 4.8.1 Foundation 18 4.8.2 Foundation interface 18 4.8.3 Payload . 18 4.8.4 Payload interface . 18 4.8.5 Payload mechanical interface 18 4.8.6 Payload electrical interface 18 4.8.7 Grounding interface . 18 4
14、.8.8 Installation effort 18 4.8.9 Control interface 19 4.9 Internal tolerances . 19 4.9.1 Primary axis tolerance . 19 4.9.2 Secondary axis tolerance 20 4.10 Tracker system elements . 20 TS 62727 IEC:2012(E) 3 4.10.1 Mechanical structure . 20 4.10.2 Tracker controller 20 4.10.3 Sensors . 20 4.11 Reli
15、ability terminology . 20 4.11.1 Mean time between failures (MTBF) 20 4.11.2 Mean time between critical failures (MTBCF) . 21 4.11.3 Mean time to repair (MTTR) . 21 4.12 Environmental conditions 21 4.12.1 Operating temperature range . 21 4.12.2 Survival temperature range 21 4.12.3 Maximum wind during
16、 operation 21 4.12.4 Maximum wind during stow 21 4.12.5 Snow load . 21 4.13 Functional tests . 22 4.13.1 Static load test 22 4.13.2 Moment testing 22 4.13.3 Limit switch operation 22 4.13.4 Manual operation . 22 5 Tracker accuracy characterization 22 5.1 Overview . 22 5.2 Pointing error (instantaneo
17、us) . 22 5.3 Measurement 23 5.3.1 Overview . 23 5.3.2 Example of experimental method to measure pointing error . 23 5.3.3 Calibration of pointing error measurement tool 24 5.4 Calculation of tracker accuracy 24 5.4.1 Overview . 24 5.4.2 Data collection . 25 5.4.3 Data binning by wind speed . 25 5.4.
18、4 Data filtering 26 5.4.5 Data quantity . 26 5.4.6 Accuracy calculations 26 6 Mechanical characterization . 27 6.1 General . 27 6.2 Backlash . 27 6.3 Stiffness 27 7 Reliability testing 28 7.1 Corrosion 28 7.2 Component durability. 28 7.3 Extreme conditions tests . 28 8 Additional optional accuracy c
19、alculations 28 8.1 Typical tracking accuracy range 28 8.2 Tracking error histogram . 29 8.3 Percent of available irradiance as a function of pointing error 29 Figure 1 = Altitude angle = 0 (zenith angle = 90) occurs when a vector normal to the module face is pointing to the horizon. Altitude angle =
20、 90 (zenith angle = 0) occurs when the module is facing the sky . 13 Figure 2 Illustration of primary axis tolerance for a polar tracking axis . 19 4 TS 62727 IEC:2012(E) Figure 3 General illustration of pointing error . 23 Figure 4 Two flat parallel plates at a specified distance, one having a pin
21、hole for sunlight to be tracked on specified-diameter circles that ultimately measure 0,1, 0,2, and 0,3 accuracy rings (more if necessary) . 24 Figure 5 Pointing error frequency distribution for the entire test period . 29 Figure 6 Available irradiance as a function of pointing error . 30 Figure 7 A
22、vailable irradiance as a function of pointing error with binning by wind speed . 30 Table 1 Tracker specification template . 8 Table 2 Alternate tracking accuracy reporting template 27 TS 62727 IEC:2012(E) 5 INTERNATIONAL ELECTROTECHNICAL COMMISSION _ PHOTOVOLTAIC SYSTEMS SPECIFICATIONS FOR SOLAR TR
23、ACKERS FOREWORD 1) The International Electrotechnical Commission (IEC) is a worldwide organization for standardization comprising all national electrotechnical committees (IEC National Committees). The object of IEC is to promote international co-operation on all questions concerning standardization
24、 in the electrical and electronic fields. To this end and in addition to other activities, IEC publishes International Standards, Technical Specifications, Technical Reports, Publicly Available Specifications (PAS) and Guides (hereafter referred to as “IEC Publication(s)”). Their preparation is entr
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