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GB/T 10489-2009: General requirements for aero-derivative gas turbines
Status: Valid GB/T 10489: Evolution and historical versions
| Standard ID | Contents [version] | USD | STEP2 | [PDF] delivered in | Standard Title (Description) | Status | PDF |
| GB/T 10489-2009 | English | 649 |
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General requirements for aero-derivative gas turbines
| Valid |
GB/T 10489-2009
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| GB/T 10489-1989 | English | 799 |
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General requirements for light gas turbines
| Obsolete |
GB/T 10489-1989
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PDF similar to GB/T 10489-2009
Basic data | Standard ID | GB/T 10489-2009 (GB/T10489-2009) | | Description (Translated English) | General requirements for aero-derivative gas turbines | | Sector / Industry | National Standard (Recommended) | | Classification of Chinese Standard | K56 | | Classification of International Standard | 27.040 | | Word Count Estimation | 28,281 | | Date of Issue | 2009-04-13 | | Date of Implementation | 2010-01-01 | | Older Standard (superseded by this standard) | GB/T 10489-1989 | | Quoted Standard | GB/T 10491; GB/T 11369; GB/T 14100; GB/T 15135 | | Regulation (derived from) | Announcement of Newly Approved National Standards No. 5, 2009 (No. 145 overall) | | Issuing agency(ies) | General Administration of Quality Supervision, Inspection and Quarantine of the People's Republic of China, Standardization Administration of the People's Republic of China | | Summary | This standard specifies supply and demand sides to discuss the purchase of light gas turbines and auxiliary equipment performance, environmental, security, fuel and other technical information. This standard applies to power generation and mechanical drive with a light open-cycle gas turbines, both supply and demand for technology is the basis for negotiations. | GB/T 10489-2009: General requirements for aero-derivative gas turbines---This is a DRAFT version for illustration, not a final translation. Full copy of true-PDF in English version (including equations, symbols, images, flow-chart, tables, and figures etc.) will be manually/carefully translated upon your order.
General requirements for aero-derivative gas turbines
ICS 27.040
K56
National Standards of People's Republic of China
Replacing GB/T 10489-1989
General technical requirements for light turbine
Posted 2009-04-13
2010-01-01 implementation
Administration of Quality Supervision, Inspection and Quarantine of People's Republic of China
Standardization Administration of China released
Table of Contents
Introduction Ⅲ
1 Scope 1
2 Normative references 1
3 Terms and definitions
4 standard reference conditions 1
5 Test Fuel 2
6 Run 2
7 rated properties 2
8 control and protection 3
9 6 fuel
10 Environment 7
11 inquiry or technical information required shall provide the tender 9
Technical Information 12 tender offer or supplier shall provide 10
Appendix A (normative) Safety measures 14
Annex B (informative) Additional information on fuel 15
Annex C (informative) Maintenance 19
References 21
Foreword
This standard is GB/T 10489-1989 "lightweight turbine General technical requirements" of the amendment. And GB/T 10489-1989 phase
Than the main modifications are as follows.
--- Increasing the standard preface;
--- Supplementary terms and definitions content;
--- Redefined the light conditions of the gas turbine compressor inlet and exhaust conditions;
--- Deleted some provisions in the light of the gas turbine and irrelevant content;
--- Reconfirmed the validity of the reference standard;
--- Of a unified terminology adjustment.
From the date of implementation of this standard instead of GB/T 10489-1989.
Appendix A of this standard is a normative appendix, Appendix B and Appendix C are informative appendices.
The standard proposed by China Machinery Industry Federation.
This standard by the National Standardization Technical Committee turbine (SAC/TC259) centralized.
This standard was drafted. China Aviation Industry Corporation, Shenyang Engine Design Institute, Shanghai Power Equipment Research
Hospital, Shanghai electric gate gas turbine power plants, China Power Machinery Institute of Aeronautics, Shanghai Turbine Company, Dongfang Steam Turbine Co.,
Aviation of China Institute of Technology, Nanjing Institute of the gas turbine, Tianjin Binhai Power Company Limited.
The main drafters of this standard. Li Xiaotang, Shen Qiu agriculture, Fan Bang Na, Wang Wei, Cuiyao Xin, Zhao whole, Zhang, the country celebrate Tu Shen Guoqiang.
This standard replaces the standards previously issued as follows.
--- GB/T 10489-1989.
General technical requirements for light turbine
1 Scope
The standard supply and demand sides to discuss the purchase of light gas turbine and auxiliary equipment providing performance, environmental, safety, technology and other aspects of the fuel
Surgery information.
This standard applies to power generation and mechanical drive with a lightweight turbine open cycle, is based on both the supply and demand for technical consultations.
2 Normative references
The following documents contain provisions which, through reference in this standard and become the standard terms. For dated references, subsequent
Amendments (not including errata content) or revisions do not apply to this standard, however, encourage the parties to the agreement are based on research
Whether the latest versions of these documents. For undated reference documents, the latest versions apply to this standard.
GB/T 10491 light gas turbine equipment and methods of measurement noise value
GB/T 11369 Flue gas turbine pollutant measuring light
GB/T 14100 gas turbine acceptance test
GB/T 15135 turbine vocabulary (GB/T 15135-2002, ISO 11086.1996, MOD)
3 Terms and Definitions
GB/T 15135 and established the following terms and definitions apply to this standard.
3.1
Aviation derived (derived) Gas Turbine
Aviation turbine engines based on modifications of the gas turbine is derived from the development of non-aviation purposes.
3.2
Including light gas turbine power plant, and to ensure the normal operation of the load device, as well as other to improve its use of performance, control its
Environmental impact types of equipment needed.
3.3
Given the stable operation of the gas turbine by the light it began to accelerate and stop speed.
4 standard reference conditions
4.1 compressor inlet conditions
Compressor inlet flange (or bell at the compressor inlet).
Total pressure 101.3kPa;
Total temperature 15 ℃;
60% relative humidity, in addition to the use of an intermediate cooling or water cooling, the humidity can generally be ignored.
4.2 exhaust conditions
Power turbine exhaust outlet flange member (such as the use of heat recovery cycle, the heat in the back at the outlet) static pressure is 101.3kPa.
4.3 Cooling water conditions
When using water-cooled refrigerant, the entrance to the water temperature is taken as 15 ℃.
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