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GB/T 33631-2017 | English | 199 |
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General requirements for inlet and exhaust system of aero-derivative gas turbine assembly
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GB/T 33631-2017
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Basic data Standard ID | GB/T 33631-2017 (GB/T33631-2017) | Description (Translated English) | General requirements for inlet and exhaust system of aero-derivative gas turbine assembly | Sector / Industry | National Standard (Recommended) | Classification of Chinese Standard | K56 | Classification of International Standard | 27.040 | Word Count Estimation | 10,163 | Date of Issue | 2017-05-12 | Date of Implementation | 2017-12-01 | Quoted Standard | GB 3095; GB/T 10489; GB/T 10491; GB 12348; GB/T 18083; GB 50009; GB 50011; GBJ 87; HB 7257; GB/T 20431; GB/T 18345.1; GB/T 18345.2 | 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 the general technical requirements for the intake and exhausting system, the silencer, and the exhaust pollution control of the air and exhaust system (hereinafter referred to as "intake and exhaust system") of the aviation-derived gas turbine complete sets of equipment. This standard applies to the power generation of aviation-derived gas turbine power plant. Gas turbine test rig, compressor test bed, injection pump station, pipeline pressurization and other aviation-derived gas turbine into the exhaust system can refer to the use. |
GB/T 33631-2017: General requirements for inlet and exhaust system of aero-derivative gas turbine assembly ---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 inlet and exhaust system of aero-derivative gas turbine assembly
ICS 27.040
K56
National Standards of People's Republic of China
Aeronautical Derivative Gas Turbine Complete Equipment
System General technical requirements
2017-05-12 released
2017-12-01 implementation
General Administration of Quality Supervision, Inspection and Quarantine of the People's Republic of China
China National Standardization Management Committee released
Foreword
This standard is drafted in accordance with the rules given in GB/T 1.1-2009.
This standard is proposed by the China Machinery Industry Federation.
This standard is under the jurisdiction of the National Gas Turbine Standardization Technical Committee (SAC/TC259).
The drafting unit of this standard. China Aviation Comprehensive Technology Research Institute, China Aviation Planning and Construction Development Co., Ltd.
The main drafters of this standard. Zhang Hua, Tang Dao-min, universal.
Aeronautical Derivative Gas Turbine Complete Equipment
System General technical requirements
1 Scope
This standard specifies the air intake and exhaust system of the air-borne gas turbine complete sets of equipment (hereinafter referred to as "intake and exhaust system").
Home, muffler, exhaust pollution control and other general technical requirements.
This standard applies to power generation with air-borne gas turbine power plant. Gas turbine test bench, compressor test bed, water injection pump station,
Piping pressurization and other aviation-derived gas turbine into the exhaust system can refer to the use.
2 normative reference documents
The following documents are indispensable for the application of this document. For dated references, only the dated edition applies to this article
Pieces. For undated references, the latest edition (including all modifications) applies to this document.
GB 3095 Ambient Air Quality Standard
GB/T 10489 General technical requirements for light gas turbines
GB/T 10491 Aeronautical derived gas turbine complete sets of equipment noise values and measurement methods
Standard for Environmental Noise Discharge of Industrial Enterprises
Standard for Designing Hygienic Protection Distance for Industrial Enterprises Based on Noise Pollution
GB/T 18345 (all parts) Gas turbine flue gas emissions
GB/T 20431 Acoustic Muffler Noise Control Guide
Specification for load of building structures GB 50009
Code for seismic design of GB 50011 buildings
Code for design of noise control for industrial enterprises GB J87
HB7257 Light Gas Turbine Intake Filter
3 environmental and operational requirements
3.1 operating environment
Before and after the exhaust system design, the geographical conditions, meteorological data, engineering geology and hydrological conditions of the site of use and the nature of the area
Circumstance and environmental planning).
3.2 Site Rules
Before and after the exhaust system design, should clear the total station location, unit layout (open-air layout and indoor layout), unit installation
(Fixed and mobile) and the number of aircraft-derived gas turbine.
3.3 Operation mode
According to GB/T 10489 light gas turbine operation mode of the relevant provisions, differentiated into the exhaust system.
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