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GB/T 33631-2017 English PDF

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GB/T 33631-2017: General requirements for inlet and exhaust system of aero-derivative gas turbine assembly
Status: Valid
Standard IDUSDBUY PDFLead-DaysStandard Title (Description)Status
GB/T 33631-2017199 Add to Cart 3 days General requirements for inlet and exhaust system of aero-derivative gas turbine assembly Valid

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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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