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GB/T 33631-2017General requirements for inlet and exhaust system of aero-derivative gas turbine assembly (English PDF)

航空派生型燃气轮机成套设备进排气系统通用技术要求

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Issued by

SAMR; SAC

Level / Type

National · Recommended

Issue date

May 12, 2017

Implementation date

December 1, 2017

Scope

GB/T 33631-2017 is the English-translated version of 航空派生型燃气轮机成套设备进排气系统通用技术要求.

GB/T 33631-2017 sets the general technical requirements for the inlet and exhaust system of aero-derivative gas turbine complete equipment, together with the silencer and the control of exhaust pollution.

It applies to aero-derivative gas turbine power plants used for power generation, while gas turbine test benches, compressor test beds, injection pump stations and pipeline pressurization installations may refer to it.

Its environmental and operating clause asks that the geography, the meteorology and the engineering geology and hydrology of the site be established before the system is designed, that the station location, the unit layout, the installation and the number of units be settled, and that the operating mode be distinguished according to GB/T 10489.

It also cites GB 3095, GB 12348, GB/T 18345 and GB 50009. It was issued on 12 May 2017 and has applied since 1 December 2017.

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Document preview — GB/T 33631-2017

National Standard of the People's Republic of China

ICS
27.040
Classification
K 56

Issued by: State Administration for Market Regulation; Standardization Administration of the PRC

Contents

  • Foreword
  • 1 Scope
  • 2 Normative reference documents
  • 3 Environmental and operational requirements

Foreword

This standard is drafted in accordance with the rules given in GB/T 1.1-2009.

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 document. 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

GB 12348 Standard for Environmental Noise Discharge of Industrial Enterprises

GB/T 18083 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

GB 50009 Specification for load of building structures

GB 50011 Code for seismic design of buildings

GBJ 87 Code for design of noise control for industrial enterprises

HB 7257 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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This preview omits tables, figures, formulas and parts of the technical clauses. The complete document — 15 pages — is available in the English PDF.

Referenced standards

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