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Position: Chinese Standard in English/GB 50454-2020
GB 50454-2020   Standard for design of aero-engine test cell (English Version)
Standard No.: GB 50454-2020 Status:valid remind me the status change

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Language:English File Format:PDF
Word Count: 19500 words Price(USD):585.0 remind me the price change

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Implemented on:2021-3-1 Delivery: via email in 1 business day
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Standard No.: GB 50454-2020
English Name: Standard for design of aero-engine test cell
Chinese Name: 航空发动机试车台设计标准
Professional Classification: GB    National Standard
Issued by: AQSIQ, MOHRUD
Issued on: 2020-06-09
Implemented on: 2021-3-1
Status: valid
Superseding:GB 50454-2008 Code for design of aero-engine test cell
Language: English
File Format: PDF
Word Count: 19500 words
Price(USD): 585.0
Delivery: via email in 1 business day
1 General provisions 1.0.1 This standard is formulated to unify the standard for design of aero-engine test cell, ensure the design quality of test cell, and realize safety, reliability, technology advancement and economical applicability. 1.0.2 This standard is applicable to the design of enclosed test cell of constructed and renovated aviation turbojet engine, turbofan engine, turboprop engine and turboshaft engine using aviation kerosene fuel. 1.0.3 In addition to this standard, the design of enclosed test cell shall also comply with those stipulated in the current relevant national standards. 2 Terms 2.0.1 aero-engine enclosed test cell ground test facility used for running test of aero-engine indoors, usually composed of aero-engine test cell building and aero-engine test equipment, hereinafter referred to as test cell 2.0.2 aero-engine test cell building building used for ground test of the complete aero-engine, usually composed of test chamber, inlet plenum, exhaust stack, and auxiliary functional rooms such as control room, instrument room and preparation room 2.0.3 aero-engine test equipment process equipment for aero-engine test, including test stand, exhaust augmentor, fuel heating device, reverse thrust exhaust collector, test process system, measurement and control system, etc. 2.0.4 test chamber space used for engine test in aero-engine test cell building 2.0.5 inlet plenum passage of external ambient air flowing into the test chamber, composed of structures such as inlet tower or inlet chamber as well as equipment such as silencing device, rectifying device and foreign object protection net 2.0.6 exhaust stack passage of air flow from test chamber to the external environment, composed of structures such as exhaust tower, exhaust silencing room and augmentor room as well as equipment such as exhaust augmentor and silencing device 2.0.7 augmentor room structure used for installing exhaust augmentor and isolating noise 2.0.8 test stand equipment used for fixing aero-engine and measuring its thrust or power 2.0.9 engine handling system suspended rail transport system used for lifting engine and matching test equipment, and completing air transport of engine between test chamber and preparation room 2.0.10 control room room equipped with measuring and control equipment such as control console, and used for engine test control and monitoring 2.0.11 instrument room room equipped with measuring instrument and used for test of engine parameters 2.0.12 hydraulic room room equipped with lubricating oil and hydraulic equipment for test 2.0.13 preparation room room used for preparation of engine and aero-engine test equipment before test and temporary storage after test 2.0.14 electrical room room equipped with equipment such as power supply and electrical cabinet for test 2.0.15 fuel room room equipped with equipment such as fuel pipeline, filter, valve and flow measuring device for test 2.0.16 fuel heating room room equipped with fuel heating equipment for test 3 Process 3.1 General requirements 3.1.1 During the design of test cell, the structural type and technical index of test cell shall be determined according to the type and parameters of engine. 3.1.2 When the exhaust direction of the engine deviates from its centerline, the exhaust system of test cell shall be kept smooth. 3.1.3 The test cell with engine reverse thrust test function shall be equipped with a reverse thrust exhaust collector. 3.1.4 The high-temperature exhaust stack of engine and normal-temperature exhaust stack of propeller should be arranged separately on the turboprop engine test cell. 3.1.5 The basic design parameters of test cell should include sectional area of inlet plenum, length of test chamber, sectional area of test chamber, sectional area of exhaust stack, diameter of exhaust augmentor, length of exhaust augmentor and center elevation of engine. 3.1.6 The room for development should be reserved in the design of building and main equipment. 3.1.7 The exhaust emission design of test cell shall meet the relevant requirements of the current national standard GB 16297 Comprehensive emission standard of air pollutants.
Foreword i 1 General provisions 2 Terms 3 Process 3.1 General requirements 3.2 Aerodynamic design 3.3 Aero-engine test equipment design 3.4 Building layout 3.5 Technical safety measures 4 Noise control 4.1 General requirements 4.2 Noise control standard 4.3 Insulation and absorption design 4.4 Noise elimination design 5 Architecture and structure 5.1 General requirements 5.2 Building layout 5.3 Fire and explosion protection design of building 5.4 Span and height of building 5.5 Selection of enclosure structure 5.6 Calculation of main structure 5.7 Seismic design 5.8 Construction of main structure 6 Electric system 6.1 Power supply 6.2 Lighting 6.3 Lightning protection and grounding 6.4 Weak current 7 Water supply, drainage and fire protection facilities 7.1 General requirements 7.2 Water supply 7.3 Drainage 7.4 Fire protection facilities 8 Heating, ventilating and air conditioning 8.1 Heating 8.2 Ventilating and air conditioning 8.3 Fire, explosion and smoke protection, smoke exhausting system 9 Motive power 9.1 Compressed air supply 9.2 Fuel supply 9.3 Waste oil tank Annex A Field measurement and verification method of aerodynamic design parameters of test cell Annex B Requirements for noise test of test cell Annex C Reference mixture ratio and test requirements of special concrete, heat-resistant concrete and heat-resistant mortar Explanation of wording in this standard List of quoted standards
Referred in GB 50454-2020:
*GB 50007-2011 Code for design of building foundation
*GB 50009-2012 Load Code for the Design of Building Structures
*GB 50010-2010(2015) Code for design of concrete structures
*GB 50011-2010(2016) Code for Seismic Design of Buildings (2016)
*GB 50015-2019 Standard for design of building water supply and drainage
*GB 50016-2014(2018)-Provisions Provisions of Code for Fire Protection Design of Buildings
*GB 50029-2014 Code for Design of Compressed Air Station
*GB 50034-2013 Standard for lighting design of buildings
*GB/T 50050-2017 Code for design of industrial recirculating cooling water treatment
*GB 50051-2013 Code for design of chimneys
*GB 50058-2014 Code for Design of Electrical Installations in Explosive Atmospheres
*GB 50074-2014 Code for design of oil depot
*GB/T 50087-2013 Code for design of noise control of industrial enterprises
*GB 50116-2013 Code for design of automatic fire alarm system
*GB 50140-2005 Code for Design of Extinguisher Distribution in Buildings
*GB 50191-2012 Design code for antiseismic of special structures
*GB 50343-2012 Technical code for protection of building electronic information system against lightning
*GB 50555-2010 Standard for water saving design in civil building
*GB 50974-2014 Code of design on fire protection water supply and hydrant systems
*GB 51245-2017 Unified standard for energy efficiency design of industrial buildings
*GB 51251-2017 Technical standard for smoke management systems in buildings
*GB 5749-2006 Standards for drinking water quality
*GB 8978-1996 Integrated Wastewater Discharge Standard
*GB 12348-2008 Emission Standard for Industrial Enterprises Noise at Boundary
*GB/T 13277.1-2008 Compressed air - Part 1:Contaminants and purity classes
*GB 16297-1996 Comprehensive emission standard of air pollutants
*GB/T 20801-2006 Pressure Piping Code - Industrial Piping (GB/T 20801.1~6-2006)
*GJB 241A-2010 General specifications for aero turbine jet and turbofan engine
*GJB242A-2018
*JGJ 52-2006 Standard for technical requirements and test method of sand and crushed stone (or gravel) for ordinary concrete
*YB/T 4252-2011 Technical specification for heat resistance concrete
Code of China
Standard
GB 50454-2020  Standard for design of aero-engine test cell (English Version)
Standard No.GB 50454-2020
Statusvalid
LanguageEnglish
File FormatPDF
Word Count19500 words
Price(USD)585.0
Implemented on2021-3-1
Deliveryvia email in 1 business day
Detail of GB 50454-2020
Standard No.
GB 50454-2020
English Name
Standard for design of aero-engine test cell
Chinese Name
航空发动机试车台设计标准
Chinese Classification
Professional Classification
GB
ICS Classification
Issued by
AQSIQ, MOHRUD
Issued on
2020-06-09
Implemented on
2021-3-1
Status
valid
Superseded by
Superseded on
Abolished on
Superseding
GB 50454-2008 Code for design of aero-engine test cell
Language
English
File Format
PDF
Word Count
19500 words
Price(USD)
585.0
Keywords
GB 50454-2020, GB/T 50454-2020, GBT 50454-2020, GB50454-2020, GB 50454, GB50454, GB/T50454-2020, GB/T 50454, GB/T50454, GBT50454-2020, GBT 50454, GBT50454
Introduction of GB 50454-2020
1 General provisions 1.0.1 This standard is formulated to unify the standard for design of aero-engine test cell, ensure the design quality of test cell, and realize safety, reliability, technology advancement and economical applicability. 1.0.2 This standard is applicable to the design of enclosed test cell of constructed and renovated aviation turbojet engine, turbofan engine, turboprop engine and turboshaft engine using aviation kerosene fuel. 1.0.3 In addition to this standard, the design of enclosed test cell shall also comply with those stipulated in the current relevant national standards. 2 Terms 2.0.1 aero-engine enclosed test cell ground test facility used for running test of aero-engine indoors, usually composed of aero-engine test cell building and aero-engine test equipment, hereinafter referred to as test cell 2.0.2 aero-engine test cell building building used for ground test of the complete aero-engine, usually composed of test chamber, inlet plenum, exhaust stack, and auxiliary functional rooms such as control room, instrument room and preparation room 2.0.3 aero-engine test equipment process equipment for aero-engine test, including test stand, exhaust augmentor, fuel heating device, reverse thrust exhaust collector, test process system, measurement and control system, etc. 2.0.4 test chamber space used for engine test in aero-engine test cell building 2.0.5 inlet plenum passage of external ambient air flowing into the test chamber, composed of structures such as inlet tower or inlet chamber as well as equipment such as silencing device, rectifying device and foreign object protection net 2.0.6 exhaust stack passage of air flow from test chamber to the external environment, composed of structures such as exhaust tower, exhaust silencing room and augmentor room as well as equipment such as exhaust augmentor and silencing device 2.0.7 augmentor room structure used for installing exhaust augmentor and isolating noise 2.0.8 test stand equipment used for fixing aero-engine and measuring its thrust or power 2.0.9 engine handling system suspended rail transport system used for lifting engine and matching test equipment, and completing air transport of engine between test chamber and preparation room 2.0.10 control room room equipped with measuring and control equipment such as control console, and used for engine test control and monitoring 2.0.11 instrument room room equipped with measuring instrument and used for test of engine parameters 2.0.12 hydraulic room room equipped with lubricating oil and hydraulic equipment for test 2.0.13 preparation room room used for preparation of engine and aero-engine test equipment before test and temporary storage after test 2.0.14 electrical room room equipped with equipment such as power supply and electrical cabinet for test 2.0.15 fuel room room equipped with equipment such as fuel pipeline, filter, valve and flow measuring device for test 2.0.16 fuel heating room room equipped with fuel heating equipment for test 3 Process 3.1 General requirements 3.1.1 During the design of test cell, the structural type and technical index of test cell shall be determined according to the type and parameters of engine. 3.1.2 When the exhaust direction of the engine deviates from its centerline, the exhaust system of test cell shall be kept smooth. 3.1.3 The test cell with engine reverse thrust test function shall be equipped with a reverse thrust exhaust collector. 3.1.4 The high-temperature exhaust stack of engine and normal-temperature exhaust stack of propeller should be arranged separately on the turboprop engine test cell. 3.1.5 The basic design parameters of test cell should include sectional area of inlet plenum, length of test chamber, sectional area of test chamber, sectional area of exhaust stack, diameter of exhaust augmentor, length of exhaust augmentor and center elevation of engine. 3.1.6 The room for development should be reserved in the design of building and main equipment. 3.1.7 The exhaust emission design of test cell shall meet the relevant requirements of the current national standard GB 16297 Comprehensive emission standard of air pollutants.
Contents of GB 50454-2020
Foreword i 1 General provisions 2 Terms 3 Process 3.1 General requirements 3.2 Aerodynamic design 3.3 Aero-engine test equipment design 3.4 Building layout 3.5 Technical safety measures 4 Noise control 4.1 General requirements 4.2 Noise control standard 4.3 Insulation and absorption design 4.4 Noise elimination design 5 Architecture and structure 5.1 General requirements 5.2 Building layout 5.3 Fire and explosion protection design of building 5.4 Span and height of building 5.5 Selection of enclosure structure 5.6 Calculation of main structure 5.7 Seismic design 5.8 Construction of main structure 6 Electric system 6.1 Power supply 6.2 Lighting 6.3 Lightning protection and grounding 6.4 Weak current 7 Water supply, drainage and fire protection facilities 7.1 General requirements 7.2 Water supply 7.3 Drainage 7.4 Fire protection facilities 8 Heating, ventilating and air conditioning 8.1 Heating 8.2 Ventilating and air conditioning 8.3 Fire, explosion and smoke protection, smoke exhausting system 9 Motive power 9.1 Compressed air supply 9.2 Fuel supply 9.3 Waste oil tank Annex A Field measurement and verification method of aerodynamic design parameters of test cell Annex B Requirements for noise test of test cell Annex C Reference mixture ratio and test requirements of special concrete, heat-resistant concrete and heat-resistant mortar Explanation of wording in this standard List of quoted standards
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Keywords:
GB 50454-2020, GB/T 50454-2020, GBT 50454-2020, GB50454-2020, GB 50454, GB50454, GB/T50454-2020, GB/T 50454, GB/T50454, GBT50454-2020, GBT 50454, GBT50454