2023-1-28 3.235.25.27
Code of China Chinese Classification Professional Classification ICS Classification Latest News Value-added Services

Position: Chinese Standard in English/GB 50454-2008
GB 50454-2008   Code for design of aero-engine test cell (English Version)
Standard No.: GB 50454-2008 Status:superseded remind me the status change

Email:

Language:English File Format:PDF
Word Count: 10000 words Price(USD):250.0 remind me the price change

Email:

Implemented on:2009-6-1 Delivery: via email in 1 business day
,,
Standard No.: GB 50454-2008
English Name: Code for design of aero-engine test cell
Chinese Name: 航空发动机试车台设计规范
Chinese Classification: V97    Special equipment for spacecraft manufacturing
Professional Classification: GB    National Standard
Issued by: AQSIQ, MOHRUD
Issued on: 2008-11-4
Implemented on: 2009-6-1
Status: superseded
Superseded by:GB 50454-2020
Superseded on:2021-3-1
Language: English
File Format: PDF
Word Count: 10000 words
Price(USD): 250.0
Delivery: via email in 1 business day
1 General Provisions 1.0.1 This code is formulated with the view to adapting the development of aero-engine test run technology, ensuring the design quality, and implementing the relevant national principles and policies in the design of test cell, and achieving safety and usability, advanced technology, economy and rationality. 1.0.2 This code is applicable to the design for newly-built aero-engine enclosed test cell of aviation turbine jet, turbofan, turbine-propeller and turbine shaft engines. 1.0.3 Besides this code, the test cell design shall also meet the requirements of the current relevant standards and codes of the nation.   2 Terminologies 2.0.1 Aero-engine enclosed test cell It is the test facility, which is the general terms of aero-engine test plant building and test equipment and used to inspect the assembly quality, working performance and durable test run of aero-engine, hereinafter referred to as test cell. 2.0.2 Master test cell It refers to the test cell used for master test run, and transmits the standard in the process of calibrating the newly-built and re-built test cells. 2.0.3 Intake stack The general terms of air intake stack, muffler device and rectifying device, etc. of test cell. 2.0.4 Test chamber The area for installing and testing the engine in the test cell. 2.0.5 Exhaust stack The general terms of exhaust injection cylinder, the exhaust noise elimination room and muffler device of test cell. 2.0.6 Thrust frame It refers to the important equipment used for fixing the engine and constitutes the engine (thrust and power) together with thrust transducer (for turbine jet and turbofan), dynamometer (for turbine shaft and turbine-propeller engine) and secondary instrument. 2.0.7 Engine handling system The transportation system of upper rail transporting the engine from preparation room to test chamber. 2.0.8 Control room The room used to place the control platform and other equipment and where the test run personnel can complete the engine test run. 2.0.9 Measurement room The room used to place various measurement instruments and where the test run personnel can complete the engine test run measurement. 2.0.10 Hydraulic room The room used to place the grease for test run, hydraulic control, hydraulic pump load systems and other equipment. 2.0.11 Preparation room The room used for the preparation before engine test run and the storage after test run. 2.0.12 Electrical room The room used to place the power supply, electrical cabinet and other equipment used for test run. 2.0.13 Fuel room The room used to place the fuel pipe, filter, valve, flow measuring device and other equipment used for test run. 2.0.14 Fuel heating room The room used to place fuel heating equipment for test run.  3 Processes 3.1 General Requirements 3.1.1 The design of test cell shall be determined according to the type and parameters of engine. The main engine types shall include turbine jet engine, turbofan engine, turbine shaft engine and turbine-propeller engine; the main engine parameters shall include the maximum thrust (power), maximum mass/diameter/length, air flow, exhaust temperature, exhaust pressure, maximum fuel consumption and sectional area of final nozzle. 3.1.2 For the test cell of engine with vector nozzle, its exhaust system shall guarantee smooth exhaust in case of the nozzle deflection of engine. 3.1.3 As for the engine test cell which is carried out with reverse thrust test run, reverse thrust exhaust collector shall be set.
1 General Provisions 2 Terminologies 3 Processes 3.1 General Requirements 3.2 Aerodynamic Design 3.3 Design for Test Equipment 3.5 Technical Safety Measures 4 Noise Control 4.1 General Requirements 4.2 Noise Standard for Plant Area 4.3 Sound Insulation and Absorption Design 4.4 Design for Noise Elimination 5 Building Structure 5.1 General Requirements 5.2 Position of Plant Building 5.3 Plant Building Span and Height 5.4 Type Selection of Main Envelop Enclosure 5.5 Calculation of Major Structure 5.6 Construction of Major Structure 6 Electrical 6.1 Electric Power 6.2 Lighting 6.3 Lightning Protection and Earthing 6.4 Measurement and Control 6.5 Weak Current 7 Water Supply/Drainage and Fire Protection 7.1 Water Supply 7.2 Water Drainage 7.3 Fire Protection 8 Heating, Ventilation and Air Conditioning 8.1 Heating 8.2 Ventilation and Air Conditioning 9 Power Facilities 9.1 General Requirements 9.2 Compressed Air Supply 9.3 Fuel Transportation 9.4 Sump Tank Appendix A Reference Mix Proportion and Test Requirements of Refractory Concrete and Mortar Explanation of Wording in This Code
Code of China
Standard
GB 50454-2008  Code for design of aero-engine test cell (English Version)
Standard No.GB 50454-2008
Statussuperseded
LanguageEnglish
File FormatPDF
Word Count10000 words
Price(USD)250.0
Implemented on2009-6-1
Deliveryvia email in 1 business day
Detail of GB 50454-2008
Standard No.
GB 50454-2008
English Name
Code for design of aero-engine test cell
Chinese Name
航空发动机试车台设计规范
Chinese Classification
V97
Professional Classification
GB
ICS Classification
Issued by
AQSIQ, MOHRUD
Issued on
2008-11-4
Implemented on
2009-6-1
Status
superseded
Superseded by
GB 50454-2020
Superseded on
2021-3-1
Abolished on
Superseding
Language
English
File Format
PDF
Word Count
10000 words
Price(USD)
250.0
Keywords
GB 50454-2008, GB/T 50454-2008, GBT 50454-2008, GB50454-2008, GB 50454, GB50454, GB/T50454-2008, GB/T 50454, GB/T50454, GBT50454-2008, GBT 50454, GBT50454
Introduction of GB 50454-2008
1 General Provisions 1.0.1 This code is formulated with the view to adapting the development of aero-engine test run technology, ensuring the design quality, and implementing the relevant national principles and policies in the design of test cell, and achieving safety and usability, advanced technology, economy and rationality. 1.0.2 This code is applicable to the design for newly-built aero-engine enclosed test cell of aviation turbine jet, turbofan, turbine-propeller and turbine shaft engines. 1.0.3 Besides this code, the test cell design shall also meet the requirements of the current relevant standards and codes of the nation.   2 Terminologies 2.0.1 Aero-engine enclosed test cell It is the test facility, which is the general terms of aero-engine test plant building and test equipment and used to inspect the assembly quality, working performance and durable test run of aero-engine, hereinafter referred to as test cell. 2.0.2 Master test cell It refers to the test cell used for master test run, and transmits the standard in the process of calibrating the newly-built and re-built test cells. 2.0.3 Intake stack The general terms of air intake stack, muffler device and rectifying device, etc. of test cell. 2.0.4 Test chamber The area for installing and testing the engine in the test cell. 2.0.5 Exhaust stack The general terms of exhaust injection cylinder, the exhaust noise elimination room and muffler device of test cell. 2.0.6 Thrust frame It refers to the important equipment used for fixing the engine and constitutes the engine (thrust and power) together with thrust transducer (for turbine jet and turbofan), dynamometer (for turbine shaft and turbine-propeller engine) and secondary instrument. 2.0.7 Engine handling system The transportation system of upper rail transporting the engine from preparation room to test chamber. 2.0.8 Control room The room used to place the control platform and other equipment and where the test run personnel can complete the engine test run. 2.0.9 Measurement room The room used to place various measurement instruments and where the test run personnel can complete the engine test run measurement. 2.0.10 Hydraulic room The room used to place the grease for test run, hydraulic control, hydraulic pump load systems and other equipment. 2.0.11 Preparation room The room used for the preparation before engine test run and the storage after test run. 2.0.12 Electrical room The room used to place the power supply, electrical cabinet and other equipment used for test run. 2.0.13 Fuel room The room used to place the fuel pipe, filter, valve, flow measuring device and other equipment used for test run. 2.0.14 Fuel heating room The room used to place fuel heating equipment for test run.  3 Processes 3.1 General Requirements 3.1.1 The design of test cell shall be determined according to the type and parameters of engine. The main engine types shall include turbine jet engine, turbofan engine, turbine shaft engine and turbine-propeller engine; the main engine parameters shall include the maximum thrust (power), maximum mass/diameter/length, air flow, exhaust temperature, exhaust pressure, maximum fuel consumption and sectional area of final nozzle. 3.1.2 For the test cell of engine with vector nozzle, its exhaust system shall guarantee smooth exhaust in case of the nozzle deflection of engine. 3.1.3 As for the engine test cell which is carried out with reverse thrust test run, reverse thrust exhaust collector shall be set.
Contents of GB 50454-2008
1 General Provisions 2 Terminologies 3 Processes 3.1 General Requirements 3.2 Aerodynamic Design 3.3 Design for Test Equipment 3.5 Technical Safety Measures 4 Noise Control 4.1 General Requirements 4.2 Noise Standard for Plant Area 4.3 Sound Insulation and Absorption Design 4.4 Design for Noise Elimination 5 Building Structure 5.1 General Requirements 5.2 Position of Plant Building 5.3 Plant Building Span and Height 5.4 Type Selection of Main Envelop Enclosure 5.5 Calculation of Major Structure 5.6 Construction of Major Structure 6 Electrical 6.1 Electric Power 6.2 Lighting 6.3 Lightning Protection and Earthing 6.4 Measurement and Control 6.5 Weak Current 7 Water Supply/Drainage and Fire Protection 7.1 Water Supply 7.2 Water Drainage 7.3 Fire Protection 8 Heating, Ventilation and Air Conditioning 8.1 Heating 8.2 Ventilation and Air Conditioning 9 Power Facilities 9.1 General Requirements 9.2 Compressed Air Supply 9.3 Fuel Transportation 9.4 Sump Tank Appendix A Reference Mix Proportion and Test Requirements of Refractory Concrete and Mortar Explanation of Wording in This Code
About Us   |    Contact Us   |    Terms of Service   |    Privacy   |    Cancellation & Refund Policy   |    Payment
Tel: +86-10-8572 5655 | Fax: +86-10-8581 9515 | Email: coc@codeofchina.com | QQ: 672269886
Copyright: Foryou Tech Co., Ltd. 2008-2040
 
 
Keywords:
GB 50454-2008, GB/T 50454-2008, GBT 50454-2008, GB50454-2008, GB 50454, GB50454, GB/T50454-2008, GB/T 50454, GB/T50454, GBT50454-2008, GBT 50454, GBT50454