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GB/T 26549-2011 | English | 209 |
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Turbocharger variable nozzle ring -- General specifications
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GB/T 26549-2011
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Basic data Standard ID | GB/T 26549-2011 (GB/T26549-2011) | Description (Translated English) | Turbocharger variable nozzle ring -- General specifications | Sector / Industry | National Standard (Recommended) | Classification of Chinese Standard | J91 | Classification of International Standard | 27.020 | Word Count Estimation | 9,963 | Date of Issue | 2011-06-16 | Date of Implementation | 2012-01-01 | Quoted Standard | GB/T 13303-1991; GB/T 23341.1-2009; GB/T 23341.2-2009; HB 5258-2000; JB/T 6002; QC/T 591-1999 | Regulation (derived from) | Announcement of Newly Approved National Standards No. 9 of 2011 | 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 variable nozzle turbocharger ring terms and definitions, technical requirements, test methods, marking, packaging, transportation and storage. This standard applies to the variable radial turbocharger turbine nozzle ring (hereinafter referred to as variable nozzle ring), a variable radial turbocharger turbine housing inlet throat section assembly (assembly) may refer to. |
GB/T 26549-2011: Turbocharger variable nozzle ring -- General specifications---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.
Turbocharger variable nozzle ring. General specifications
ICS 27.020
J91
National Standards of People's Republic of China
Turbocharger variable nozzle ring General technical conditions
Issued on. 2011-06-16
2012-01-01 implementation
Administration of Quality Supervision, Inspection and Quarantine of People's Republic of China
Standardization Administration of China released
Foreword
This standard was drafted in accordance with GB/T 1.1-2009 given rules.
The standard proposed by China Machinery Industry Federation.
The standard internal combustion engine by the National Standardization Technical Committee (SAC/TC177) centralized.
This standard was drafted. Beijing Institute of Technology, Deborah Pingxiang City of Jiangxi Science and Technology Development Co., Ltd. Ningbo days of the supercharger,
Hunan days Yan Machinery Co., Ltd., Shanghai Institute of the internal combustion engine, supercharger Ltd. No Xi Kebo.
The main drafters of this standard. Huang Ruo, Wang Jian, Huang Jie, Wang Yidi, Bi Jinguang, Chen Yunqing, the benefits of subsets.
Turbocharger variable nozzle ring General technical conditions
1 Scope
This standard specifies the variable nozzle turbocharger loop terms and definitions, technical requirements, test methods, marking, packaging, transportation and storage.
This standard applies to runoff turbocharger variable turbine nozzle ring (hereinafter referred to as variable nozzle ring), radial variable turbocharger
Turbine housing intake throat cross-sectional assembly (assembly) may refer to.
This standard does not apply to axial flow turbocharger.
2 Normative references
The following documents for the application of this document is essential. For dated references, only the dated version suitable for use herein
Member. For undated references, the latest edition (including any amendments) applies to this document.
Antioxidant properties GB/T 13303-1991 Determination of steel
GB/T 23341.1-2009 turbocharger - Part 1. General technical conditions
GB/T 23341.2-2009 turbocharger - Part 2. Test methods
Antioxidant Activity Test Method HB5258-2000 steel and superalloys
JB/T 6002 turbocharger cleanliness Limits and measurement methods
QC/T 591-1999 Automobile Turbocharger Test Method
3 Terms and Definitions
The following terms and definitions apply to this document.
3.1
Nozzle ring nozzlering
Turbocharger turbine wheel inlet leading edge, a plurality of gas guide vane ring combination thereof.
3.2
Nozzle ring assembly nozzleringassemblyparts
Assembly by the nozzle ring blades and other parts of the installation disk.
3.3
Nozzle ring assembly nozzleringassembly
It consists of all parts and assemblies nozzle ring nozzle ring assembly, cover, turbine sets, and other components of the drive components.
3.4
Variable nozzle ring variablenozzlering
By the nozzle ring assembly or nozzle ring assembly constituted blades (group) can be adjusted within a certain range and control of the nozzle ring.
3.5
Vane vane
The leading edge of the turbine impeller inlet, the gas flow from the guide and regulate parts.
3.6
Installation disk instalationdisk
Holds the disc-shaped nozzle ring vane parts.
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