GB/T 13673-2010 English PDFUS$579.00 · In stock
Delivery: <= 5 days. True-PDF full-copy in English will be manually translated and delivered via email. GB/T 13673-2010: General requirements for aero-derivative gas turbines auxiliary equipment Status: Valid GB/T 13673: Historical versions
Basic dataStandard ID: GB/T 13673-2010 (GB/T13673-2010)Description (Translated English): General requirements for aero-derivative gas turbines auxiliary equipment Sector / Industry: National Standard (Recommended) Classification of Chinese Standard: K56 Classification of International Standard: 27.040 Word Count Estimation: 25,291 Date of Issue: 2010-11-10 Date of Implementation: 2011-03-01 Older Standard (superseded by this standard): GB/T 13673-1992 Quoted Standard: GB 150; GB 4066.1; GB/T 10489; GB/T 10491; GB/T 11369; GB/T 14099; GB/T 15135; GB 50009; GB 50016-2006; GB 50058; GB 50084; GB 50193; HB 6712 Regulation (derived from): Announcement of Newly Approved National Standards No. 8 of 2010 (total 163) 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 aviation derived gas turbine auxiliary system design requirements as well as in different working conditions constitute the system components required, the procurement side, turbine manufacturer based technical consultations between the two sides. This standard applies to power generation, marine and mechanical drive gas turbines. GB/T 13673-2010: General requirements for aero-derivative gas turbines auxiliary equipment---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 aero-derivative gas turbines auxiliary equipment ICS 27.040 K56 National Standards of People's Republic of China Replacing GB/T 13673-1992 Aviation derivative gas turbine General technical requirements for auxiliary equipment Issued on. 2010-11-10 2011-03-01 implementation Administration of Quality Supervision, Inspection and Quarantine of People's Republic of China Standardization Administration of China released Table of ContentsIntroduction Ⅲ 1 Scope 1 2 Normative references 1 3 Terms and definitions 4 1 General 5 Lubricating System 1 6 fuel system 3 7 atomizing air system 6 8 starting system 7 Cooling system 8 9 10 Heating - Ventilation System 9 11 10 Fire Fighting System 12 Cleaning System 12 13 13 Intake System Exhaust system 14 16 15 crates body 18 16 Coupling 18 17 transmission 18 18 Piping Systems 19 Installation 19 19 Painting 20 20 21 water/steam system 21ForewordThis revision to the national standard GB/T 14099.3 (equivalent to using the original ANSIB133.3-1981 "ProcurementStandardfor GasTurbine Auxiliary Equipment "of the latest ISO standards similar ISO 3977-3.2004" Gasturbines- Procurement-Part 3. Designrequirements ") as an important reference. This standard replaces GB/T 13673-1992 "lightweight gas turbine auxiliary equipment general technical conditions." This standard compared with GB/T 13673-1992, the main changes are as follows. --- Of GB/T 13673-1992 "lightweight gas turbine auxiliary equipment common technical requirements" of the contents of the standardization Amendment press GB/T 15135 "gas turbine word" requirement standard name will be changed to "aviation derivative gas turbine auxiliary General technical requirements. " --- Specification words and names, the full text of "combustion engine" to "gas turbine", "start" to "start", "light" to "Aviation variant" "Oil" is replaced by "oil", "steam turbine" to "Turbine." --- Original criteria for the purchaser, complete business, supply-side, demand side, users and other terms are not unified, now, "the purchaser, both sets of providers" Subject to subsection Chapter 1 "Scope" reservations, the rest throughout all be replaced by "both parties", "purchaser" to "demand-side", "Complete business" reform The "supply side." --- Chapter 2, the original standard GB J9 and other references, the latest version of the standards adopted similar standards. It adds a reference to GB/T 15135 "Burning Gas turbine vocabulary "and GB 150" steel pressure vessel. " --- Chapter 6, an increase of 6.4 "dual-fuel system." --- Chapter 8, "8.3 car means" of "it can also be used in the normal starting sequence terminated start" amended to read "it can also be used in normal Start the program moving rotor disk "from a standstill. --- Chapter 12 adds "12.6 cleaning mode." --- Chapter 14, "14.3 Design" in (corresponding to GB/T 13673-1992 14.2) adds "14.3.4 expansion joints." --- Chapter 21 heading "water or steam injection system" to "water/steam system" in this chapter all "water injection system" to "Water system" all "steam injection system" to "steam injection system", all the "steam injection" to "steam injection." The standard proposed by China Machinery Industry Federation. This standard by the National Standardization Technical Committee turbine (SAC/TC259) centralized. This standard was drafted are. Jiangsu Air Power Control Co., Ltd. Suzhou high thermoelectric, Zhuzhou Southern gas turbine sets Manufacture and installation Co., Ltd., China United Engineering Corporation, Shanghai Electric gas turbine power plant gate, Nanjing Turbine & Electric Machinery (Group) Co., Ltd. The main drafters of this standard. Xueyin Chun, Hu Xinghui, Chen Wenfeng, in Zhiping, Fanbang TY, Deng Aiping. This standard replaces the standards previously issued as follows. --- GB/T 13673-1992. Aviation derivative gas turbine General technical requirements for auxiliary equipment1 ScopeThis standard specifies requirements for the design variants aviation gas turbine (hereinafter referred to as GT) as well as auxiliary systems in different working conditions By constituting components required by the system, it is the purchaser, turnkey provider based on technical consultations between the two sides. This standard applies to power generation, ship and mechanical drive gas turbines.2 Normative referencesThe following documents contain provisions which, through reference in this standard and become the standard terms. For dated references, subsequent Amendments (not including errata content) or revisions do not apply to this standard, however, encourage the parties to the agreement are based on research Whether the latest versions of these documents. For undated reference documents, the latest versions apply to this standard. GB 150 steel pressure vessels GB 4066.1 powder extinguishing agent Part 1. BC powder extinguishing agent (GB 4066.1-2004, ISO 7202. 1987, NEQ) GB/T 10489 General requirements for light turbine GB/T 10491 Aviation derivative gas turbine equipment and methods of measurement noise value GB/T 11369 Flue gas turbine pollutant measuring light GB/T 14099 turbines - Procurement GB/T 15135 turbine vocabulary (GB/T 15135-2002, ISO 11086.1996, MOD) GB 50009 building structural load specifications GB 50016-2006 architectural design code for fire protection GB 50058 Explosion and fire hazard electrical installation design specifications GB 50084 sprinkler system design specifications GB 50193 Carbon dioxide fire extinguishing systems HB6712 Lightweight turbine couplings General technical requirements3 Terms and DefinitionsGB/T 15135, the terms and definitions GB/T 10489 and GB/T 14099 apply to this standard established.4 General4.1 Due to the gas turbine using the occasion, operation mode, environmental conditions and so affect the composition of the auxiliary systems, the provisions of this standard to the lowest Seeking project also provides a number of options, according to project needs determined by the supply and demand sides. 4.2 turbine auxiliary systems, control systems and other necessary equipment, functional requirements should be rational distribution. Layout should consider the operation of the device For the convenience of maintenance, installation, operation and maintenance cost and appearance. 4.3 Unless otherwise specified, lubricants, antifreeze and other supplies provided by the demand side.5 lube oil system5.1 General Lube oil system shall be capable of starting, running and stopping the process of the gas turbine, gas turbine or gas turbine and the driven machine shaft ......Tips & Frequently Asked Questions:Question 1: How long will the true-PDF of GB/T 13673-2010_English be delivered?Answer: Upon your order, we will start to translate GB/T 13673-2010_English as soon as possible, and keep you informed of the progress. The lead time is typically 3 ~ 5 working days. The lengthier the document the longer the lead time.Question 2: Can I share the purchased PDF of GB/T 13673-2010_English with my colleagues?Answer: Yes. 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