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GB/T 14411-2008 English PDF

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GB/T 14411-2008: Control and protective system for aero-derivative gas turbine
Status: Valid

GB/T 14411: Historical versions

Standard IDUSDBUY PDFLead-DaysStandard Title (Description)Status
GB/T 14411-2008299 Add to Cart 3 days Control and protective system for aero-derivative gas turbine Valid
GB/T 14411-1993519 Add to Cart 4 days Control and protective system for light weight gas turbine Obsolete

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GB/T 14478   GB/T 15468   JB/T 6688   GB/T 11371   GB/T 16637   GB/T 11369   

Basic data

Standard ID: GB/T 14411-2008 (GB/T14411-2008)
Description (Translated English): Control and protective system for aero-derivative gas turbine
Sector / Industry: National Standard (Recommended)
Classification of Chinese Standard: K58
Classification of International Standard: 27.040
Word Count Estimation: 13,163
Date of Issue: 2008-07-18
Date of Implementation: 2009-01-01
Older Standard (superseded by this standard): GB/T 14411-1993
Quoted Standard: GB/T 10489
Regulation (derived from): Announcement of Newly Approved National Standards No. 12 of 2008 (No. 125 overall)
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 light gas turbine (hereinafter referred to as gas turbine) control system control functions and performance requirements, the protection system of protection and protection devices and their test requirements. This standard applies to terrestrial power generation and mechanical drive gas turbine control and protection, other uses gas turbines for implementation.

GB/T 14411-2008: Control and protective system for aero-derivative gas turbine

---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.
Control and protective system for aero-derivative gas turbine ICS 27.040 K58 National Standards of People's Republic of China Replacing GB/T 14411-1993 Light turbine control and protection system Posted 2008-07-18 2009-01-01 implementation Administration of Quality Supervision, Inspection and Quarantine of People's Republic of China Standardization Administration of China released

Foreword

This standard replaces GB/T 14411-1993 "lightweight gas turbine control and protection systems." This standard and GB/T 14411-1993 compared to the main changes are as follows. --- Modify the standard scope (Chapter 1 of this edition); --- Modify the requirement is purged (Excerpts 3.2.1.5); --- Complements the normal stop and emergency stop requirement (Excerpts 3.2.3.2,3.2.3.3); --- Increased synchronization control, the instantaneous speed limit and the output power limits (Excerpts 3.3.5,3.4.8,3.4.9); --- Complement the performance requirements of digital electronic control system (this edition 3.4.3.2); --- Deleted environmental testing provisions (1993 Version 5.3); --- Modify the requirements of the digital control system, integrated into 3.1 (Chapter 7, 1993 edition); --- Modify the protection and monitoring of the signal parameters requirements (Excerpts 4.3.4,4.3.5); --- Increase the environmental conditions (Chapter 7 of this edition). The standard proposed by China Aviation Industry Corporation. The standard by the China Aviation Industry Corporation. This standard was drafted. AVIC Shixin turbine Co., Ltd., of China Aviation Technology Institute, Jiangsu Air Power Control Limited. The main drafters of this standard. Tianxiang Tai at Pei Min, Zhang, Meng Tao, Yu Jianfeng. This standard replaces the standards previously issued as follows. --- GB/T 14411-1993. Light turbine control and protection system

1 Scope

This standard specifies the light gas turbine (hereinafter referred to as GT) security control system control functions and performance requirements, protection systems Protection and protective devices and test requirements. This standard applies to terrestrial power generation and mechanical drive gas turbine control and protection, the gas turbine may refer to other purposes.

2 Normative references

The 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/T 10489 General requirements for light turbine

3 control system

3.1 Basic requirements 3.1.1 gas turbine control system should be able to meet the need for control, regulation, monitoring and protection functions, as well as a high degree of reliability, safety And availability, should be consistent with GB/T 10489 requirements. 3.1.2 digital electronic control system should be redundant, fault-tolerant and self-diagnostic function. System hardware should be modular, universal, and easy maintenance. Control software should have excellent real-time, fault tolerance and security, programming convenience, easy to use. 3.1.3 digital electronic control system should provide a good man-machine interface, convenient connection with other control devices, is scalable and open Caving. 3.1.4 digital electronic control system should have the standard communication interface. The system can exchange data through the use of open communication interface with the outside world , Standard communication protocols, should be able to easily integrate into the upper system. 3.2 Control Function 3.2.1 Start 3.2.1.1 Overview Starting from the beginning until the gas turbine auxiliary equipment to reach the empty load speed (slow speed) the whole process of starting the process. Starting manual Start, start semi-automatic, automatic starting, etc., may have to start a program, starting times and special start functions. 3.2.1.2 Starting method 3.2.1.2.1 Manually starting device according to supply and demand sides agreed programs. Manual start requires the operator to manually start auxiliary device Equipment, and gradually complete the start-up procedure until you reach the empty gas turbine load speed (slow speed). 3.2.1.2.2 semi-automatic starting aids manually start, but by the time the operator should operate the gas turbine automatically subsequent full Unit start-up process. 3.2.1.2.3 automatic start start command is issued by the operator, automatically complete all of the gas turbine start-up process. 3.2.1.3 Starting Process To start the process of a complete set of start-up procedure to ensure reliable ignition and fuel supply as required, so that the gas turbine rapid, stable, Reliably reach the empty load speed (slow speed). Typically, with the turbine speed or by varying the starting time of the fuel supplied to the curve. Such as Necessary, should be able to fix this by starting curve ambient atmospheric pressure and temperature. Other parameters may also change or correction curve control start burning Quantity.
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