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GB/T 9169-2023: Standard test method for thermal oxidation stability of aviation turbine fuels
Status: Valid GB/T 9169: Evolution and historical versions
| Standard ID | Contents [version] | USD | STEP2 | [PDF] delivered in | Standard Title (Description) | Status | PDF |
| GB/T 9169-2023 | English | 459 |
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Standard test method for thermal oxidation stability of aviation turbine fuels
| Valid |
GB/T 9169-2023
|
| GB/T 9169-2010 | English | 1199 |
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Standard test method for thermal oxidation stability of aviation turbine fuels -- JFTOT procedure
| Obsolete |
GB/T 9169-2010
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| GB/T 9169-1988 | English | RFQ |
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6 days [Need to translate]
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Jet fuels--Determination of thermal oxidation stability--JFTOT method
| Obsolete |
GB/T 9169-1988
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PDF similar to GB/T 9169-2023
Standard similar to GB/T 9169-2023 GB 6537 GB/T 2430 GB/T 8019 GB 1787 Basic data | Standard ID | GB/T 9169-2023 (GB/T9169-2023) | | Description (Translated English) | Standard test method for thermal oxidation stability of aviation turbine fuels | | Sector / Industry | National Standard (Recommended) | | Classification of Chinese Standard | E31 | | Classification of International Standard | 75.160.20 | | Word Count Estimation | 22,258 | | Date of Issue | 2023-05-23 | | Date of Implementation | 2023-12-01 | | Older Standard (superseded by this standard) | GB/T 9169-2010 | | Issuing agency(ies) | State Administration for Market Regulation, China National Standardization Administration | GB/T 9169-2023: Standard test method for thermal oxidation stability of aviation turbine fuels---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.
ICS 75:160:20
CCSE31
National Standards of People's Republic of China
Replacing GB/T 9169-2010
Jet Fuel Thermal Oxidation Stability Determination Method
Released on 2023-05-23
2023-12-01 implementation
State Administration for Market Regulation
Released by the National Standardization Management Committee
foreword
This document is in accordance with the provisions of GB/T 1:1-2020 "Guidelines for Standardization Work Part 1: Structure and Drafting Rules for Standardization Documents"
drafting:
This document replaces GB/T 9169-2010 "Determination of Thermal Oxidation Stability of Jet Fuels JFTOT Method", and GB/T 9169-2010
In comparison, except for structural adjustments and editorial changes, the main technical changes are as follows:
--- Added the content of three types of jet fuel thermal oxidation tester, 230MARKⅣ, F400 and DRYA-2601 (see
Table 1);
--- Increased quality control inspection (see 9:2);
---Deleted the content about the three types of instruments 202, 203 and 215 (see Table 1, Chapter 10, 11:3:2, 11:
3:3, 11:7:1, Chapter 13, Appendix C, Appendix D and Appendix E);
--- Deleted the structural differences between this document and ASTMD3241-08a (see Appendix A of the:2010 edition):
Please note that some contents of this document may refer to patents: The issuing agency of this document assumes no responsibility for identifying patents:
This document is proposed and managed by the National Petroleum Products and Lubricants Standardization Technical Committee (SAC/TC280):
This document is drafted by: Sinopec Petrochemical Research Institute, China Aviation Fuel Co:, Ltd:,
Boer Instruments (Tianjin) Co:, Ltd:
The main drafters of this document: Zhang Cuijun, Chang Chunyan, Zhao Jie, Li Lusheng, Zhang Chenmeng, Tao Zhiping, Tian Heng:
This document was first published in 1988, revised for the first time in:2010, and this is the second revision:
Jet Fuel Thermal Oxidation Stability Determination Method
WARNING: Personnel using this document need to have practical experience in formal laboratory work: Use of this document may involve certain hazardous
materials, equipment and handling, this document does not address all possible safety issues: It is the user's responsibility to take appropriate safety and health precautions
implementation, and ensure compliance with the conditions stipulated in the relevant national laws and regulations:
1 Scope
This document describes a method for assessing the propensity of jet fuels to generate deposits in the engine fuel system:
This document applies to the determination of thermal oxidation stability of jet fuel:
2 Normative references
The contents of the following documents constitute the essential provisions of this document through normative references in the text: Among them, dated references
For documents, only the version corresponding to the date is applicable to this document; for undated reference documents, the latest version (including all amendments) is applicable to
this document:
GB/T 4756 Petroleum liquid manual sampling method
GB/T 27867 Petroleum Liquid Pipeline Automatic Sampling Method
SH/T 0635 Sampling method for liquid petroleum products (semi-automatic method)
3 Terms and Definitions
The following terms and definitions apply to this document:
3:1
sediment deposits
Oxidation products deposited on the heated tube test area and/or trapped on the test filter:
NOTE: Fuel deposits tend to be concentrated in the hottest part of the heating tube, i:e: between 30 mm and 50 mm:
3:2
heater tube
Aluminum sample tubes with controlled heating surfaces:
NOTE: The tube is heat-resistant and has a built-in thermocouple to control the temperature: The effective test area of the tube is located between the two shoulders of the tube, that is, the thinner part with a length of 60mm: try
The sample enters from 0mm and exits from 60mm:
3:3
breakpoint breakpoint
The sample meets the maximum temperature required by the heater tube wall rating and differential pressure (ΔP) specification across the filter:
4 Overview
This document uses jet fuel thermal oxidation stability tester to measure the high temperature oxidation stability of jet fuel, the test conditions can be set
Linked to actual operating conditions of jet turbine engine fuel systems: The sample is pumped through the heating tube at a fixed volume flow rate, and then enters the
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