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MHT6106-2014 English PDF

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MHT6106-2014: (Technical requirements for aviation jet fuel containing synthetic hydrocarbons)
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MH/T 6106-2014English279 Add to Cart 3 days [Need to translate] (Technical requirements for aviation jet fuel containing synthetic hydrocarbons) Valid MH/T 6106-2014

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Basic data

Standard ID MH/T 6106-2014 (MH/T6106-2014)
Description (Translated English) (Technical requirements for aviation jet fuel containing synthetic hydrocarbons)
Sector / Industry Civil Aviation Industry Standard (Recommended)
Word Count Estimation 11,178
Date of Issue 23/7/2014
Date of Implementation 1/10/2014
Issuing agency(ies) Civil Aviation Administration of China

MHT6106-2014: (Technical requirements for aviation jet fuel containing synthetic hydrocarbons)

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Technological requirements of aviation turbine fuel containing synthesized hydrocarbons ICS 75.160.20 E 31 Civil Aviation Industry Standard of the People's Republic of China Technical requirements for aviation jet fuel containing synthetic hydrocarbons 2014 – 07 – 23 released 2014 – 10 – 01 implementation Issued by Civil Aviation Administration of China

Foreword

This standard was drafted in accordance with the rules given in GB/T 1.1-2009. This standard was approved by the Aircraft Airworthiness Certification Department of the Civil Aviation Administration of China. This standard is under the jurisdiction of the China Academy of Civil Aviation Science and Technology. This standard was drafted by the Second Research Institute of Civil Aviation Administration of China. The main drafters of this standard. Xia Zuxi, Yang Zhiyuan, Liu Hua, Chen Kai, Su Zhengliang, Ma Dechao. Technical requirements for aviation jet fuel containing synthetic hydrocarbons

1 Scope

This standard specifies the manufacturing and technical requirements for synthetic hydrocarbon-containing aviation jet fuel and its components. This standard only applies to the manufacture of initial batches containing synthetic hydrocarbon aviation jet fuel and its components.

2 Normative references

The following documents are indispensable for the application of this document. For dated reference documents, only the dated version applies to this article Pieces. For undated references, the latest version (including all amendments) applies to this document. GB 6537-2006 No. 3 jet fuel ASTM D 56 Test method for flash point determination using Tiger closed cup tester ASTM D 86 Test method for distillation of petroleum products under atmospheric pressure ASTM D 130 Test method for determining the corrosivity of petroleum products to copper by copper sheet corrosion test ASTM D 381 Test method for determination of actual colloidal content of fuel by spray evaporation ASTM D 445 transparent and opaque liquid kinematic viscosity test method (and calculation of dynamic viscosity) ASTM D 1266 Test method for sulfur content in petroleum products (burning lamp method) ASTM D 1298 Density test method for determining the density, relative density (specific gravity) or API specific gravity of crude oil and liquid petroleum products ASTM D 1319 Fluorescent Indicator Adsorption Method for Determination of Hydrocarbon Types in Liquid Petroleum Products ASTM D 1322 Test Method for Smoke Point of Aviation Turbine Fuel and Kerosene ASTM D 1655 Aviation Turbine Fuel Standard ASTM D 1840 Test Method for Determination of Naphthalene Hydrocarbon Content in Aviation Turbine Fuel by UV Spectrophotometer ASTM D 2386 Aviation Fuel Freezing Point Test Method ASTM D 2425 Test Method for Determination of Hydrocarbons in Middle Distillates by Mass Spectrometry ASTM D 2622 Test Method for Determination of Sulfur Content in Petroleum Products by Wavelength Dispersive X-ray Fluorescence Spectrometry ASTM D 2624 Test Method for Electrical Conductivity of Aviation and Distillate Fuels ASTM D 2887 Test method for determining the boiling point distribution of petroleum fractions by gas chromatography ASTM D 3227 Test method for mercaptan sulfur in gasoline, kerosene, aviation turbine and distillate fuel (potentiometric method) ASTM D 3241 Test Method for Thermal Oxidation Stability of Aviation Turbine Fuel ASTM D 3242 Test Method for Acid Value of Aviation Turbine Fuel ASTM D 3338 Test Method for Estimating Net Heating Value of Aviation Fuel ASTM D 3828 Test method for flash point determination by small closed cup ASTM D 3948 Test Method for Determining Water Separation Characteristics of Aviation Turbine Fuel by Portable Separator ASTM D 4052 Digital Density Meter Test Method for Measuring Liquid Density, Relative Density and API Degree ASTM D 4294 Test Method for Determination of Sulfur Content in Petroleum Products by Energy Dispersive X-ray Fluorescence Spectrometry ASTM D 4529 Test Method for Estimating Net Heating Value of Aviation Fuel Combustion ASTM D 4629 Test Method for Determination of Trace Nitrogen in Liquid Petroleum Hydrocarbons by Oxidative Combustion and Chemiluminescence Detection ASTM D 4809 Test method for determining the net calorific value of liquid hydrocarbon fuels by bomb calorimeter method (precision method) ASTM D 5001 The test method for determining the lubricity of aviation turbine fuels with the ball cylinder lubricity evaluation instrument (BOCLE) ASTM D 5291 Test method for measuring carbon, hydrogen and nitrogen content in petroleum products and lubricants with instruments ASTM D 5453 determines light hydrocarbons, spark-ignition engine fuel, diesel engine fuel, and engine engine fuels by ultraviolet fluorescence Test method for total sulfur content in oil ASTM D 5972 Test method for freezing point of aviation fuel (automatic phase change method) ASTM D 6304 Coulometric Karl Fischer Titration Method for Determination of Water Content in Petroleum Products, Lubricants, and Additives ASTM D 6379 High Performance Liquid Chromatography Refractive Index Method for Determination of Aromatics in Aviation Fuels and Petroleum Fractions ASTM D 7153 Test method for freezing point of aviation fuel (automatic laser method) ASTM D 7154 Test Method for Freezing Point of Aviation Fuel (Automatic Optical Fiber Method) ASTM D 7359 uses ion chromatography to detect aromatic hydrocarbons (combustion ion chromatography-CIC) and their mixture after oxidation, high temperature hydrolysis, combustion Test method for total fluorine, chlorine and sulfur content in Determination of IP 12 specific heat value IP 16 aviation fuel freezing point test (manual method) IP 57 Determination of kerosene smoke point IP 71 Part 1 Determination and calculation of dynamic viscosity of transparent and opaque petroleum products IP 123 Determination of distillation properties at atmospheric pressure IP 154 Copper Corrosion Test of Petroleum Products IP 156 Determination of Hydrocarbon Types in Petroleum and Related Products-Fluorescence Method IP 160 Laboratory determination of the density of crude oil and liquid petroleum products-hydrometer method IP 170 Flash Point Determination-Abbe Closed Cup Method IP 274 Determination of the conductivity of jet fuel and distillate fuels IP 323 Determination of Thermal Oxidation Stability of Jet Fuel Turbine Fuel IP 336 Determination of Sulfur Content in Petroleum Products-Energy Dispersive X-ray Fluorescence Spectrometry IP 342 Determination of mercaptan content in light and mid-distillate fuels of petroleum products-potentiometric titration IP 354 Determination of Aviation Fuel Acid Value-Fuel Color Indicator Titration Method IP 365 Density determination of crude oil and petroleum products-U-tube oscillation method IP 379 Determination of Constant Nitrogen Oxide-Chemiluminescence Method IP 406 Gas Chromatography Method for Determination of Petroleum Products IP 435 Determination of the freezing point of aviation fuel-automatic phase transition method IP 436 Determination of Aromatics and Hydrocarbon Types-High Performance Liquid Chromatography with Differential Refractive Index Detection IP 438 moisture determination-Karl Fischer titration IP 523 flash point determination-fast balanced closed cup method IP 528 aviation fuel freezing point determination-automatic optical fiber method IP 529 Aviation Fuel Freezing Point Determination-Automatic Laser Method IP 540 Determination of the actual colloidal content of aviation turbine fuel-jet evaporation method IP 585 Determination of Fatty Acid Methyl Ester (FAME) in Biodiesel and Aviation Fuel-GC-MS Selective Ion Scanning and Monitoring Method IP 590 Determination of Fatty Acid Methyl Ester (FAME) in Aviation Fuel-High Performance Liquid Chromatography Evaporative Light Scattering Detection Method Def-Stan 91-91 turbine fuel, aviation kerosene type, Jet A-1 UOP 389 Method for determination of trace metals in oil The following terms and definitions apply to this document.

3 Terms and definitions

3.1 Conventional jet-fuel Conventional hydrocarbon derivatives derived from crude oil, liquid natural gas condensate, heavy oil, shale oil and oil sands. 3.2 Initial batch batch origination The batch of fuel production site. 3.3 Hydroprocessed Under the action of a catalyst, hydrogen reacts with organic compounds to remove oxygen, sulfur and nitrogen impurities, saturate unsaturated hydrocarbons or change the molecular structure of hydrocarbons. Structure of conventional chemical processes. 3.4 Synthesized hydrocarbons Through gasification, Fischer-Tropsch synthesis process and hydroprocessing process, from alternative raw material sources (such as coal, natural gas, biomass and hydrogenated fat and Oil esters). 3.5 Synthesized paraffinic kerosene SPK Synthetic blending components mainly composed of isoparaffins, normal alkanes and cycloalkanes. 3.6 Synthetic blending component A synthetic hydrocarbon meeting the requirements of Appendix A or Appendix B.

4 General

This standard is the quality standard for synthetic hydrocarbon-containing aviation turbine fuel and its synthetic components at the production site. The aviation turbine engine fuel produced, certified and issued in accordance with this standard meets the requirements of GB 6537/DEF-STAN 91-91/ASTM D1655 Requirements, once issued, it should be considered to be based on No. 3 jet fuel or Jet A-1 in compliance with GB 6537/DEF-STAN 91-91/ASTM D1655.

5 Component ratio

Unless otherwise defined in this standard, synthetic hydrocarbon-containing aviation turbine fuel components are. a) Conventional jet fuel (No. 3 jet fuel, Jet A, Jet A-1 fuel) and those with a volume fraction of not more than 50% meet Appendix A The required synthetic blending components; b) Conventional jet fuel (No. 3 jet fuel, Jet A, Jet A-1 fuel) and the volume fraction not higher than 50% meets Appendix B The required synthetic blending components.

6 Technical requirements

6.1 The additives used in blending of No. 3 jet fuel and SPK that comply with GB 6537 shall meet the requirements of Appendix A of GB 6537-2006. In addition to the requirements for civil aviation fuel in Table 1 of GB 6537-2006, the combined jet fuel containing synthetic hydrocarbons should also meet the following requirements. a) The volume fraction of aromatics content is not less than 8.0% (tested according to GB/T 11132 method); b) Distillation temperature T50-T10 is not less than 15 ℃, T90-T10 is not less than 40 ℃. 6.2 Jet A or Jet A-1 conforming to ASTM D 1655 or DEF STAN 91-91 are blended with SPK components, and the blend contains synthetic hydrocarbon Jet fuel should meet the requirements of Table 1, and the additives used should meet the requirements of Table 2. AA

Appendix A

(Informative appendix) Fischer-Tropsch synthetic hydrogenated paraffin kerosene fraction A.1 Scope This appendix specifies the manufacturing and performance requirements of a Fischer-Tropsch synthetic hydrogenated paraffin kerosene (SPK) blending component, unless it is combined with traditional fuel The materials are blended in accordance with the provisions of Chapter 5, otherwise they cannot be used on aero engines. A.2 Materials and manufacturing The Fischer-Tropsch hydrogenated synthetic paraffin kerosene fraction (FT-SPK) is a synthetic paraffinic kerosene prepared through Fischer-Tropsch synthesis and subsequent hydrogenation processes. The FT-SPK synthesis blending components should contain the paraffin kerosene fractions synthesized by hydrogenation, all of which are Fischer-Tropsch synthesis catalyzed by synthesis gas through iron or cobalt catalysts Craft (FT) made. The further processing of the product shall include hydrofining, hydrocracking and hydroisomerization, and may include but not limited to It is combined with other conventional refining processes, such as polymerization, isomerization and fractionation. A.3 Technical requirements FT-SPK components should meet the requirements of Table A.1 and Table A.2. BB

Appendix B

(Informative appendix) Ester and fatty acid hydrogenated paraffin kerosene fraction B.1 Scope This appendix specifies the manufacturing and performance requirements for a blending component of esters and fatty acids hydrogenated synthetic paraffin kerosene (SPK), except for If it is not blended with traditional fuels in accordance with Chapter 5, it cannot be used in aero engines. B.2 Materials and manufacturing Hydrogenation of esters and fatty acids (HEFAs) refers to the removal of all mono-, di-, and triglycerides, free fatty acids and fatty acid esters through a hydrogenation process (Such as fatty acid methyl esters) in oxygen. The blending components of bio-jet fuel containing synthetic hydrocarbons should include hydrogenated synthetic paraffin kerosene fractions, all composed of fatty acid esters Class and free fatty acids are hydrogenated and deoxygenated. The further processing of the product shall include hydrofining, hydrocracking and hydroisomerization. It can include, but is not limited to, other conventional refining process combinations, such as polymerization, isomerization, and fractionation. B.3 Technical requirements The components of HEFA-SPK shall meet the requirements of Table B.1 and Table B.2.

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