ASTM D3241-20a
(Test Method)Standard Test Method for Thermal Oxidation Stability of Aviation Turbine Fuels
Standard Test Method for Thermal Oxidation Stability of Aviation Turbine Fuels
SIGNIFICANCE AND USE
5.1 The test results are indicative of fuel performance during gas turbine operation and can be used to assess the level of deposits that form when liquid fuel contacts a heated surface that is at a specified temperature.
SCOPE
1.1 This test method covers the procedure for rating the tendencies of gas turbine fuels to deposit decomposition products within the fuel system.
1.2 The differential pressure values in mm Hg are defined only in terms of this test method.
1.3 The deposition values stated in SI units shall be regarded as the referee value.
1.4 The pressure values stated in SI units are to be regarded as standard. The psi comparison is included for operational safety with certain older instruments that cannot report pressure in SI units.
1.5 No other units of measurement are included in this standard.
1.6 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. For specific warning statements, see 6.1.1, 7.2, 7.2.1, 7.3, 12.1.1, and Annex A6.
1.7 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
General Information
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Designation: D3241 − 20a An American National Standard
Designation 323/16
Standard Test Method for
1
Thermal Oxidation Stability of Aviation Turbine Fuels
This standard is issued under the fixed designation D3241; the number immediately following the designation indicates the year of
original adoption or, in the case of revision, the year of last revision.Anumber in parentheses indicates the year of last reapproval.A
superscript epsilon (´) indicates an editorial change since the last revision or reapproval.
This standard has been approved for use by agencies of the U.S. Department of Defense.
1. Scope* 2. Referenced Documents
2
2.1 ASTM Standards:
1.1 This test method covers the procedure for rating the
D1655Specification for Aviation Turbine Fuels
tendencies of gas turbine fuels to deposit decomposition
D4057Practice for Manual Sampling of Petroleum and
products within the fuel system.
Petroleum Products
1.2 The differential pressure values in mm Hg are defined
D4306Practice for Aviation Fuel Sample Containers for
only in terms of this test method.
Tests Affected by Trace Contamination
E177Practice for Use of the Terms Precision and Bias in
1.3 The deposition values stated in SI units shall be re-
ASTM Test Methods
garded as the referee value.
E691Practice for Conducting an Interlaboratory Study to
1.4 The pressure values stated in SI units are to be regarded Determine the Precision of a Test Method
3
as standard. The psi comparison is included for operational
2.2 ISO Standards:
safety with certain older instruments that cannot report pres-
ISO 3274 Geometrical Product Specifications (GPS)—
sure in SI units.
Surface texture: Profile method—Nominal characteristics
of contact (stylus) instruments
1.5 No other units of measurement are included in this
ISO 4288 Geometrical Product Specifications (GPS)—
standard.
Surface texture: Profile method—Rules and procedures
1.6 This standard does not purport to address all of the
for the assessment of surface texture
4
safety concerns, if any, associated with its use. It is the
2.3 ASTM Adjuncts:
responsibility of the user of this standard to establish appro-
Color Standard for Tube Deposit Rating
priate safety, health, and environmental practices and deter-
mine the applicability of regulatory limitations prior to use. 3. Terminology
For specific warning statements, see 6.1.1, 7.2, 7.2.1, 7.3,
3.1 Definitions of Terms Specific to This Standard:
12.1.1, and Annex A6.
3.1.1 deposits, n—oxidative products laid down on the test
1.7 This international standard was developed in accor- area of the heater tube or caught in the test filter, or both.
dance with internationally recognized principles on standard- 3.1.1.1 Discussion—Fuel deposits will tend to predominate
ization established in the Decision on Principles for the at the hottest portion of the heater tube, which is between the
30mm and 50mm position.
Development of International Standards, Guides and Recom-
mendations issued by the World Trade Organization Technical
3.1.2 heater tube, n—an aluminum coupon controlled at
Barriers to Trade (TBT) Committee.
elevated temperature, over which the test fuel is pumped.
3.1.2.1 Discussion—The tube is resistively heated and con-
trolled in temperature by a thermocouple positioned inside.
2
For referenced ASTM standards, visit the ASTM website, www.astm.org, or
contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
1
This test method is under the jurisdiction of ASTM Committee D02 on Standards volume information, refer to the standard’s Document Summary page on
Petroleum Products, Liquid Fuels, and Lubricants and is the direct responsibility of the ASTM website.
3
Subcommittee D02.J0.03 on Combustion and Thermal Properties. Available from International Organization for Standardization (ISO), 1, ch. de
CurrenteditionapprovedJuly1,2020.PublishedJuly2020.Originallyapproved la Voie-Creuse, CP 56, CH-1211 Geneva 20, Switzerland, http://www.iso.org.
4
in 1973. Last previous edition approved in 2020 as D3241–20. DOI: 10.1520/ Available from ASTM International Headquarters. Order Adjunct No.
D3241-20A. ADJD3241. Original adjunct produced in 1986.
*A Summary of Changes section appears at the end of this standard
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1
---------------------- Page: 1 ----------------------
D3241 − 20a
The critical test area is the thinner portion, 60mm in length, with each test rig. (Warning—No attempt should be made to
betweentheshouldersofthetube.Fuelinlettothetubeisatthe operate the instrument without first becoming acquainted with
0mm position, and fuel exit is at 60mm. all components and the function of each.)
6.1.2 Certain operational parameters used with the instru-
3.2 Abbreviations:
ment are critically important to
...
This document is not an ASTM standard and is intended only to provide the user of an ASTM standard an indication of what changes have been made to the previous version. Because
it may not be technically possible to adequately depict all changes accurately, ASTM recommends that users consult prior editions as appropriate. In all cases only the current version
of the standard as published by ASTM is to be considered the official document.
Designation: D3241 − 20 D3241 − 20a An American National Standard
Designation 323/16
Standard Test Method for
1
Thermal Oxidation Stability of Aviation Turbine Fuels
This standard is issued under the fixed designation D3241; the number immediately following the designation indicates the year of
original adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. A
superscript epsilon (´) indicates an editorial change since the last revision or reapproval.
This standard has been approved for use by agencies of the U.S. Department of Defense.
1. Scope*
1.1 This test method covers the procedure for rating the tendencies of gas turbine fuels to deposit decomposition products within
the fuel system.
1.2 The differential pressure values in mm Hg are defined only in terms of this test method.
1.3 The deposition values stated in SI units shall be regarded as the referee value.
1.4 The pressure values stated in SI units are to be regarded as standard. The psi comparison is included for operational safety
with certain older instruments that cannot report pressure in SI units.
1.5 No other units of measurement are included in this standard.
1.6 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility
of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of
regulatory limitations prior to use. For specific warning statements, see 6.1.1, 7.2, 7.2.1, 7.3, 12.1.1, and Annex A6.
1.7 This international standard was developed in accordance with internationally recognized principles on standardization
established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued
by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
2. Referenced Documents
2
2.1 ASTM Standards:
D1655 Specification for Aviation Turbine Fuels
D4057 Practice for Manual Sampling of Petroleum and Petroleum Products
D4306 Practice for Aviation Fuel Sample Containers for Tests Affected by Trace Contamination
E177 Practice for Use of the Terms Precision and Bias in ASTM Test Methods
E691 Practice for Conducting an Interlaboratory Study to Determine the Precision of a Test Method
3
2.2 ISO Standards:
ISO 3274 Geometrical Product Specifications (GPS)—Surface texture: Profile method—Nominal characteristics of contact
(stylus) instruments
ISO 4288 Geometrical Product Specifications (GPS)—Surface texture: Profile method—Rules and procedures for the
assessment of surface texture
4
2.3 ASTM Adjuncts:
Color Standard for Tube Deposit Rating
3. Terminology
3.1 Definitions of Terms Specific to This Standard:
3.1.1 deposits, n—oxidative products laid down on the test area of the heater tube or caught in the test filter, or both.
1
This test method is under the jurisdiction of ASTM Committee D02 on Petroleum Products, Liquid Fuels, and Lubricants and is the direct responsibility of Subcommittee
D02.J0.03 on Combustion and Thermal Properties.
Current edition approved March 1, 2020July 1, 2020. Published March 2020July 2020. Originally approved in 1973. Last previous edition approved in 20192020 as
D3241 – 19b.D3241 – 20. DOI: 10.1520/D3241-20.10.1520/D3241-20A.
2
For referenced ASTM standards, visit the ASTM website, www.astm.org, or contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM Standards
volume information, refer to the standard’s Document Summary page on the ASTM website.
3
Available from International Organization for Standardization (ISO), 1, ch. de la Voie-Creuse, CP 56, CH-1211 Geneva 20, Switzerland, http://www.iso.org.
4
Available from ASTM International Headquarters. Order Adjunct No. ADJD3241. Original adjunct produced in 1986.
*A Summary of Changes section appears at the end of this standard
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1
---------------------- Page: 1 ----------------------
D3241 − 20a
3.1.1.1 Discussion—
Fuel deposits will tend to predominate at the hottest portion of the heater tube, which is between the 30 mm and 50 mm position.
3.1.2 heater tube, n—an aluminum coupon controlled at elevated temperature, over which the test fuel is pumped.
3.1.2.1 Discussion—
The tube is resistively heated and controlled in temperature by a thermocouple positioned inside. The critical test area is the thinner
portion, 60 mm in length, between the sho
...
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