ASTM D2532-2016 Standard Test Method for Viscosity and Viscosity Change After Standing at Low Temperature of Aircraft Turbine Lubricants《航空汽轮机润滑剂承受低温后粘度和粘度变化的标准测试方法》.pdf
《ASTM D2532-2016 Standard Test Method for Viscosity and Viscosity Change After Standing at Low Temperature of Aircraft Turbine Lubricants《航空汽轮机润滑剂承受低温后粘度和粘度变化的标准测试方法》.pdf》由会员分享,可在线阅读,更多相关《ASTM D2532-2016 Standard Test Method for Viscosity and Viscosity Change After Standing at Low Temperature of Aircraft Turbine Lubricants《航空汽轮机润滑剂承受低温后粘度和粘度变化的标准测试方法》.pdf(4页珍藏版)》请在麦多课文档分享上搜索。
1、Designation: D2532 16Standard Test Method forViscosity and Viscosity Change After Standing at LowTemperature of Aircraft Turbine Lubricants1This standard is issued under the fixed designation D2532; the number immediately following the designation indicates the year oforiginal adoption or, in the ca
2、se of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. Asuperscript 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 Thi
3、s test method covers the determination of the kine-matic viscosity of aircraft turbine lubricants at lowtemperature, and the percent change of viscosity after a 3 h anda 72 h standing period at low temperature.1.1.1 The range of kinematic viscosities covered by this testmethod is from 7700 mm2/s to
4、14 000 mm2/s at 40 C andfrom 7000 mm2/s to 17 500 mm2/s at 51 C. The precisionhas only been determined for those materials, kinematicviscosity ranges, and temperatures as shown in the precisionsection. Kinematic viscosities and percent change of viscositymay be measured and reported at other tempera
5、tures and otherthermal soak period intervals as agreed by the contractingparties.1.2 The values stated in SI units are to be regarded asstandard. No other units of measurement are included in thisstandard.1.2.1 The SI unit used in this test method for KinematicViscosity is mm2/s. For user reference,
6、 1 mm2/s=10-6m2/s =1 cSt.1.3 WarningMercury has been designated by many regu-latory agencies as a hazardous material that can cause centralnervous system, kidney and liver damage. Mercury, or itsvapor, may be hazardous to health and corrosive to materials.Caution should be taken when handling mercur
7、y and mercurycontaining products. See the applicable product MaterialSafety Data Sheet (MSDS) for details and EPAs websitehttp:/www.epa.gov/mercury/faq.htmfor additional informa-tion. Users should be aware that selling mercury and/ormercury containing products into your state or country may beprohib
8、ited by law.1.4 This standard does not purport to address all of thesafety concerns, if any, associated with its use. It is theresponsibility of the user of this standard to establish appro-priate safety and health practices and determine the applica-bility of regulatory limitations prior to use. Fo
9、r specific hazardstatements, see Section 7.2. Referenced Documents2.1 ASTM Standards:2D445 Test Method for Kinematic Viscosity of Transparentand Opaque Liquids (and Calculation of Dynamic Viscos-ity)D446 Specifications and Operating Instructions for GlassCapillary Kinematic ViscometersD6300 Practice
10、 for Determination of Precision and BiasData for Use in Test Methods for Petroleum Products andLubricantsE1 Specification for ASTM Liquid-in-Glass ThermometersE563 Practice for Preparation and Use of an Ice-Point Bathas a Reference TemperatureE644 Test Methods for Testing Industrial Resistance Ther-
11、mometersE1137 Specification for Industrial Platinum Resistance Ther-mometersE1750 Guide for Use of Water Triple Point CellsE2593 Guide for Accuracy Verification of Industrial Plati-num Resistance ThermometersE2877 Guide for Digital Contact Thermometers2.2 Other Documents:MIL-PRF-7808 Lubricating Oil
12、, Aircraft Turbine Engine,Synthetic Base3MIL-PRF-23699 Lubricating Oil, Aircraft Turbine Engine,Synthetic Base, NATO Code Number O-15633. Terminology3.1 Definitions:1This test method is under the jurisdiction of ASTM Committee D02 onPetroleum Products, Liquid Fuels, and Lubricants and is the direct
13、responsibility ofSubcommittee D02.07 on Flow Properties.Current edition approved Dec. 1, 2016. Published January 2017. Originallyapproved in 1966. Last previous edition approved in 2014 as D2532 14. DOI:10.1520/D2532-16.2For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact
14、ASTM Customer Service at serviceastm.org. For Annual Book of ASTMStandards volume information, refer to the standards Document Summary page onthe ASTM website.3Available from Standardization Documents Order Desk, DODSSP, Bldg. 4,Section D, 700 Robbins Ave., Philadelphia, PA 19111-5098, http:/dodssp.
15、daps.dla.mil.*A Summary of Changes section appears at the end of this standardCopyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United StatesThis international standard was developed in accordance with internationally recognized principles on standar
16、dization established in the Decision on Principles for theDevelopment of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.13.1.1 digital contact thermometer (DCT), nan electronicdevice consisting of a digital displ
17、ay and associated tempera-ture sensing probe.4. Summary of Test Method4.1 Kinematic viscosity and percent change is determined atlow temperature using apparatus defined in Test Method D445and Specifications D446 at time intervals of 3 h and 72 hfollowing an initial measurement at 35 min.5. Significa
18、nce and Use5.1 Aircraft turbine lubricants, upon standing at low tem-peratures for prolonged periods of time, may show an increasein kinematic viscosity. This increase may cause lubricationproblems in aircraft engines. Thus, this test method is used toensure that the kinematic viscosity does not exc
19、eed themaximum kinematic viscosity in certain specifications foraircraft turbine lubricants.6. Apparatus6.1 Viscometers, drying tubes, low-temperature bath,thermometer, timer, secondary viscosity standard, filter, andcleaning supplies are described in detail in Test Method D445.6.2 ViscometerThe vis
20、cometer shall meet the require-ments of Test Method D445 and Specifications D446 and be ofthe type in which the sample can be rerun without cleaning theviscometer. Suitable holders should be used. For convenienceit is recommended that the viscometer size be chosen to keepthe efflux time between 200
21、s and 1000 s.NOTE 1Consult Specifications D446 regarding calibration constantcorrection for the actual test temperature when using Specifications D446viscometers that are not suspended level types.6.3 Drying TubesFit the viscometer openings with dryingtubes filled with indicating silica gel, using c
22、otton at top andbottom to hold the loosely packed desiccant in place. Providea cross-connection on the viscometer side of the drying tubes(which can be closed by a pinch clamp or stopcock while liquidis being drawn into the efflux bulb) so that the restriction to airflow will not cause error. Replac
23、e the silica gel when alavender color is noticeable.6.4 Viscosity Temperature BathThe constant-temperaturebath must be capable of holding several viscometers at once. Itmust have adequate stirring of the liquid medium (Note 2) andbalance between heat losses such that the bath temperature canbe maint
24、ained at the required temperature 60.03 C.NOTE 2Isopropanol or other clear, low-freezing point liquid may beused as a bath liquid.6.5 Temperature Measuring DeviceUse either a digitalcontact thermometer as described in 6.5.2 with equal or betteraccuracy or a calibrated ASTM Kinematic Viscosity TestTh
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