AIR FORCE MIL-PRF-6085 E-2011 LUBRICATING OIL INSTRUMENT AIRCRAFT LOW VOLATILITY《低挥发航空仪表润滑油》.pdf
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1、MIL-PRF-6085E 8 December 2011 SUPERSEDING MIL-PRF-6085D 20 February 1998 PERFORMANCE SPECIFICATION LUBRICATING OIL, INSTRUMENT, AIRCRAFT, LOW VOLATILITY AMSC N/A FSC 9150 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. METRIC Comments, suggestions, or questions on t
2、his document should be addressed to AFPA/PTPT, 2430 C Street, Bldg 70, Area B, Wright-Patterson AFB OH 45433-7632 or e-mailed to AFPET.AFTTwpafb.af.mil. Since contact information can change, you may want to verify the currency of this address information using the ASSIST Online database at https:/as
3、sist.daps.dla.mil. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-6085E 2 This specification is approved for use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope1.2 . This specification covers one grade of air
4、craft instrument lubricating oil only (see 6.1). The lubricating oil is identified by military symbol OAI and NATO Code No. 0-147 (see 6.5). Part or identifying number (PINM6085 - X ). The PIN to be used for lubricating oil acquired to this specification is created as follows: Container Size 1 = 1.5
5、 oz. 2 = 4 oz. 3 = 8 oz. 4 = 1 quart 5 = 5 gallon 2 APPLICABLE DOCUMENTS 2.1 Genera2.2 l. The documents listed in this section are specified in sections 3, 4, or 5 of this specification. This section does not include documents cited in other sections of this specification or recommended for addition
6、al information or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet all specified requirements of documents cited in sections 3, 4, or 5 of this specification, whether or not they are listed. Government documents2.
7、2.1 . Specifications, standards, and handbooksFEDERAL SPECIFICATIONS . The following specifications, standards and handbooks form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract. QQ-S-69
8、8 Steel, Sheet and Strip, Low Carbon DEPARTMENT OF DEFENSE SPECIFICATIONS MIL-PRF-680 Degreasing Solvent (Copies of these documents are available online at https:/assist.daps.dla.mil or from the Standardization Document Order Desk, 700 Robbins Avenue, Bldg 4D, Philadelphia PA 19111-5094.) 2.3 Non-go
9、vernment publicationsASTM INTERNATIONAL . The following documents form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract. ASTM A29/A29M Standard Specification for Steel Bars, Carbon and Al
10、loy, Hot-Wrought, General Requirements for (DoD Adopted) ASTM B36/B36M Standard Specification for Brass Plate, Sheet, Strip, And Rolled Bar (DoD Adopted) ASTM D91 Standard Test Method for Precipitation Number of Lubricating Oils (DoD Adopted) ASTM D92 Standard Test Method for Flash and Fire Points b
11、y Cleveland Open Cup Tester (DoD Adopted) ASTM D97 Standard Test Method for Pour Point of Petroleum Products (DoD Adopted) Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-6085E 3 ASTM D445 Standard Test Method for Kinematic Viscosity of Trans
12、parent and Opaque Liquids (and Calculation of Dynamic Viscosity) (DoD Adopted) ASTM D972 Standard Test Method for Evaporation Loss of Lubricating Greases and Oils (DoD Adopted) ASTM D974 Standard Test Method for Acid and Base Number by Color-Indicator Titration (DoD Adopted) ASTM D1500 Standard Test
13、 Method for ASTM Color of Petroleum Products (ASTM Color Scale) (DoD Adopted) ASTM D1748 Standard Test Method for Rust Protection by Metal Preservatives in the Humidity Cabinet (DoD Adopted) ASTM D4057 Standard Practice for Manual Sampling of Petroleum and Petroleum Products (DoD Adopted) ASTM D4636
14、 Standard Test Method for Corrosiveness and Oxidation Stability of Hydraulic Oils, Aircraft Turbine Engine Lubricants, and Other Highly Refined Oils (DoD Adopted) (Copies of these documents are available online at http:/www.astm.org or from ASTM International, 100 Barr Harbor Drive, West Conshohocke
15、n PA 19428-2959) 2.4 Order of precedence3. REQUIREMENTS . Unless otherwise noted herein or in the contract, in the event of a conflict between the text of this document and the references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicab
16、le laws and regulations unless a specific exemption has been obtained. 3.1 Qualification3.2 . The instrument oil furnished under this specification shall be products that are authorized by the qualifying activity for listing on the applicable qualified products list before contract award (see 4.2 an
17、d 6.3). Materials3.3 . Aircraft instrument lubricating oil (low volatility) shall consist substantially of synthetic base oil and additive materials to impart oxidation stability and corrosion-protective properties. Certain esters of the dibasic organic acids containing six to ten carbon atoms are k
18、nown to be suitable for use but are not mandatory. The right is reserved to subject oils of new or unusual composition to such additional tests as are considered necessary to ensure serviceability of the material. Viscosity-temperature coefficient (VI) improvers or pour point depressants shall not b
19、e used. Properties. Products shall conform to the requirements as specified in Table I and 3.4 through 3.6 when tested as specified in Section 4. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-6085E 4 TABLE I. Properties of the finished oilC
20、haracteristic . Value Viscosity in centistokes at 54C (min) at -54C (max) Pour point (max) Flash point (min) Precipitation number (max) Acid number 8 12,000 -57C 185C 0 report 3.4 3.4.1 Performance Corrosion and oxidation stability3.4.2 . When tested as specified in section 4 the change in weight of
21、 cadmium-plated steel, copper, steel aluminum alloy, and magnesium alloy, when subjected to the action of the oil for 168 hours at 121C +1C, shall be not greater than 0.2 mg per square cm of surface for each strip. There shall be no pitting, etching, or visible corrosion on the surface of any of the
22、 metals when viewed under magnification of 20 diameters. Slight discoloration of the surface of the copper will be permitted, but dark brown, gray or black stain shall be cause for rejection. Resistance to oxidation3.4.3 . When tested as specified in section 4, the oil shall not have changed more th
23、an +5 percent from the original viscosity in centistokes at 54.4C after the oxidation-corrosion test (see 4.4.2). The neutralization number increase shall be not greater than 0.5 after oxidation. There shall be no evidence of separation of insoluble materials or gumming of the oil. Low temperature s
24、tability3.4.4 . When tested as specified in section 4, there shall be no gelling or separation of solid or liquid phases in the oil after storage at a temperature at or below -54C for 72 hours. The presence of a dense cloud, which does not “settle out”, shall not be the cause for rejection. Evaporat
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