AIR FORCE MIL-PRF-87100 A-1997 LUBRICATING OIL AIRCRAFT TURBINE ENGINE POLYPHENYL ETHER BASE《飞机涡轮发动机用聚苯醚基润滑油》.pdf

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1、MIL-PRF-87100A m 9999906 2056877 204 I INCH-POUND I 28 November 1997 SUPERSEDING 12 November 1976 MIL-PW-871 OOA(USAF) MILL-87100(USAF) PERFORMANCE SPECIFICATION LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, POLYPEENYL ETHER BASE This specification is approved for use by the Department of the Air Force

2、and is available for use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope. This specification covers the requirements for one grade of aircraft turbine engine lubricating OS. 2. APPLICABLE DOCUMENTS 2.1 General. The documents listed in this section are specified in se

3、ctions 3 and 4 of this specification. This section does not include documents cited in other sections of this specification or recommended for additional information or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned that they must

4、meet all specified requirements documents cited in sections 3 and 4 of this specification, whether or not they are listed. Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to: ASCENSI, 2530 Loop Road

5、 W, Wright-Patterson AFB OH 45433-7101, by using the self-addressed Standardization Document Improvement Proposal OD Form 1426) appearing at the end of this document, or by letter. AMSC NIA FSC 9150 DISTRIBUTION STATEMENT A. Approved for pubiic release; distribution is unlimited. Provided by IHSNot

6、for ResaleNo reproduction or networking permitted without license from IHS-,-,-HIL-PRF-87LOOA 9999906 2056878 140 MJL-PRF-871OOA(USAF) 2.2 Government documents 2.2.1 Specifications, standards, and handbooks. The following specifications, standards, and handbooks form a part of this document to the e

7、xtent specified herein. Unless otherwise specified, the issues of these documents will be those listed in the issue of the Deparnent of Defense Index of Specifications and Standards (DoDISS) and supplement thereto, cited in the solicitation (see 6.2). SPECIFICATIONS FEDERAL A-A-5 1057 QQ-A-250J4 DEP

8、ARTMENT OF DEFENSE MIL-S-13282 FEDERAL FED-STD-3 13 FED-STD-79 1 MILITARY MIL-STD-290 TECHNICAL ORDERS TO 33A6-7-24- 1 1 Steel, Straight Aluminum Alloy 2024, Plate and Sheet Silver and Silver Alloys Material Safety Data Sheets, Preparation and Submission of Lubricants, Liquid Fuels, and Related Prod

9、ucts; Methods of Testing Packaging of Petroleum and Related Products Operations and Maintenance Instnictions for Fluid Analysis Spectrometer, Type AiE35U-3A (Unless otherwise indicated, copies of the above specifications, standards, and handbooks are available from the Defense Automated Printing Ser

10、vice, 700 Robbins Avenue, Bidg 4D, Philadelphia PA 191 11-5094.) 2.2.2 Other Government documents, drawings, and publications. The following other Government documents, rawings, and publications form a part of this doment to the extent specified herein. Unless otherwise specified the issues are thos

11、e cited in the solicitation. CODE OF FEDERAL REGULATIONS (CFR) DEPARTMENT OF LABOR 29 CFR 1910.1200 Occupational Safety and Health Standards - Hazard Communications (Application for copies should be addressed to the Superintendent of Documents, Government Printing Office, Washington DC 20402.) 23 No

12、n-govermnent publications. The following documents form a part of this document to the extent specified herein. Unless otherwise specified, the issues of the documents which are DOD adopted are those listed in the issue of the DoDISS cited in the solicitation. Unless otherwise specified, the issues

13、of documents not listed in the DoDISS are the issues of the documents cited in the solicitation (see 6.2). SOCIETY OF AUTOMOTIVE ENGINEERS (SAE) AEROSPACE MATERIAL SPECIFICATIONS (AMs) AMS 4908 AMs 5544 Titanium Alloy Sheet and Strip - 8Mn Annealed, 110,000 psi (760 ma) Yield Strength OD adopted) AI

14、ioy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 57Ni -19.50 - 13.5Co - 4.2Mo - 3.0Ti - 1.4A1- 0.05Zr - O.O06B, Consumable Electrode or Vacuum induction Melted, Annealed (DoD adopted) 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-9 flIL

15、-PRF-7LOOA 9999906 20Sb839 087 * MIL-PRF-S71OOA(USAF) AMs 6260 AMs 6475 AMs 6490 Steel Bars, Forgings, and Tubing 1.2Cr - 3.25Ni - 0.12Mo (0.07 - 0.13) (SAE 93 10) OD adopted) Steel Bars, Forgings, and Tubing, Nitriding 1.1Cr - 3.5Ni - 0.25Mo - 1.25A1(0.21- 0.26C) (DoD adopted) Steel Bars, Forgings

16、and Tubing 4.OCr - 4.2Mo - 1.OV - (0.77-0.85(7), Premium Aircraft Quaiity for Bearing Applications, Consumable Electrode Vacuum Melted OD adopted) (Application for copies should be addressed to the Society of Automotive Engineers, Inc., 400 Commonwealth Drive, Warrendale PA 15096-0001; telephone (41

17、2) 776-4841.) AMERICAN SOCIETY FOR QUALITY CONTROL (ASQC) ASQC- Z1.4 Sampling Procedures and Tables for Inspection by Attributes (DoD adopted) (Application for copies should be addressed to the American Society for Quaiity Control, PO Box 3005, 61 1 East Wisconsin Avenue, Milwaukee WI 53201-4606.) A

18、MERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM) ASTM D92 ASTM D97 ASTM D445 ASTM D664 ASTM D892 ASTM D972 ASTM D1218 ASTM D1298 ASTM D 1947 ASTM D2273 ASTM D2532 ASTM D2766 ASTM D4057 ASTM D4177 ASTM D4636 ASTM El O0 ASTM E659 Standard Test Method for Flash and Fire Points by Cleveland Open Cup, (A

19、ASHTO No. T48) OD-adopted) Standard Test Method for Pour Point of Petroleum Products Standard Test Method for Kinematic Viscosity of Transparent and Opaque Liquids (And the Calculation of Dynamic Viscosity) (DoD adopted) Standard Test Method for Acid Number of Petroleum Products by Potentiometric Ti

20、tration (British Standard 4457) (DoD adopted) Standard Test Method for Foaming Characteristics of Lubricating Oils (DoD adopted) Standard Test Method for Evaporation Loss of Lubricating Greases and Oils OD adopted) Standard Method for Testing Refractive Index and Refractive Dispersion of Hydrocarbon

21、 Liquids (DoD adopted) Standard Practice for Density, Relative Density (Specific Gravity), or API Gravity of Crude Petroleum and Liquid Petroleum products by Hydrometer Method OD adopted) Standard Test Method for Load-Carrying Capacity of Petroleum Oil and Synthetic Fluid Gear Lubricants (DoD adopte

22、d) Standard Test Method for Trace Sediment in Lubricating Oils (DoD adopted) Standard Test Method for Viscosity and Viscosity Change After Standing at Low Temperature of Aircraft Turbine Lubricants (DoD adopted) Standard Test Method for Specific Heat of Liquids and Solids (DoD adopted) Standard Prac

23、tice for Manual Sampling of Petroleum hoducts Standard Practice for Automatic Sampling of Petroleum and Petroleum Products (DoD adopted) Standard Test Method for Corrosiveness and Oxidation Stability of Hydraulic Oils, Aircraft Turbine Engine Lubricants, and Other Highly Refined Oils Standard Specif

24、ication for ASTM Hydrometers (DoD adopted) Standard Test Method for Autoignition Temperature of Liquid Chemicals (Application for copies should be addressed to the American Society for Testing and Materials, 100 Barr Harbor Drive, West Conshohocken PA 19428-2959.) 3 Provided by IHSNot for ResaleNo r

25、eproduction or networking permitted without license from IHS-,-,-MIL-PRF-BLOOA 9O6 2056880 8T9 P MIGpRF-871 OOAO 2.4 Order of precedence. 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

26、, however, supersedes applicable laws and regulations unless a specific exemption has been obtained. 3. REQUIREMENTS 3.1 Qualification. The lubricating oils furnished under this specification shall be products that are authorized by the Quaidjing Activity for listing on the applicable Qualified Prod

27、ucts List (QPL) before contract award (see 4.2 and 6.3). 3.2 Materials. The composition of this lubricating oil is not limited; however, known or suspected human carcinogens (as defined by the Occupational Safety and Health Standards - Hazard Communications, 29 CFR 1910.1200) are prohibited. The bas

28、estock shall be essentially bis(phenoxyphenoxy)benzene. The engine lubricating oil shali have no adverse effect on the health of personnel when used for its intended purpose. Recycled basestocks are permitted; however, each batch must be fully tested in accordance with ail qualification requirements

29、 of this specification. The manufacturer may be required to submit cdication of conformance to this paragraph (see 6.2). 3.3 Chemical and physical requirements. Ali classifications of the finished iubncating oil shall conform to the requirements listed in section 3 and table I when tested in accorda

30、nce with the applicable test methods. 3.4 Bench performance requirements. Bench performance requirements shall be as specified in 3.4. I and 3.4.2. 3.4.1 Bearing deposition. Bearing deposition of the lubricating oil shall be determined in accordance with 4.4.3. Results of the determinations shall co

31、mply with the following: Deposit rating 60 max Filter deposit weight, g oil consumption, ml Viscosity at 4OoC, % chauge Acid number change, mg KOWg 2.5 max 1440 max 25 max 0.20 max Metai specimen weight change, mg/cm* 10.2 max 3.4.2 Gear Ioad-carrying capacity. The gear load-canying capacity shall b

32、e conducted as specified in 3.4.2.1 and 3.4.2.2. The average of six determinations shail be required to determine load-carrying capacity. Test results of ail determinations shall be included in reporting data. 3.4.2.1 Gear loadearrying capacity requirement conducted at 74“C(165“F). Load-carrying cap

33、acity shall be determined in accordance with ASTM 01947 using AMs 6260 test gears. only those gear machines having a reference oil “C“ average rating within the range 438 to 578 kN/m (2500 to 3300 Win) are acceptable. Test resuits must include reporting data on all determinations conducted. The aver

34、age percentage of the relative rating determinations shall be multiplied by the reference oil specified average of 508 kN/m (2900 lbflin). Determinations 2minimum Load-Canying Capacity AVE % Reiative Rating x 508 kN/m (2900 ibflin) 336 kN/m (1920 Min) min 4 Provided by IHSNot for ResaleNo reproducti

35、on or networking permitted without license from IHS-,-,-NIL-PRF-873OOA m 0b 2056883 735 m MIEPRF-871OOASAF) TABLE I. Chemical, physical, and performance requirements. Characteristic ,cid number (T.A.N.), mg KOWg iscosity at 260C (500F) ,cs z iscosity at 98.9“C (210“F), cs U iscosity at 373C (100“F),

36、 cs z iscosity at -5 1 “C (-60F) 35% by weight diluent), cs E at 35 minutes at 3 hours iutoignition temperature “C(“F) lash point, OC( OF) our point, “C(T) ivaporation loss at: 260C(500“F), % g 30O0C(572“F), % r/ Lefractive index at 25“C(77T) race sediment, ml / 200 ml of oil z Ipecific gravity at 1

37、 OO0F/60“F a/ :Odg/ Foam volume, ml at: 24“C(75“F) 93“C(2OO0F) 24“C(after test at 93C) Foam volume afta 1 O minute settle period, mi 24“C( 75F) 93“C(200T) 2CC(after test at 93C) rrace metai content, ppm, maximum o Aluminum (Al) iron (Fe) Chromium (Cr) Silver (Ag) Copper (a) in (in) Magnesium (Mg) Ni

38、ckel (Ni) Titanium (Ti) Silicon (Si) Requirement 0.05 -1 1.0 min 12.5 min 330 min, 375 max 17 x 103 max 17 x lo3 max 610(1130) min 275(527) min 5(41) max 15 max 35 max 1.6284 min ; 1.6324 max 0.005 max 1.180min; 1.200max 625 max z 250 max 625 max 2 550 none 550 3 2 3 1 1 200 min, 400 max 1 2 1 1 Tes

39、t Method ASTM 0664 0445 0445 0445 02532 E659 092 097 0972 01218 022 73 01298 0892 mD-STD-791 5 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-87LOOA 9997706 2056882 671 MILPRF-8710OA(USA.l?) TABLE I. Chemical, physical, and performance requi

40、rements. (cont) Characteristic Specific heat at: 26OoC(50Q“F) 160C(3200F) 60C( 140F) Compatibility Turbidity Sediment, mV200 ml oil, maximum MIL-PRF-871 O0 Corrosion and oxidation stability at 32OoC( 608T) Viscosity change at 4OoC, % Acid number change, Metal weight change, mg/cm* mg KOWg Al Ag Fe M

41、-50 WSP Ti Reauirement 0.45 min 0.40 min 0.35 min none 0.005 -5 to +25 IIUX 0.20 max Hl.2 max 10.2 max *0.2 max *0.2 max I0.2 max *0.2 max Test Method ASTM 02766 04636 FED-STD-791 FTM 3403- FTM 5307- ! Titrate to a pH I i end point 2 Viscometer shall be in accordance with ASTIULM45. Test conditions

42、will be spec$ed by the activiv responsible for qualcation (see 6.3). 2 Diluent shall be reagent grade. ! Use a 6 hour tes: period, ambient atmospheric pressure, and a bath temperahue controlled within I2“C of test temperature. Air temperature shall be maintained within d2“c of bath temperature, usin

43、g aprehenter ifnecessay. Report total ml sediment per 200 ml of oil instead of average ml sediment per 100 ml of oii. 0 Use ASiU i14H-62 hydrometer. &! Report foam collapse period in secomis. Complete foam collapse is adjudged to be thatpoin: at which no more than a single row of bubbles remain arou

44、nd the cyiinder wail and the air inlet tube. If this ring of bubbles around :he cylinder wall contains segments having two or more layers of bubbles and the di$rence in height of the foam in the ring is not greater than i0 ml, complete foam collapse is &judged to be tha: point at which a break occur

45、s in :he ring of bubbles without subsequent reforming of :he ring. 8! Foam volume measurements :ah after 5 minute aeration. 91 See paragrqh (4.4.2) for test method details. 10/ Values may bicaiculatedjhm an equation of specflc heat YS. temperature derived from minimum Oifive determinations of enthal

46、py change made over the speci$ced femperature range, ese shall include determinations of enthalpy change made at elevated iemperatures within I2OoC(+36 F) of each of the three required test :emperaturn. Ir/ See paragraph (4.4.4) for :est method detaik. -See paragraph (4.4.5) for tat methoddetails. 3

47、.4.2.2 Gear loadearrying capacity requirement conducted at 22O0C(4280F). Load-carrying capacity shall be determined in accordance with FED-Sm-791, Method 651 7, and the following test conditions: Gear Material Gear Temperature 22WoC(428f5OF) Test-oii-in-Temperature 205SC(401f5T) Support Oii-in Tempe

48、rature 74fi0C(1 65fiT) AMs 6475 (Nitralloy N) only those gear machines with a reference oil “C“ average rating (using AMs 6260 test gears) within the range of 438 to 578 kN/m (2500 to 3300 lbflin) are acceptable. Gears shall be finished machined including gear tooth profile grinding after nitriding.

49、 Load-carrying Capacity AVE % Relative rat in x 508 kN/m (2900 lbflin) 168 kN/m (960 lbflin) min Determinations 2minimum 6 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-?, MIL-PRF-7LOOA D 9Ob 205b883 508 D 3.5 Workmanship. The finished lubricating oil shall be transparent and uniform in appearance, and free from cloudiness, suspended matter, or other adulteration