NAVY MIL-PRF-907 F-2004 ANTISEIZE THREAD COMPOUND HIGH TEMPERATURE《高温抗扯裂线化合物》.pdf

1、 INCH-POUND MIL-PRF-907F 17 November 2004 SUPERSEDING MIL-PRF-907E 18 June 1985 PERFORMANCE SPECIFICATION ANTISEIZE THREAD COMPOUND, HIGH TEMPERATURE This specification is approved for use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope. This specification covers ant

2、iseize compound for use on threads of steel nuts, studs, bolts and other mating surfaces, including those of superheated steam installations, at temperatures up to 1050 degrees Fahrenheit (F) (566 degrees Celsius (C). 2. APPLICABLE DOCUMENTS 2.1 General. The documents listed in this section are spec

3、ified 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 additional information or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned t

4、hat they must meet all specified requirements of documents cited in sections 3, 4, or 5 of this specification, whether or not they are listed. 2.2 Government documents. 2.2.1 Specifications, standards and handbooks. The following specifications, standards, and handbooks form a part of this document

5、to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract. DEPARTMENT OF DEFENSE SPECIFICATIONS MIL-PRF-680 - Degreasing Solvent. MIL-DTL-1222 - Studs, Bolts, Hex Cap Screws and Nuts. Comments, suggestions, or questions

6、on this document should be addressed to Commander, Naval Sea Systems Command, ATTN: SEA 05Q, 1333 Isaac Hull Avenue, SE, Stop 5160, Washington Navy Yard DC 20376-5160 or emailed to commandstandardsnavsea.navy.mil, with the subject line “Document Comment“. Since contact information can change, you ma

7、y want to verify the currency of this address information using the ASSIST Online database at http:/assist.daps.dla.mil. AMSC N/A FSC 8030 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-907F 2DEPARTMENT OF DEFENSE STANDARDS MIL-STD-1916 - Do

8、D Preferred Methods for Acceptance of Product. FEDERAL STANDARDS FED-STD-791 - Lubricants, Liquid Fuels and Related Products; Methods of Testing. (Copies of these documents are available online at http:/assist.daps.dla.mil/quicksearch or dodssp.daps.dla.mil or from the Standardization Document Order

9、 Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094.) 2.2.2 Other Government documents, drawings, and publications. The following other Government documents, drawings, and publications form a part of this document to the extent specified herein. Unless otherwise specified, the issues

10、 of these documents are those cited in the solicitation or contract. BUREAU OF MEDICINE AND SURGERY (BUMED) BUMED INST 6270.8 - Procedures for Obtaining Health Hazard Assessments Pertaining to Operational Use of a Hazardous Material. (Copies of this document are available online at https:/bumed.med.

11、navy.mil or from Bureau of Medicine and Surgery, Department of the Navy, 2300 E Street, NW, Washington, DC 20372-5300.) NAVAL SEA SYSTEMS COMMAND (NAVSEA) S9510-AB-ATM-010 Rev 2 of 30 July 1992 - Nuclear Powered Submarine Atmosphere Control Manual. (Copies of this document are available from the Nav

12、al Sea Systems Command, Code SEA 05Z9, 1333 Isaac Hull Avenue, SE, Stop 5133, Washington Navy Yard DC 20376-5133.) 2.3 Non-Government publications. The following documents form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those

13、 cited in the solicitation or contract. ASTM INTERNATIONAL ASTM A 109 - Standard Specification for Steel, Strip, Carbon (0.25 Maximum Percent), Cold-Rolled. (DOD adopted) ASTM A 193 - Standard Specification for Alloy-Steel and Stainless Steel Bolting Materials for High-Temperature Service. (DOD adop

14、ted) ASTM A 194 - Standard Specification for Carbon and Alloy Steel Nuts for Bolts for High Pressure or High Temperature Service, or Both. (DoD adopted) ASTM A 515 - Standard Specification for Pressure Vessel Plates, Carbon Steel, for Intermediate- and Higher-Temperature Service. (DOD adopted) (Copi

15、es of these documents are available from www.astm.org or ASTM International, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959.) 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. No

16、thing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-907F 33. REQUIREMENTS 3.1 Qualification. The compound furnished under t

17、his 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 and 6.3). 3.2 Material. The compound supplied under this specification shall be a smooth homogeneous mixture, uniform in appearance,

18、 free from lumps, abrasive materials, or other undesirable fillers or impurities. The shall be no odor of rancidity or perfume. 3.3 Corrosion on copper. After 24 hour exposure, the compound shall show no green color, no pitting or etching on the copper, nor shall a dark brown or black stain remain o

19、n the copper strip after washing with N-hexane. A slight brown stain shall not be cause for failure. 3.4 Toxicity. When evaluated in accordance with 4.4.4, the compound shall have no adverse effect on the health of personnel when used for its intended purpose and shall not cause any environmental pr

20、oblems during waste disposal (see 4.4.4 and 6.5). 3.5 Homogeneity. The compound shall be completely homogeneous at the time of inspection or during storage awaiting completion of the qualification tests. It shall possess a smooth greasy consistency without lumps, crusts or granular particles when ex

21、amined. 3.6 Oil separation. The vehicle of the compound shall separate not more than 10 percent of the compounds weight in 30 hours when tested at 150 5F (66 3 C). 3.7 Storage stability. After the compound has been stored for 6 months at a temperature of 150 5F (66 3C), it shall be examined. The com

22、pound shall be a smooth homogeneous mixture free from lumps and granular materials. 3.8 Performance. There shall be no galling of the stud threads, the nut threads, the nut contacting surface and the corresponding plate contacting surface when the test apparatus is disassembled following the perform

23、ance test. The average breakaway torque for loosening of the nuts from the studs shall be as specified in 4.4.2.1.4. 3.9 Recycled, recovered, or environmentally preferable materials. Recycled, recovered, or environmentally preferable materials should be used to the maximum extent possible, provided

24、that the material meets or exceeds the operational and maintenance requirements, and promotes economically advantageous life cycle costs. 3.10 Off-gassing. The compound shall meet the requirements in the Nuclear Powered Submarine Atmosphere Control Manual, NAVSEA Technical Manual S9510-AB-ATM-010 Re

25、v 2 of 30 July 1992, for a usage category of Limited (see 4.4.5 and 6.7). 4. VERIFICATION 4.1 Classification of inspections. The inspection requirements specified herein are classified as follows: a. Qualification inspection (see 4.2). b. Conformance inspection (see 4.3). 4.2 Qualification inspectio

26、n. Qualification inspection shall be conducted at a laboratory acceptable to the command or agency concerned. Qualification inspection shall consist of examination and tests specified in 4.3 and 4.4. 4.3 Conformance inspection. 4.3.1 Lot. For the purposes of sampling, a lot shall consist of all comp

27、ound manufactured as one batch. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-907F 44.3.2 Examination of filled containers. A sample of filled containers selected from each lot in accordance with MIL-STD-1916 as specified in the contract or

28、 order shall be examined to verify compliance with all stipulations of this specification regarding fill, closure, marking and other requirements not involving tests. Containers shall be examined for defects of the container and the closure, for evidence of leakage, and for unacceptable markings; ea

29、ch sample filled container shall also be weighed to determine the amount of the contents. Any container in the sample having one or more defects, or under required fill shall cause rejection of the container and if the number of defective containers in any sample exceeds the acceptable number for th

30、e appropriate sampling plan as specified in the contract or order, this shall cause rejection of the lot represented by the sample. 4.3.2.1 Examination of compound material. Portions of the compound material shall be taken from top, bottom and intermediate parts of the sample of containers and exami

31、ned visually to determine that there is no apparent difference in appearance or consistency. The material shall be homogeneous and show a smooth greasy consistency without lumps, crusts or granular particles. It shall not have an odor of rancidity or perfume. 4.3.3 Sample material for testing. From

32、each lot, a 5-pound container shall be selected, sealed and marked. The 5-pound sample specimen shall be retained by the manufacturer or contractor for verification testing, if required, at a later date. 4.3.4 Sampling for production check tests. Unless otherwise specified (see 6.2), from the first

33、lot produced on a contract or order and thereafter at such intervals as may be considered necessary by the command or agency concerned to verify the consistency of production quality, one 2-pound sample and two 1-pound samples of compound shall be forwarded to a laboratory acceptable to the command

34、or agency concerned. These samples shall meet the requirements of 3.6 and any other tests deemed necessary by the command or agency concerned to determine conformance of the product. 4.4 Tests. 4.4.1 Test procedures. The following tests shall be performed in accordance with Table I. TABLE I. Test me

35、thods. Test Applicable FED-STD-791 test method Test paragraph Acceptance criteria Required for qualification Corrosion on copper 5309 - 3.3 X Oil separation (150F) 321 - 3.6 X Storage stability 3467 4.4.3 3.7 X Performance 4.4.2 3.8 X 4.4.2 Performance tests. 4.4.2.1 Torque, galling and seizing test

36、. 4.4.2.1.1 Apparatus. The test apparatus shall consist of the following: A fixture made of carbon steel, using material in accordance with ASTM A 515, grade 70, 13 by 3 inches by approximately 1-1/2 inches thick for the end blocks which have 5 equally spaced holes, 13/16 inch in diameter, with surf

37、ace finish of 250 roughness height rating (RHR), to allow for insertion of inch 10 UNC studs (see Figure 1). The top and bottom faces of the steel end blocks shall have a surface finish of 250 RHR and be parallel within 0.002. Five unused coarse thread studs, in accordance with grade B16 of MIL-DTL-

38、1222, ASTM A 193 or equal, cut from the same length of a continuously threaded stud stock and ten unused nuts, in accordance with grade 4 of MIL-DTL-1222, ASTM A 194 or equal, shall be used for this test. Each stud shall be 12.000 0.125 inches long and shall have end surfaces which are perpendicular

39、 to the axis of the stud to a degree which shall allow stud length measurements of the required Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-907F 5accuracy. Two carbon steel face places in accordance with ASTM A 109, 13 by 3 inches and 0.1

40、25 inch thick with a surface finish of 62 RHR or smoother and five equally spaced holes to match those of the above described end blocks, shall be furnished for this test. Components for this test shall be as shown on Figure 1. A torque wrench shall be used which is easily readable, graduated in foo

41、t-pounds (ft-lb) and has a degree of accuracy of 5 percent. The overall length of each stud shall be measured with a dial indicator type device or equal, graduated in 0.0001 inch divisions, having an overall accuracy of 0.0001 inch. 4.4.2.1.2 Preparation. Dry-cleaning solvent shall be in accordance

42、with type I of MIL-PRF-680. Each component shall be cleaned in the dry-cleaning solvent and dried just prior to lubrication. The test equipment shall be assembled using the two plates as specified in 4.4.2.1.1. The threads of the studs and nuts shall be evenly coated with the antiseize compound as f

43、ollows: a. A liberal quantity of compound shall be applied to the studs and nuts. b. The nuts shall then be run to the ends of the studs (prior to assembly with the block). c. The excess compound shall be removed from the ends of nut travel on the studs and from the edges of the nuts after removal f

44、rom the studs. The block and plate shall be assembled with a stud in each of the five holes. The surface of the plates and the mating surfaces of the nuts shall be coated with a light coating of the antiseize compound. The nuts shall be run on to the studs, hand tight, against the plates. The overal

45、l length of each stud shall be measured to 0.0001 inch and recorded. 4.4.2.1.3 Procedure. The nuts shall be tightened until an elongation of 0.0162 0.0001 inch is obtained, which corresponds to a stress of approximately 50,000 pounds per square inch (PSI) at the root area of the stud thread. The tor

46、que required for each nut and stud tightening shall be recorded. The test block assembly shall be placed in an electronically heated oven and subjected to 1050 + 10 - 0F for 6 hours. Then the assembly shall be removed from the oven and allowed to cool to room temperature. The breakaway torque to loo

47、sen the nuts shall be measured and recorded. The length of the studs shall be measured. The nuts shall be tightened to re-establish the elongation of the stud length (that is, 0.0162 0.0001 inch) and the torque required recorded. The heating, cooling, torque measurements, and stud length measurement

48、s shall be repeated. Then for the third time the assembly shall be heated, cooled and subjected to a spray of 20 percent aqueous solution of sodium chloride for 7 days. At the end of this period, the assembly shall be removed and allowed to dry at room temperature for 24 hours. The torque required t

49、o loosen the nuts shall be determined and recorded. The condition of the threads and other contact surfaces, seizing of the nuts and shearing of the studs shall be noted and properly recorded. A five-point check of the torque wrench calibration against another calibrated wrench at 150 ft-lb shall be made prior to torquing and untorquing each assembly. If the torque wrench is dropped or otherwise damaged during its use, its calibration shall be c