AIR FORCE MIL-C-6529 C-1958 CORROSION PREVENTIVE AIRCRAFT ENGINE《航空器发动机预防腐蚀》.pdf
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1、a71IioIMIUX529C21 AUIW 155$SvpemdilvMIL.C-CKISS2SB IS.A2s Aw-il1957USED IS LIE1”OiMIL-C.6S29A27Awl 19s3MILITARY SPECIFICATIONCORROSION PREVENT, AIRCRAFT ENGINEThi. aprn”k.tw. ha: k. .Pp,.,.d b IfI, Dmrttt*nf Of W-,1 O.d I: .Iondo.(OW .I., w by IfIC Morg-f o. (hpirisJI, LJ7., EYJA”-H -79? Humi6!y (:
2、fibille: OPWB-tlon ofo-d,.- s.llL-D-3716-Desiccants (.civaed I forDynnmic Dehumidlficatio:fIbG-55i2Gasol ine. A.ialion: Gr. IIosSO18Y, 91 W. 100/130. 11514:.:.1I LA-6061-Oil. Lubricating. JcI En-fginelIL-L-60E2-Lubrica ti!lg Oil: AircrafcRecipmcaing (Piston) Er)gim,lIL-C-1 Ii96Cormsio 1 r e $ e I i
3、i v ePetmlatum, HOI Applicaliol,lIL-C-16173-Corrosion prp$pnll,.Solvent Cutback, Coid-.kpplicuiotSTANDARDSFEDCR.LFed. Test Lubricants. Liquid Fuel:,hletbod Std and Reletvd Imduris;-0, 791 lehnds O( Testi!tgblIL17.49 CFR In Iers!a!r Commerce Commi=-71-78 sion Rules and Regulationsfor the Transport ul
4、olt of Ex-Plosi-es and Olhr IJarqmrousArticles(The l,)(rr!lslr Commerre Comrriss ion rcwulat ia,!+am now a part cd !h, Cod P c.! Federal Reuul. tiom(lu4Q Edition-Re,.i4 I!J50$ avaikble from IrIrSuperi”tmdrnl of Document:. Gowrnmcnl Printingi)fir, mnl iscosity, at ?10” F,xchen determined as specified
5、 in 4.5,4. I.3.3.2.5 I-iscosifyinrff. The.iscosity indexnha be not less than 95 wlmn calculated asspecified in 4.5.4.1.3.3.2.6 Fia.d. point, TI,P Rash point shhllbee.tiw+stqf) Fwhendptrrmir)vd asspevifirdin 4.5.4.13.3.2.7 Pwripifion nttmbcr. Thr precipi.tataon numbe: sha!l not exceed 0.1 xvhrn deter
6、.mined = specified in 4.5.4. I3.3.2.8 orro.rion. When tesledassperifirdin 4.5.4.1, thecopper strip shall show no pittinga71nd the discolomtion shall not exceed 2aMI14-6529caccording 10 ASTl copper strip cocrosio”sts.ndards.3.3.2.9. AsA. The h content shall notexceed O.O15 percen when deerminr.d assp
7、ecified in 4,5.4.3.3.2.10 Hydrobromic arid ruu/ml il SUCI) lime = thr 12-month period mmagc-slnbili:y test is mmpleledC.3 Acceptance testri. T%? .4ccepmnc,. testsshrill mnsis: of Samplmg tes.4.3.1 .Samylin IrKl* Acceptnnre tests Ofni-tyw. rormsinr,-nrcvenl ive matrrir.i. Abel!ronsm oi tlie tests spe
8、cified for sampiw seiectedin ncenrtinnre with either Plan A nr Pkm R.ns anulimble. Plan A samrdes shsll be selected,Imm 111Pfirst Iol of Lhe Ib= been rejected may be re=Orked Or rePlato correct the defects, and reaubmittcd foracceptance. Before resubmitting, full particu-Ian concerning previous reje
9、ction and the actiontaken w mrrect the delects found in tbeoriginnl shall be furnished the Inspector.Jla(erial rejected after retest shall not be re-submitted rritbout specific appmral of thepmc,u.ring ectitity.4.4 Tc64 conditions. The *L nditiO -shrdl be as specified for each particular test.4.5 Te
10、st methods.4.5.1 High- and Lm-fcrnpcmtcuc 8Ui.Approximately 25 cc of tbe mateiid 6pecified icr3.3.1.1 sbnl be pmcred ir.ta a heaWe8iSLantglc=s tube 50 mm long by 19 mm difimeter.ThP tat tube shall be placed in an oven main-ain al Z050 + 5. F Ior 24 houm, allowed tomol w mum tempcmture in still sir.
11、and thenfurther mcIlcd by phcing the tube in s coldbox maintainwJ *I 0“ * 5 for 16 hOum,follows-d by the sample being allowed la returnLO mom temperature. The MALerid sbnll thenbe allowed to stand for 0 daya at mom Tem-perature. At the end of thin period, tbe tutwshall b examined by tmit iiFh for We
12、vidence of separation of inanluble material.4.5.2 Prolcctbn LC.d.4.5.2.1 Pane! mmpmi.fti. aw A. Steelpaneis shall bc Inbricated fmm open hcnrth,cold-finish, dead+oft-t.cmper, )nw-rbc$n steelcmfnrming w Spccificstinn QQ-S-636, 1020steel. The panea sh !( by 2 by 4 inch=5Provided by IHSNot for ResaleNo
13、 reproduction or networking permitted without license from IHS-,-,-MXTAX529Cconforming to the dwcriptioc contaiced inSpecification JAN-H-79?.4.5.2.2 PaIKl jinishing and ckanif+g. Thepanel test surface shall be so prepared, by uso or?40- or 28 fJ-grit A. fundum or CarborundumAbrasive with cloth or ps
14、per backing, as toprodu,e a surface finish 0 6 m 12 microincimrrns Tbe use cd iron oxide abrasives, “wet ordry” rluths, or “WC or dry” papers is pro.hibi! ed. The find fibrasion marks shall be inthe dimctmn parallel to the lengh of pm, cl,Tbr sds,.p shs!l b, thorOugh; cler.nvti l,) amethod whirh wil
15、l rmfuce all !yprc of SiIPErSCMIcontamination 10 tlI(- pmlics rl, ininlum,. A:.etining meti, od WI):C!) htis pro red sstlsxroryis ciescrlhec! iu t3.3 4.5.2.3 Procedure Fire pal,ek ;m.prwed MSaboie shall be so dippeJ in a sui Lable saInp!oof Type II or Type 111 nluterii. es applicabr,as 10 cfrmpictel
16、.r sulunergr s) surfaces. Thepanels sIwJ1 then hp suspsmded by stainlesssteel hooks for 4 hours in a chamber or cnhinetwhere tbe relntive humidity does no, exceed 5CIpercent and the temperature is 77 =5” F,.4t the end of this period, the paneIa shall besuspended in a humidi(y cnbinet conforming toSp
17、ecification JAN-H-79? for a period of atleast 336 boura (I4 days) tnking care that thelop of thr panel is love, brnding the books ifnecmsa for minor adjustment. The humidityctbine shrill be nmintained a( a dry-bulbtemperswe of l?OO +2 F. The pmeb ahalfbe remo.ed from the cabinet, cleaned withrmphtha
18、 (Spccfi-tion TT-T-291, Gmde I),and examined.A panel shsll be considered u having failedthe protection teat if at the eztd of the u+.?n 1 and 2 mm diamelr.rand ? OF more dots of less tIla” I mmdiameter.(d) Four or more dots of less than 1 mmdiameter.tfore thrm I panel in 5 faifing as definedabove sh
19、all be sufficient cause for retest, R,. a71tests ehrdl consist of repeating the protectiontest, using an additional 10 panels. por,compl?ticm of the retest, the failure of moreban 4 pmefs, a71dding failures of both lest andretests, shall be cause for rejeclion of thematerial,4.5.3 Sfomgf stability.
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