NAVY MS14223-1982 TIRE PNEUMATIC AIRCRAFT 26 0 X 8 75-11 (NAVY) (AV-8B NLG)《26 0 X 8 75-11(NAVY)(AV-8B NLG)飞机汽轮胎》.pdf

1、MS34223 2b 9999932 000838b 8 m k -2 4-6 TUE IlU SBALI. BE XR ACCOIUUHCE UIiB 3lB APPLICABLE rapUrihmrrS OF MIL-T-5041 mCEPT AS SPeCLpuD IXREIN FED. wvr CLAU I 2620 ?LY STATIC VZtT. MPL. BURST Bru) STATIC WXD rl ria UTLIC UUD LOAD PneSS. ?RESS. UIMH WEIGHT UNBAL. fBpAD SKID DEFLEC. EATING US. PSI PSI

2、 INCH POUNDS or-in ?/ DEPTH + 2% Ids. iin. nx. iin. 21 -xi YI. nx. da. &I - 4X 26.0 X 8.75-11 16 TL 11,ooO 19.300 125 440 1.85 26.0 0 RIB .25 38% - I/ D“BESS TIRE - 2/ 3/ TESTED TIRE OR NBW AT LEAST FGIR, BUT NOT IIOBE IIUH SEVEN CMTMuMISi ClRCUWERWTUL RIBS. THE GROOVES SALL BE WED SUCH TIUT FOREIGN

3、 OBJECTS WILL NOT BECOI(B TUPPED BEWEE24 BE RIBS. - 1IwD SHALL BE FABRIC BEINFORCED. - 4/ RETWAMBILITY NOT REsqOrilra) Tilt MU A. Sl%TIC TIST TRE mIDt mFLA?pD SECTION iFUTE SHWLDER INFUZED SHOuLDgR D- (niCtI) m (INcti) DIMET= (INCH) UIDTH AT KU. SE. DIA. m. Mx. nm. KU. M. K4x (INCH) 25.75 26.55 8.45

4、 9.10 23.75 7.90 B, DYHAIIIC TEST TIM g/ GW AND IHm Gum INFLATED MITSIDE MVUTED SECTION DIMETER (INCH) WIDTH (INCH) w. M. 27.79 9.30 CRMRI INFLATED SHOULDER WIDTH AT W. Sli. DIA. M. (INCH) 8.20 - S/ AND THROVN DIHMSIQIS TO BE CONPIRHED WRING CYCLE 39 O? TEST A AD CYCLE 1 O? TPST D. RIn MTA - wm MHGE

5、 LKME LEDGE WE HEEL ?UNGE BEWER4 Ulm DUNETER UIDM BEICHT WIUS MDIUS . ?LANGES (INCH) (INCH) (INCH) (WCH) (INCH) (INCH) o- - - - - - 7.25 0.66 11.00 1.85 0.875 0.218 0.30 IIE TIRE com BY nixs DRAWING mu BE SUITAELE FOR USE AND PROVIDE RFASONMLE SERVICE LIFE WRING ALL NOW OPERATIONS AT TAKE-OFF AND LA

6、NDING SEEDS INDICA= EEREIN ON ALL TYPES OF RUMIAYS AND ON AIRCRAFT CARRIERS AND AWHIBIOUS ASSAULT SfIIPS. IEST TIRES NUlBeR 1 ANZ StULL CMSECUTIVELY UIIHSTAND IBE FOLUMMC DYwAI(1C TEST SPECTBUH IN ALMETICAL SegVmCE. TESTA B C D E F C U J KI It2 L CICLES40 7 1 1 29 14 5 1 1 ?9 49. 1 TEST TIRE NIll0n

7、3 ayY. BE SUBJECTED To TEST 1,MLUXW BY 15 CYCLES OF TEST A i15 CfCLES OF TEST B AND POLLOYBD BY TEST L. . A MAW-AS TITLE MILITARY STANDAU hui, TIRE. RIMTIC. AIRCRAFT, 26.0 18.75 - 11 (NAVY) (AV-8B NLC) MIS142 23 (AS) - . - I Provided by IHSNot for ResaleNo reproduction or networking permitted withou

8、t license from IHS-,-,- . - MS11i223 2b E 9999932 0008387 T E I. I 2620 TESTA RST 1 TESTC TEST D TEST E TEST F TEST 0 TEST n TESTJ TEST K1 TEST K2 TEST L UrI/WX UEICHT SHORT TAKE-OFF - THE TI= SHALL BE TAXIED ON IXE FLWlEFL AT 34.5 HPH FOR 9000 FEET WITH 11,070 POUHD LMD. ACCELERATED AT A RATE OF 15

9、.97 FEEl/SEC/SEC p1u( O TO 136 HPK UPON COHPLETION OF ME TAXI ROLL, ME FLWEEL SHAIL BE STOPPED. lMEN IW(EIED1ATELY ME TIRE SHALL BE UHLANDED AFTER A TAKEOFF . _ - ROLL OF 1240 FEET HAS BEM COVERED IN 12 M 13 SeCONDS. DECREASED LINEARLY WITH TIW. TO 10.W MWS AT 1 SECRIO. THpdl DECREASED L1NEARI.Y WlT

10、ll TltE TO 6500 POUNDS AT 12 SECONDS. THEN TU O DOUHDS AT THE TUe ME TUE IS ULILAHDED. CYCLE WITU TIRE INDERIIFIATED ZOX. ME INITIAL LOAD OF 11.070 POUNDS SIWLL BE WLETE 39 CYCLES. COOL, RUN 40TH TAXI/NORIUL WEICHT TAKE-OFF. - 11.070 POUND LOAD. ACCELERATED AT A IUTE OF 14.40 QUEl/SEC/SEC ROn O TO 2

11、07 WH. THE TIBE ML BE TAXIED ON THE FLYWEEL AT 34.5 MPH FOR 9000 FEET WITH UPON COMPLETIO# OF THE TU1 ROLL, ME FLYVYEEL SHALL BE STOPPED, THEN IHNEDIATELY nlE TIRE SWL BE U“DED AFTER A TAKEOFF OLL OF 3200 FEET UAS BEM COVERCD IN 21 M 22 SecOSrnS. DECREASED LIWMRLY WITH TIME TU 9200 POIRIDS AT l.l.WO

12、NDS, nigii LINEARLY OECWSED TO 3000 POUNDS AT 20 SECONDS. THM DecIEASED fo O pUiD6 AT ME TIHE mE TIRE IS uyL*HDED. lYE WITZU LW OF 11.070 POUNDS SHALL BE EXTESDED TAXI 11,070 PW#D LOAD. UPON co1IpLETIoN OF TE TAXI EDLL, IILE FLYYBEEL SHALL BE STOPPED, THEN IWEDIATELY ACCELERATED AT A RATE OF 15.97 F

13、EET/SEC/SEC m o TO 1% m. THE TIRE SHALL BE INLANDED AFTER A TAKE-OFF - MQRT TAKE-OFF - aiE TIRE SHALL BE TAXIEI OH ME FLYWHEEL AT 34.5 MH FOR 13,200 FEET WIM - - _ - . _ _ - . - . ROLL OF 1240 FEET WS PEEN CWERED CREASED LINEARLY WITH TIHE TO 1O.OOO POIRIDS AT 1 SECOHD, Mw DECILPASED LINEARLY WITH T

14、IME TO 6500 POUNDS AT 12 SECONDS. EN M O AT iilE TlH TaE TIRE IS UNLANDED. CONVENTIONAL TAKE-OFF (OVERSPEED) - 11.070 POWU LOAD. ACCELERATED AT A RATE OP 14.78 FEETISECISEC FW O TO 230 HPH. POLL OF 3850 FEET IiAS BEM COVERED IN 22 TO 23 SECONDS. LINEARLY WITH TIHE TO 10,000 PDUHDS AT 1.8 SECONDS, TH

15、EN DECREASED LINEARLY WITH TlflE TO 2000 POUNDS AT 22.5 SECOSDS. THE!: TO O POUNDS AT THE TUS THE TIRE IS UNLANDED. WORT LANDING-TAXI - IHE TIRE SHALL BE LANDED AGAINST THE FLYWHEEL ROTATING AT A PERIPHEIUL SPEED OF 118 HPH. THE FLYWHEEL SPEED W.LL BE DECREASED UNTIL A ROLL DISTANCE OF APPROXIHATELY

16、 2600 FEET HAS BEEN COVERED. INCREASED LINEARLY WITH TIHE FROH 3750 POUNOS AT TOUCHDOWN TO 5500 POUNDS AS 12.6 SECONDS. MEN INCREASED YITHlN 0.5 SECONDS TO 7800 POUNDS, THM INCREASED LINEARLY WITH TIME To 9200 POUNDS AT THE END OF THE TOTAL LANDING TIME OF APPROXIlIATELY 30 SECONDS. IHHEDIATELY FOLL

17、OWING THE LANDING, THE TIRE SHALL BE TAXIED ON THE FLYWHEEL FOR 9000 FEET AT 34.5 KPH WITH 7.070 POUND LMD. COHPLETE 28 CYCLES. COOL, RiN 29TH CYCLE WITH TIRE UNDERINFLATED 20%. ROLLING VERTICAL LANDING - TAXI. TUE TIRE WL BE LANDED AGAINST A FLYWHEEL ROTATING AT A PERIPHERAL SPEED OF 69 WH. BEEN CO

18、VERED. ME TOUCHDOWN TIRE LOAD OF 7700 PWNDS SHALL BE INCREASED LINPARLY WITH TM? TO 9050 POUNDS AFTER 8 SECONDS, THEN LINEARLY INCREASED LITH TItE TO 9200 POUNDS AT THE END OF %E LANDING TIE OF APPROXIHATELY 15 SECONDS. IHNEDIATELY POLLOWING THE UNDING. THE TIRE SHALL BE TAXIED ON THE FLYWHEEL FOR g

19、oo0 FEET AT 34.5 HPH WITH 7.070 POUND LMD. CONVENTIONAL LANDING - TAXI. OF 183 MP11. SHALL BE INCRWSED LINPARLY WITH TIME FROH 1600 POUNDS AT TOUCHW TO 7000 POUNDS AT 21 SECONDS, THEN LLVEARLY INCRUSED WITH TIHE TO 9500 POUHDS AT THE END OF THE TOTAL LANDING TIHE OF APPROXItlATELY 50 SECOtlDS. IllED

20、IATELY FOLLOWING ME LANDING, ME TIRE SHALL BE TAXIED ON ME FLYWHEEL AT 34.5 HPH FOR 9000 FEET WITH 7070 POUND LOAD. SHORT UNDING - MTENDED TAXI. OF 118 HPII. COVERED. INCREASED L1NWRI.Y WI. TlNE FROH 3750 POUNDS AT TOUCHWWN TO 5500 POUNDS AT 12.6 SECONDS, THM INCREASED WITHIN 0.5 SECcriDS To 7800 PO

21、UNDS, FOLU#W BY A LINEAR INCREASE WITH TIkE TO 9200 POUNDS AT THE END OF THE TOTAL LANDING TIHE OF APPROXIMATELY 30 SECONDS. ON lME FLYUIIEEL AT 34.5 HPH FOR 13200 FEET WITH 11,070 PWND REJECTED TAKE-OFF - I?CEDIATELY BY LANDING THE TIRE AGAINST THE FLYWHEEL ROTATING AT A PERIPHERAL SPEED OF 138 MH

22、AND AN IW- DIATE TIRE LOADING OF 9200 POUNDS. ME ?LWEEL SPEED SHALL DE DECREASED UNTIL A ROLL DISTUCE OF APPROXIHATELY 3800 FEET HAS BEEN COVERED. BETUEEN 138 AND O WH. POUNDS AT 7.5 SECONDS, THEN INCREASED LINEARLY TO 14,200 POUNDS AT THE CWLETION OF THE TOTAL LANDING TIHE OF APPROXIMTELY 37 SECOND

23、S. FLYWHEEL AT 34.5 WH FOR 9000 FEET WITH 14200 POUND NRNING TAXI (LEFT) - THE TIRE SHALL BE LANDED AGAINST A FLYWHEEL ROTATING AT A PERIPHERAL SPEED OF 34.5 WH WITH 10.500 POUND LOAD FOR A DISTANCE OF 300 FEET WIM THE PLANE OF THE TIRE YAWED LEFT TO PRODUCE A SIDE LOAD OF 2710 POUNDS. 12 TO 13 SJXO

24、HDS. THE MITUL Uun OE 11,070 POUNDS SHALL BE DE- ME TIRE SHALL BE TAXIED OH TAE FLYWHEEL AT 34.5 !IPH FOR 9000 FEET WITH UWN COIIPLETION OF THE TAXI POLL. THE FLYWEEL SHALL BE STOPPED. MEN IkMEDUTELY lE TIRE SHALL BE UNLANDED AFTER A TAKE-OFF THE INITIAL LWD OF 11,070 POUNDS SIIALL BE DECREASED THF

25、AVERAGE DECELERATION RATE SHALL BE 5.76 FE/SEC/SEC BETUEW 118 AND o HPH. THE TIRE LOAD SHALL BE THE FLYWHEEL SPEED SHALL BE DECREASED UNTIL A ROLL DISTANCE OF APPROXIHATELY 775 FEET HAS THE AVERAGE DECELERATION RATE SHALL BE 6.61 FEET/SEC/SEC BETWEEN 69 AND O HPH. THE TIRE SHALL BE LANDED AGAINST TR

26、E FLYUHEEL ROTATING AT A PERIPHERAL SPEED THE FLWHEEL SPEED SHALL BE DECRUSED UNTIL A ROLL DISTANCE OF APPROXIHATELY 6680 FEET HAS BEM COVERED. THE AVEBAGE DECELERATION RATE WL BE 5.39 FEET/SEC/SEC BETWEEN 183 AND o WH. THE TIRE LOAD THE TIRE SALL BE LANDED ACAINST ME FLYWHEEL ROTATING AT A PERIPHER

27、AL SPEED TUE FLYMIEEL SPEED SIULL BE DECREASED UNTIL A ROLL DISTANCE OF APPROXIMATELY 2600 FEET HAS BEEN THE LOAD SHALL BE TIIE AVRMCE OECEI.EMTION RATE SIiALL BE 5.76 FE!ZT/SEC/SEC BElWEm 118 AND O WH. IWDIATELY FOLLWING THE LANDING, THE TIRE SHALL BE TAXIED LOAD. THIS TEST SHALL CONSIST OF 1HE PBd

28、cEDURE TEST “A“ TO SIMJlATE TAKE-OFF, FOLLMIED THE AVERAGE DECELERATION RATE SHALL BE 5.39 FEETISECISEC THE TOUCHDWI LOAD OF 9200 POUNDS SHALL BE INCREASED LINEARLY WITH TIME TO 11.2M) M5DIATELY FOLL4WINC THE LANDING, THE TIRE SHALL BE TAXIED ON THE LOAD. TURNING TAXI (RIGHT) - MHE AS K EXCEPTWITH M

29、E PIANE OF THE TIRE YAVED RIGHT M PRODUCE A SIDE LAD OF 2710 BURST TEST - THE TIW SHALL BE SUBJECTED TO A HYDROSTATIC BURST TEST. THE TIRE FAILS. IN THE QUALIFICATIOH TEST REPORT. THE PRESSURE SHALL BE INCREASED UNTIL THE FAILING PRESSURE, DESCRIPTION OF FAILURE, AND LOCATION OF FAILURE SHALL BE REP

30、ORTED I MILITARY STANDARD A NAVY-At TITLE ikrur, TIRE, PNEUMATIC. AIRCRAFT. 26.0 X 8.75 - 11 (NAVY) (AV-8B NLC) I IMS 14223(AS) Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MSLY223 26 H 9999912 0008388 L H I I 2620 TEST I BRUISE TIST - A TIXC MIUT

31、ED To 125 ?SI SEUL BE WED AGAINST A 1-3D INCII DUHETER LENGTH OF PLAIN mm m SIOCT ox IlIICsTm cuu CMLE VIM A VRTICAG LOAD OF 19300 POUNDS. IKHZDUTELY FOLLOWING THE WE OF MIS LOAD ME TIRE SHALL BE SUBJECTED To TRE WIE LOADING CMDITION AT A LOCATION IBO DECREES M WATICM Mn ME INITIAL. POOM1 OF LOADING

32、. aUALI?ICATIOH TEST REPORT - COLISTRUCTION DnAILS OF ilE QUALIFICATION TEST WLE IN IlfE GENEPAL wRI( SRMI IN FIGURE 6 OF MIL-1-5041 WITH DI!EtiSIONS LISTED AT RATED INFLATION AHD AT 200 PSI. IEPORT. TUE MTA AND UTERIAL SPECIFIED ABOVE AND IN HE-T-5041 TU ME NAVAL AIR SYSTEMS COHHAND, WASHINGTON. D.

33、C. ATEJiTIQI: AIR 53032. NOTES: I11E QLJALIFICATION TEST BEP0F.T SHALL LIST TE RCSDLTS Op ALL qUALIFICATION TESTS AND A sIECH Op ME TIRE PROFILE AT RATED AND 200 PSI SALL BE INCLUDED IN THE THE REPORT SHALL LIST ME HANUFACTURERS TEST “BER. SUBHIT TWO COPIES OF THE TEST REPORT, TOGETHER WITH 20361. 1

34、. wmcm mcvnmrs SWL BE OF ME ISSUE IN EFFECT ON MTE OF INVITATION MR BIDS, OR REQUEST MB PaopOsAL EXCEPT MAT REFERENCE INDUSIW STANMRDS SALL GIVE ME DATE OF THE ISSUE ADOPTED. 2. mcl DESICN FEATURE ?uIIpoSES, IHIS STANMRD TAKES PMCEDWCB OVER PILOCU DOCUMENTS mCK HEREIN. * US. OOVERNMENT PRINTINQ OFFICE 1WZ O - 505-022/1659 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-