NAVY MS18060 REV B-1981 TIRE PNEUMATIC AIRCRAFT 24 X 5 5 (200 MPH) FABRIC TREAD TYPE VII (NAVY)《24 X 5 5(200 MPH) VII(NAVY)纤维踏板飞机汽轮胎》.pdf
《NAVY MS18060 REV B-1981 TIRE PNEUMATIC AIRCRAFT 24 X 5 5 (200 MPH) FABRIC TREAD TYPE VII (NAVY)《24 X 5 5(200 MPH) VII(NAVY)纤维踏板飞机汽轮胎》.pdf》由会员分享,可在线阅读,更多相关《NAVY MS18060 REV B-1981 TIRE PNEUMATIC AIRCRAFT 24 X 5 5 (200 MPH) FABRIC TREAD TYPE VII (NAVY)《24 X 5 5(200 MPH) VII(NAVY)纤维踏板飞机汽轮胎》.pdf(2页珍藏版)》请在麦多课文档分享上搜索。
1、1 MS38060 REV B 2b = 9999932 0008433 2 U k-2 9-6/ I , .- ._ . IBE TIRE SHALL BE IN ACcoRpAHCE UIM IliE APPLICABLE WraenniTS OF SPECIFICATION MIL-T-5041 EI(CEPT AS SPECIFIED BEREIN SIZE rLT STATIC PERT. IRFL. BURST BFAD UEICBT STATIC TREAD .WLD DEFLEC . mATMG LMD LMD PRESS. mss. YIDTtl POUNDS UNBAL.
2、%ID .l. 3% IATIIK: LBS. PSI. PSI. IN. w. Oz-in. DEPM - 4% Ias. m. HIN. m.21 Lux. M. . - 31 mi. - 245.5 16TI 11,500 52.000 355 1420 1.4 29.5 15 Rib .35 32.0 - i/ Ti-Tube Type Tire 21 Rcv tire 21 Three continuous circumferential Grooves - one groove in center of tread. caicept shall be used with radiu
3、s at bottom of grooves to preclude stress risers and circum- ferential cracking. reinforced. Wide groove Tread shall be fabric- INFLATED DiI(WSI0NS 355 PSI (INCH) CROSS SECTION SRMILDER HDM SAOULDER DIANETER WTSIDE DUWER “M - .- K4x - mHlrx - mlux - 5.35 5.70 - 4.95 23.30 23.55 24.15 TilC TIRE BIMW
4、IL BU1TABLL FOR USE AND PROVIDE REASONABLE SERVICE LIFE UUHING ALL HOWL OlI!MTIoNS AT TAKE-OFF SPEWS OP Yo1 MPC liAN 200 !Pli AID LANDlNC SPEEDS OP NOT WJRE TILAN 185 WH ON ALL TYPES OF RUNWAYS AND ON AIRCRAFT CARRlERS. TEST TIRE NUIBER 1 SWU WITHSTAND TESTS A AND B WITHOUT FAIUIRE AND MM USED FOR T
5、EST C. TEST TIRE NUIBER 2 S“,L WIHSTAND TESTS D AND E WITHOUT FAILURE AND THEN USED FOR TEST C. TEST TIRE NIMBER 3 SHALL WITHSTAN A HINIMRI HYDROSTATIC BURST PRESSURE OF 1420 PSI. FAILURE AND LOCATIOH SHALL BE REPORTED IN THE QUALIFICATIN TEST REPORT AS TEST F. TEST A - BRUISE TESTS iXE FALING PRESS
6、URE. DESCRWION OF - A NEW TIRE SHALL BE INFLATED WITH AIR TU 475 PSI AND LOADED AGAINST A ONE AND TRREE EIGUTHC INCH (1-318“) DUER LmGTH OF PUIN ROUND BAR STOCK OR CABLE. A VERTICAL LOAD OF 52.000 POUNDS SHALL BE APPLIED WITH ME VERTICAL CENTER-LINE OF ME HUNTED TIRE HAKING AN ANGLE OF 87 DEGREES WI
7、TH THE PLATFH. FOLLOWING THE RELEASE OF MIS LOAD TllE TIRE SlIA1.L BE SUBJECTFJI TO TIlE SAPE LMDINC CONDITION AT A SPOT 180 DECREES PROII THE INITIAL POINT OF LOADING. IWDUTELY TEST B - DYNAMIC TEST - FOLLOWING TEST A, “NE SAME TIRE SHALL BE SUBJECTED TO 25 DYNAMMETER LANDINGS AGAINST A FLYWHEEL TI
8、lE FLYWHEEL SPEED SHALL BE DECREASED UNT-IL A ROLL DISTANCE OF 5500 ROTATING AT A PERIPIIERAL SPEED OF 185 WU. FEET HAS BEEN COVERED, AT HIICI1 TIHE ME TIRE SIIALL BE UNLANDED. FT/SEC/SEC THROUCHOUT ME RUN. FURTHER INCREASED LINEARLY HIM TINE TU A MXlMUH OF 11.500 POUNDS WITHIN 14 TO 16 SECONDS AFTE
9、R UNDING. SHALL THW BE MINTAINED AT 11,500 POUNDS UNTIL ME TIRE IS U“DED AT APPROXIELATELY 37 SECONDS FROM TIME OF LANDING. InE INFLATION PRESSURE WALL BE VARIED AS NECESSARY M OBAN A STATIC INFLECTION OF 32% ON THE FLYWHEEL SURFACE AT A LOM OF 11.500 PWNDS. TE37 C - BURST TEST YO.l - FOLLOWING TEST
10、 B, IRE SAME TIRE SHALL BE SUBJECTED To A HYDROSTATIC BURST TEST,ilE PRESSUBE SULLI INCREASED UNTIL THE TIRE FAILS AND lW FAILING PRESSURE. DESCRIPTION OF FAILURE AND LOCATION SHALL BE REPORTED IN itlp. QUALIFICATION TEST REPORT. ME AVERAGE DECELERATION RATE SHALL BE 6.6 TllE TIRE LOAD SHALL BE INCR
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- NAVYMS18060REVB1981TIREPNEUMATICAIRCRAFT24X55200MPHFABRICTREADTYPEVIINAVY24X55200MPHVIINAVY 纤维 踏板 飞机

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