NAVY MS26563 REV C-1986 TIRE PNEUMATIC AIRCRAFT 40 X 14 (200 MPH) TYPE VII (NAVY)《40 X 14 (200 MPH) VII(NAVY)飞机汽轮胎》.pdf

《NAVY MS26563 REV C-1986 TIRE PNEUMATIC AIRCRAFT 40 X 14 (200 MPH) TYPE VII (NAVY)《40 X 14 (200 MPH) VII(NAVY)飞机汽轮胎》.pdf》由会员分享，可在线阅读，更多相关《NAVY MS26563 REV C-1986 TIRE PNEUMATIC AIRCRAFT 40 X 14 (200 MPH) TYPE VII (NAVY)《40 X 14 (200 MPH) VII(NAVY)飞机汽轮胎》.pdf（1页珍藏版）》请在麦多课文档分享上搜索。

1、 MS2b563 REV C 26 = 7999712 0008715 I THE TIRE SHALL BE IU ACCORDANCE WITH RIE APPLICABLE REQUIREMNTS of SPECIFICATION MIL-T-5041 EXCEPT AS SPECIFIED HEREIN 2620 I. - MOLD DEFLEC DEPTB PLY STATIC INFL. BURST BEAD STATIC RATING LlXLl PRESS. PRESS. WIDTH WEIGHT UNBAL. WD SKID - ns PART i/ RATING PSI.

2、PSI IN. LBS. oz-IN NO. SIZE - LBS. RATED nm. HAX. W. HAX. 3t m. HS26563-1 40x14 26TL 24,500 175 - 2/700 3.10 133 17 Rib .30 32% Hc26563-2 40x14 28TL 33,500 200 - 2/800 3.10 133 17 Rib .30 32% i/ TL - hibeless 2/ New Tire 3/ At least three, but no more than seven continuous circumferential - .Ribs -

3、- TIRE MTA (INCH) CENTER LRiE DIAMETER CRSS ,SECTION WIDTH SiimER DIAHFiER MIN HAX MIN K4x HAX SHOuLdlER WIDTH HAX 38.85 38.90 13.25 14.00 35.10 12.00 RIM DATA (INCH) WIDTH HIN FLILYGE BETWEEN FLANGE LEDGE LEDGE FLANGE EEL FLANGE EDGE FLANGES WIDTH DIAMETER WIDTH HEIGHT RADIUS RADIUS RADIUS 11.0 1.1

4、25 16.0 3.10 1.625 0.366 0.812 0.094 - THE TIRE COVERED BY THIS DRAWING SHALL BE SUITABLE FOR USE AND PROVIDE RFASQUABLE SERVICE LIFE DURING ALL NOW OPERATIONS AT TAKE-OFF SPEEDS OF NOT MORE THAN 200 MPH AND LANDING SPEEDS OF NOT HORE THAN 185 MPH. THE TIRE SHALL WITHSTAND WITHOUT FAILURE THE FOLLOW

5、ING TESTS: (1) DYNAMIC TEST - THE TIRE SHALL SATICFACTORILY WITHSTAND 50 CYCLES OF TEST “A“ FOLLOWED BY 100 CYCLES OF TEST “B“ WITHOUT EVIDENCE OF FAILURE. TEST A - THE TIRE SHALL BE LANDED AGAINST A FLYWHEEL RXATING AT A PERIPHERAL SPEED OF 200 MPH (174 KN(Ms). FLYWREEL SPEED SHALL THEN BE DECREGED

6、 UNTIL A ROLL DISTANCE OF 9ooo FEET HAC BEEN COVERED, AT WICH TIME RIE TIRE SHALL BE UNLANDED. WE AVEMGE DECELERATION RATE SHALL BE 4.5 E“l/SEC/SEC =WEN 200 AND 100 MPHI AND RIE 6.0 FT/SEC/SEC FROM 100 MPH To O, AT WHICH TINE THE TIRE SHALL BE UNLANDED. FROM ZERO To 6ooo LBS IN 2 lU 4 SECONDS AFTB L

7、ANDING, AND WEN FURTHER IWREGED LINEARLY WITH TIME To THE THE TIRE LOAD SHALL BE INCREASED RATED WAD IN 56 To 57 SECONDC AFPER LANDING, Rie WAD SHALL THEN BE MAIKPAINED AT RATED UKPIG THE TIRE IS UNLANDED. THE TIRE DEFLECTION AT RATED WAD ON FLYWLIEEL SHALL BE THE SAHE AS OBTAINED mRI RIE RATFJl LOA

8、D AND INFLATION PRECCURE ON A FLAT PLATE. TEST B - THE TEST CYCLE SHALL BE IDENTICAL TO THE LOW SPEED (90 TO O HPR) MNAElIC TEST DESCRIBED IN SFECIFICATI(M MIL-T-5041. THE TIRE DEFLECTION AT RATED LOD ON RIE FLYWHEEL SHALL BE %E SAME AS OBTAINED WITH THE RATED LOAD AND INFLATION PRESSURE ON A FLAT P

9、LATE. BURST TEST - FOLLOWING THE ABOVE DYNAMIC TESTS THE SAME TIRE SHALL BE SUBJECTED TO A HYDROSTATIC BURST TEST. PRESSURE SHALL BE INCREASED UNTIL RIE TIRE FAILS AND RIE FAILING PRESSURE REPORTED IN THE QUALIFICATION TEST REPORT. (2) THE AIR RETENTION - %E NBELESS TIRE SHALL BE INFLATED TO A PRESS

10、URE OF 280 PSI FOR THE 26PR OR 320 PSI FOR THE 28 PR AND ALLOWED TO STAND FOR A PERIOD OF 24 HOURS AT WHICH TIME THE PRESSURE DROP DUE TO GROKIH SHALL BE REPLACED. THE TIRE SHW THEN STAND FOR AN ADDITIONAL 24 HOURS AT WHICH TIME THE PRESSURE SHALL BE NPASURED AND THE TIRE INSPECTED. THE AIR PRESSURE

11、 LOSS SHALL NOT EXCEED 5 PER CENT AND THE TIRE SHALL NOT REVUU. ANY APPEARANCE AND PERFORHANCE DEFECTS SUCH AS SIDEWLLL BLISTERS, TREAD SEPARATION, ETC. QLIALIFICATION TEST REPORT - THE QUALIFICATION TEST REPORT SHALL LIST RIE RESULTS OF ALL QUALIFICATION TESTS AND RIE COiYSTRUC- TIOA DFXAILS OF THE

12、 QUALIFICATION TEST SAHPLE IN THE GENERAL FOIIH SHOWN IN FIGURE 2 OF SPECIFICATION MIL-T-5041 WITH DIHFNSIONS LISTED AT RATED INFLATION. INFLATED TO 280 PSI FOR THE 26 PR OR 320 PSI FOR THE 28 PR. IWO (2) COPIES OF THE QUALIFICATION TEST REPORT, TOGETHE: HIni THE MTA AND SPECIFIED ABOVE AND IN MIL-T

13、-5041. ?JiALL BE SUBMITTED TO THE NAVAL AIR SYSTEMS CWD. WSHINGTCN. DC 20361, ATTENTION: AIR 53032. NOTES: IN ADDITION, IT SHALL ALSO LIST THE ACTUAL TIRE DIHWSIONS WHEN THE TIRE IS 1. 2. REFERENCED DOCUHWTS SHALL BE OF THE ISSUE IN EFFECT ON DATE OF INVITATIONS FOR BIDS, OR WUEST FOR PROPOSAL EXCEP

14、T THAT REFERKNCE ADOPTED INDUSTRY STANDARDS SUL GIVE THE MTE OF THE ISSUE ADOPTED. FOR DESIGN FPATURE PURPOSES, niIS STANDh TAKES PRECEDENCE OVER PROCURHENT WCUHFNTC REFERENCED HEREIN. C EiJTESCWNES ., NAVY-AS TITLE 1 MILITAIY STAWDAI hhrcn, TIRE, PNEUHATIC, AIRCRAFT, 40x14, (200 WH), TYPE VI1 (NAVY) Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-