NAVY MS14186 REV B-1990 TIRE PNEUMATIC AIRCRAFT REBUILT 36 X 11《36 X 11飞机整修汽轮胎》.pdf

1、FORM APPROVED OMB NO. 0704-0188 THE TIRE SHALL BE IN ACCORDANCE WITH THE APPLICABLE REQUIREMENTS OF MIL-R-7726 EXCEPT AS SPECIFIED HEREIN. STATIC INFL BEAD STATIC SIZE PLY LOAD PRESS. WIDTH WEIGHT UNBAL. TREAD RDLD OEFLEC RATING RATING PSI INCH PWNDS DEIN. SKI0 +32 LBS. RATEO MAX. MAX. MAX. DEPTH -4

2、2 36 X 11 24 TL i/ 26.500 235 2.80 97.0 15 RIB z/ 0.36 325 N.O1 METRIC: 914.4 X 279.4 (WO 1/ TL - TUBELESS TIRE z/ Ki LEAST FOUR, BUT NOT MRE THAN SEVEN CONTINUOUS CIRCUMFEREHTIAL RIBS. HAVE THO FABRIC REIHFORCEHENT PLIES. THE TREAD SHALL TIRE DATA (INCH) (STATIC TEST TIRE) I INFLATED OUTSIDE INFLAT

3、ED SECTIOH INFLATED SHOULDER INFLATED SHOULDER DIAMETER WIDTH DIAMETER WIDTH MIN. MAX. MIN. MAX. MAX , MAX. 34.00 35.67 10.80 11.85 32.12 10.40 RIM DATA (INCH) WIDTH FLANGE LEDGE LEDGE FLANGE HEEL FLANGE FLANGE BETWEEN WIDTH DIAMETER WIDTH HEIGHT RADIUS RADIUS EDGE FLANGES 9.00 0.938 16.00 2.130 1.3

4、75 0.250 0.688 .125 THE TIRE COVERED BY THIS DRAWING SHALL BE SUITABLE FOR USE AND PROVIDE REASONABLE SERVICE LIFE WRING ALL NOML OPERATIONS AT TAKEOFF AND LANDING SPEEDS INDICATED HEREIN ON ALL TYPES OF RUNWAYS AND ON AIRCRAFT CARRIERS. THREE TIRES SHALL BE SUWITTED BY THE CONTRACTOR. PROCESSING TE

5、CHNIQUES. TIRES SHALL BE EXIVIINED AS SPECIFIED BELOW: bIMITS. THE TIRES SHALL BE REBUILT USING THE SAME CWOUNDS AND TEST INFLATION PRESSURE THE TEST INFLATION PRESSURE FOR DYNAMIC TESTS SHALL BE ADJUSTED TO ENSURE TIRE DENOTES CHANGES PREPARING ACTIVITY: NAW - AS CUSTODIANS ARMY - NAVY - AIR FORCE

6、- DIA - MILITARY SPECIFICATION SHEET TITLE SUPERSEOING AMSC - N/A FSC 2620 REVIEW TIRE, PNEWTIC, AIRCW, REBUILT, 36 X 11 MS1486A(AS) 23 AUG 85 USER: PROJECT NUMBER: 2620-1262 -. DISTRIBUTION STATEMENT - A. APPROVED FOR PUBLIC RELEASP DISTRIBUTION IS UNUMITED. DD 12 672 Provided by IHSNot for ResaleN

7、o reproduction or networking permitted without license from IHS-,-,-TIRE 1: FORM APPROVED I OMB NO. 0704-Olt OIMENSIONS - THE TIRE SHALL BE INFLATED TO 235 PSI ANO ALLOWED TO STAND FOR 4 HOURS MINIMUM AT ROOM TEMPERATURE AFTER WHICH TIME THE PRESSURE DUE TO GROWTH SHALL BE REPLACED. TIRE DIMENSIONS

8、AT 350 PSI SHALL BE WITHIN THE DIMENSIONAL LIMITS SPECIFIED ABOVE. WITHOUT FAILURE OR VISIBLE DETERIORATION OTHER THAN NORMAL EXPECTED TREAD WEAR. THE REBUILT DYNAMIC TEST THE TIRE SHALL WITHSTAND 50 CYCLES OF TEST A, 44 CYCLES OF TEST B AND 1 CYCLE OF TEST C DYNAMIC TESTS: TEST A - TAXI - TAKEOFF -

9、 THE TIRE SHALL BE TAXIED OH THE FLYWHEEL AT 30 MPH FOR 10.000 FEET WITH POUNDS AT THE TIME THE TIRE-IS UNLANDED;- TEST B - LANDING - TAXI - THE TIRE SHALL BE LANDED AGAINST A FLYWHEEL ROTATIHG AT A PERIPHERAL SPEED OF LYWHEEL SPEED SHALL THEN BE DECREASED UNTIL A ROLL DISTANCE OF APPROXIMATELY 3,70

10、0 130 MPH. ANO 10.63 FEET/SEC/SEC BETWEEN 130 AND O MPH. THE LANDING ROLL DISTANCE OF 3.700 FEET . . _._ SHALL Bi CVERD IN- PPRXMTLY-B-SCDS.THE INITIAL TIRE LOAD SHALL BE 21 .o00 POUNDS. DECREASED LINEARLY TO 20,500 POUNDS IN 2,000 FEET. THE LOAD SHALL THEN BE DECREASED TO i9,oo AT 2,000 FEET AND DE

11、CREASED LINEARLY TO 17,000 POUNDS AFTER AN ADDITIONAL 1,700 FEET. FOLLOWING THE LANDING, THE TIRE SHALL BE TAXIED ON THE FLYWHEEL FOR 10,000 FEET AT 30 MPH WITH 21,000 POUND LOAD. IMMEDIATELY AT AN AVERAGE UTE OF 5.34 FT/SEC/SEC FROM 201 HPH TO 150 MPH. AND 6.11 FT/SEC/SEC FROM 150 MPH TO O MPH. THE

12、 INITIAL LOAD OF 26.500 POUNDS SHALL BE DECREASED LINEARLY TO 10.000 POUNDS IN 47 TO 48 SECONDS, INCREASED TO 30,500-PUNOS IN 14 SECONDS (61 TO 62 SECONDS FROM START). THEN DECREASE0 TO 26,500 POUNDS IN 36 SECONDS (97 TO 98 SECONDS FROM START). THE TOTAL ROLL DISTANCE OF 14,000 FEET SHALL BE COVERED

13、 IN APPROXIMATELY 97 TO 98 SECONDS. TIRE SHALL BE TAXIED ON THE FLYWHEEL AT 30 MPH FOR 10.000 FEET AT 26,500 POUND LOAD. IWEDIATELY FOLLOWING THE ABOVE CYCLE, THE TIRES 2 AND 3: TIRES 2 AND 3 SHALL NOT BE SUBJECTED TO CONTRACTOR TESTING; HOWEVER, A HALF SECTION OF TIRE 2 ANO THE COMPLETE TIRE 3. ALO

14、HG WITH A REPRESENTIVE HALF SECTION OF TIRE 1 AFTER DYNAMIC TESTS SHALL BE SUBMITTED TO THE COGNIZANT GOVERNMEHT LABORATORY AS SPECIFIED IN MS3377. -! NOTE: II 1. IN THE EVENT OF A CONFLICT BETWEEN THE TEXT OF THIS STANDARD AND THE REFERENCES CITED HEREIN, THE TEXT OF THIS STANDARD SHALL TAKE PRECED

15、ENCE. 2. REFERENCED GOVERNMENT (OR NOW-GOVERNMENT) DOCUMENTS OF THE ISSUE LISTED IN THAT ISSUE OF THE DEPARTMENT OF DEFENSE INDEX OF SPECIFICATIONS AND STANDARDS (OoDISS) SPECIFIED IN THE SOLICITATION FORM A PART OF THIS STANDARD TO THE EXTENT SPECIFIED HEREIN. 3. ALL TIRES MANUFACTURED PRIOR TO 198

16、4 SHALL NOT BE REBUILT EXCEPT GOODYEAR QTR 461B-2205-TL TIRES. !CARING ACTIVITY: NAVY -AS SPECIFICATION SHEET NUMBER 18 JuI, 30 MIL,-ARY SPECIFICATION SHEET ISTODIANS: ARMY - NAVY - TITLE - MS14186B(AS) SUPERSEDING AIR FORCE - DLA - TIRE, PNEUHATIC. AIRCRAFT, REBUILT, 36 x 11 MS14186A(AS) 23 AUG 85 VIEW: #ER: OJECT NUMBER: 2620-8262 CTRIBUTION STATEMENT AMSC - N/A FSC 2620 A. APPROVED FOR PUBLIC RELEASE DISTRIBUTION IS UNLIMITED. PAGE 7 OF 3 - DD iEm 672 PRMOUS EDITIONS OF THIS FORM ARE OBSOLETE Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-