1、r. K4TRfi MS33600 27 7777712 0008877 5 - FED. SUP Ciy4S.S. F TAP, NC 2B, b HOLES. SHALL FIT A HATING PART HAVING A PUT DIA W AND b PINS, FACH WITHIN AN AREA HAVING X DIA CENTALLY MCATFD ON ITS BASC POSITION. SURFACE SHALL BE FLAT AND SQUARE WIDI AXIS OF ROZ#TION KIMIN .o02 TIR PER INCH OF DIAMETER,F
2、LANGE AND SHAFT RELATIVELY ROTATING COHPOSITE ERROR, lWTH IO 10OTH AND TOTAL WITH REFERENCE 10 AXIS OF ROTATION, FLANGE AND SHAFT RELATIVELY ROTATING MIN LENGTH OF FULL DEPTH OF TOOTH SPLINE-PINION DATA N = NMBER OF TEETH P = DIAMEIRAL PIWH 20. PRESSWE ANGLE ROCKWELL C OR EQUIVALENT WNESS: SURFACE b
3、5 MIN, 55 MAX HOB RUNOUT OR WER UNDERCUT y SCREdS ENTITEXTNG PILOT E DIAMETER TO BE CONCENTRIC WITH AXIS OF ROTATION WIT“ .o01 FOR WINDING WPES 1 AND 2, .o015 FOR TYPES 3 AND b, .O02 FOR WPES 5 AND 6 AND .o03 FOR BETOND mS DEPTH MAY DAMAGE HOTOR WPFS 7 AND 8 TIR, FLANGE AND SHAFT RELATIVELY ROTATING
4、 TOOTH FORM OUTSIDE THIS DIAMETW SHALL B5 IRUE INVOLUTE SPLINE-PINION DEMIL (a) A IS GREATEST DIAMETER OR DMENSION OF ACCESORY nXCLUSIVE OF A.fTACHED DEVICES. (b) OUTSIDE DIAHETERS OF SMALL PINIONS ARE ENLARGED TO AVOID UNDERCUT. To MAINTAIN STANDARD CENTER DISTANCE, THE GEAR DIAHETERS MUST BE DECRE
5、ASED BY WE AMOUNT OF ME PINION ENLARGEMEW GIm AT Q. WITH STANDARD TOOTH PROPORTIONS, THE CENTER DISTANCES MUST BE INCREASED APPROXIMATELY 1/2 Q. IF MATING GEARS ARE MADE (c) R HAX HAS ESEN REDUCED FROM THEORETICAL BY IOTAL CMPOSITE WROR OF PINION ONLY. (d) OTHZR HASTER GEARS HAY BE USK IF CMTER DIST
6、ANCE IS PROPERLY RECALCULAED. (e) RANGE OF c6NTEFI DISTANCE IS THAT RESULTIETG FRCM RMS SUHMATJON OF ALL VARIABLES IN “E STRUCTJRE. SIZE DETERMINATION OF MATING GEAR MUST RECOGNIZE FURTHER VARIATIONS IN ITS SUPPORTING STRUCTURE. SPLIM-PINION DIMENSIONS ARE BASIC MAXIHUM. PINION DMEKSIOILS ARE ILDEQU
7、ATE FOR TPPE SHOWN BUT ALL PINIOAS SW BE CHECKED FOR APPLICATION. RWOVE ALL BURRS AND SHARP EDGES. DMDSIONS IN INCHES. NOIIINAL USE OF THIS MTVE FOR AC OR DC ELECTRICAL MOMRS. RANGE RESULTS FROH SIZE VARIABLE ONLY. UNLESS OiEiKISE SPECIFIED, MLKRANCES: DECIMALS i.010, ANGLES t2 THIS IS A DESIGN STAN
8、DARD. NOT To BE USED AS A PART NWEEX. THIS DOCUIIENT HAS BEB4 PROMJLMTED BY THE DEPARI?4ENT OF DEFENSE AS THE MILITARY STANDARD TO LIHIT THE SELECTION OF THE ITM, RODUCT, OR DEIGN COVEXFD HEREIN IN ENGINEEXING, DLSIGN, AND PROCURWENT. THIS STANDARD SHALL BECOME EFFECTIVE NOT LATEX WAN 90 YYS AFTEX T
9、HE LATECT DATE OF AWROVAL SH(NIN. USTOIAIIS OTHER IHT. xavy - BuAer A- Ur Force k: - MS33600 M Il ITARY STAN DA RD (ASG) . DRIVE, MINIATURE, POWER MOTOR WITB AF- INVOLUTE SPLINE - PINION SHEET 1 OF Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MS33
10、600 27 = 9999912 0008878 7 W USTODIAW &vy - BuAer rir Force c -s.- - MS33600 MIL IT ARY ST AN DA RD OTHER IHT. A - li- M- DRIVE, MINIATURE, P(klER MOTOR WITH INVOLUTE SPLINE - PINION FED. CUP CLASS, .I LOQIRWIT S#CiFlCATla( THIS IS A DESIGN STANDARD. NOT To BE USED AS A PART NUMBER. (ASG) SUPERSEDES
11、 SHEET 2 OF II a !? i1 O i! 4 a 3 L C - Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MS33600 29 m 9999932 0008879 9 m I. I FED. sup LAss. L UM OF SCREII LENGTH -Ci DATA FOR EASIC DRIVE hITH ROUN PLATE ATTACHMENT C H K L HAXIMUM SEE SHEET 2 MR CIM
12、ENSIONS NOT SHOXN. THIS IS A DESIGN STANDARD, NOT TO BE USD AS A PART NUMBER. ?HIS DOCUHENT HAS BEEH PROXTLGATD BY THE DEPARIMENT OF DEFENSE AS WE MILITARY STANDARD To LIMZT THE SELECTION OF WE ITMI PRODUCT, OR DEIGR COVERED HEREIN IN ENGINEWING. DESIGN, AND PROCUREMENT. THIS STANDARD SHALL BECOME E
13、FFECTIVE NOT LATER MAN 90 8% 7 E i i MYS AF!3 THE LATEST DATE OF AFROVAL SH&?i. CUSTOOIAHS OTHER IHT. Navy - BuAer A- Air Force l - . MIL IT ARY ST AN DA RD MS33600 (ASG) DRIVE, HINNIATURE, PoWfI HOTOB WITH INVOLUTE SPLINE - PINION pRocuR”T SPECIFICATIOW SUPERSEDES: SHEET 3 of. Ii -Y MI# 672-1 I 15!
14、2 g.5 : AF- Sag. 1 NONE - PROBLEM HARD COPY (-J 1 n E W W 0: W ln 2 r rl O W w O 0: n n - Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-c FED, SUP CdASS. I A PILOT DIA U AND li STUDS EACH WI?“ AN ARE4 HAVNG X DIA CENTRALLY MCATED ON ITS BASIC POSIT
15、ION DATA FOR BASIC DRIVE WITH SQUARE PLATE ATACtiMEtiT 28 I I 20 12.271 12.031 12.000 1 .a03 I I SEE SKEET 2 FOR DIHENSIONS NOT SHOdN. THIS IS A DESIGN STANDARD, NOT TO BE USED A8 A PART NUMBER. lKIS DOCUHNT HAS BEDI PROdTJLG4TK BY THE DEPARTMmT OF DEFENSE AS WE MILITARY STANDARD TO LIMIT THE SEECTI
16、ON OF ?HE ITM, PRODUCT, CA DESIGN COVERLH) HEREIN IN ENGJNEWING, DESIGN, AND PROCUREMENT. THIS STANDARD SHALL BECOME EFFECTIVE NOT LATW WAN 90 DAYS AITEX THE LATEST DATE OF APPROVAL SHM. MS33600 MILITARY ST AN DA RD CUSTODIANS OTHER IHT. Navy - BuAer A- Air Force li - (ASG) DRIVE, MINIATURE, P(x.IER MOMR WITH INVOLUTE SPLINE - PINION AF- WT SPECIFICATIOW SUPERSEDES: SHEET b OF ll I L _. NONE I I dom 672-1 1 aTa2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
