MS90708D
(h) LOAD CAPACITY, WITH THE RETAINED PART RADIUSED OR CHAMFERED:
WHEN THE RADIUS OR CHAMFER OF THE RETAINED PART DOES NOT EXCEED THE MAXIMUM RADIUS ALLOWED FOR THE BOTTOM OF THE RING GROOVE, THE LESSER LOAD CAPACITY COMPUTED FROM THE FORMULAS ON PAGE 4 WILL APPLY. THE CORNER RADII AND CHAMFERS LISTED ON PAGE 2
WERE CHOSEN AS LARGE AS POSSIBLE FOR THE RING SIZES INVOLVED AND ARE RELATED TO THE MAXIMUM THRUST LOADS LISTED IN TABLE VI.
IF THE CORNER RADII OR CHAMFERS ARE SMALLER THAN THOSE LISTED, THEN THE THRUST LOADS INCREASE PROPORTIONALLY IN ACCORDANCE WITH THE FOLLOWING FORMULAS:
1 1
P = PCH OR P
= NEW ALLOWABLE THRUST LOAD.
CH1 P = LISTED ALLOWABLE THRUST LOAD.
1
WHERE: CH
= NEW (SMALLER) CHAMFER.
CH = LISTED CHAMFER.
1 1
P = PR R
1
= NEW (SMALLER) CORNER RADIUS.
R R = LISTED CORNER RADIUS.
LIMIT LOADS LISTED BELOW ARE BASED ON RINGS OF STEEL (WORKING STRESS = 250,000 P.S.I.) AND OF BERYLLIUM COPPER (WORKING STRESS = 180,000 P.S.I.). IF THE ALLOWABLE GROOVE CAPACITY LOADS AS CALCULATED BY USING THE FORMULA GIVEN ABOVE ARE LESS, THEN THEY SHOULD BE USED.
.
TABLE VI. LIMIT LOADS.
NOMINAL RING SIZE |
ALLOWABLE THRUST LOAD FOR RING ASSEMBLIES WITH PARTS HAVING MAXIMUM CORNER RADII OR CHAMFERS |
||
FROM |
TO |
CARBON STEEL OR CORROSION RESISTANT STEEL |
BERYLLIUM COPPER |
.496 .669 .984 1.562 1.969 2.750 3.375 |
.625 .875 1.500 1.875 2.625 3.250 -- |
610 LB 880 LB 1250 LB 1900 LB 3050 LB 4300 LB 5950 LB |
440 LB 630 LB 900 LB 1370 LB -- -- -- |
5. CHANGES FROM PREVIOUS ISSUE. MARGINAL NOTATIONS ARE NOT USED IN THIS REVISION TO IDENTIFY CHANGES WITH RESPECT TO THE PREVIOUS ISSUE DUE TO THE EXTENT OF THE CHANGES.
MILITARY INTEREST
Custodians: Preparing activity: Army - AR DLA - IS
Navy - AS
Air Force - 99 (Project 5325-2012-018)
Review activities:
Army - AT, AV, CR, CR4
Navy - MC, SH, YD Air Force - 71
NOTE: The activities listed above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information above using the
ASSIST Online database at https://assist.dla.mil.
8
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