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Refer to the 1.914 dimension. A) Where is the tolerance specified ? _________________________________ B) What is its tolerance ? ________________________________ C) What is the MMC? ______________________________ D) What is the LMC? _______________________________

Refer to the 1.914 dimension. A) Where is the tolerance specified ? _________________________________ B) What is its tolerance ? ________________________________ C) What is the MMC? ______________________________ D) What is the LMC? _______________________________

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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Refer to the 1.914 dimension.


A) Where is the tolerance specified ? _________________________________ B) What is its tolerance ? ________________________________
C) What is the MMC? ______________________________

D) What is the LMC? _______________________________

 

REVISIONS DESCRIPTION -PROPRIETARY- THIS DOCUMENT AND DATA DISCLOSED HEREIN OR HEREWITH IS NOT TO BE REPRODUCED, USED, OR DISCLOSED IN WHOLE OR IN PART TO ANYONE WITHOUT THE PERMISSION OF FLIR SYSTEMS INC. ZONE LTR DATE APPROVED NOTES: 1. INTERPRET DRAWING IAW MIL-STD-100. 2. INTERPRET DIMENSIONS AND TOLERANCES PER ASME Y14.5-2009. 3. PART TO BE FREE OF BURRS AND SHARP EDGES. O.001 VACUUM BAKE (10-4 TO 10 TORR). TEMP RISE 300 C/10 MIN TO 900 C. HOLD FOR 15 MIN AT 900 C. COOL TO 500 C IN 10 MIN, 500 C TO 100 C IN 30 MIN, REMOVE AND AIR COOL TO ROOM TEMP (20 C). 2.125 A .001 A /5 THREAD RELIEF .10 LONG MAX. 2.059 6. IDENTIFY IAW MIL-STD-130 BY BAG AND TAG INCLUDE LATEST REV LEVEL. 1.914- /A ELECTROLESS NICKEL PLATE PER MIL-C-26074, CL 2 (.0001/.0002 THK). .867 8. DIMENSIONS TO APPLY AFTER FINISH. 9 GOLD PLATE INDICATED SURFACE PER MIL-G-45204, TYPE_ I, GRADE A, CLASS OPTIONAL, THICKNESS TO BE LESS THAN .0005 PER SURFACE. 696 2X 45° X .010 - 45° X .015 ø1.274 ø.674 Ø.750 /9 +ø.028© AB E.010 B +ø.0280 AB |+ 0.014@ A| Ø.8740±.0005 I0.001 A .875-40 UNS-2A R.005 MAX - Ø.107±.001 THRU Uø.218 TO FULL DIAMETER FAR SIDE ONLY ø.028@ A B PROJECT: UNLESS OTHERWISE SPECIFIED DIMENSIONS ARE IN INCHES ALL DIMENSIONS IN [] ARE MM DRAWN DO NOT SCALE DRAWING FLIR FLIR Systems Inc. 16505 sw 72nd Ave Portland Or 97224 PROJECT FRACTIONS + 1/32 DECIMALS XX 1.015 STRAIGHTNESS &/OR FLATNESS: .005/IN DATE TITLE G00'F XXX THREADS: SLEEVE DEWAR CHECK HOLE ±.005 EXTERNAL-CLASS 2A INTERNAL-CLASS 28 ANGLES,BENDS,& INTERSECTIONS:90 PERPEND. I .003/IN MACHINED SURFACES: Y OR BETTER SAMPLES MUST BE APPROVED BY ENG. XX MATERIAL REIMAGING -.001 C00+ XXX DESIGN KOVAR ANGLES O'30' BENDS FINISH ENGR DWG. NO. REV CONCEN. O.003/IN 64869 APPR PRIOR TO STARTING PRODUCTION CALC. WT. SCALE 2:1 PRINTED: SHEET 1 OF
Transcribed Image Text:REVISIONS DESCRIPTION -PROPRIETARY- THIS DOCUMENT AND DATA DISCLOSED HEREIN OR HEREWITH IS NOT TO BE REPRODUCED, USED, OR DISCLOSED IN WHOLE OR IN PART TO ANYONE WITHOUT THE PERMISSION OF FLIR SYSTEMS INC. ZONE LTR DATE APPROVED NOTES: 1. INTERPRET DRAWING IAW MIL-STD-100. 2. INTERPRET DIMENSIONS AND TOLERANCES PER ASME Y14.5-2009. 3. PART TO BE FREE OF BURRS AND SHARP EDGES. O.001 VACUUM BAKE (10-4 TO 10 TORR). TEMP RISE 300 C/10 MIN TO 900 C. HOLD FOR 15 MIN AT 900 C. COOL TO 500 C IN 10 MIN, 500 C TO 100 C IN 30 MIN, REMOVE AND AIR COOL TO ROOM TEMP (20 C). 2.125 A .001 A /5 THREAD RELIEF .10 LONG MAX. 2.059 6. IDENTIFY IAW MIL-STD-130 BY BAG AND TAG INCLUDE LATEST REV LEVEL. 1.914- /A ELECTROLESS NICKEL PLATE PER MIL-C-26074, CL 2 (.0001/.0002 THK). .867 8. DIMENSIONS TO APPLY AFTER FINISH. 9 GOLD PLATE INDICATED SURFACE PER MIL-G-45204, TYPE_ I, GRADE A, CLASS OPTIONAL, THICKNESS TO BE LESS THAN .0005 PER SURFACE. 696 2X 45° X .010 - 45° X .015 ø1.274 ø.674 Ø.750 /9 +ø.028© AB E.010 B +ø.0280 AB |+ 0.014@ A| Ø.8740±.0005 I0.001 A .875-40 UNS-2A R.005 MAX - Ø.107±.001 THRU Uø.218 TO FULL DIAMETER FAR SIDE ONLY ø.028@ A B PROJECT: UNLESS OTHERWISE SPECIFIED DIMENSIONS ARE IN INCHES ALL DIMENSIONS IN [] ARE MM DRAWN DO NOT SCALE DRAWING FLIR FLIR Systems Inc. 16505 sw 72nd Ave Portland Or 97224 PROJECT FRACTIONS + 1/32 DECIMALS XX 1.015 STRAIGHTNESS &/OR FLATNESS: .005/IN DATE TITLE G00'F XXX THREADS: SLEEVE DEWAR CHECK HOLE ±.005 EXTERNAL-CLASS 2A INTERNAL-CLASS 28 ANGLES,BENDS,& INTERSECTIONS:90 PERPEND. I .003/IN MACHINED SURFACES: Y OR BETTER SAMPLES MUST BE APPROVED BY ENG. XX MATERIAL REIMAGING -.001 C00+ XXX DESIGN KOVAR ANGLES O'30' BENDS FINISH ENGR DWG. NO. REV CONCEN. O.003/IN 64869 APPR PRIOR TO STARTING PRODUCTION CALC. WT. SCALE 2:1 PRINTED: SHEET 1 OF
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