- 4 0 Ref Sharp 5 16 24 Unf 3a Thread 375 Dia 125 Deep 1 Required 45 To The Left From Top 680 670 510 490 368 3 1 (447.44 KiB) Viewed 22 times
aerial vehicle. The design department is in the material selection
stage and since it is a piece that is subjected to high tensile
stresses, the use of a ferrous alloy is required. Due to its
availability and low cost, steel was selected as the base material,
but the design and manufacturing department is in the process of
selecting the type of steel that has the highest efficiency.
From the following table of properties, select the steel that
meets the requirements of the mentioned application.
- 4 0 Ref Sharp 5 16 24 Unf 3a Thread 375 Dia 125 Deep 1 Required 45 To The Left From Top 680 670 510 490 368 3 2 (6.57 KiB) Viewed 22 times
C)
4.0 REF SHARP 5/16-24 UNF-3A THREAD .375 DIA .125 DEEP-1 REQUIRED (45° TO THE LEFT FROM TOP) .680 .670 .510 .490 .368 .367 .255 .245 32 .250 .187 DIA THRU 1 REQUIRED .031 x 45° CHAMFER NOM SIZE - . 125/LC-2 THRU-1 REQUIRED 6a \ .438 .437 .81 R 32 I NOM SIZE .375 D/RC-5 .438 5b .312 REF 1.440 1.437 DIA .68 R .437 11 1 132 32 63 45 .125 .625 .620 NOM SIZE .562 DIA RC-5 4b .406 DIA 1.125 DEEP 1 REQUIRED WITH .062 DP x 45° CHAMFER 1.260 1.240 .250 245 3.315 3.312 .380 .370
bon Steel 1008 1018 1045 4140 6150 8740 Tensile Strength (Psi) Yield Strength (Psi) Elongation (%) Area reduction (%) 44,000 24,500 30 55 58,000 32,000 25 50 82,000 45,000 16 40 95,000 61,000 26 32 96,000 59,000 23 30 95,000 60,000 25 20