The figure shows a connection that employs three SAE grade 4 bolts. The tensile shear load on the joint is 4000 lbf. The members are bars of AISI 1020 HR steel. Assume the bolt threads do not extend into the joint. Find the factor of safety for each possible mode of failure. (Refer example problem 8.6 on pg. 445). in 1 in ← 12/in -1-in- -2 in in-20 UNC in .5
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- (11) The figure shows a connection that employs three SAE grade 5 bolts. The tensile shear load on the joint is 5400 lbf. The members are cold-drawn bars of AISI 1020 steel. Find the factor of safety for each possible mode of failure. (Ans./ 3.26, 5.99, 3.71, 5.36) in- 글im 16 UNC in I in -24 in-Agui - 4550/2 =2276 two plates each with thickness t - 16 mm are bolted together with 6-222 mndia. bolts firming alap Joint Bolt spacing are follows St- $40mm S2 - 80mm, S3=150mm effective bolt hole dia. is 25mm A36 is used. Compute the allowable tensile Strength P t = 16 mm &t 52 747₁ 0 O O 40 60 80 40 +=16mm S-400 $3-100 S2-40 7 @ 4umm PTwo plates are clamped by a 3/4-10 UNC SAE Grade 5 bolt and regular nut with a 3/4-W plain washer as shown in figure. Top plate is made of grey cast iron and bottom plate is steel. An axial force of 12kN is acted upon the joint. Round off the length of the bolt to nearest 1/4in. Assume bolts are preloaded to 75% of proof load. 1. Determine the bolt stiffness kb. 2. Determine the member stiffness km. 3. Determine the yielding factor of safety of the bolt. 4. Determine the load factor for the bolt. 5. Determine the load factor guarding against joint separation. 1.25 in 1.00 in
- An M 14 x 2 hex-head bolt with a nut and a 14R washer under each of bolt head and the nut is used to clamp together two 18-mm steel plates. NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. Determine the bolt stiffness. The bolt stiffness kb is 592.69 MN/m.The section of sealed joint shown in figure below is loaded by a force cycling between 2 and 6 kips. The member have E = 30 Mpsi. The bolts have been preloaded to F; =35 kip each. ž in-16 UNF x 24 in SAE grade 5 No. 40 CI (a) Find the fatigue factor of safety using Goodman criterion for above loading. (b) Find the fatigue factor of safety using Goodman criterion if force cycling between 0 and 6 kips.Required information The bolted connection shown in the figure is subjected to a tensile shear load of 90 kN. The bolts are ISO class 5.8, and the material is cold-drawn AISI 1015 steel. Assume the bolt threads do not extend into the joint. Find the factor of safety of the connection for all possible modes of failure. Give the overall joint factor of safety. Given: t = 15 mm and t2 = 25 mm. NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. 35 60 60 - 35 t1 M20 x 2.5 35 35 + t2 Find the overall joint factor of safety. The overall joint factor of safety noverall is
- 8-68 Engineering Design + 40 1 plem 8-68 70 millimeters. 40 A bolted lap joint using ISO class 5.8 bolts and members made of cold-drawn SAE 1040 steel is shown in the figure. Assume the bolt threads do not extend into the joint. Find the tensile shear load F that can be applied to this connection to provide a minimum factor of safety of 2.5 for the fol- lowing failure modes: shear of bolts, bearing on bolts, bearing on members, and tension of members. 20 M20x2.5 20A M20 × C4 bolt of mild steel is having yield stress of 320 MPa and factor of safety 3. The safe static tensile load in kN will beAn M30 x 3.5 ISO 8.8 bolt is used in a joint at recommended preload, and the joint is subject to a tensile load of P = 65 kN per bolt. The joint constant is C= 0.28. Find the static load factor of safety against yielding.
- 3. An M16 x 2 bolt with a slotted hex nut is used to clamp together two 25 mm steel plates. The joint is assembled with a size 16 N washer underneath the bolt head. The bolt is a 5.8 class metric grade, with a proof strength of 380 MPa. The joint is intended to be permanent. Determine a suitable length for the bolt, rounded up to the nearest standard size in millimeters. Calculate the bolt stiffness, the elongation of the bolt after the necessary preload is developed, and the bolt torque required to apply the preload. Assume that coefficients of friction between the bolt, nut, and collar are all ~0.15. For steel, use E = 207 GPa. Standard threaded fastener lengths, dimensions of hexagonal nuts, and dimensions of metric plain washers are provided in the textbook appendices.4. Determine the design stress for bolts in a cylinder cover where the load is fluctuating due to gas pressure. The maximum load on the bolt is 50 kN and the minimum is 30 kN. The load is unpredict- able and factor of safety is 3. The surface of the bolt is hot rolled and the suface finish factor is 0.9. During a simple tension test and rotating beam test on ductile materials (40 C 8 steel annealed), the following results were obtained : Diameter of specimen =12.5 mm; Yield strength= 240 MPa; Ultimate strength= 450 MPa; Endurance limit = 180 MPa. [Ans. 65.4 MPa](8) The bolted connection shown in the figure uses SAE grade 5 bolts. The members are hot-rolled AISI 1018 steel. A tensile shear load F = 4000 lbf is applied to the connection. Find the factor of safety for all possible modes of failure. (Ans/2.93, 4.32, 1.5, 3.25) in in-16 UNC ț in in