Answer for the Original Poster...
I took the case from this - you will see what I've taken as your situation fromteh numbers I settle on.
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I note Ray Hayes' explanation, where he looks to have used the same methodology Ray Hayes posted on February 23, 2018, 2:31 pm # replying to mjacobsen925, Ray Hayes wrote: Your reply is # foolish. This appears to be a valid question about using a pipe # section to support a hoist - an overhead lifting design that # requires calculation. 1.5" black iron pipe is the support beam # suggested for available electric garage hoists.
# For any who care, stress = M*c/I = M/s. Bending moment = M = WL/2, s # = 0.326 in^3 for 1.5" sch 40 pipe. Assume yield strength0,000 # psi. L`". stress = M/s = W*L/(2*s). If Safety Factor = 2.0 (low for # a lifting operation - F.S> should be 6 for overhead lifting): # Yield/F.S = 30000 psi/2.0 = 15000 psi = W*60/(2*0.326); W = 163 # lbs. Yield Strength (30,000 psi) is the load where the pipe will # bend without springing back to straight. Original request was for a # 1" deflection at the center. This is way overloaded - typical beam # limit might be L/360 = 0.167". But just for yucks: max deflection = # y = W*L^3/(48*E*I); E)e6, I = 0.310 in^4 (1.5" sch 40 pipe). y/W = # 60^3/(48*29e6&*0.310) = 0.0005, or W/y = 2000, or W = 2000*y. So to # get a 1.0" deflection on a 60" pipe (if it did not yield) would be W # 00 * 1.0 = 2000 lbs. *BUT the stress with that 2000# load would be # M/s = W*L/(2*s) 2000*60/(2*.326) = 184,000 psi - 6 times the yield # strength (meaning the pipe would bend to failure). *For reference, # limiting deflection to L/360 would allow a load of: W = 2000*y = # 2000*(60/360) = 333 lbs. This corresponds to a F.S. = about 1.0.
Dimensions for 1~1/2" Sched 40 tube Nom OD ID w-thk
1.5 1.900 1.61 0.15
(* 1.9 25.4) ;; 48.26 (* 0.15 25.4) ;; 3.8099999999999996
If I'm not mistaken, that's the dimensions of scaffold tube as we know it here in the UK.
I can tell you - a 6m length (- (/ 6e3 25.4) (* 12 19)) ;; 8.220472440944889
19ft 8in length !!! of scaffold tube supported on its ends will just take my weight in the middle - about 87kg (/ 87 0.4536) ;; 191.7989417989418
192lb
I'm going to use a yield strength of 235MPa There is every likelihood the yield is higher than that. So the value I'll calculate is the minimum load-bearing possible.
The Young's modulus at 2.1e11Pa is almost independent of steel strength, so the deflection prediction is invariant of steel grade.
Using my functions ;; moment cap (* 235e6 (beam-sect-mod-z-d ;; args I, d (ma2nd-annulus-dia-wthk-cx 48.3e-3 3.8e-3) ; 1.3245821667837055e-07 ; m^4 48.3e-3) ; 5.484812284818656e-06 ; m^3 ) ; 1288.9308869323843 ; N.m
So moment capacity is 1289 Newton-metres
(* 60 25.4 1e-3) ;; 1.524 ;; m length
(/ (simple-support-dblbeam-loadcap ;; M_cap, l 1288.9308869323843 1.524) ;; 3383.0207006099326 ;; N (Newtons) 9.81) ; 344.8543017951001 ; kg-f
(/ 345 0.4536) ;; 760.5820105820105 So your curtain rail will bear 760lb at the middle That's more than enough for a kid swinging on it.
Deflection - which is your question...
(dblsupport-centralload-beam-deflect ;; F(central), l, E, I (* 344.8543017951001 9.8) ;; 3379.5721575919815 ;; N 1.524 ;; m length of curtain rail 2e11 ;; Elastic modulus of steel (Pa) (ma2nd-annulus-dia-wthk-cx 48.3e-3 3.8e-3) ;; 1.3245821667837055e-07 ;; m^4 ma-2nd ) ;; 0.00940733235828569 ;; m of deflection at onset of deformation
(/ (* 0.00940733235828569 1e3) ;; 9.40733235828569 ;; mm deflection
25.4) ;; 0.370367415680539
(* 0.370367415680539 8) ;; 2.962939325444312 ;; about 3/8th-inch
Even at maximum loading of 345kg / 760lb the middle of the curtain rail will be only 9.4mm / 3/8th"
I hope that's the answer to the question.