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Leahy
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Dec 7, 2017
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% Given Parameters: | ||
% Shaft Material - AISI 4130 Q&T CD | ||
E = 29*10^6; %psi (Young's Modulus) | ||
sut = 118*10^3; %psi (ultimate strength) | ||
sy = 102*10^3; %psi (yield strength) | ||
p = 0.3; %(poisson's ratio) | ||
ga_w = 4; %lbf - make as input value | ||
ga_t = 50; %teeth number - input | ||
ga_a = 20; %deg - input | ||
ga_d = 4; %diametric pitch - input | ||
gc_w = 2; %lbf - make as input value | ||
gc_t = 25; %teeth number - input | ||
gc_a = 20; %deg - input | ||
gc_d = 4; %diametric pitch - input | ||
ss = 3000; %rpm (shaft speed) | ||
T = 3500; %lbf-in (torque) | ||
% Reliability for fatigue life = 0.99 | ||
% nd, Safety factor for fatigue life = 2 | ||
% nd, safety factor for all other criteria = 1 | ||
% r/d = 0.02 - woodruff key | ||
gear_def = 0.01; % deflection at gears - from table 7-2 | ||
bearing_slope = 0.001; %rad | ||
gear_slope = 0.005; %rad | ||
d_a = ga_t/ga_d; % diameter of gear a | ||
d_c = gc_t/gc_d; % diameter of gear c | ||
Fct = T/(d_c/2); % tangential force on gear c | ||
Fat = T/(d_a/2); % tangential force on gear a | ||
Fcn = Fct * tand(gc_a); | ||
Fan = Fat * tand(ga_a); | ||
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% Find Reaction Forces - XY plane | ||
Rby = ((Fcn*3)+(Fan*9))/6; | ||
Rdy = Fan + Fcn - Rby; | ||
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% Calculate C1 and C2 - XY Plane | ||
c1 = (117*Fan-36*Rby+4.5*Fcn)/6; | ||
c2 = 4.5*Fan - 3*c1; | ||
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% Singularity Functions - x = 0 - 9 inches | ||
for i = 0:length(i) | ||
if (0<=i) && (i<=3) | ||
EIdy_x = -Fan/2*(i)^2+c1; | ||
EIy_x = -Fan/6*(i)^3+c1*i+c2; | ||
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elseif (3<i) && (i<=6) | ||
EIdy_x = -Fan/2*(i)^2+Rby/2*(i-3)^2+c1; | ||
EIy_x = -Fan/6*(i)^3+Rby/6*(i-3)^2+c1*i+c2; | ||
elseif (6<i) && (i<=9) | ||
EIdy_x = -Fan/2*(i)^2+Rby/2*(i-3)^2-Fcn/2*(i-6)^2+c1; | ||
EIy_x = -Fan/6*(i)^3+Rby/6*(i-3)^2-Fcn/6*(i-6)^3+c1*i+c2; | ||
end | ||
end | ||
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% Diameter of the shaft due to slope at the bearings - Points B,D | ||
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This file contains bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters.
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Original file line number | Diff line number | Diff line change |
---|---|---|
@@ -0,0 +1,61 @@ | ||
% Given Parameters: | ||
% Shaft Material - AISI 4130 Q&T CD | ||
E = 29*10^6; %psi (Young's Modulus) | ||
sut = 118*10^3; %psi (ultimate stress) | ||
sy = 102*10^3; %psi (yield stress) | ||
p = 0.3; %(poisson's ratio) | ||
ga_w = 4; %lbf - make as input value | ||
ga_t = 50; %teeth number - input | ||
ga_a = 20; %deg - input | ||
ga_d = 4; %diametric pitch - input | ||
gc_w = 2; %lbf - make as input value | ||
gc_t = 25; %teeth number - input | ||
gc_a = 20; %deg - input | ||
gc_d = 4; %diametric pitch - input | ||
ss = 3000; %rpm (shaft speed) | ||
T = 3500; %lbf-in (torque) | ||
% Reliability for fatigue life = 0.99 | ||
% nd, Safety factor for fatigue life = 2 | ||
% nd, safety factor for all other criteria = 1 | ||
% r/d = 0.02 - woodruff key | ||
gear_def = 0.01; % deflection at gears - from table 7-2 | ||
bearing_slope = 0.001; %rad | ||
gear_slope = 0.005; %rad | ||
d_a = ga_t/ga_d; % diameter of gear a | ||
d_c = gc_t/gc_d; % diameter of gear c | ||
Fct = T/(d_c/2); % tangential force on gear c | ||
Fat = T/(d_a/2); % tangential force on gear a | ||
Fcn = Fct * tand(gc_a); | ||
Fan = Fat * tand(ga_a); | ||
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% Find Reaction Forces - XY plane | ||
Rby = ((Fcn*3)+(Fan*9))/6; | ||
Rdy = Fan + Fcn - Rby; | ||
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% Calculate C1 and C2 - XY Plane | ||
c1 = (117*Fan-36*Rby+4.5*Fcn)/6; | ||
c2 = 4.5*Fan - 3*c1; | ||
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% Singularity Functions - x = 0 - 9 inches | ||
for x = linspace(0,9,10) | ||
if (0<=x) && (x<=3) | ||
EIdy_x = -Fan/2*(x)^2+c1; | ||
EIy_x = -Fan/6*(x)^3+c1*x+c2; | ||
elseif (3<x) && (x<=6) | ||
EIdy_x = -Fan/2*(x)^2+Rby/2*(x-3)^2+c1; | ||
EIy_x = -Fan/6*(x)^3+Rby/6*(x-3)^2+c1*x+c2; | ||
elseif (6<x) && (x<=9) | ||
EIdy_x = -Fan/2*(x)^2+Rby/2*(x-3)^2-Fcn/2*(x-6)^2+c1; | ||
EIy_x = -Fan/6*(x)^3+Rby/6*(x-3)^2-Fcn/6*(x-6)^3+c1*x+c2; | ||
end | ||
end | ||
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% Diameter of the shaft due to slope at the bearings - Points B,D | ||
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