turbo fan ring gear - jeremy cuddihy's official website

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Turbo Fan Ring Gear Rules Sheet Rules June 21, 2012 5:30:55 PM 1 7 Page of TURBOFANRING.TKW

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Page 1: Turbo Fan Ring Gear - Jeremy Cuddihy's Official WebSite

Turbo Fan Ring GearRules SheetRules

June 21, 2012 5:30:55 PM1 7Page of TURBOFANRING.TKW

Page 2: Turbo Fan Ring Gear - Jeremy Cuddihy's Official WebSite

Rules

June 21, 2012 5:30:55 PM2 7Page of TURBOFANRING.TKW

Page 3: Turbo Fan Ring Gear - Jeremy Cuddihy's Official WebSite

Rules

June 21, 2012 5:30:55 PM3 7Page of TURBOFANRING.TKW

Page 4: Turbo Fan Ring Gear - Jeremy Cuddihy's Official WebSite

Rules

June 21, 2012 5:30:55 PM4 7Page of TURBOFANRING.TKW

Page 5: Turbo Fan Ring Gear - Jeremy Cuddihy's Official WebSite

Rules

Variables SheetInput Name Output Unit Comment

6 P diametral pitch, it is a standard size, table13-3 [teeth/inch]

34 N_s number of teeth sun piniond_s 5.666667 pitch diameter of sun pinion [in]

31 N_p number of teeth planet pinionsd_p 5.166667 pitch diameter of planet pinions [in]

96 N_r number of teeth internal geard_r 16 pitch diameter of internal gear [in]V 13351.768778 pitch line velocity [ft/min]

9000 n_s sun pinion speed [rev/min]n_r 3187.5 ring gear speed [rev/min]n_p 9870.967742 planetary pinion speed [rev/min]W_t 7909.064466 total transmitted load [lbf]

32000 Hp shaft horsepower to the sun pinion [hp]W_r 2705.059362 radial component [lbf]

20 φ_n normal pressure angle, choose a standard20 degrees

W_a 3140.936752 axial component, thrust load, cancel fordouble helical [lbf]

25 ψ helix angle, ASSUME choose 25 degrees,thats what prob 14-39 has

W 9286.746430 total force [lbf]ratio 2.823529 gear ratio & speed ratio, sun to ring

2300 C_p elastic coefficient, steel on steel, table 14-5,[psi]

1 C_a application factor, ASSUME, sec 14-8C_v 1 AGMA dynamic factor, eq 14-27

1 C_s size factor, MOST OFTEN UNITY, section14-10

2.5 F face width [in], ASSUMED1.2 C_m load distribution factor, table 14-6, ASSUME

accurate helical1 C_f surface condition factor > 1 for obvious

defects, section 14-9I 0.438935 geometry factorφ_t 21.880233 transverse pressure anglem_F 2.226455 face contact ratio, should be > 2 eq 14-19p_x 1.122861 axial pitch [in], eq 13-13m_N 0.581810 load sharing ratiom_G 3.096774 speed ratio of ring to planet pinionsAA 106 used in dynamic factor eqBB 0 used in dynamic factor eq

June 21, 2012 5:30:55 PM5 7Page of TURBOFANRING.TKW

Page 6: Turbo Fan Ring Gear - Jeremy Cuddihy's Official WebSite

Input Name Output Unit Comment

QUALITY MUST BE AT LEAST 12 !!!12 Q_v transmission accuracy-level #, quality #,

ASSUME 12, sec 14-7reference aerogear.com, manufacturing,sizes

p_N 0.445923 normal base pitch [in], eq 14-24Z 0.806781 length of line of action in the transverse

plane [in]p_n 0.474542 normal circular pitch [in], eq 13-12p_t 0.523599 circular pitch [in], eq 13-4a 0.166667 addendum distance [in], p 266r_p 2.583333 pitch radius planet [in]r_bp 2.397243 planet base radius [in]r_r 8 pitch radius of ring [in]r_br 7.423719 ring base radius [in]σ_c 94103.498871 contact stress from total force, [psi]

---------------------------------------------------------215000 S_c surface fatigue strength, table 14-4,

ASSUME intermediate value, [psi]C_L 0.837524 life factor, average of upper & lower limits fig

14-8, p340C_L_high 0.900441 upper limit for N_life > 10^7C_L_low 0.774606 lower limit for N_life > 10^7C_H 1.001447 hardness ratio factor

1 C_T temperature factor, sec14-15, ASSUME T <150 F

1 C_R reliability factor, table 14-7 ASSUME 99%N_life 956250000 life cyclesA .00069 part of hardness factor eq

630 H_B_s Brinell hardness of the sun pinion,ASSUMED AISI 9310 steel

630 H_B_p Brinell hardness of the planets, ASSUMEDAISI 9310 steelReference gear materials paper we weregiven

σ_c_all 180328.118005 allowable contact stress, [psi]------------------------------------------------------------------

n_surface 1.916274 surface fatigue factor of safety------------------------------------------------------------------

1000 hours Design gear to last 1000 hours------------------------------------------------------------------

K_a 1 application factorK_v 1 dynamic factorK_s 1 size factorK_m 1.2 load-distribution factor

June 21, 2012 5:30:55 PM6 7Page of TURBOFANRING.TKW

Page 7: Turbo Fan Ring Gear - Jeremy Cuddihy's Official WebSite

Input Name Output Unit Comment

.582 J_75 geometry factor for 75-tooth mate, bending,fig 14-5, p335

.96 J_mod modifying factor for other than 75-toothmate, fig 14-6

J .55872 modified geometry factor for use in theequation

σ_bend 40768.373537 bending stress [psi]------------------------------------------------------------------

70000 S_t bending strength, table 14-3,carburized/case hardened, [psi]

K_L 0.900676 life factor, average of upper & lower limits fig14-9, p341

K_L_high 0.938299 upper limit for N_life > 10^7K_L_low 0.863053 lower limit for N_life > 10^7K_T 1 temperature factorK_R 1 reliability factorσ_bend_all 63047.335151 allowable bending stress [psi]

------------------------------------------------------------------

n_bending 1.546477 factor of safety pertaining to bending

June 21, 2012 5:30:55 PM7 7Page of TURBOFANRING.TKW