barcode vb.net 2010 These figures are extracted from AGMA 908-B89 with the permission of the AGMA. in Software

Drawing EAN13 in Software These figures are extracted from AGMA 908-B89 with the permission of the AGMA.

These figures are extracted from AGMA 908-B89 with the permission of the AGMA.
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HELICAL GEARS 10.24
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FIGURE 10.13 Basic geometry factors for 25 spur teeth; N = 25 , a = 1.00, b = 1.35, rT = 0.24, t = 0.
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of dimensions obtained from an accurate layout of the tooth profile in the normal plane at a scale of 1 normal diametral pitch. Actually, any scale can be used, but the use of 1 normal diametral pitch is most convenient. Depending on the face-contact ratio, the load is considered to be applied at the highest point of single-tooth contact (HPSTC), Fig. 10.37, or at the tooth tip, Fig. 10.38. The equation is Y= K Ps [cos ( L)/cos ( No)][(1.5/uCh) tan ( L)/t]
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(10.49)
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The terms in Eq. (10.49) are defined as follows: K = helix-angle factor No = normal operating pressure angle [Eq. (10.14)] L = load angle Ch = helical factor t = tooth thickness from layout, in u = radial distance from layout, in Ps = normal diametral pitch of layout (scale pitch), usually 1.0 in 1
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HELICAL GEARS 10.25
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HELICAL GEARS
FIGURE 10.14 Tool-tip radius adjustment factor for 20 spur teeth. Tool-tip radius = rT for a 1-diametral-pitch gear.
FIGURE 10.15 Tool-tip radius adjustment factor for 221 2 spur teeth. Tool-tip radius = rT for a 1-diametral-pitch gear.
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HELICAL GEARS 10.26
GEARING
FIGURE 10.16 Tool-tip radius adjustment factor for 25 spur teeth. Tool-tip radius = rT for a 1-diametral-pitch gear.
FIGURE 10.17 Tooth thickness adjustment factor QTT for 20 spur teeth. Tooth thickness modification = t for 1-diametral-pitch gears.
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HELICAL GEARS 10.27
HELICAL GEARS
FIGURE 10.18 Tooth thickness adjustment factor QTT for 221 2 spur teeth. Tooth thickness modification = t for 1-diametral-pitch gears.
FIGURE 10.19 Tooth thickness adjustment factor QTT for 25 spur teeth. Tooth thickness modification = t for 1-diametral-pitch gears.
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HELICAL GEARS 10.28
GEARING
FIGURE 10.20 Addendum adjustment factor QA for 20 spur teeth. Addendum factor modification = a for 1-diametral-pitch gears.
FIGURE 10.21 Addendum adjustment factor QA for 221 2 spur teeth. Addendum factor modification = a for 1-diametral-pitch gears.
To make the Y factor layout for a helical gear, an equivalent normal-plane gear tooth must be created, as follows: Ne = NP cos3 dPnd cos2 (10.50)
dc =
(10.51)
dbe = de cos n = Ne cos c
(10.52)
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HELICAL GEARS 10.29
HELICAL GEARS
FIGURE 10.22 Addendum adjustment factor QA for 25 spur teeth. Addendum factor modification = a for 1-diametral-pitch gears.
FIGURE 10.23 Helix-angle adjustment factor QH for N = 20 .
a= b=
do d Pnd 2 d dR Pnd 2
(10.53) (10.54) (10.55) (10.56) (10.57)
doe = de + 2a dRe = de 2b r1 = (b rTe)2 Ro + b rTe
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HELICAL GEARS 10.30
GEARING
FIGURE 10.24 Helix-angle adjustment factor QH for N = 221 2 .
FIGURE 10.25 Helix-angle adjustment factor QH for N = 25 .
rf = r1 + rTe rTe = rT Pnd For a hob or rack-shaped cutting tool, Ro = For a pinion-shaped cutting tool, Ro = dseDcPnd 2(dse + DcPnd) dse 2
(10.58) (10.59)
(10.60)
(10.61)
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