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Tiêu đề Formulas for Computing Dedendum Angles and Their Sum
Trường học American Gear Manufacturers Association
Chuyên ngành Machine Design
Thể loại handbook
Thành phố Alexandria
Định dạng
Số trang 32
Dung lượng 1,95 MB

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Geometry Factor IFIGURE 34.23 Geometry factor / for durability of spiral-bevel gears with 20° pressure angle, 35° spiral angle, and 90° shaft angle.. Number of Teeth in Mate Geometry Fac

Trang 1

TABLE 34.9 Formulas for Computing Dedendum Angles and Their Sum

Type of taper Formula

Use E5 = 9Q[I-(4JrJ sin »]

Tilted root line (P^ 0 tan <j> cos ^)

AGMA Rating Standard for Bevel Gears, 2003

These are available through American Gear Manufacturer's Association, 1500 KingStreet, Suite 201, Alexandria, VA 22314-2730

Trang 2

Pitch diameter of gear

Pinion pitch angle

Pinion spiral angle

No

1

234567

8910

1112

13

141516

Trang 3

Gear spiral angle

Gear pitch angle

Gear mean cone

distance

Pinion mean cone

distance

Limit pressure angle

Gear pitch apex

23

24252627

28

2930

3132

33343536

Trang 4

TABLE 34.10 Formulas for Computing Blank and Tooth Dimensions of Hypoid Gears

Gear dedendum angle

Gear addendum angle

Gear outer addendum

Gear outer dedendum

Gear whole depth

Gear working depth

Gear root angle

Gear face angle

42

43

44

45 46

47

48

49

50 51

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TABLE 34.10 Formulas for Computing Blank and Tooth Dimensions of Hypoid Gears

Pinion face angle

Pinion root angle

Pinion face apex

Trang 6

TABLE 34.10 Formulas for Computing Blank and Tooth Dimensions of Hypoid Gears

Pinion face width

Mean circular pitch

Mean diametral pitch

Thickness factor

Mean pitch diameter

Mean normal circular

Trang 7

area The recommendations and rating formulas which follow are designed for a toothcontact developed to give the correct pattern in the final mountings under full load.

34.6.1 Formulas for Contact and Bending Stress

The basic equation for contact stress in bevel and hypoid gears is

where S t = calculated tensile bending stress at root of gear tooth, pounds

per square inch (lb/in2)

S c = calculated contact stress at point on tooth where its value will

be maximum, lb/in2

Cp = elastic coefficient of the gear-and-pinion materials combination,

(lb)1/2/in

TPJ T G = transmitted torques of pinion and gear, respectively,

pound-inches (Ib • in)

K 0 , C 0 = overload factors for strength and durability, respectively

K v , C v = dynamic factors for strength and durability, respectively

Kn 0 C m = load-distribution factors for strength and durability, respectively

Cf = surface-condition factor for durability

7 = geometry factor for durability

/ = geometry factor for strength

34.6.2 Explanation of Strength Formulas and Terms

The elastic coefficient for bevel and hypoid gears with localized tooth contact tern is given by

pat-Cf = ^ (1-Vi 2 P)IEp + (I-V^)IE 0 (343)

where |i/>, JIG - Poisson's ratio for materials of pinion and gear, respectively (use

0.30 for ferrous materials)

Ep 9 E G = Young's modulus of elasticity for materials of pinion and gear,

respectively (use 30.0 x IQ6 lb/in2 for steel)The overload factor makes allowance for the roughness or smoothness of opera-tion of both the driving and driven units Use Table 34.11 as a guide in selecting theoverload factor

The dynamic factor reflects the effect of inaccuracies in tooth profile, tooth ing, and runout on instantaneous tooth loading For gears manufactured to AGMAclass 11 tolerances or higher, a value of 1.0 may be used for dynamic factor Curve 2

spac-in Fig 34.18 gives the values of C v for spiral bevels and hypoids of lower accuracy or

for large, planed spiral-bevel gears Curve 3 gives the values of C v for bevels of loweraccuracy or for large, planed straight-bevel gears

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Pitch line velocity V, ft/min

FIGURE 34.18 Dynamic factors K v and C v

The load-distribution factor allows for misalignment of the gear set under ating conditions This factor is based on the magnitude of the displacements of thegear and pinion from their theoretical correct locations Use Table 34.12 as a guide

oper-in selectoper-ing the load-distribution factor

The surface-condition factor depends on surface finish as affected by cutting, ping, and grinding It also depends on surface treatment such as lubrizing And C/can

lap-be taken as 1.0 provided good gear manufacturing practices are followed

Use Table 34.13 to locate the charts for the two geometry factors / and /.The geometry factor for durability 7 takes into consideration the relative radius

of curvature between mating tooth surfaces, load location, load sharing, effectiveface width, and inertia factor

The geometry factor for strength / takes into consideration the tooth form factor,load location, load distribution, effective face width, stress correction factor, andinertia factor

Character of load on driven memberPrime mover Uniform Medium shock Heavy shock

Uniform 1.00 1.25 1.75

Medium shock 1.25 1.50 2.00

Heavy shock 1.50 1.75 2.25

fThis table is for speed-decreasing drive; for speed-increasing

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TABLE 34.12 Load-Distribution Factors K m C m

Both members One member Neither memberApplication straddle-mounted straddle-mounted straddle-mountedGeneral industrial 1.00-1.10 1.10-1.25 1.25-1.40Automotive 1.00-1.10 1.10-1.25

Aircraft 1.00-1.25 1.10-1.40 1.25-1.50

TABLE 34.13 Location of Geometry Factors

Figure no.Gear type Pressure angle, (j) Shaft angle, Z Helix angle, \j/ / Factor / FactorStraight bevel 20° 90° 0° 34.19 34.20

25° 90° 0° 34.21 34.22Spiral bevel 20° 90° 35° 34.23 34.24

20° 90° 25° 34.25 34.2620° 90° 15° 34.27 34.2825° 90° 35° 34.29 34.3020° 60° 35° 34.31 34.3220° 120° 35° 34.33 34.34

Hypoid 19° EID = OAO 34.37 34.38

19° EID = 0.15 34.39 34.40 19° EID -0.20 34.41 34.42 22/2° EID = 0.10 34.43 34.44 22/2° EfD = 0.15 34.45 34.46

Carburized case-hardened gears require a core hardness in the range of 260 to

350 H 8 (26 to 37 R c ) and a total case depth in the range shown by Fig 34.49.

The calculated contact stress S c times a safety factor should be less than the

allowable contact stress S ac The calculated bending stress S t times a safety factor

should be less than the allowable bending stress S

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Geometry Factor I

FIGURE 34.19 Geometry factor / for durability of straight-bevel gears with 20° pressure

angle and 90° shaft angle.

Geometry Factor J

FIGURE 34.20 Geometry factor / for strength of straight-bevel gears with 20° pressure

angle and 90° shaft angle.

Trang 11

Geometry Factor I

FIGURE 34.21 Geometry factor 7 for durability of straight-bevel gears with 25°

pres-sure angle and 90° shaft angle.

Geometry Factor J

FIGURE 34.22 Geometry factor / for strength of straight-bevel gears with 25° pressure angle

and 90° shaft angle.

Trang 12

Geometry Factor I

FIGURE 34.23 Geometry factor / for durability of spiral-bevel gears with 20° pressure

angle, 35° spiral angle, and 90° shaft angle.

Number of Teeth in Mate

Geometry Factor J

FIGURE 34.24 Geometry factor / for strength of spiral-bevel gears with 20° pressure

angle, 35° spiral angle, and 90° shaft angle.

Trang 13

Geometry Factor I

FIGURE 34.25 Geometry factor 7 for durability of spiral-bevel gears with 20° pressure

angle, 25° spiral angle, and 90° shaft angle.

Number of Teeth in Mate

Geometry Factor J

FIGURE 34.26 Geometry factor J for strength of spiral-bevel gears with 20° pressure angle,

25° spiral angle, and 90° shaft angle.

Trang 14

Geometry Factor I

FIGURE 34.27 Geometry factor / for durability of spiral-bevel gears with 20°

pres-sure angle, 15° spiral angle, and 90° shaft angle.

Number of Teeth in Mate

Geometry Factor J

FIGURE 34.28 Geometry factor / for strength of spiral-bevel gears with 20° pressure angle, 15°

spiral angle, and 90° shaft angle.

Trang 15

Geometry Factor I

FIGURE 34.29 Geometry factor / for durability of spiral-bevel gears with 25°

pres-sure angle, 35° spiral angle, and 90° shaft angle.

Number of Teeth in Mate

Geometry Factor J

FIGURE 34.30 Geometry factor / for strength of spiral-bevel gears with 25° pressure angle, 35°

spiral angle, and 90° shaft angle.

Trang 16

Geometry Factor I

FIGURE 34.31 Geometry factor / for durability of spiral-bevel gears with 20° pressure

angle, 35° spiral angle, and 60° shaft angle.

Number of Teeth in Mate

Geometry Factor J

FIGURE 34.32 Geometry factor / for strength of spiral-bevel gears with 20° pressure

angle, 35° spiral angle, and 60° shaft angle.

Trang 17

Geometry Factor I

FIGURE 34.33 Geometry factor / for durability of spiral-bevel gears with 20° pressure

angle, 35° spiral angle, and 120° shaft angle.

Number of Teeth in Mate

Geometry Factor J

FIGURE 34.34 Geometry factor J for strength of spiral-bevel gears with 20° pressure

angle, 35° spiral angle, and 120° shaft angle.

Number of Teeth in Gear

Trang 18

Geometry Factor I

FIGURE 34.35 Geometry factor 7 for durability of automotive spiral-bevel gears with 20° pressure

angle, 35° spiral angle, and 90° shaft angle.

34.6.4 Scoring Resistance

Scoring is a temperature-related process in which the surfaces actually tend to weldtogether The oil film breaks down, and the tooth surfaces roll and slide on oneanother, metal against metal Friction between the surfaces causes heat whichreaches the melting point of the tooth material, and scoring results The factorswhich could cause scoring are the sliding velocity, surface finish, and load concen-trations along with the lubricant temperature, viscosity, and application But see alsoChap 6 If you follow the recommendations under Sec 34.7.6 on lubrication and themanufacturer uses acceptable practices in processing the gears, then scoring shouldnot be a problem

Trang 19

Geometry Factor J

FIGURE 34.36 Geometry factor / for strength of automotive spiral-bevel gears with 20° pressure angle, 35°

spiral angle, and 90° shaft angle.

Number of Teeth in Mate

Trang 20

Geometry Factor I

FIGURE 34.37 Geometry factor / for hypoid gears with 19° average pressure angle and EID ratio of 0.10.

Gear Geometry Factor JG

Pinion Geometry Factor Jp'

FIGURE 34.38 Geometry factor / for strength of hypoid gears with 19° average pressure angle and

Trang 21

Geometry Factor I

FIGURE 34.39 Geometry factor 7 for durability of hypoid gears with 19° average pressure angle and

EID ratio of 0.15.

Gear Geometry Factor JG

Pinion Geometry Factor Jp'

FIGURE 34.40 Geometry factor / for strength of hypoid gears with 19° average pressure angle and

Trang 22

Geometry Factor I

FIGURE 34.41 Geometry factor / for durability of hypoid gears with 19° average pressure angle

and EID ratio of 0.20.

Gear Geometry Factor JG

Pinion Geometry Factor Jp'

FIGURE 34.42 Geometry factor / for strength of hypoid gears with 19° average pressure angle and

Trang 23

Geometry Factor I

FIGURE 34.43 Geometry factor 7 for durability of hypoid gears with 221^ 0 average pressure angle

and EID ratio of 0.10.

Gear Geometry Factor JG

Pinion Geometry Factor Jp'

FIGURE 34.44 Geometry factor / for strength of hypoid gears with 22M>° average pressure angle and

Trang 24

Geometry Factor I

FIGURE 34.45 Geometry factor / for durability of hypoid gears with 221^ 0 average pressure angle

and EID ratio of 0.15.

Gear Geometry Factor JG

Pinion Geometry Factor Jp'

FIGURE 34.46 Geometry factor / for strength of hypoid gears with 221^ 0 average pressure angle and

Trang 25

Geometry Factor I

FIGURE 34.47 Geometry factor / for durability of hypoid gears with 22M>° average pressure angle and

EID ratio of 0.20.

Gear Geometry Factor JG

Pinion Geometry Factor Jp'

FIGURE 34.48 Geometry factor / for strength of hypoid gears with 22i^° average pressure angle and

Trang 26

TABLE 34.14 Allowable Contact Stress S ac

Minimum hardness

T Contact stress

Material Heat treatment Brinell Rockwell C S 00 lb/in2

Steel Carburized (case-hardened) 60 250000Steel Carburized (case-hardened) 55 210000Steel Flame-or induction- 500 50 200000

hardenedSteel and nodular iron Hardened and tempered 400 180 000Steel Nitrided 60 180000Steel and nodular iron Hardened and tempered 300 140 000Steel and nodular iron Hardened and tempered 180 100000Cast iron As cast 200 80000Cast iron As cast 175 70000Cast iron As cast 60 000

34.7 DESIGNOFMOUNTINGS

The normal load on the tooth surfaces of bevel and hypoid gears may be resolvedinto two components: one in the direction along the axis of the gear and the otherperpendicular to the axis The direction and magnitude of the normal load depend

on the ratio, pressure angle, spiral angle, hand of spiral, and direction of rotation aswell as on whether the gear is the driving or driven member

34.7.1 Hand of Spiral

In general, a left-hand pinion driving clockwise (viewed from the back) tends tomove axially away from the cone center; a right-hand pinion tends to move towardthe center because of the oblique direction of the curved teeth If possible, the hand

of spiral should be selected so that both the pinion and the gear tend to move out ofmesh, which prevents the possibility of tooth wedging because of reduced backlash.Otherwise, the hand of spiral should be selected to give an axial thrust that tends tomove the pinion out of mesh In a reversible drive, there is no choice unless the pairperforms a heavier duty in one direction for a greater part of the time

Trang 27

TABLE 34.15 Allowable Bending Stress S

Surface hardness

I Bending stress

Steel Carburized (case-hardened) 575-625 55 min 60 000Steel Flame-or induction- 450-500 50 min 27000

hardened (unhardened

root fillet)

Steel Hardened and tempered 450 min 50000Steel Hardened and tempered 300 min 42000Steel Hardened and tempered 180 min 28000Steel Normalized 140 min 22000Cast iron As cast 200 min 13000Cast iron As cast 175 min 8500Cast iron As cast 5 000

On hypoids when the pinion is below center and to the right (when you are ing the front of the gear), the pinion hand of spiral should always be left-hand Withthe pinion above center and to the right, the pinion hand should always be right-hand See Fig 34.15

N - speed of gear, r/min

The tangential force on the mating pinion is given by the equation

WtGcosVp = 27>

cos \|fG d m where T = pinion torque in pound-inches.

Trang 28

Approximate Total Depth of Case

FIGURE 34.49 Diametral pitch versus total case depth If in doubt, use the greater case depth

on ground gears or on short face widths.

Trang 29

34.7.3 Axial Thrust and Radial Separating Forces

separating force W R for bevel and hypoid gears The direction of the pinion (driver)rotation should be viewed from the pinion back

For a pinion (driver) with a right-hand (RH) spiral with clockwise (cw) rotation or

a left-hand (LH) spiral with counterclockwise (ccw) rotation, the axial and ing force components acting on the pinion are, respectively,

WRP = W t p sec xj/p (tan ty cos y + sin \\r p sin y) (34.7)

For a pinion (driver) with an LH spiral with cw rotation or an RH spiral with ccw

rotation, the force components acting on the pinion are, respectively,

WRP = W tP sec \|/p (tan (|) cos y - sin \|//> sin y) (34.9)

For a pinion (driver) with an RH spiral with cw rotation or an LH spiral with ccw

rotation, the force components acting on the gear (driven) are, respectively,

For a pinion (driver) with an LH spiral and cw rotation or an RH spiral with ccw

rotation, the force components acting on the gear are, respectively,

WRG = W,G sec \|/G (tan (|) cos F + sin \|/G sin F) (34.13)These equations apply to straight-bevel, Zerol bevel, spiral-bevel, and hypoid gears.When you use them for hypoid gears, be sure that the pressure angle corresponds tothe driving face of the pinion tooth

A plus sign for Eqs (34.6), (34.8), (34.10), and (34.12) indicates that the direction

of the axial thrust is outward, or away from the cone center Thus a minus sign cates that the direction of the axial thrust is inward, or toward the cone center.

indi-A plus sign for Eqs (34.7), (34.9), (34.11), and (34.13) indicates that the direction

of the separating force is away from the mating gear So a minus sign indicates an

attracting force toward the mating member.

Example A hypoid-gear set consists of an 11-tooth pinion with LH spiral and ccw

rotation driving a 45-tooth gear Data for the gear are as follows: 4.286 diametralpitch, 8.965-inch (in) mean diameter, 70.03° pitch angle, 31.48° spiral angle, and 30 x

con-cave pressure angle 18.13°, convex pressure angle 21.87°, pitch angle 19.02°, and ral angle 50° Determine the force components and their directions for each member

spi-of the set

Solution From Eq (34.4) we find the tangential load on the gear to be

* %.&£&.«»*

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