GB2373304A - Tapered involute gear profile - Google Patents

Tapered involute gear profile Download PDF

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Publication number
GB2373304A
GB2373304A GB0104114A GB0104114A GB2373304A GB 2373304 A GB2373304 A GB 2373304A GB 0104114 A GB0104114 A GB 0104114A GB 0104114 A GB0104114 A GB 0104114A GB 2373304 A GB2373304 A GB 2373304A
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United Kingdom
Prior art keywords
gear
tooth
sectional profile
cross
axial distance
Prior art date
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Withdrawn
Application number
GB0104114A
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GB0104114D0 (en
Inventor
Bryan Nigel Victor Parsons
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Individual
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Individual
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Priority to GB0104114A priority Critical patent/GB2373304A/en
Publication of GB0104114D0 publication Critical patent/GB0104114D0/en
Publication of GB2373304A publication Critical patent/GB2373304A/en
Withdrawn legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H55/00Elements with teeth or friction surfaces for conveying motion; Worms, pulleys or sheaves for gearing mechanisms
    • F16H55/02Toothed members; Worms
    • F16H55/08Profiling
    • F16H55/0806Involute profile
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H55/00Elements with teeth or friction surfaces for conveying motion; Worms, pulleys or sheaves for gearing mechanisms
    • F16H55/02Toothed members; Worms
    • F16H55/08Profiling
    • F16H2055/0893Profiling for parallel shaft arrangement of toothed members

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Gears, Cams (AREA)

Abstract

A tapered involute gear profile for a parallel shaft transmission wherein the cross-sectional profile of the gear reduces across the axial distance of the gear, wherein the tooth thickness (T and t) measured at a constant radius, such as the pitch circle radius, reduces in linear proportion to the axial distance so that the flanks of the tooth in cross-sectional profile remain involute curves on a common base circle for all cross-sections. Tapered involute gears having a helical tooth profile are also discloses (figs 5-8).

Description

Tapered Gear Profile
This invention applies to gear profiles suitable for parallel shaft transmissions and particularly to gear profiles that are manufactured from a die process, such as injection moulding or forging.
Applying a simple draft angle to gear profile designed for parallel shaft transmission, such as spur gear, to facilitate manufacture by, for example, forging, would result in gear inaccuracy and non-conjugate motion between mating gears. This patent defines a profile that fulfils the requirements of the gears whilst providing a shape that can be easily forged or moulded.
According to the present invention a tapered involute gear profile for a parallel shaft transmission is characterised in that the cross-sectional profile of the whole gear reduces in accordance with the axial distance of the said cross-sectional profile from the maximum cross-sectional profile of the gear, wherein the tooth thickness measured at a constant radius, such as the pitch circle radius, reduces in linear proportion to the axial distance from the said maximum cross-sectional profile, so that the flanks of the tooth in cross-sectional profile remain involute curves on a common base circle for all cross-sections.
According to a preferred embodiment of the invention, the radial distance of the centre of the gear to the tips of the gears in cross-sectional profile reduces in linear proportion to the axial distance of the said cross-sectional profile to the maximum cross-sectional profile.
According to a further preferred embodiment of the invention, the radial distance of the centre of the gear to the root of the gear teeth reduces in linear proportion to the axial distance of the said cross-sectional profile to the maximum cross-sectional profile.
According to a further aspect of the invention the gradient of the variation of the tooth thickness with the axial distance from the maximum cross-section is substantially one module reduction for every five modules axial distance.
According to a further aspect of the invention the gradient of the variation of the tooth addendum with the axial distance from the maximum cross-section is substantially one module reduction for every ten modules axial distance.
According to a further aspect of the invention the gradient of the variation of the tooth dedendum with the axial distance from the maximum cross-section is substantially one module reduction for every ten modules axial distance.
According to a further aspect of the invention the mid plane of the tooth in section might be translated helically as the axial distance from the maximum cross-sectional profile increases.
According to a further aspect of the invention the helical translation of the mid plane of the tooth in section is such that the flank of one side of the tooth remains in axial alignment.
Various embodiments of the invention will now be described, by example only, with reference to the accompanying drawings, where: Figure I represents a plan transparent view of a gear designed in accordance with the invention with no helical translation of the section.
Figure 2 represents an isometric view of two gears designed in accordance with the invention, in mesh, with no helical translation of the section.
Figure 3 represents an isometric view of a gear meshing with a rack designed in accordance with the invention, with no helical translation of the section.
Figure 4 represents an isometric view of an internal gear designed in accordance with the invention with no helical translation of the section.
Figure 5 represents a gear, designed in accordance with the invention, with a helical translation where one flank of the tooth remains in axial alignment.
Figure 6 represents an isometric view of two gears designed in accordance with the invention, in mesh with a helical translation where the helical translation ensures one flank is axially aligned.
Figure 7 represents a gear, designed in accordance with the invention, with a helical translation of the profile equal to half of the angular pitch.
Figure 8 represents an isometric view of two gears designed in accordance with the invention, in mesh with a helical translation of the profile equal to half of the angular pitch.
Figure I represents the geometry of the gear profile of a gear with twenty teeth where outline 21 represents the gear tooth shape at one end of a gear whilst outline 22 represents the gear tooth shape at the opposite end of the gear to outline 21. Circle 31 is the addendum at the large end of the gear whilst circle 32 is the addendum at the small end of the gear. The circle 33 is the dedendum at the large end of the gear whilst circle 34 is the dedendum at the small end of the gear. The involute flanks of the gear teeth are developed from the base circle 36 for the whole gear profile. The pitch circle 35 depends on the base circle 36 and the nominal pressure angle of the gear A. The tooth thickness varies from T at the large end of the gear to t at the small end of the gear. The change in tooth tip height is denoted by H and the change in tooth depth is denoted by d. The line of action 37 of the gear is tangential to the base circle 36 and passes through the pitch point 40. the angle subtended from the centre of the gear between the pitch point and the tangent point of the line of action 37 to the base circle 36 is equal to the nominal pressure angle A. The thickness of the tooth form varies linearly with axial position between T and t. For a standard gear the tooth thickness t the pitch circle diameter would be equal to the pitch circle circumference divided by twice the number of teeth. The thickness T for the gear shown is equal to the standard gear tooth thickness plus one module, whilst the thickness t is equal to the standard thickness minus one module.
Where a module is equal to the pitch circle diameter divided by the number of teeth on the gear. The thickness of the gear is ten modules. The ratio of the change in thickness for the
tooth with axial distance is for this gear equal to 1 : 5. This gives an apparent draft angle of 60 for the tooth flank. The ratio of the change in the addendum for the gear with axial distance between the large and small ends of the gear is 1: 10. this gives an apparent draft angle for the tooth tips of 60. The ratio of the change in the dedendum for the gear with axial distance between the large and small ends of the gear is 1: 10. this gives an apparent draft angle for the tooth roots of 60. the gear has thus an overall draft angle of about 60 making the manufacture by means of forging, die casting or moulding easier than a conventional straight cut gear. The axial mid plane of the gear (halfway between large and small ends of the gear) corresponds to the standard proportions for a gear tooth in that the addendum is equal to one module whilst the dedendum is one and one quarter modules whilst the tooth thickness is half the circular pitch.
Figure 2 shows the gear AA of figure I in isometric elevation engaged with a similar gear BB being identical to gear AA except inverted to mesh the large end of gear AA with the small end of gear BB.
Figure 3 shows the gear CC of figure 1 in isometric elevation in mesh with a rack DD formed in accordance with the same condition for gradient for tooth thickness, addendum height and dedendum depth. The profile of the rack DD being inverted so that the large end of the gear CC meshes with the thin end of the tooth form of the rack DD.
Figure 4 shows an internal gear constructed to the same constraint on the tooth thickness, addendum height and dedendum depth. In this case the large end of the internal gear is shown at the top whilst the external surface of the gear is given a draft angle of 6 so that the largest external diameter is also at the top to enable the gear to be easily ejected from the forming die.
Figure 5 shows an external gear with substantially the same constraint on the tooth thickness, addendum height and dedendum depth but with a helical twist with axial position such that the flank 38 is axially aligned whilst the back face is helical.
Figure 6 shows an isometric elevation of the gear EE of figure 5 meshing with a mirror image gear FF of the gear EE. The large end of the gear EE meshes with the small end of the gear FF.
Figure 7 shows an external gear with substantially the same constraint on the tooth thickness, addendum height and dedendum depth but with a helical twist with axial position such that the helical twist is half of the pitch. In this case the angle between the mid-plane of tooth 42 and the mid-plane of tooth 43 is half of the angular pitch of the gear.
Figure 8 shows an isometric elevation of the gear GG of figure 5 meshing with a mirror image gear HH of the gear GG. The large end of the gear GG meshes with the small end of the gear HH. This arrangement is only really applicable to gears of equal tooth numbers, but might be an advantage in certain applications such as hydraulic gear pumps.
The general form of the gears allows the degree of backlash between a pair of gears to be adjusted by altering the relative axial position of the gears. This should have applications where zero backlash is a requirement for a transmission system.
Various modifications might be made without departing from the invention. For example the change in profile has generally been described as linear with axial position, however other degrees of variation might be used provided the inverse for the meshing gear can also be applied. A sinusoidal variation could be applied to the tooth thickness, addendum and dedendum parameters with axial position.

Claims (11)

1. According to the present invention a tapered involute gear profile for a parallel shaft transmission is characterised in that the cross-sectional profile of the whole gear reduces in accordance with the axial distance of the said cross-sectional profile from the maximum cross-sectional profile of the gear, wherein the tooth thickness measured at a constant radius, such as the pitch circle radius, reduces in linear proportion to the axial distance from the said maximum cross-sectional profile, so that the flanks of the tooth in cross-sectional profile remain involute curves on a common base circle for all cross sections..
2. A gear according to claim I where the radial distance of the centre of the gear to the tips of the gears in cross-sectional profile reduces in a linear proportion to the axial distance of the said cross-sectional profile to the maximum cross-sectional profile.
3. A gear according to claim 1 where the radial distance of the centre of the gear to the root of the gear teeth reduces in a linear proportion to the axial distance of the said cross sectional profile to the maximum cross-sectional profile.
4. A gear according to claim 2 in which the gradient of the variation of the tooth thickness with the axial distance from the maximum cross-section is substantially one module reduction for every five modules axial distance.
5. A gear according to claims 2 in which the gradient of the variation of the tooth addendum with the axial distance from the maximum cross-section is substantially one module reduction for every ten modules axial distance.
6. A gear according to claim 3 wherein the gradient of the variation of the tooth dedendum with the axial distance from the maximum cross-section is substantially one module reduction for every ten modules axial distance.
7. A gear according to claim 6 in which the mid plane of the tooth in section might be translated helically as the axial distance from the maximum cross-sectional profile increases.
8. A gear according to claim 6 the helical translation of the mid plane of the tooth in section is such that the flank of one side of the tooth remains in axial alignment.
9. A gear designed according to any of the above claims in which the gradient of the tooth thickness with axial position is adjusted to provide optimum angle for manufacture.
10. A gear transmission according to any of the above claims in which the backlash is adjusted by axially adjusting the relative position of two meshing gears.
11. A gear pair in accordance with any of the above claims used to form a hydraulic gear pump
GB0104114A 2001-02-20 2001-02-20 Tapered involute gear profile Withdrawn GB2373304A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0104114A GB2373304A (en) 2001-02-20 2001-02-20 Tapered involute gear profile

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0104114A GB2373304A (en) 2001-02-20 2001-02-20 Tapered involute gear profile

Publications (2)

Publication Number Publication Date
GB0104114D0 GB0104114D0 (en) 2001-04-11
GB2373304A true GB2373304A (en) 2002-09-18

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL1026324C2 (en) * 2004-06-03 2005-12-06 Iku Holding Montfoort Bv Method for assembling a gear transmission, as well as gear transmission.
FR2879276A1 (en) * 2004-12-15 2006-06-16 Renault Sas Drive shaft e.g. cam shaft, and driven shaft e.g. crankshaft, clearance compensation system for e.g. gasoline engine, has sprocket wheels with teeth whose one of two flanks converge towards other flanks to form wedge between teeth of wheels
WO2018218363A1 (en) * 2017-05-31 2018-12-06 Genesis Robotics And Motion Technologies Canada, Ulc Actuator with speed reducer
CN111062879A (en) * 2019-11-13 2020-04-24 南京工业大学 Image algorithm for detecting involute in image

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2836014A (en) * 1952-06-18 1958-05-27 W E Sykes Ltd Machines for grinding gear tooth and like profiles
US2887015A (en) * 1956-01-30 1959-05-19 Nat Broach & Mach Method of shaving conical involute gears
US3862585A (en) * 1971-06-28 1975-01-28 Gen Motors Corp Method of manufacturing tapered involute splines
DE2446172A1 (en) * 1974-09-27 1976-04-15 Daimler Benz Ag Involute gear teeth with varying form correction - produces teeth with longer arc of contact to reduce shock loading
JPS5846260A (en) * 1981-09-12 1983-03-17 Keiichi Komiyama Gear arrangement
US4524643A (en) * 1982-01-18 1985-06-25 Mavilor Systemes S.A. Epicyclic gear
SU1558586A1 (en) * 1988-04-25 1990-04-23 Челябинский Политехнический Институт Им.Ленинского Комсомола Arrangement for milling internal thread

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2836014A (en) * 1952-06-18 1958-05-27 W E Sykes Ltd Machines for grinding gear tooth and like profiles
US2887015A (en) * 1956-01-30 1959-05-19 Nat Broach & Mach Method of shaving conical involute gears
US3862585A (en) * 1971-06-28 1975-01-28 Gen Motors Corp Method of manufacturing tapered involute splines
DE2446172A1 (en) * 1974-09-27 1976-04-15 Daimler Benz Ag Involute gear teeth with varying form correction - produces teeth with longer arc of contact to reduce shock loading
JPS5846260A (en) * 1981-09-12 1983-03-17 Keiichi Komiyama Gear arrangement
US4524643A (en) * 1982-01-18 1985-06-25 Mavilor Systemes S.A. Epicyclic gear
SU1558586A1 (en) * 1988-04-25 1990-04-23 Челябинский Политехнический Институт Им.Ленинского Комсомола Arrangement for milling internal thread

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL1026324C2 (en) * 2004-06-03 2005-12-06 Iku Holding Montfoort Bv Method for assembling a gear transmission, as well as gear transmission.
FR2879276A1 (en) * 2004-12-15 2006-06-16 Renault Sas Drive shaft e.g. cam shaft, and driven shaft e.g. crankshaft, clearance compensation system for e.g. gasoline engine, has sprocket wheels with teeth whose one of two flanks converge towards other flanks to form wedge between teeth of wheels
WO2018218363A1 (en) * 2017-05-31 2018-12-06 Genesis Robotics And Motion Technologies Canada, Ulc Actuator with speed reducer
CN111062879A (en) * 2019-11-13 2020-04-24 南京工业大学 Image algorithm for detecting involute in image
CN111062879B (en) * 2019-11-13 2023-11-14 南京工业大学 Image method for detecting involute in image

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