GB2175668A - Gear box - Google Patents

Gear box Download PDF

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Publication number
GB2175668A
GB2175668A GB8513033A GB8513033A GB2175668A GB 2175668 A GB2175668 A GB 2175668A GB 8513033 A GB8513033 A GB 8513033A GB 8513033 A GB8513033 A GB 8513033A GB 2175668 A GB2175668 A GB 2175668A
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GB
United Kingdom
Prior art keywords
members
gear box
gear
rotatable
coaxial
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
GB8513033A
Other versions
GB8513033D0 (en
Inventor
Nicholas John Peter Wirth
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to GB8513033A priority Critical patent/GB2175668A/en
Publication of GB8513033D0 publication Critical patent/GB8513033D0/en
Publication of GB2175668A publication Critical patent/GB2175668A/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Withdrawn legal-status Critical Current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
    • F16H1/00Toothed gearings for conveying rotary motion
    • F16H1/28Toothed gearings for conveying rotary motion with gears having orbital motion
    • F16H1/46Systems consisting of a plurality of gear trains each with orbital gears, i.e. systems having three or more central gears
    • 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
    • F16H57/00General details of gearing
    • F16H57/02Gearboxes; Mounting gearing therein
    • F16H57/021Shaft support structures, e.g. partition walls, bearing eyes, casing walls or covers with bearings
    • 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
    • F16H1/00Toothed gearings for conveying rotary motion
    • F16H1/28Toothed gearings for conveying rotary motion with gears having orbital motion
    • F16H2001/2881Toothed gearings for conveying rotary motion with gears having orbital motion comprising two axially spaced central gears, i.e. ring or sun gear, engaged by at least one common orbital gear wherein one of the central gears is forming the output

Abstract

A gear box which provides a high velocity ratio comprising first and second coaxial toothed members (4,6) which have different radii, one member (4) of which is fixed and one member (6) of which is rotatable, third and fourth toothed members (3,5) which mesh respectively with the first and second toothed members (4,6) and which rotate in unison about an axis (9) which is offset to the axis (12) of the first and second members (4,6). There are input drive means (1) arranged to drive the third and fourth members (3,5) so that they execute an epicyclic motion with respect to the first and second members (4,6) and output drive means (8) drivable by the rotatable one (6) of the first and second members (4,6). <IMAGE>

Description

SPECIFICATION Gear box This invention relates to a gear box, and has particular application to a gear box having a high velocity ratio.
Gear boxes having a high velocity ratio are required in a number of applications. For example, in powering a helicopter it is conventional to use a turbine having a high rotational velocity which must be coupled via a gear box to the rotor which rotates at a relatively low speed. A similar problem arises in powering various types of marine vessel, in which a high velocity turbine is used as the source of power, and this must be coupled via a gear box to a propeller rotating at low speed. One conventional way of providing the gear box needed in such applications is to stack a number of epicyclic gear boxes one on another, but the result, as one would expect, is a gear box which is bulky, heavy, complicated and expensive.
According to the present invention there is provided a gear box comprising first and second coaxial toothed members which have differing radii from one another, one of which members is fixed and one of which is rotatable, third and fourth toothed members which mesh respectively with the first and second toothed members and are rotatable in unison about an axis offset with respect to the axis of the first and second members, input drive means arranged to drive the third and fourth members so that they execute an epicyclic motion with respect to the first and second members, and output drive means drivable by the rotatable one of the first and second members.
Preferably the difference between the radii of the first and second members is relatively small compared to the radius which each of those members has. This provides for a large velocity ratio.
The accompanying drawing shows diagrammatically one form of gear box according to the present invention. This comprises an input shaft 1 which drives a sun gear 2 of the epicyclic gear system. Meshing with the sun gear 2 are a plurality of planetary gears 3. For simplicity of illustration two such gears are shown, though in practice three or more such gears might be provided, or even only a single such gear. The planetary gears 3 also mesh with the inside of a fixed annular gear ring 4. Fixed to each of the planetary gears 3, for rotation in unison therewith, is a further planetary gear 5. The gears 3 should be stronger than the gears 5 as they carry a greater load. The gears 5 mesh with the inside of a second annular ring 6 which is arranged to be rotatable with respect to the ring 4. A bearing 7 is provided to permit this relative rotation.
An input shaft 8 is connected to the ring 6 for rotation thereby. Each of the planetary gears 5 has a stub shaft 9 which is received in a plate 10 common to all the stub shafts. kelative rotation between the stub shaft 9 and the plate 10 is permitted by bearings 11. The plate 10 3150 has a central aperture which receives a stub shaft 12 connected to the sun gear 2, and relative rotation between the stub shafts 12 and the plate 10 is permitted by a bearing 13.
In use, drive provided by the input shaft 1 causes the sun gear 2 to rotate and this in turn causes the planetary gears 3 and 5 to execute an epicyclic movement while meshing with their respective ring gears 4 and 6. Because the ring gears 4 and 6 having differing radii this causes the ring gear 6 to rotate, the ring gear 4 being fixed. Because the difference in the radii is small compared to the radius which each ring gear possesses the rotational speed of the ring gear 6 is small compared to the rotational speed at which the gears 3 and 5 rotate about the axis of the input shaft.The fact that drive to the gears 3 and 5 is provided by a sun gear 2, rather than having these gears driven directly, means that the ratio of the rotational speed tJOUT of the ring gear 6 (and hence of the output shaft 8) to the rotational speed sIN of the input shaft 1 is even lower. These rotational speeds can be expressed by the following relationship:
where r2=radius of gear 2 r3=radius of gear 3 radius of gear 5 If the additional gear reduction provided by the sun gear 2 is not required the gears 3 can be driven directly by an input shaft, and this possibility is indicated diagrammatically by broken lines in the drawing.
In this case the relationship between the rotational speed "'IN of the input shaft to the rotational speed OUT is:
wherein r3 and r5 have the same meanings as before and r2 is the radius of the gap between the gears 3, where the gear 2 was in the previous arrangement.
In the illustrated embodiment in which the ring gear 6 has a greater radius than the ring gear 4, the shaft 8 rotates in the opposite sense to the shaft 1. If the position were reversed, and the ring gear 4 had a greater radius than the ring gear 6, the shafts 1 and 8 would rotate in the same direction.
Various modifications can be made to the embodiment described above. For example, it may be appropriate for the connection between each gear 3 and its respective gear 5 to be made not wholly rigid, so as to allow for some flexing between the two gears. This may be desirable to allow for machining tolerances in the manufacture of the gear box. Also the plate 10 and the stub shafts 9 may be eliminated if instead a free running gear is mounted between the shaft 12 and the gears 5.
Another possible modification is to have the ring gear 4 rotatable and the ring gear 6 fixed, with the output shaft fixed to the ring gear 4. In the construction of this type the input and output shafts are concentric and enter the gear box from the same side.
Also, it would be possible to operate the gear box in such a way as to interchange the functions of the input and output shafts, thus creating, for example, a gear box in which a high velocity increase is achieved. However, there are disadvantages in this, notatably the high friction which results.

Claims (6)

1. A gear box comprising first and second coaxial toothed members which have differing radii from one another, one of which members is fixed and one of which is rotatable, third and fourth toothed members which mesh respectively with the first and second toothed members and are rotatable in unison about an axis offset with respect to the axis of the first and second members, input drive means arranged to drive the third and fourth members so that they execute an epicyclic motion with respect to the first and second members, and output drive means drivable by the rotatable one of the first and second members.
2. A gear box as claimed in claim 1 wherein of the first and second coaxial members the fixed coaxial member is of smaller radius than the rotatable coaxial member.
3. A gear box as claimed in claim 1 wherein of the first and second coaxial members the fixed coaxial member is of larger radius than the rotatable coaxial member.
4. A gear box as claimed in any of claims 1, 2 or 3, wherein the difference between the radii of first and second coaxial members is small in comparison to the radius which each of those members has.
5. A gear box as claimed in any preceding claim wherein the connection between third and fourth toothed members is not wholly rigid.
6. A gear box substantially as herein described and as illustrated in the accompanying drawing.
GB8513033A 1985-05-23 1985-05-23 Gear box Withdrawn GB2175668A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8513033A GB2175668A (en) 1985-05-23 1985-05-23 Gear box

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8513033A GB2175668A (en) 1985-05-23 1985-05-23 Gear box

Publications (2)

Publication Number Publication Date
GB8513033D0 GB8513033D0 (en) 1985-06-26
GB2175668A true GB2175668A (en) 1986-12-03

Family

ID=10579557

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8513033A Withdrawn GB2175668A (en) 1985-05-23 1985-05-23 Gear box

Country Status (1)

Country Link
GB (1) GB2175668A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2704038A1 (en) * 1993-04-16 1994-10-21 Desgardin Marcel Mechanical device for reducing and varying rotational speed.
GB2377740A (en) * 2001-07-19 2003-01-22 Luk Lamellen & Kupplungsbau Electric motor actuator having planetary reduction gear
EP0936382B1 (en) * 1998-02-16 2004-06-16 Moteurs Alexandre S.A. Mechanical device for rotational speed reduction
ES2320082A1 (en) * 2007-11-16 2009-05-18 GAMESA INNOVATION &amp; TECHNOLOGY, SL. Power transmission with high gear ratio, intended for a wind turbine
ES2377697A1 (en) * 2009-05-29 2012-03-30 GAMESA INNOVATION &amp; TECHNOLOGY, S.L. Transmission of high numerical relationship for a wind turbine. (Machine-translation by Google Translate, not legally binding)
FR3011053A1 (en) * 2013-09-24 2015-03-27 Moteurs Alexandre ANGULAR SPEED REDUCING DEVICE
WO2018028204A1 (en) * 2016-08-11 2018-02-15 谭国荣 Pitch-circle differential speed-reduction device

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1021644A (en) * 1961-07-27 1966-03-09 Gross Hans Improvements in and relating to roller shutter electromotive drive units
GB1131962A (en) * 1966-01-12 1968-10-30 Ingersoll Rand Co Improvements in or relating to planetary gear trains and hoists incorporating such gears
GB1488787A (en) * 1975-06-30 1977-10-12 Caterpillar Tractor Co Epicyclic final drive for track-type vehicles
GB1534649A (en) * 1976-11-19 1978-12-06 Caterpillar Tractor Co Floating carrier retention for a planetary gearset
GB1534648A (en) * 1976-11-19 1978-12-06 Caterpillar Tractor Co Planet gear positioning and retaining mechanism
GB2034434A (en) * 1978-10-02 1980-06-04 Jonsson S Planetary gearing
GB2107424A (en) * 1981-10-05 1983-04-27 Metal Box Co Ltd Power-operated can opener having epicyclic reduction gearing

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1021644A (en) * 1961-07-27 1966-03-09 Gross Hans Improvements in and relating to roller shutter electromotive drive units
GB1131962A (en) * 1966-01-12 1968-10-30 Ingersoll Rand Co Improvements in or relating to planetary gear trains and hoists incorporating such gears
GB1488787A (en) * 1975-06-30 1977-10-12 Caterpillar Tractor Co Epicyclic final drive for track-type vehicles
GB1534649A (en) * 1976-11-19 1978-12-06 Caterpillar Tractor Co Floating carrier retention for a planetary gearset
GB1534648A (en) * 1976-11-19 1978-12-06 Caterpillar Tractor Co Planet gear positioning and retaining mechanism
GB2034434A (en) * 1978-10-02 1980-06-04 Jonsson S Planetary gearing
GB2107424A (en) * 1981-10-05 1983-04-27 Metal Box Co Ltd Power-operated can opener having epicyclic reduction gearing

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2704038A1 (en) * 1993-04-16 1994-10-21 Desgardin Marcel Mechanical device for reducing and varying rotational speed.
WO1994024460A1 (en) * 1993-04-16 1994-10-27 Marcel Desgardin Mechanical device for rotation speed reduction, multiplication and variation
EP0936382B1 (en) * 1998-02-16 2004-06-16 Moteurs Alexandre S.A. Mechanical device for rotational speed reduction
GB2377740A (en) * 2001-07-19 2003-01-22 Luk Lamellen & Kupplungsbau Electric motor actuator having planetary reduction gear
ES2320082A1 (en) * 2007-11-16 2009-05-18 GAMESA INNOVATION &amp; TECHNOLOGY, SL. Power transmission with high gear ratio, intended for a wind turbine
WO2009063119A1 (en) * 2007-11-16 2009-05-22 Gamesa Innovation & Technology, S.L. Power transmission with high gear ratio, intended for a wind turbine
ES2377697A1 (en) * 2009-05-29 2012-03-30 GAMESA INNOVATION &amp; TECHNOLOGY, S.L. Transmission of high numerical relationship for a wind turbine. (Machine-translation by Google Translate, not legally binding)
FR3011053A1 (en) * 2013-09-24 2015-03-27 Moteurs Alexandre ANGULAR SPEED REDUCING DEVICE
WO2015044200A3 (en) * 2013-09-24 2015-06-11 Moteurs Alexandre Angular speed reduction device
WO2018028204A1 (en) * 2016-08-11 2018-02-15 谭国荣 Pitch-circle differential speed-reduction device

Also Published As

Publication number Publication date
GB8513033D0 (en) 1985-06-26

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WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)