WO2001046605A1 - Gear and procedure of achievement - Google Patents

Gear and procedure of achievement Download PDF

Info

Publication number
WO2001046605A1
WO2001046605A1 PCT/RO2000/000026 RO0000026W WO0146605A1 WO 2001046605 A1 WO2001046605 A1 WO 2001046605A1 RO 0000026 W RO0000026 W RO 0000026W WO 0146605 A1 WO0146605 A1 WO 0146605A1
Authority
WO
WIPO (PCT)
Prior art keywords
gear
rollers
achievement
wheels
cylindrical
Prior art date
Application number
PCT/RO2000/000026
Other languages
French (fr)
Inventor
St. Constantin Ion
Original Assignee
Ion St Constantin
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 Ion St Constantin filed Critical Ion St Constantin
Priority to AU39608/01A priority Critical patent/AU3960801A/en
Publication of WO2001046605A1 publication Critical patent/WO2001046605A1/en

Links

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
    • F16H1/02Toothed gearings for conveying rotary motion without gears having orbital motion
    • F16H1/04Toothed gearings for conveying rotary motion without gears having orbital motion involving only two intermeshing members
    • F16H1/06Toothed gearings for conveying rotary motion without gears having orbital motion involving only two intermeshing members with parallel axes
    • 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
    • F16H55/10Constructively simple tooth shapes, e.g. shaped as pins, as balls

Definitions

  • the invention refers to a gear and to a procedure of its achievement being used in mechanical transmissions with a heavy operating regime e.g. metalurgical equipment and heavy transport.
  • the gear is provided with tubular rollers instead of cylindrical rollers, which permit the functioning even in case the wheel axis are not rigurously parallel.
  • the gear consists of two parallel gears displaced with helf of a pitch.
  • the rollers are cylindrical or tubular.
  • the procedure for the achievement of the gear consists, according to the invention, in manufacturing the rollers without teething, which are placed on the divider of the teething machine with the dividing circles tangent.
  • the gear shown in fig.5 and 6 according to the invention, consists of the wheels 1 and 2 provided with pockets a distributed uniformly on the wheel 1 and 2 circumference in order to allow the arrangement of cylindrical rollers 3, maintained in the pockets a by means of some caps 5.
  • the caps 4 are fixed axially by means of elastic rings 5 (ZEGER type).
  • the gear consists, in other achievement versions, shown in the figures 7 and 8, of the same constructive elements like the gear in the first version, unlike the fact that instead of cylindrical rollers 3 are used tubular rollers 6 in order to permit to take over the angle tolerances due to manufacturing and mounting.
  • the gear consists in two parallel gears 7 and 8, fixed according to each case.
  • a first assembly of wheels 7 and 8 is displaced with half of a pitch.
  • the displaced parallel gears provide the increase of the covering degree.
  • gear we use cylindrical rollers for the parallel gears, as well as side caps 4 fixed axially with safety rings 5.
  • the gear consists of the same components like the gear shown in fig. 8,10 unlike the fact, that instead the cylindrical rollers 3 are used tubular rollers 6, like in the case of the gear shown in the fig. 7 and 8.
  • the gear of the last achievement version shown in the figures 13 and 14, consists of the same components like the gear in fig. 5 and 6, unlike the fact that instead of the cylindrical rollers and the side caps 4 we use a chain of GALL - type.
  • the achievement procedure of the gear according to the invention consists in the manufacturing of two wheels (wheel - pinion), without outside teething, which are placed on the machine-tool (dividing head) tangent after the dividing circles (equal with the external diameters).
  • machine-tool dividing head
  • tangent point we make a hole along the common generator of the dividing cylinders and implicit parallel to the wheels axis, as it is shown in fig. 1 and 2.

Landscapes

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

Abstract

The gear and the achievement procedure consist in the wheels (1 and 2) which have outside pockets (a) in which we mount: cylindrical rollers (3) in order to form the gear with cylindrical rollers; tubular rollers (6) in order to form the gear with tubular rollers. For the increase of the covering degree of the transmission two parallel gears, displaced with half a pitch have been used. The cylindrical and the tubular rollers are fixed axially with side caps (4). As a constructive version an oilfield chain of GALL-type (10), mounted on the pinion, can be used.

Description

GEAR AND PROCEDURE OF ACHIEVEMENT
The invention refers to a gear and to a procedure of its achievement being used in mechanical transmissions with a heavy operating regime e.g. metalurgical equipment and heavy transport.
The gears with flanks in arc of circle are well known (the holes part in the wheel and the full part in the pinion).
These gears have the disadvantage that they need a high precission machining.
The procedures for the achievement of the gears with NOVICOV teeth (with arc of circle profile) are well known; they consist in teething the wheel by means of a cutter in order to achieve the holes in the wheel and with another cutter we make the teeth with arc of circle profile on the pinion.
These procedure have the disadvantage that they request complicated mechanical machining operations with high casts and high precision.
The problem which appears at the achievement of the gears consists in the appearance of some clearances or blocks between the flanks because of the dimensional tolerances of the processing tools.
The problem has been solved with a gear consisting of wheels which have holes on the circumference, obtained by dividing the teething; in the holes we mount rollers on one of the wheels (pinion).
In order to maintain the rollers in their pockets we use side caps which are fixed axially by safety rings (of ZEGER Type).
In another achievement version the gear is provided with tubular rollers instead of cylindrical rollers, which permit the functioning even in case the wheel axis are not rigurously parallel. In another achievement version the gear consists of two parallel gears displaced with helf of a pitch. The rollers are cylindrical or tubular.
The procedure for the achievement of the gear consists, according to the invention, in manufacturing the rollers without teething, which are placed on the divider of the teething machine with the dividing circles tangent.
In the tangent point along the common generator we make a hole, achieving equal pockets in both wheels.
The invention presents the following advantages:
- it permits the taking over of the axial tolerances from processing and mounting;
- it has a low cost;
- it does not request a high precision.
Further we achieve by dividing, all the holes which form the teeth. The invention will be shown further on in connection with the figures
1 ÷ 14, wh ch represent the following:
- F g. 1, section through the wheels assembly;
- F g. 2, frontal view of the gear;
- F g. 3, frontal view of the gear with all pockets achieved;
- F g. 4, section after plan A-A, ace. to fig. 3 through the gear;
- F g.5, axial section through the gear assembly;
- F g.6, section after plan B-B, ace. to fig. 5 through the gear;
- F g.7, section through the gear in other achievement versions;
- F g.8, section through the gear ace. to fιg.7 after plan C-C;
- F g.9, axial section through the gear in other versions;
- F g.10, section in plan D-D, acc.to fϊg.9 through the gear; - Fig.11 , axial section through the gear in another achievement version;
- Fig.12,section E-E through the gear according to fig.1 1 ;
- Fig.13, axial section through the gear in the last achievement version;
- Fig.14, section after plan F-F, according to fig.13. The gear shown in fig.5 and 6, according to the invention, consists of the wheels 1 and 2 provided with pockets a distributed uniformly on the wheel 1 and 2 circumference in order to allow the arrangement of cylindrical rollers 3, maintained in the pockets a by means of some caps 5. The caps 4 are fixed axially by means of elastic rings 5 (ZEGER type).
According to the invention the gear consists, in other achievement versions, shown in the figures 7 and 8, of the same constructive elements like the gear in the first version, unlike the fact that instead of cylindrical rollers 3 are used tubular rollers 6 in order to permit to take over the angle tolerances due to manufacturing and mounting.
According to the invention, in other achievement versions shown in fig. 9 and 10 the gear consists in two parallel gears 7 and 8, fixed according to each case.
A first assembly of wheels 7 and 8 is displaced with half of a pitch.
The displaced parallel gears provide the increase of the covering degree. In this case of gear we use cylindrical rollers for the parallel gears, as well as side caps 4 fixed axially with safety rings 5.
The limit of axial displacement of the rollers 3 at the inside is given also by the caps 4.
According to the invention, in other achievement versions shown in the figures 11 and 12, the gear consists of the same components like the gear shown in fig. 8,10 unlike the fact, that instead the cylindrical rollers 3 are used tubular rollers 6, like in the case of the gear shown in the fig. 7 and 8.
The gear of the last achievement version, shown in the figures 13 and 14, consists of the same components like the gear in fig. 5 and 6, unlike the fact that instead of the cylindrical rollers and the side caps 4 we use a chain of GALL - type.
The achievement procedure of the gear according to the invention consists in the manufacturing of two wheels (wheel - pinion), without outside teething, which are placed on the machine-tool (dividing head) tangent after the dividing circles (equal with the external diameters). In the tangent point we make a hole along the common generator of the dividing cylinders and implicit parallel to the wheels axis, as it is shown in fig. 1 and 2.
Further we manufacture similarly and succesively the other holes by division in order to achieve the pockets a, in which the cylindric and the tubular rollers will be mounted.

Claims

1. Gear consisting of wheels fixed on shafts, characterized by the fact , that on the outside part of the wheels (1 and 2) some pockets (a) have been provided in which rollers (3 and 6) are mounted, maintained axially by means of caps (4).
2. Assembly, according to the claim 1, characterized by the fact, that the rollers (3 and 6) have a cylindrical or tubular form.
3. Assembly according to the claim 1, characterized by the fact, that it consists of two groups of wheels (7 and 8), which form two parallel gears, displaced by half of a pitch.
4. Assembly according to the claims 1 and 3, characterized by the fact, that in the pocket of the rollers (3 and 6) we use a GALL - chain, pos. (10).
PCT/RO2000/000026 1999-12-20 2000-12-20 Gear and procedure of achievement WO2001046605A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU39608/01A AU3960801A (en) 1999-12-20 2000-12-20 Gear and procedure of achievement

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RO99-01354 1999-12-20
RO99-01354A RO117639B1 (en) 1999-12-20 1999-12-20 Toothed gear and process for manufacturing a gear toothing

Publications (1)

Publication Number Publication Date
WO2001046605A1 true WO2001046605A1 (en) 2001-06-28

Family

ID=20107477

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RO2000/000026 WO2001046605A1 (en) 1999-12-20 2000-12-20 Gear and procedure of achievement

Country Status (3)

Country Link
AU (1) AU3960801A (en)
RO (1) RO117639B1 (en)
WO (1) WO2001046605A1 (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10105835C2 (en) * 2001-02-07 2003-12-24 Karl-Heinz Goebel transmission
DE10328421A1 (en) * 2003-06-25 2005-01-20 Sauer, Marcus, Dipl.-Kaufm. Pin wheel gear has one gearwheel with cycloidal toothing and which in straight toothed form has symmetrical or asymmetrical ground recess, and pins roll on other gearwheel and are fitted in sealed, lifetime lubricated bearings
FR2872560A1 (en) * 2004-07-05 2006-01-06 Buhler Ag Ag Propulsion unit, e.g. for malt germination and kilning tables, has at least one motorised pegged wheel meshing with a toothed crown wheel
WO2006002568A1 (en) * 2004-07-05 2006-01-12 Bühler AG Travelling gear
WO2014023939A1 (en) * 2012-08-08 2014-02-13 Airbus Operations Limited Landing gear drive systems
WO2014023941A1 (en) * 2012-08-08 2014-02-13 Airbus Operations Limited Landing gear drive systems
CN103867688A (en) * 2013-10-11 2014-06-18 北京国网富达科技发展有限责任公司 Gear rack with anticorrosion structure
WO2015033125A1 (en) * 2013-09-05 2015-03-12 Airbus Operations Limited Landing gear drive system flexible interface
DE102014208418A1 (en) 2014-05-06 2015-11-12 Schaeffler Technologies AG & Co. KG Rolling gear
CN106068407A (en) * 2014-03-05 2016-11-02 空中客车英国运营有限责任公司 Drive system and drive system connection control method for undercarriage
US10093413B2 (en) 2014-02-13 2018-10-09 Airbus Operations Limited Drive system for aircraft landing gear
US10124887B2 (en) 2014-03-14 2018-11-13 Airbus Operations Limited Landing gear drive system and method
US10144506B2 (en) 2014-03-17 2018-12-04 Airbus Operations Limited Drive system for aircraft landing gear

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE416050C (en) * 1923-03-16 1925-07-04 Alexander Fraser Mackay Interlocking
US1914797A (en) * 1931-12-14 1933-06-20 Clarence P Baker Roller gearing
DE807576C (en) * 1950-01-31 1951-07-02 Emil Emde Toothed rolling gear
FR2091648A5 (en) * 1970-05-28 1972-01-14 Dso Cherna Metalurgia
US3974710A (en) * 1975-06-02 1976-08-17 Granger Wallace H Gear drive for rotary press and the like
DE29910033U1 (en) * 1999-06-09 1999-08-05 Landgraf Richard Gear with rolling elements

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE416050C (en) * 1923-03-16 1925-07-04 Alexander Fraser Mackay Interlocking
US1914797A (en) * 1931-12-14 1933-06-20 Clarence P Baker Roller gearing
DE807576C (en) * 1950-01-31 1951-07-02 Emil Emde Toothed rolling gear
FR2091648A5 (en) * 1970-05-28 1972-01-14 Dso Cherna Metalurgia
US3974710A (en) * 1975-06-02 1976-08-17 Granger Wallace H Gear drive for rotary press and the like
DE29910033U1 (en) * 1999-06-09 1999-08-05 Landgraf Richard Gear with rolling elements

Cited By (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10105835C2 (en) * 2001-02-07 2003-12-24 Karl-Heinz Goebel transmission
DE10328421A1 (en) * 2003-06-25 2005-01-20 Sauer, Marcus, Dipl.-Kaufm. Pin wheel gear has one gearwheel with cycloidal toothing and which in straight toothed form has symmetrical or asymmetrical ground recess, and pins roll on other gearwheel and are fitted in sealed, lifetime lubricated bearings
AU2005259749B2 (en) * 2004-07-05 2011-09-01 Buhler Ag Travelling gear
FR2872560A1 (en) * 2004-07-05 2006-01-06 Buhler Ag Ag Propulsion unit, e.g. for malt germination and kilning tables, has at least one motorised pegged wheel meshing with a toothed crown wheel
JP2008505285A (en) * 2004-07-05 2008-02-21 ビューラー・アクチエンゲゼルシャフト Travel drive device
WO2006002568A1 (en) * 2004-07-05 2006-01-12 Bühler AG Travelling gear
US8502119B2 (en) 2004-07-05 2013-08-06 Buehler Ag Travel drive
CN104520185A (en) * 2012-08-08 2015-04-15 空中客车营运有限公司 Landing gear drive systems
WO2014023941A1 (en) * 2012-08-08 2014-02-13 Airbus Operations Limited Landing gear drive systems
US9908621B2 (en) 2012-08-08 2018-03-06 Airbus Operations Limited Landing gear drive systems
WO2014023939A1 (en) * 2012-08-08 2014-02-13 Airbus Operations Limited Landing gear drive systems
US9738376B2 (en) 2012-08-08 2017-08-22 Airbus Operations Limited Landing gear drive systems
CN104520186A (en) * 2012-08-08 2015-04-15 空中客车营运有限公司 Landing gear drive systems
JP2015530305A (en) * 2012-08-08 2015-10-15 エアバス オペレーションズ リミテッドAirbus Operations Limited Landing gear drive system
JP2015530304A (en) * 2012-08-08 2015-10-15 エアバス オペレーションズ リミテッドAirbus Operations Limited Landing gear drive system
RU2643857C2 (en) * 2012-08-08 2018-02-06 Эрбас Оперэйшнс Лимитед Chassis drive system
RU2643114C2 (en) * 2012-08-08 2018-01-30 Эрбас Оперэйшнс Лимитед Chassis drive system (versions)
EP3260368A1 (en) * 2012-08-08 2017-12-27 Airbus Operations Limited Landing gear drive systems
US9469397B2 (en) 2012-08-08 2016-10-18 Airbus Operations Limited Landing gear drive systems
EP3241745A1 (en) * 2012-08-08 2017-11-08 Airbus Operations Limited Landing gear drive systems
CN107719650A (en) * 2013-09-05 2018-02-23 空中客车英国运营有限责任公司 Drive system for the undercarriage of aircraft
JP2016533966A (en) * 2013-09-05 2016-11-04 エアバス オペレーションズ リミテッドAirbus Operations Limited Flexible interface for landing gear drive system
EP4215438A1 (en) * 2013-09-05 2023-07-26 Airbus Operations Limited Landing gear drive system flexible interface
US10864984B2 (en) 2013-09-05 2020-12-15 Airbus Operations Limited Landing gear drive system flexible interface
CN105517895A (en) * 2013-09-05 2016-04-20 空中客车营运有限公司 Landing gear drive system flexible interface
US9884678B2 (en) 2013-09-05 2018-02-06 Airbus Operations Limited Landing gear drive system flexible interface
EP3581487A1 (en) * 2013-09-05 2019-12-18 Airbus Operations Limited Landing gear drive system flexible interface
WO2015033125A1 (en) * 2013-09-05 2015-03-12 Airbus Operations Limited Landing gear drive system flexible interface
CN103867688A (en) * 2013-10-11 2014-06-18 北京国网富达科技发展有限责任公司 Gear rack with anticorrosion structure
US10093413B2 (en) 2014-02-13 2018-10-09 Airbus Operations Limited Drive system for aircraft landing gear
US10196134B2 (en) 2014-02-13 2019-02-05 Airbus Operations Limited Drive system for aircraft landing gear
US10611470B2 (en) 2014-02-13 2020-04-07 Airbus Operations Limited Drive system for aircraft landing gear
US10112703B2 (en) 2014-03-05 2018-10-30 Airbus Operations Limited Drive system for landing gear and drive system control method
CN106068407A (en) * 2014-03-05 2016-11-02 空中客车英国运营有限责任公司 Drive system and drive system connection control method for undercarriage
US10124887B2 (en) 2014-03-14 2018-11-13 Airbus Operations Limited Landing gear drive system and method
US10144506B2 (en) 2014-03-17 2018-12-04 Airbus Operations Limited Drive system for aircraft landing gear
DE102014208418A1 (en) 2014-05-06 2015-11-12 Schaeffler Technologies AG & Co. KG Rolling gear
DE102014208418B4 (en) * 2014-05-06 2016-07-28 Schaeffler Technologies AG & Co. KG Rolling gear

Also Published As

Publication number Publication date
RO117639B1 (en) 2002-05-30
AU3960801A (en) 2001-07-03

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