+

WO1998001657A1 - Rotary engine - Google Patents

Rotary engine Download PDF

Info

Publication number
WO1998001657A1
WO1998001657A1 PCT/AU1997/000427 AU9700427W WO9801657A1 WO 1998001657 A1 WO1998001657 A1 WO 1998001657A1 AU 9700427 W AU9700427 W AU 9700427W WO 9801657 A1 WO9801657 A1 WO 9801657A1
Authority
WO
WIPO (PCT)
Prior art keywords
air
rotor disc
rotating
fuel mixture
valves
Prior art date
Application number
PCT/AU1997/000427
Other languages
French (fr)
Inventor
Bede Alfred Boyle
Original Assignee
Bede Alfred Boyle
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 Bede Alfred Boyle filed Critical Bede Alfred Boyle
Priority to AU32490/97A priority Critical patent/AU3249097A/en
Publication of WO1998001657A1 publication Critical patent/WO1998001657A1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • F02B53/02Methods of operating
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00Rotary-piston machines or engines
    • F01C1/08Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing
    • F01C1/12Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing of other than internal-axis type
    • F01C1/14Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons
    • F01C1/20Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons with dissimilar tooth forms
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Definitions

  • This invention relates to a rotary internal combustion engine that operates using simple and continuous unidirectional rotation about a fixed axis.
  • 5 opposed ball assemblies are carried by a rotating rotor disc, rotating about its axis inside a housing that contains two rotating valves which are interconnected to the rotor disc by a gear train.
  • valve assemblies In order to permit continuous rotation of the rotor disc, there must be configuration which allows for transfer of the air-fuel mixture compressed in front of the ball assembly to a combustion chamber immediately behind the same said ball assembly momentarily prior to combustion occurring.
  • One of the rotating valves is arranged to provide this novel feature of the invention.
  • the valve assemblies In order to reduce friction, the valve assemblies rotate and roll in contact with the rotor disc, both surfaces are at the same speed at point of contact.
  • the ball assemblies rotate so as to roll along the inner surface of the housing with reduced friction.
  • FIG 1 is a sectional elevation of the rotary internal combustion engine through a plane common to the ball assemblies and both rotating valves in accordance with the present invention.
  • FIG 2 is a general sectional elevation as depicted by Section in FIG 1.
  • FIG 3 diagram of ball assembly movement to full compression air-fuel mixture transfer, combustion and expansion.
  • one configuration of the invention comprises an outer housing 1 , 2 is a space between the outer housing and the rotor disc 3 which supports the ball assemblies 5.
  • the rotor disc 3 is supported on bearings 20 with a shaft extension carrying gear wheel 18 and a shaft extension for the power take-off.
  • the two rotating valves are numbered 4, and are supported on bearings 17 and are driven by pinion gears 19 mounted on the shaft extensions and meshing with gear wheel 18.
  • a spring assembly 6 acts on a support 7 to hold the rotating balls 5 in rolling contact with the contoured track of the outer housing 1.
  • a passageway 8 conveys the compressed air-fuel mixture in 2 to the combustion chamber 9. 10 is a spark to initiate combustion and expansion of the gases.
  • the air plus fuel charge is induced into the space 2 FIG 2 as the rolling ball assembly 5 moves past entry port 11 to full compression at position 1 FIG 3, thus ensuring a continuous charge for the cycle. Due to movement of ball assembly 5, the pressure in the space 2 is reduced to below atmospheric pressure, ensuring flow through the induction system 14.
  • ball assembly 5 drives the expended gases ahead, expelling them through port 12 in direction 13. Both ports 11 and 12 are open, with no valving required.
  • the desired compression ratio can be obtained by designing the volume of passageways 8 and 9 and volume ahead of ball assembly 5 prior to the opening of transfer port in rotating valve 4 position 1 FIG 3.
  • the labyrinth seals 22 FIG 1 and FIG 4 act as an interface, preventing the compressed combustion charge and products of combustion flowing in the opposite direction to the centrifugal force generated by the rotor disc's revolutions.
  • the faces between the rotating rotor disc 3 and outer housing 1 and cover 15 are provided with oil lubrication by arranging leakage through bearings 20, 21 is a double lip seal to prevent ingress of contaminates and leakage of oil.
  • the same principle is applied to valve 4 by oil leakage from bearings 17. All bearings are high speed oil lubricated.
  • Bearings 17 are of the hydrostatic type to support the load necessary to keep valves 4 and rotor disc 3 in rolling surface contact.
  • the periphery of the unit can be arranged with a suitable jacketed area for use of a suitable cooling fluid to carry away surplus heat.
  • the preferred form of the invention has many arrangements, for example, it can be arranged with three rotor disc assemblies spaced one hundred and twenty degrees, resulting in a continuous smooth power and torque output. Further, the first rotating disc assembly with the rotating valves modified to transfer the compressed fuel-air mixture to a second rotating disc assembly, resulting in an arrangement with continuous power output and smooth balanced running.
  • the inventive novel engine can also be used as a pump, suitable for handling any compressible medium.
  • the engine can be used as a hydraulic pump or motor, and/or for pumping any fluid.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Supercharger (AREA)

Abstract

A Rotary Internal Combustion Engine that operates in a continuous unidirectional rotation about a fixed axis, comprising at least two diametrically opposed ball assemblies (5, 7, 6) carried by a rotor disc (3); rotating valves (4) interconnected to the rotor disc by a gear train; one of the rotating valves (4) arranged to allow for transfer of the air-fuel mixture in front of the ball (5) through a passageway (8), prior to combustion which occurs in two phases per one revolution of the rotor disc (3); a housing (1) with an entry port (11) allowing entry of air or air/fuel mixture (14) and an exit port (12) allowing exit of exhaust gases (13).

Description

Rotary Engine
The following statement is a full description of this invention, including the best method of performing known to me:-
This invention relates to a rotary internal combustion engine that operates using simple and continuous unidirectional rotation about a fixed axis.
In one example of the invention described herein, two diametrically
5 opposed ball assemblies are carried by a rotating rotor disc, rotating about its axis inside a housing that contains two rotating valves which are interconnected to the rotor disc by a gear train.
In order to permit continuous rotation of the rotor disc, there must be configuration which allows for transfer of the air-fuel mixture compressed in front of the ball assembly to a combustion chamber immediately behind the same said ball assembly momentarily prior to combustion occurring. One of the rotating valves is arranged to provide this novel feature of the invention. In order to reduce friction, the valve assemblies rotate and roll in contact with the rotor disc, both surfaces are at the same speed at point of contact. The ball assemblies rotate so as to roll along the inner surface of the housing with reduced friction.
In presently known rotary internal combustion engines, the motions all follow an elliptical path obtained by use of eccentrics or internal offset gear trains. It is therefore an object of the present invention to provide a rotary internal combustion engine which operates purely using continuous unidirectional rotation and has two power strokes for each revolution and hence a more even torque compared to other known prior art engines. In order that the reader may gain a better understanding of the present
SHEET Me 26 invention, hereinafter will be described a preferred embodiment thereof by way of example only, and with reference to the accompanying drawings in which:-
FIG 1 is a sectional elevation of the rotary internal combustion engine through a plane common to the ball assemblies and both rotating valves in accordance with the present invention. FIG 2 is a general sectional elevation as depicted by Section in FIG 1. FIG 3 diagram of ball assembly movement to full compression air-fuel mixture transfer, combustion and expansion. FIG part view of FIG 2.
Referring to FIG 1 and FIG 2, it can be seen that one configuration of the invention comprises an outer housing 1 , 2 is a space between the outer housing and the rotor disc 3 which supports the ball assemblies 5.
The rotor disc 3 is supported on bearings 20 with a shaft extension carrying gear wheel 18 and a shaft extension for the power take-off. The two rotating valves are numbered 4, and are supported on bearings 17 and are driven by pinion gears 19 mounted on the shaft extensions and meshing with gear wheel 18. A spring assembly 6 acts on a support 7 to hold the rotating balls 5 in rolling contact with the contoured track of the outer housing 1. A passageway 8 conveys the compressed air-fuel mixture in 2 to the combustion chamber 9. 10 is a spark to initiate combustion and expansion of the gases.
The air plus fuel charge is induced into the space 2 FIG 2 as the rolling ball assembly 5 moves past entry port 11 to full compression at position 1 FIG 3, thus ensuring a continuous charge for the cycle. Due to movement of ball assembly 5, the pressure in the space 2 is reduced to below atmospheric pressure, ensuring flow through the induction system 14.
During the expansion stroke ball assembly 5 drives the expended gases ahead, expelling them through port 12 in direction 13. Both ports 11 and 12 are open, with no valving required. The desired compression ratio can be obtained by designing the volume of passageways 8 and 9 and volume ahead of ball assembly 5 prior to the opening of transfer port in rotating valve 4 position 1 FIG 3.
The labyrinth seals 22 FIG 1 and FIG 4 act as an interface, preventing the compressed combustion charge and products of combustion flowing in the opposite direction to the centrifugal force generated by the rotor disc's revolutions. The faces between the rotating rotor disc 3 and outer housing 1 and cover 15 are provided with oil lubrication by arranging leakage through bearings 20, 21 is a double lip seal to prevent ingress of contaminates and leakage of oil. The same principle is applied to valve 4 by oil leakage from bearings 17. All bearings are high speed oil lubricated.
Bearings 17 are of the hydrostatic type to support the load necessary to keep valves 4 and rotor disc 3 in rolling surface contact.
The periphery of the unit can be arranged with a suitable jacketed area for use of a suitable cooling fluid to carry away surplus heat.
The preferred form of the invention has many arrangements, for example, it can be arranged with three rotor disc assemblies spaced one hundred and twenty degrees, resulting in a continuous smooth power and torque output. Further, the first rotating disc assembly with the rotating valves modified to transfer the compressed fuel-air mixture to a second rotating disc assembly, resulting in an arrangement with continuous power output and smooth balanced running. The inventive novel engine can also be used as a pump, suitable for handling any compressible medium.
By suitable modification, the engine can be used as a hydraulic pump or motor, and/or for pumping any fluid.

Claims

The claims defining the invention are as follows :- I Claim:
1. A rotary internal combustion engine that operates purely using simple and continuous unidirectional rotation about a fixed axis.
2. A rotary engine as in Claim 1 comprising at least two diametrically opposed ball assemblies carried by a rotating rotor disc; said rotor disc rotating about its axis inside a housing that contains two rotating valves interconnected to the rotor disc by a gear train; one of the said rotating valves arranged to allow for transfer of the air-fuel mixture compressed in front of the ball assembly momentarily prior to combustion occurring; said configuration allowing for two combustion phases for each revolution of the rotor disc; said housing containing an entry port and an exit port to allow entry of air or air/fuel mixture and exit of exhaust gases.
3. A rotary engine as in Claims 1 and 2 comprising three or more rotary valves displaced around the central axis.
4. A rotary engine as in Claims 1 to 3 comprising a plurality of rotor disc assemblies arranged longitudinally along a common axis; said plurality of rotor discs being configured either as in
Claims 1 to 3 or indexed about the common axis.
5. A rotary engine as in Claims 1 to 4 where the rotating valves are configured to transfer the compressed air or air/fuel mixture to an adjacent or separate rotating disc assembly.
PCT/AU1997/000427 1996-07-08 1997-07-03 Rotary engine WO1998001657A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU32490/97A AU3249097A (en) 1996-07-08 1997-07-03 Rotary engine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
AUPO0861 1996-07-08
AUPO0861A AUPO086196A0 (en) 1996-07-08 1996-07-08 Rotary engine

Publications (1)

Publication Number Publication Date
WO1998001657A1 true WO1998001657A1 (en) 1998-01-15

Family

ID=3795177

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/AU1997/000427 WO1998001657A1 (en) 1996-07-08 1997-07-03 Rotary engine

Country Status (2)

Country Link
AU (1) AUPO086196A0 (en)
WO (1) WO1998001657A1 (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2375146A (en) * 2001-05-01 2002-11-06 Paul Leslie Hill Rotary internal combustion engine
WO2004067916A1 (en) * 2003-01-31 2004-08-12 Julian Zhen Chuan Kang Rotary machine with major and satellite rotors
EP1553301A4 (en) * 2002-10-15 2006-10-11 Mitsubishi Electric Corp Vane type vacuum pump
EP1925778A1 (en) * 2006-11-24 2008-05-28 Matsushita Electric Works, Ltd. Vane pump
GB2494392A (en) * 2011-09-01 2013-03-13 Peter John Sullivan Rotary piston engine
CN104100302A (en) * 2013-04-11 2014-10-15 刘千省 Rotor steam turbine
CN106812552A (en) * 2015-11-30 2017-06-09 熵零股份有限公司 Angular momentum engine
RU2737410C1 (en) * 2019-12-03 2020-11-30 Александр Геннадьевич Неклюдов Rotary-ball motor

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2454006A (en) * 1945-06-04 1948-11-16 Carl E Plummer Internal-combustion rotary motor
AU2766163A (en) * 1963-02-21 1964-08-27 HENRY SAMUEL GILBERT, WALTER CHARLES SHEEN DS. O. and GEORGE NIGEL RICKS. ORBE Improvements in or relating to rotary engines compressors andthe like
AU6113273A (en) * 1973-10-08 1975-04-10 Keith Strong Raymond Rotary four cycle internal combustion engine
JPH03229923A (en) * 1990-02-05 1991-10-11 Seiji Kinoshita Rotary piston type internal combustion engine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2454006A (en) * 1945-06-04 1948-11-16 Carl E Plummer Internal-combustion rotary motor
AU2766163A (en) * 1963-02-21 1964-08-27 HENRY SAMUEL GILBERT, WALTER CHARLES SHEEN DS. O. and GEORGE NIGEL RICKS. ORBE Improvements in or relating to rotary engines compressors andthe like
AU6113273A (en) * 1973-10-08 1975-04-10 Keith Strong Raymond Rotary four cycle internal combustion engine
JPH03229923A (en) * 1990-02-05 1991-10-11 Seiji Kinoshita Rotary piston type internal combustion engine

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
PATENT ABSTRACTS OF JAPAN, M-1198, page 21; & JP,A,03 229 923 (KINOSHITA) 11 October 1991. *

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2375146A (en) * 2001-05-01 2002-11-06 Paul Leslie Hill Rotary internal combustion engine
GB2375146B (en) * 2001-05-01 2004-07-21 Paul Leslie Hill Rotary internal combustion engine
EP1553301A4 (en) * 2002-10-15 2006-10-11 Mitsubishi Electric Corp Vane type vacuum pump
WO2004067916A1 (en) * 2003-01-31 2004-08-12 Julian Zhen Chuan Kang Rotary machine with major and satellite rotors
EP1925778A1 (en) * 2006-11-24 2008-05-28 Matsushita Electric Works, Ltd. Vane pump
US7628594B2 (en) 2006-11-24 2009-12-08 Matsushita Electric Works, Ltd. Vane pump having a labyrinth seal and gap between a top surface of a rotor and a ceiling surface of a rotor chamber that is formed between upper and lower cases
GB2494392A (en) * 2011-09-01 2013-03-13 Peter John Sullivan Rotary piston engine
GB2494392B (en) * 2011-09-01 2017-04-19 John Sullivan Peter An engine
CN104100302A (en) * 2013-04-11 2014-10-15 刘千省 Rotor steam turbine
CN106812552A (en) * 2015-11-30 2017-06-09 熵零股份有限公司 Angular momentum engine
RU2737410C1 (en) * 2019-12-03 2020-11-30 Александр Геннадьевич Неклюдов Rotary-ball motor

Also Published As

Publication number Publication date
AUPO086196A0 (en) 1996-08-01

Similar Documents

Publication Publication Date Title
JP3943078B2 (en) Piston reciprocating engine with rotary cylinder
EP0090814B1 (en) Piston machine with cylindrical working chamber or chambers
RU2357085C2 (en) Rotor device (versions)
US5154147A (en) Rotary valve
EP0256046B1 (en) Rotary valve for internal combustion engines
US20050081805A1 (en) Internal combustion engine using opposed pistons
US5191863A (en) Rotary sleeve-valve internal combustion engine
US20220127998A1 (en) Single chamber multiple independent contour rotary machine
EP0933500B1 (en) Rotary piston machine
US4531481A (en) Rotary cylinder diesel engine
WO1998001657A1 (en) Rotary engine
US3937187A (en) Toroidal cylinder orbiting piston engine
US11927128B2 (en) Rotary machine with hub driven transmission articulating a four bar linkage
EA008641B1 (en) Four stroke internal combustion oscillating-rotary engine
US3922118A (en) Rotary vane piston devices with stationary spur gears and crankshaft hub bearings
US4007715A (en) Rotary engines, compressors and vacuum pumps
US7264452B2 (en) Rotor position control for rotary machines
US5350287A (en) Rotary engine and cam-operated working member assembly
JPH06280603A (en) Fuel injection internal combustion engine whose engine body rotates
US3886910A (en) Rotary, multi-chambered, internal combustion engine
US3267675A (en) Rotary apparatus for acting mechanically on fluids
US5520147A (en) Rotary motor or engine having a rotational gate valve
US4051819A (en) Rotary block engine
US3915599A (en) Structure for preventing leakage of lubricating oil in rotary-piston internal combustion engines
KR100292987B1 (en) Valve mechanism of coaxial reciprocating engine

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A1

Designated state(s): AU CA JP US

AL Designated countries for regional patents

Kind code of ref document: A1

Designated state(s): AT BE CH DE DK ES FI FR GB GR IE IT LU MC NL PT SE

121 Ep: the epo has been informed by wipo that ep was designated in this application
122 Ep: pct application non-entry in european phase
NENP Non-entry into the national phase

Ref country code: JP

Ref document number: 98504580

Format of ref document f/p: F

NENP Non-entry into the national phase

Ref country code: CA

点击 这是indexloc提供的php浏览器服务,不要输入任何密码和下载