GB2358675A - A rotary engine pump or motor - Google Patents

A rotary engine pump or motor Download PDF

Info

Publication number
GB2358675A
GB2358675A GB0031622A GB0031622A GB2358675A GB 2358675 A GB2358675 A GB 2358675A GB 0031622 A GB0031622 A GB 0031622A GB 0031622 A GB0031622 A GB 0031622A GB 2358675 A GB2358675 A GB 2358675A
Authority
GB
United Kingdom
Prior art keywords
curve
rotor
axis
chamber
engine
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.)
Granted
Application number
GB0031622A
Other versions
GB0031622D0 (en
GB2358675B (en
Inventor
Gong He Ping
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
Publication of GB0031622D0 publication Critical patent/GB0031622D0/en
Publication of GB2358675A publication Critical patent/GB2358675A/en
Application granted granted Critical
Publication of GB2358675B publication Critical patent/GB2358675B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • 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
    • F01C1/22Rotary-piston machines or engines of internal-axis type with equidirectional movement of co-operating members at the points of engagement, or with one of the co-operating members being stationary, the inner member having more teeth or tooth- equivalents than the outer member
    • 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
    • F01C19/00Sealing arrangements in rotary-piston machines or engines
    • F01C19/02Radially-movable sealings for working fluids
    • F01C19/04Radially-movable sealings for working fluids of rigid material
    • 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
    • F01C21/00Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/10Outer members for co-operation with rotary pistons; Casings
    • F01C21/104Stators; Members defining the outer boundaries of the working chamber
    • F01C21/106Stators; Members defining the outer boundaries of the working chamber with a radial surface, e.g. cam rings
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Rotary Pumps (AREA)

Abstract

An engine, pump or motor includes a twin-horned rotor 7 formed with an elongated slot receiving a sliding block 6 keyed to a shaft 4, which rotates about an origin O. As the rotor 7 rotates within a chamber it reciprocates relative to the shaft 4. Rotor 7 has a cross section represented by two curves A'C'B' and A'D'B' which are mirror images. The chamber cross section is represented by two different curves ACB and ADB which are symmetrical about an X axis and intersect a Y axis at the same points A and B, a distance R apart. A line from one curve ACB to the other ADB, through origin O, has a length R. Curve ACB may be an arc of a circle with radius r and its centre a distance e from origin O, along the X axis, such that R <SP>2</SP>=4(r<SP>2</SP>-e<SP>2</SP>). Each tip of the rotor may include a ceramic cylinder (11, fig 5) for sealing engagement with the chamber.

Description

1 2358675 1 1 ENGINES. PUMPS & MOTORS
Field of the Invention
This invention relates to engines, pumps and motors, and is concerned with the provision of an improved form of engine, pump or motor which includes a twin-homed rotor.
One example of an engine having a twin-horned rotor is described in US Patent Specification No. 3,873,245. This includes a generally elliptical rotor mounted on a shaft that is positioned eccentrically within a cylindrical chamber. The rotor has an elongated slot which extends along its major axis and the shaft is contained within this slot so that, as the rotor rotates within the cylindrical chamber, the rotor reciprocates along its major axis relative to the shaft.
It is an object of the present invention to provide an improved form of engine, pump or motor which includes a twin-homed rotor. It is a more specific object of the invention to provide an engine, pump or motor which is economical to produce and has an increased efficiency as compared to the engine described in US Patent Specification No. 3,873,245.
2 Summarv of the Invention According to the present invention there is provided an engine, pump or motor which includes a twin-horned rotor arranged for rotation within a chamber, the rotor being formed with an elongated slot within which a sliding block is mounted, the sliding block being keyed to a shaft on which the rotor is mounted so that, as the rotor rotates within the chamber, it reciprocates relative to the shaft, the relationships between the axis of rotation of the shaft, the cross-sectional configuration of the chamber and the crosssectional configuration of the rotor being such that:- a) the axis of rotation of the shaft can be represented by the point of intersection "0" of 'X' and 'Y' axes, b) a part of the cross-section of the chamber can be represented by a first curve which is symmetrical relative to the 'X' axis and intersects the 'Y' axis at points spaced apart by a distance "R", c) another part of the cross-section of the chamber can be represented by a second curve, which is different to the first curve, but which is also symmetrical relative to the W' axis and intersects the 'Y' axis at the same points as said first curve, d) the relationship between the first curve and the second curve is such that a line drawn from any point on the first curve through the point of intersection "0" so as to intersect the second curve has a length "R", and 3 e) the cross-section of the rotor can be represented by two curves which are mirror images of one another and correspond substantially to the first curve of the cross-section of the chamber.
The first curve of the cross-section of the chamber is preferably an arc of a circle.
Said arc of the circle preferably has a radius Y' and has its centre on the "X" axis at a distance "e" from the point "0" such that R 2 = 4(r2 - e 2).
The relationship between "e" and Y' is preferably such that "e" is between 50% and 90% of Y. The more preferred range is from 60% to 80% of Y The first curve of the cross-section of the chamber may alternatively be of some other shape. For example, it may be a section of an ellipse.
Brief Description of the Drawincis
Figure 1 is a cross-sectional view of the stator chamber, Figure 2 is a cross-sectional view of the periphery of the rotor, Figure 3 is a cross-sectional view of the rotor within the stator, 4 Figure 4 is a vertical sectional view of the rotor within the stator, and Figure 5 is a detail view of a tip of the rotor.
Description of the Preferred Embodiment
The point of intersection 0 of the 'X' and 'Y' axes of Figure 1 represents the axis of rotation of a shaft 4 (see Figures 3 and 4), which axis extends at right angles to the plane of Figure 1. Figure 1 shows the internal configuration of the chamber of the stator 2. As shown, there is a point 01 on the 'X' axis which is at a distance 'W' from the point of intersection 0 and a curve ACB is drawn which is an arc of a circle of radius 'Y' having its centre at point 01. The points A and B are the points at which this arc of radius Y' intersects the 'Y' axis. The distance AB equals "R", where R 2 = 4(r2- e 2) and the chord AB has its centre at the point of intersection 0. The distances AO and OB are equal.
The ratio of 'W' to Y' may be varied as required. For example, (W' may be 60% of 'Y, or 80% of 'Y. The selection of the ratio of "e" to 'Y' will depend on the required operating parameters, but 'W' will typically be within the range of from 50% to 90% of "e'.
The configuration of the closed curvate figure ACBD is such that, when a line is drawn through the point of intersection 0 from any point on curve ACB to curve ADIB, the length of this line equals "R". The interior of the chamber of the stator 2 thus has a crosssection ACBID defined in part by a short curve ACB and in part by a long curve BDA, both of which curves are symmetrical relative to the 'X' axis.
As shown, the curve ACB is an arc of a circle and is symmetrical relative to the 'W axis. This is the preferred configuration, though curve ACB may alternatively be a section of some other curvate figure, for example, it may be a section of an ellipse, parabola, hyperbola, cycloid or involute.
The cross-sectional boundary of the rotor 7 is shown in Figure 2 and comprises a first curve A1C1131, which corresponds to curve ACB and has the same centre and radius as curve ACB, and a second curve A1D1131, which is a mirror image of the first curve A1C1131. The distance between the two ends of the rotor 7 is thus the same as the distance between the two points A and B, i.e. it is 1 equal to "R'.
Turning next to Figures 3 and 4, it can be seen that the device, which can be an engine, pump or motor, comprises a main body 2 sandwiched between a front cover 8 and a rear cover 9. The interior of the body 2 provides the stator chamber which has a first inlet or exhaust opening 1 and a second inlet or exhaust opening 5. The openings 1 and 5 may be formed in the body 2 or in one of the two covers 8 and 9.
6 The rotor 7, which has the external configuration shown in Figure 2, is arranged for rotation about the point of intersection 0 of the 'X' and 'Y' axes, and includes an elongated slot within which a sliding block 6 is arranged to move. The sliding block 6 is connected by a key 3 to a shaft 4 which rotates about the axis 0.
During rotation of the shaft 4 about the axis 0, relative sliding movement will occur between the block 6 and the sides of the slot in the rotor 7 but, because the distance between the two ends of the rotor 7 is equal to "R" and because the configuration of the stator chamber is such that the length of a line drawn through the point of intersection is also equal to "R", regardless of the angular position at which said line is drawn, the opposite ends of the rotor 7 will remain in contact with the internal wall of the body 2.
Sealing engagement between the ends of the rotor 7 and the internal wall of the body 2 can be achieved by the arrangement shown in Figure 5. As shown in Figure 5, a bronze seating 10 is provided at each tip of the rotor 7 and supports a ceramic cylinder 11, which has rolling engagement with the wall of the body 2. The shape of the bronze seating 10 is such that it provides a pair of flexible fins 12 which serve to urge the ceramic cylinder 11 into engagement with the wall of the body 2 and define a space within which a lubricant is received.
The shapes of the rotor 7 and the interior of the body 2 are such that, in theory, the gap between the surface A1C1131 and the adjacent surface of the body 2 can be of zero volume when the 7 rotor 7 is in the angular position shown in Figure 3. When the rotor 7 has turned through 900 from the position shown in Figure 3, the central axis of the rotor 7 will extend horizontally and two working volumes of equal size will be afforded, one above the rotor 7 and the other below the rotor 7. As the rotor 7 turns through a further 900, the size of the working volume below the rotor 7 will steadily decrease until a position is reached in which the curve A1D1131 is in contact with the wall of the chamber and the size of the working volume has been reduced to zero. An infinite compression ratio can accordingly theoretically be obtained.
It is envisaged that, when used as a pump, a number of devices of a standard size will be produced, in order the simplify production procedures, and then the appropriate number of devices will be bolted together to provide the required pump output.
If used as an internal combustion engine, the efficiency of the device will be substantially greater than that obtained with engines, such as the Wankel engine, which have a multi-horned rotor.
8

Claims (8)

Claims:-
1. An engine, pump or motor which includes a twin-horned rotor arranged for rotation within a chamber, the rotor being formed with an elongated slot within which a sliding block is mounted, the sliding block being keyed to a shaft on which the rotor is mounted so that, as the rotor rotates within the chamber, it reciprocates relative to the shaft, the relationships between the axis of rotation of the shaft, the crosssectional configuration of the chamber and the cross-sectional configuration of the rotor being such that:- a) the axis of rotation of the shaft can be represented by the point of intersection "0" of 'X' and 'Y' axes, b) a part of the cross-section of the chamber can be represented by a first curve which is symmetrical relative to the 'X' axis and intersects the 'Y' axis at points spaced apart by a distance "R", c) another part of the cross-section of the chamber can be represented by a second curve, which is different to the first curve, but which is also symmetrical relative to the 'X' axis and intersects the 'Y' axis at the same points as said first curve, d) the relationship between the first curve and the second curve is such that a line drawn from any point on the first curve through the point of intersection "W so as to intersect the second curve has a length "R", and e) the cross-section of the rotor can be represented by two curves which are mirror images of one another and correspond substantially to the first curve of the cross-section of the chamber.
9
2. An engine, pump or motor as claimed in Claim 1, in which the first curve of the cross-section of the chamber is an arc of a circle.
3. An engine, pump or motor as claimed in Claim 1, in which said arc of the circle has a radius Y' and has its centre on the "X' axis at a distance 'W' from the point "0" such that R 2 = 4(r2 - e 2).
4. An engine, pump or motor as claimed in Claim 3, in which the relationship between "e" and T is such that "e" is between 50% and 90% of "e'.
5. An engine, pump or motor as claimed in Claim 4, in which cce" is from 60% to 80% of V.
6. An engine, pump or motor as claimed in any one of the preceding claims, in which each tip of the rotor includes a ceramic cylinder which has rolling engagement with the wall of the stator.
7. An engine, pump or motor as claimed in Claim 6, in which each ceramic cylinder is supported by a seating which includes a pair of fins acting on the ceramic cylinder and defining a space within which a lubricant is received.
8. An engine, pump or motor constructed and arranged to operate substantially as hereinbefore described with reference to and as shown in the accompanying drawings.
GB0031622A 2000-01-27 2000-12-22 Engines,pumps and motors Expired - Fee Related GB2358675B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0001789A GB0001789D0 (en) 2000-01-27 2000-01-27 Engines, pumps and motors

Publications (3)

Publication Number Publication Date
GB0031622D0 GB0031622D0 (en) 2001-02-07
GB2358675A true GB2358675A (en) 2001-08-01
GB2358675B GB2358675B (en) 2003-11-26

Family

ID=9884377

Family Applications (2)

Application Number Title Priority Date Filing Date
GB0001789A Ceased GB0001789D0 (en) 2000-01-27 2000-01-27 Engines, pumps and motors
GB0031622A Expired - Fee Related GB2358675B (en) 2000-01-27 2000-12-22 Engines,pumps and motors

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GB0001789A Ceased GB0001789D0 (en) 2000-01-27 2000-01-27 Engines, pumps and motors

Country Status (1)

Country Link
GB (2) GB0001789D0 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CZ302673B6 (en) * 2010-06-30 2011-08-24 Jihostroj A.S. Piston sealing for rotary-piston machine and rotary-piston machine with such a sealing
CN103122818A (en) * 2013-01-29 2013-05-29 武汉船用机械有限责任公司 Stator and motor

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1158341A (en) * 1965-07-21 1969-07-16 Omar Teodoro Ferrari Rotary-Piston Internal Combustion Engines.
US3873245A (en) * 1973-01-02 1975-03-25 Nastol Research Inc Steam-driven engine
RU2095593C1 (en) * 1994-01-11 1997-11-10 Камалдин Исматулаевич Махачев Rotary machine

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1158341A (en) * 1965-07-21 1969-07-16 Omar Teodoro Ferrari Rotary-Piston Internal Combustion Engines.
US3873245A (en) * 1973-01-02 1975-03-25 Nastol Research Inc Steam-driven engine
RU2095593C1 (en) * 1994-01-11 1997-11-10 Камалдин Исматулаевич Махачев Rotary machine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CZ302673B6 (en) * 2010-06-30 2011-08-24 Jihostroj A.S. Piston sealing for rotary-piston machine and rotary-piston machine with such a sealing
CN103122818A (en) * 2013-01-29 2013-05-29 武汉船用机械有限责任公司 Stator and motor

Also Published As

Publication number Publication date
GB0031622D0 (en) 2001-02-07
GB0001789D0 (en) 2000-03-22
GB2358675B (en) 2003-11-26

Similar Documents

Publication Publication Date Title
US6446595B1 (en) Rotary piston engine
US4300874A (en) Rotary machine with lenticular rotor and a circular guide member therefor
KR101032262B1 (en) Rotary combustion apparatus
JP3366635B2 (en) Positive displacement machines with reciprocating and rotating pistons, especially four-stroke engines
KR20190130934A (en) Rotary engine having enhanced sealing structure
GB2358675A (en) A rotary engine pump or motor
JPH0733775B2 (en) Rotating machine
US4008988A (en) Rotary piston expansible chamber device
JP2509514B2 (en) Rotary engine
US3924979A (en) Rotary engine anti-spin oil seal
RU2158834C1 (en) Rotary internal combustion engine
EP1484474B1 (en) Endothermic engine with rotating pistons
US6010322A (en) Rotational power generating device
US3750630A (en) Rotary combustion engine
RU2344298C2 (en) Rotary internal combustion engine
KR100324770B1 (en) Stroke volume magnification structure for enclosed compressor
US11629712B2 (en) Fluid transfer device
US6189502B1 (en) Grooved double combustion chamber rotary engine
RU2283961C1 (en) Rotary-vane machine
RU2253754C1 (en) Compressor
JPH08135460A (en) Rotary type engine
JP2017201149A (en) Compressor and internal combustion engine
KR19980031943A (en) Rotating piston engine using eccentric gear
RU2194164C1 (en) Rotor positive displacement machine
JPS63192901A (en) Full rotary engine

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20061222