US3595018A - Rotary engine - Google Patents
Rotary engine Download PDFInfo
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- US3595018A US3595018A US886421A US3595018DA US3595018A US 3595018 A US3595018 A US 3595018A US 886421 A US886421 A US 886421A US 3595018D A US3595018D A US 3595018DA US 3595018 A US3595018 A US 3595018A
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- 239000007788 liquid Substances 0.000 claims abstract description 26
- 238000002485 combustion reaction Methods 0.000 claims abstract description 12
- 238000006073 displacement reaction Methods 0.000 claims description 15
- 230000006835 compression Effects 0.000 claims description 10
- 238000007906 compression Methods 0.000 claims description 10
- 239000000203 mixture Substances 0.000 claims description 9
- 239000012530 fluid Substances 0.000 claims description 8
- 238000007789 sealing Methods 0.000 claims description 6
- 230000000694 effects Effects 0.000 claims description 4
- 238000010304 firing Methods 0.000 claims description 4
- 239000000463 material Substances 0.000 claims description 3
- 238000005192 partition Methods 0.000 claims description 2
- 239000007789 gas Substances 0.000 description 55
- 239000000446 fuel Substances 0.000 description 7
- 238000010438 heat treatment Methods 0.000 description 6
- 238000006243 chemical reaction Methods 0.000 description 1
- -1 for example Substances 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B57/00—Internal-combustion aspects of rotary engines in which the combusted gases displace one or more reciprocating pistons
- F02B57/08—Engines with star-shaped cylinder arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
- F01B1/00—Reciprocating-piston machines or engines characterised by number or relative disposition of cylinders or by being built-up from separate cylinder-crankcase elements
- F01B1/06—Reciprocating-piston machines or engines characterised by number or relative disposition of cylinders or by being built-up from separate cylinder-crankcase elements with cylinders in star or fan arrangement
- F01B1/0641—Details, component parts specially adapted for such machines
- F01B1/0644—Pistons
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
- F01B13/00—Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion
- F01B13/04—Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion with more than one cylinder
- F01B13/06—Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion with more than one cylinder in star arrangement
- F01B13/061—Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion with more than one cylinder in star arrangement the connection of the pistons with the actuated or actuating element being at the outer ends of the cylinders
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/02—Engines characterised by their cycles, e.g. six-stroke
- F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
- F02B2075/027—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle four
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/16—Engines characterised by number of cylinders, e.g. single-cylinder engines
- F02B75/18—Multi-cylinder engines
- F02B2075/1804—Number of cylinders
- F02B2075/1824—Number of cylinders six
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B2730/00—Internal-combustion engines with pistons rotating or oscillating with relation to the housing
- F02B2730/01—Internal-combustion engines with pistons rotating or oscillating with relation to the housing with one or more pistons in the form of a disk or rotor rotating with relation to the housing; with annular working chamber
- F02B2730/012—Internal-combustion engines with pistons rotating or oscillating with relation to the housing with one or more pistons in the form of a disk or rotor rotating with relation to the housing; with annular working chamber with vanes sliding in the piston
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- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Definitions
- the present invention comprises rotary engine configurations each of which basically includes an eccentric outer casing and a rotor internally mounted for relative rotationwith respect to the casing, the rotor having vanes which define peripherally located cells about the circumference of the rotor and means for introducing into each of the cells a motive gas.
- Each cell further includes liquid circumferentially located adjacent to the outer casing and in several embodiments, pistons separate the liquid from the motive gas which is introduced internally of the rotor to flow into radially inward portions of the cells.
- Various means are provided in different configurations for introducing motive gas into the aforementioned cells during a rotary segment of movement and for exhausting such gas thereafter.
- Such means comprises poppet valving and cams controlling movements thereof; or, alternatively, various porting arrangements are shown.
- the engine may be of the internal combustion type having conventional spark plugs or may be indirectly powered by a remote internal combustion source.
- FIG. 1 is a cross-sectional view of one form of rotary engine according to the invention which includes spark plugs and cam actuated exhaust and intake valving;
- FIG. 2 is a fragmentary cross-sectional view taken along lines 2-2 ofFIG. 1;
- FIG. 3 is a cross-sectional view taken in the direction of arrows 3-3 of FIG. 1;
- FIG. 4 is a fragmentary cross section of an end portion of the engine of FIG. 1;
- FIG. 5 is a cross section showing the arrangement of exhaust and intake parts used in conjunction with the engine of FIG. 1;
- FIG. 6 is a second embodiment of rotary engine utilizing the injection ofa motive gas such as steam to obtain power;
- FIG. 7 is a third embodiment of rotary engine according to the invention wherein pressure is exerted by the motive gas acting through a gas/liquid interface;
- FIG. 8 is a fourth embodiment of internal combustion engine wherein a remotely fired combustion source is used
- FIG. 9 is a cross section showing a sealing arrangement between the end plate and rotor which may be used in conjunction with the engine of FIG. 7;
- FIG. 10 is a view taken in the direction of the arrows I040 of FIG. 9.
- Engine 10 has an outer casing 11 which is eccentric for a reason which will be explained.
- a rotor having radially outward sections 12.
- Each of the sections 12 is slotted to hold a plurality of vanes 13.
- Each of the vanes is spring loaded outwardly toward the casing 11 and during relative rotation between the rotor and easing, will provide sliding sealing contact.
- the sections 12, together with the vanes 13, define a plurali ty of compartments or cells having upper portions 14 and radially inwardly portions 16. Separating the two portions of the compartments are pistons 17 which are each in sliding contact with the opposing sides of adjacent rotor sections 12 and may though not necessarily be in sealing contact therewith. In some instances the material of the pistons 17 may be of such density as to float at the interface between the outer liquid and inner motive gas.
- each of the upper compartments sections 14 are filled with a liquid, for example, water or hydraulic fluid.
- a pressure or motive fluid will be introduced sequentially into each of the compartments 16 which will have the affect of driving the pistons 17, outwardly toward the casing 11.
- the liquid in each compartment section 14 will be under a pressure substantially equal to the pressure beneath the respective pistons and such pressure will be distributed against the inner surface of the casing 11, against inner surfaces of each adjacent vane 13, and against the interior rotor sections 12.
- a four cycle internal combustion engine has been illustrated. Accordingly, a fuel air mixture is introduced into compartment sections 16 (by a means which will be further described) beginning, for example, at station 1 and continuing through station 4. Thereafter, continued rotation of the rotor 15 relative to the casing will cause the fluid trapped in each of the respective upper compartment sections 14 to force the pistons 17 radially inwardly through stations 4-7. At station 7, the fuel air mixture will achieve maximum compression and the mixture will be fired by means to be described so that the pistons 17 will be driven outwardly exerting pressure against the liquid in the upper compartments 14.
- each piston 17 is driven radially inwardly in order to exhaust the expanded gases.
- intake and exhaust poppet valves 18 and 18' which are associated with cams 2 0 and 21 for causing sequential opening and closing of the valves in a known manner.
- spark plugs 21 which are electrically connected through suitable lead wiring in respective each to contact terminal 23 at the end of the rotor 11.
- the contact 23 will receive a high voltage impulse from the terminal 24 which is connected by a lead 25 to an induction coil.
- Rotary support between the rotor 15 and casing 11 is effected by roller bearings 26 which circumferentially encompasses the end of the rotor 15. The rotor develops power which is delivered to shaft 19.
- Shaft 19' is fixed by a suitable means to the casing 11 and supports earns 20 and 21 in fixed relation to the rotor.
- the opposite end of the rotor will also be arranged similarly with respect to the outer casing II.
- a provision of an end plate 27 which is threaded internally to the casing I I at 28 is provided.
- FIG. 5 is transverse sectional view of one form of arrangement which may be provided for permitting intake and exhaust to each of the compartments 14.
- the view shown in FIG, 5 is of the casing 11 at the opposite end of or relative to that shown in FIG. 4. Accordingly, as illustrated diagrammatically, the end plate closing the opposite end of the engine will be provided with intake slot 29 and as shown in phantom the opposite end will have an exhaust slot 30.
- each of the poppet valves 18 and 19 have longitudinal passages 31 which connect up with the slots 29 and 30 during prescribed angular travel of the rotor relative to the end plates 27.
- the slots 29 and 30 are in turn appropriately connected to passages 29' and 30' for the introduction of fuel air mixture during he intake portion of the cycle and for the exhaust of gases during the exhaust portion of the cycle.
- the engine shown is one which might be powered by the introduction thereto of a high-pressure fluid which is steam, for example, for an external steam generation source.
- a high-pressure fluid which is steam, for example, for an external steam generation source.
- the principle of operation is essentially similar to that of the engine shown in FIGS. l5 except for modifications attendant upon the fact that the fluid engine is not internally fired.
- ports 40 are provided to each of the lower compartments l4 and which serve the duel function of intake and exhaust. It will be understood that as the rotor rotates relative to an end plate such as has been shown in FIG. 9, highpressure steam will first be admitted via conduit 50 to the slot 411 and therefrom through passage 45 into compartments 14'.
- the slot 41 may be connected to a suitable external source of steam pressure and will admit steam into the respective compartments 14 to positions 1-4 thereby producing power by forcing the pistons 17 against a liquid intermediate of the pistons outer casing l 1'. Thereafter, through continued rotation of the rotor 17, the expanded steam will exhaust through that portion of the cycle represented by positions 4-7.
- the end cap 27' will be provided with a slot 43 which will suitably come into registry with the ports 41 and which will permit the exhausted steam to escape.
- a similar intake and exhaust cycle will occur through l80 of rotation of the rotor relative to the casing as represented by positions 7-1.
- FIG. 9 there has been illustrated one means for providing sealing of the representative slots 41 etc. against the rotor 15. Pressure fluid will flow from adjacent the outer casing 11 through the passages 46, 47 and 48 surrounding the manifold ring 49 which defines the slot 41.
- the slot 31 is connected to intake or exhaust as the gas comes through tube 50. Consequently, the working pressure of the engine will be reflected upon the manifold member 49 to hold such member effectively sealed against the face of the rotor 15.
- FIG. 8 yet another configuration of rotary engine has been illustrated which again employs cammcd popped valves for intake and exhaust.
- the arrangement is similar to that shown in FIG. 1 except that the engine of FIG. 7 is not internally fired. Rather, a gas under pressure will be admitted to the engine through the respective ports 41'. No pistons are provided but rather gas admitted under pressure to each of the compartment sections 14 will effect a gas liquid interface 51. Although some mixing of gas and liquid may be expected, nevertheless centrifugal amount will tend to maintain the liquid more or less adjacent to the outer casing 11" and the effect of the gas pressure in compartment 14 will be felt through the liquid against the casing to cause relative rotation between the rotor and easing.
- gas is introduced at the appropriate slot 53 in an end plate (not shown) and through passages and ports 54, 55 into the compartments 14 which are in positions 1-4.
- the engine is applicable to many different cycles because the engine displacement at any part of a cycle may be varied by the reshaping of the wall of the casing.
- the change of volume during compression may be less than that during expansion so that the engine could function as a closed cycle Sterling engine.
- the gas may be air or an air fuel mixture.
- a smogless engine could result if the compressed gas is ducted into the heating chamber at a relatively constant velocity which in turn would produce a constant and efficient combustion.
- An air fuel mixture is burned directly in the heating chamber, but air if used as the compressed gas is first mixed with fuel injected into the heating chamber and is then burned. The increased gas volume after heating would provide the mechanical energy during the expansion cycle of the engine.
- a rotary fluid motor comprising:
- a casing having an inner and outer wall, said inner wall being of an approximately circular shape defined by points at nonuniform radial distances from a center point, said points being located at angular displacements defined with respect to said center point and measured from a reference point in a direction of rotation, said inner wall being at minimum radial distances from said center point at minimum points located at angular displacements of about 90 and about 270 from said reference point, said inner wall at maximum radial distances from said center point being at maximum points located at angular displacements of about 0 and about l from said reference point,
- a circular vaned wheel arranged within said casing for rotation about said center point in said direction of rotation and spaced from said inner wall, said wheel including a central hub and fixed vanes extending radially from said hub at substantially uniform radial distances from said center point, said fixed vanes forming channels adapted to accommodate a gas and a liquid in the form of a liquid cell adjacent to the inner wall and a gas cell adjacent to the central hub, a piston located in each channel slidably mounted therein to partition each channel into said gas and liquid cells, said fixed vanes and channels located at angular displacements defined with respect to said center point and measured from said reference point in said direction of rotation,
- valve means for introducing a motive gas through gas port means within said central hub into said gas cells of said vaned wheel located at angular displacements of about 0 to about from said reference point, said valve means further being adapted to close gas port means thereby sealing gas cells at angular displacements of about 90 to about 270 and said gas port means further adapted to allow the exhaust of said gas of said gas cells located at about angular displacements of about 270 to about 360, end placed closing said casing and means for journaling said vaned wheel and central hub for rotation within said casing,
- said ignition means includes spark-producing means and means for sequentially producing a spark in each gas cell after compression of gas therein.
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- Engineering & Computer Science (AREA)
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- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
Various configurations of rotary engines including internal combustion rotary engines are disclosed wherein pressure exerted by the motive gas is transmitted by means of an intermediate liquid against the outer eccentric casing, thus causing relative rotary movement between the casing and a central rotor.
Description
United States Patent Inventor Edward T. Saylor, Jr.
144 E. 22 St., New York, NX. 10010 Appl. No. 886,421
Filed Dec. 18, 1969 Patented July 27, 1971 Continuation-impart of application Ser. No. 687,947, Nov. 9, 1967, now Patent No. 3,485,174.
US. Cl 60/396] 91/202, 92/58,]23/19, 123/44 B, 123/44 E Int. Cl F02g 3/00,
F02b 5 7/10 Field ofSearch 60/3961;
Primary Examiner-Douglas Hart ArtomeyPennie, Edmonds, Morton, Taylor and Adams ABSTRACT: Various configurations of rotary engines including internal combustion rotary engines are disclosed wherein pressure exerted by the motive gas is transmitted by means of an intermediate liquid against the outer eccentric casing, thus causing relative rotary movement between the casing and a central rotor.
SHEET 1 BF 7 1N VENTOR. EDWARD T. SAYLOR, J'R.
ATTORNEYS PATENTEU m2? I971 SHEET 2 BF 7 ill mv a m 0E my INVENTOR. EDWARD T. SAYLOR, JR.
ATTORNEYS PATENTED m2? I971 SHEET '4 0F 7 l ZNTOR. EDWARD T'. YLORJR.
ATTORNEYS -PATENTEO .mm mm SHEET 5 BF 7 INVENTOR. EDWARD T. SAYLOR, J'R.
ATTORNEYS FIG. 8
PATENTEUJULNIQ?! 3,595,018
PATENTEU JUL2T |97| SHEET 7 [1F 7 FIG. 9
FIG. 10
YNVENTOR. EDWARD'T. SAYLOR, JR.
ATTORNEYS ROTARY ENGINE This invention is a continuation-in-part of our copending US. Pat. application entitled Apparatus for Transferring Energy from a Gas to a Liquid filed Nov. 9, 1967 and bearing Ser. No. 687,947, U.S. Pat. No. 3,485,174.
BACKGROUND OF THE INVENTION In the copending case, there was shown an apparatus in the form ofa rotary pump which comprised flowing together a gas and a liquid at the same velocity within portioned cells, increasing the volume of the portioned cells to allow the gas to expand to produce work against the liquid as the liquid is allowed to escape from the cells.
SUMMARY OF THE INVENTION The present invention comprises rotary engine configurations each of which basically includes an eccentric outer casing and a rotor internally mounted for relative rotationwith respect to the casing, the rotor having vanes which define peripherally located cells about the circumference of the rotor and means for introducing into each of the cells a motive gas. Each cell further includes liquid circumferentially located adjacent to the outer casing and in several embodiments, pistons separate the liquid from the motive gas which is introduced internally of the rotor to flow into radially inward portions of the cells.
Various means are provided in different configurations for introducing motive gas into the aforementioned cells during a rotary segment of movement and for exhausting such gas thereafter. Such means comprises poppet valving and cams controlling movements thereof; or, alternatively, various porting arrangements are shown. The engine may be of the internal combustion type having conventional spark plugs or may be indirectly powered by a remote internal combustion source.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a cross-sectional view of one form of rotary engine according to the invention which includes spark plugs and cam actuated exhaust and intake valving;
FIG. 2 is a fragmentary cross-sectional view taken along lines 2-2 ofFIG. 1;
FIG. 3 is a cross-sectional view taken in the direction of arrows 3-3 of FIG. 1;
FIG. 4 is a fragmentary cross section of an end portion of the engine of FIG. 1;
FIG. 5 is a cross section showing the arrangement of exhaust and intake parts used in conjunction with the engine of FIG. 1;
FIG. 6 is a second embodiment of rotary engine utilizing the injection ofa motive gas such as steam to obtain power;
FIG. 7 is a third embodiment of rotary engine according to the invention wherein pressure is exerted by the motive gas acting through a gas/liquid interface;
FIG. 8 is a fourth embodiment of internal combustion engine wherein a remotely fired combustion source is used;
FIG. 9 is a cross section showing a sealing arrangement between the end plate and rotor which may be used in conjunction with the engine of FIG. 7; and,
FIG. 10 is a view taken in the direction of the arrows I040 of FIG. 9.
DESCRIPTION OF PREFERRED EMBODIMENTS Referring to the drawings and initially to FIGS. I5 thereof, a rotary internal combustion engine 10 incorporating the principles of the present invention has been illustrated. Engine 10 has an outer casing 11 which is eccentric for a reason which will be explained. Located within the casing 10 in sealed relation thereto is a rotor having radially outward sections 12. Each of the sections 12 is slotted to hold a plurality of vanes 13. Each of the vanes is spring loaded outwardly toward the casing 11 and during relative rotation between the rotor and easing, will provide sliding sealing contact.
The sections 12, together with the vanes 13, define a plurali ty of compartments or cells having upper portions 14 and radially inwardly portions 16. Separating the two portions of the compartments are pistons 17 which are each in sliding contact with the opposing sides of adjacent rotor sections 12 and may though not necessarily be in sealing contact therewith. In some instances the material of the pistons 17 may be of such density as to float at the interface between the outer liquid and inner motive gas.
For purposes of illustration, and in further describing intake and exhaust cycles, the rotary engine of FIG. I has been de picted as having station segments 1-12, segments 1-4 comprising of rotation, 1-8 etc. As shown, each of the upper compartments sections 14 are filled with a liquid, for example, water or hydraulic fluid. In order to produce relative movement between the rotor and easing, a pressure or motive fluid will be introduced sequentially into each of the compartments 16 which will have the affect of driving the pistons 17, outwardly toward the casing 11. During such movement of the pistons, the liquid in each compartment section 14 will be under a pressure substantially equal to the pressure beneath the respective pistons and such pressure will be distributed against the inner surface of the casing 11, against inner surfaces of each adjacent vane 13, and against the interior rotor sections 12. It will be observed that due to the eccentricity of the outer casing 11, that in each compartment sections 14, pressure will be unevenly exerted against the different lengths of adjacent vanes 13, since in each case, the casing will be closer to the center of rotation with respect to one ofthe vanes and further away with respect to the next adjacent vane. In the case of the illustrated embodiment of FIG. 1, such pressure unbalance will cause the rotor 15 to rotate in the direction of the arrow at such times when the piston exerts pressure against the liquid intermediate pistons and the casing 11. This action will now be further explained as follows: I
In the embodiment of FIG. I, a four cycle internal combustion engine has been illustrated. Accordingly, a fuel air mixture is introduced into compartment sections 16 (by a means which will be further described) beginning, for example, at station 1 and continuing through station 4. Thereafter, continued rotation of the rotor 15 relative to the casing will cause the fluid trapped in each of the respective upper compartment sections 14 to force the pistons 17 radially inwardly through stations 4-7. At station 7, the fuel air mixture will achieve maximum compression and the mixture will be fired by means to be described so that the pistons 17 will be driven outwardly exerting pressure against the liquid in the upper compartments 14. It will be noticed that due to the eccentricity of the casing in respect to each of the successive stations 7-10, that a greater reaction force is felt against one of the vanes 13 defining each compartment section 14 such that relative rotation of the rotor 15 with respect to the casing 11 will result. Thus from stations 7l0 movement of the pistons out wardly will result in power being transmitted to the rotor to cause its rotation.
From stations I0-1, again the eccentricity of the casing 11 causes each piston 17 to be driven radially inwardly in order to exhaust the expanded gases.
In order to accomplish the foregoing cycle, in association with each lower compartment 16 are intake and exhaust poppet valves 18 and 18' which are associated with cams 2 0 and 21 for causing sequential opening and closing of the valves in a known manner. Furthermore, as best shown in FIGS. 3 and 4, there are provided spark plugs 21 which are electrically connected through suitable lead wiring in respective each to contact terminal 23 at the end of the rotor 11. The contact 23 will receive a high voltage impulse from the terminal 24 which is connected by a lead 25 to an induction coil. Rotary support between the rotor 15 and casing 11 is effected by roller bearings 26 which circumferentially encompasses the end of the rotor 15. The rotor develops power which is delivered to shaft 19. Shaft 19' is fixed by a suitable means to the casing 11 and supports earns 20 and 21 in fixed relation to the rotor. The opposite end of the rotor will also be arranged similarly with respect to the outer casing II. As shown in FIG. 4 a provision of an end plate 27 which is threaded internally to the casing I I at 28 is provided.
FIG. 5 is transverse sectional view of one form of arrangement which may be provided for permitting intake and exhaust to each of the compartments 14. The view shown in FIG, 5 is of the casing 11 at the opposite end of or relative to that shown in FIG. 4. Accordingly, as illustrated diagrammatically, the end plate closing the opposite end of the engine will be provided with intake slot 29 and as shown in phantom the opposite end will have an exhaust slot 30. As seen in FIG. 3, each of the poppet valves 18 and 19 have longitudinal passages 31 which connect up with the slots 29 and 30 during prescribed angular travel of the rotor relative to the end plates 27. The slots 29 and 30 are in turn appropriately connected to passages 29' and 30' for the introduction of fuel air mixture during he intake portion of the cycle and for the exhaust of gases during the exhaust portion of the cycle.
Referring to an alternate embodiment illustrated in FIG. 6, the engine shown is one which might be powered by the introduction thereto of a high-pressure fluid which is steam, for example, for an external steam generation source. The principle of operation is essentially similar to that of the engine shown in FIGS. l5 except for modifications attendant upon the fact that the fluid engine is not internally fired. Accordingly, ports 40 are provided to each of the lower compartments l4 and which serve the duel function of intake and exhaust. It will be understood that as the rotor rotates relative to an end plate such as has been shown in FIG. 9, highpressure steam will first be admitted via conduit 50 to the slot 411 and therefrom through passage 45 into compartments 14'. As illustrated, the slot 41 may be connected to a suitable external source of steam pressure and will admit steam into the respective compartments 14 to positions 1-4 thereby producing power by forcing the pistons 17 against a liquid intermediate of the pistons outer casing l 1'. Thereafter, through continued rotation of the rotor 17, the expanded steam will exhaust through that portion of the cycle represented by positions 4-7. For this purpose the end cap 27' will be provided with a slot 43 which will suitably come into registry with the ports 41 and which will permit the exhausted steam to escape. A similar intake and exhaust cycle will occur through l80 of rotation of the rotor relative to the casing as represented by positions 7-1.
With further reference to FIG. 9, there has been illustrated one means for providing sealing of the representative slots 41 etc. against the rotor 15. Pressure fluid will flow from adjacent the outer casing 11 through the passages 46, 47 and 48 surrounding the manifold ring 49 which defines the slot 41. The slot 31 is connected to intake or exhaust as the gas comes through tube 50. Consequently, the working pressure of the engine will be reflected upon the manifold member 49 to hold such member effectively sealed against the face of the rotor 15.
Referring next to FIG. 8, yet another configuration of rotary engine has been illustrated which again employs cammcd popped valves for intake and exhaust. The arrangement is similar to that shown in FIG. 1 except that the engine of FIG. 7 is not internally fired. Rather, a gas under pressure will be admitted to the engine through the respective ports 41'. No pistons are provided but rather gas admitted under pressure to each of the compartment sections 14 will effect a gas liquid interface 51. Although some mixing of gas and liquid may be expected, nevertheless centrifugal amount will tend to maintain the liquid more or less adjacent to the outer casing 11" and the effect of the gas pressure in compartment 14 will be felt through the liquid against the casing to cause relative rotation between the rotor and easing.
In the final embodiment shown in FIG. 8, an externally fired combustion powered engine has been illustrated. In the embodiment depicted, gas is introduced at the appropriate slot 53 in an end plate (not shown) and through passages and ports 54, 55 into the compartments 14 which are in positions 1-4.
Thereafter, relative movement of the rotor and casing will cause the compression of the gas until it is fully compressed at positions 6 and 7. At this point the gas will be permitted to escape by means ofa passage 56 to a remote heating chamber 57. After heating, the hot gas will be returned through passage 58 into compartment 14 at positions 7 and 8. The expanding gas will then produce a torque from positions 7l0 to be followed by exhaust through positions I ll-l.
The engine is applicable to many different cycles because the engine displacement at any part of a cycle may be varied by the reshaping of the wall of the casing. For example, the change of volume during compression may be less than that during expansion so that the engine could function as a closed cycle Sterling engine. In other cycles the gas may be air or an air fuel mixture. A smogless engine could result if the compressed gas is ducted into the heating chamber at a relatively constant velocity which in turn would produce a constant and efficient combustion. An air fuel mixture is burned directly in the heating chamber, but air if used as the compressed gas is first mixed with fuel injected into the heating chamber and is then burned. The increased gas volume after heating would provide the mechanical energy during the expansion cycle of the engine.
It will be understood that the foregoing description has related to particular embodiments of the invention and has therefore been merely representative. For example, instead of providing ignition means in the form of plugs as shown in the embodiment of FIG. I, the motor may be fired relying upon autoignition solely due to compression of the fuel air mixture. Accordingly, in order to appreciate fully the spirit and scope of the present invention, reference should be made to the appended claims.
I claim:
1. A rotary fluid motor comprising:
a. a casing having an inner and outer wall, said inner wall being of an approximately circular shape defined by points at nonuniform radial distances from a center point, said points being located at angular displacements defined with respect to said center point and measured from a reference point in a direction of rotation, said inner wall being at minimum radial distances from said center point at minimum points located at angular displacements of about 90 and about 270 from said reference point, said inner wall at maximum radial distances from said center point being at maximum points located at angular displacements of about 0 and about l from said reference point,
b. a circular vaned wheel arranged within said casing for rotation about said center point in said direction of rotation and spaced from said inner wall, said wheel including a central hub and fixed vanes extending radially from said hub at substantially uniform radial distances from said center point, said fixed vanes forming channels adapted to accommodate a gas and a liquid in the form of a liquid cell adjacent to the inner wall and a gas cell adjacent to the central hub, a piston located in each channel slidably mounted therein to partition each channel into said gas and liquid cells, said fixed vanes and channels located at angular displacements defined with respect to said center point and measured from said reference point in said direction of rotation,
c. movable vanes incorporated in said fixed vanes and extendable and retractable therefrom, means for urging said movable vanes into continuous contact with said inner wall to seal said channels,
d. valve means for introducing a motive gas through gas port means within said central hub into said gas cells of said vaned wheel located at angular displacements of about 0 to about from said reference point, said valve means further being adapted to close gas port means thereby sealing gas cells at angular displacements of about 90 to about 270 and said gas port means further adapted to allow the exhaust of said gas of said gas cells located at about angular displacements of about 270 to about 360, end placed closing said casing and means for journaling said vaned wheel and central hub for rotation within said casing,
e. means in conjunction with said casing and central hub for introducing a motive gas through said central hub into each of said gas cells, said gas being introduced under high pressure into a selected sequence of said gas cells to drive said wheel relative to said casing,
2. An apparatus according to claim 1 wherein said motive gas in (e) is capable of rapid expansion upon ignition and ignition means are provided for sequentially firing said gas in each cell after said gas has been compressed therein by relative rotation between said wheel and casing, in order to expand said ignited gas to drive said wheel relative to said casing.
3 An apparatus according to claim 2 in which said ignition means effects ignition solely by compression of said gas as a result of relative rotation between said casing and wheel.
4. An apparatus according to claim 2 in which said ignition means includes spark-producing means and means for sequentially producing a spark in each gas cell after compression of gas therein.
5. An apparatus according to claim 4 in which said means (f) and (g) includes poppet valves and camming means controlling the operation olsaid valves.
6. An apparatus according to claim I wherein said pistons under (e) are of a material having a density intermediate that ofsaid gas and liquid.
7. An apparatus according to claim I wherein said gas is a combustible mixture and means are provided externally of said casing for receiving said gas from each cell at substan tially maximum compression, means for firing said gas externally and means for returning said gas after combustion at increased energy to each cell to drive said wheel relative to said casing.
Claims (7)
1. A rotary fluid motor comprising: a. a casing having an inner and outer wall, said inner wall being of an approximately circular shape defined by points at nonuniform radial distances from a center point, said points being located at angular displacements defined with respect to said center point and measured from a reference point in a direction of rotation, said inner wall being at minimum radial distances from said center point at minimum points located at angular displacements of about 90* and about 270* from said reference point, said inner wall at maximum radial distances from said center point being at maximum points located at angular displacements of about 0* and about 180* from said reference point, b. a circular vaned wheel arranged within said casing for rotation about said center point in said direction of rotation and spaced from said inner wall, said wheel including a central hub and fixed vanes extending radially from said hub at substantially uniform radial distances from said center point, said fixed vanes forming channels adapted to accommodate a gas and a liquid in the form of a liquid cell adjacent to the inner wall and a gas cell adjacent to the central hub, a piston located in each channel slidably mounted therein to partition each channel into said gas and liquid cells, said fixed vanes and channels located at angular displacements defined with respect to said center point and measured from said reference point in said direction of rotation, c. movable vanes incorporated in said fixed vanes and extendable and retractable therefrom, means for urging said movable vanes into continuous contact with said inner wall to seal said channels, d. valve means for introducing a motive gas through gas port means within said central hub into said gas cells of said vaned wheel located at angular displacements of about 0* to about 90* from said reference point, said valve means further being adapted to close gas port means thereby sealing gas cells at angular displacements of about 90* to about 270* and said gas port means further adapted to allow the exhaust of said gas of said gas cells located at about angular displacements of about 270* to about 360*, end placed closing said casing and means for journaling said vaned wheel and central hub for rotation within said casing, e. means in conjunction with said casing and central hub for introducing a motive gas through said central hub into each of said gas cells, said gas being introduced under high pressure into a selected sequence of said gas cells to drive said wheel relative to said casing.
2. An apparatus according to claim 1 wherein said motive gas in (e) is capable of rapid expansion upon ignition and ignition means are provided for sequentially firing said gas in each cell after said gas has been compressed therein by relative rotation between said wheel and casing, in order to expand said ignited gas to drive said wheel relative to said casing.
3. An apparatus according to claim 2 in which said ignition means effects ignition solely by compression of said gas as a result of relative rotation between said casing and wheel.
4. An apparatus according to claim 2 in which said ignition means includes spark-producing means and means for sequentially producing a spark in each gas cell after compression of gas therein.
5. An apparatus according to claim 4 in which said means (f) and (g) includes poppet valves and camming means controlling the operation of said valves.
6. An apparatus according to claim 1 wherein said pistons under (c) are of a material having a density intermediate that of said gas and liquid.
7. An apparatus according to claim 1 wherein said gas is a combustible mixture and means are provided externally of said casing for receiving said gas from each cell at substantially maximum compression, means for firing said gas externally and means for returning said gas after combustion at increased energy to each cell to drive said wheel relative to said casing.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US88642169A | 1969-12-18 | 1969-12-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3595018A true US3595018A (en) | 1971-07-27 |
Family
ID=25389024
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US886421A Expired - Lifetime US3595018A (en) | 1969-12-18 | 1969-12-18 | Rotary engine |
Country Status (1)
Country | Link |
---|---|
US (1) | US3595018A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4867042A (en) * | 1987-07-07 | 1989-09-19 | Yasuo Kita | Casing and cover for fluid energy converter |
US20120073296A1 (en) * | 2010-09-23 | 2012-03-29 | Courson Michael W | Rotary cam radial steam engine |
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US1094919A (en) * | 1905-05-09 | 1914-04-28 | Nash Engineering Co | Turbo-displacement engine. |
US1603613A (en) * | 1924-08-16 | 1926-10-19 | F J Cunningham | Rotary engine |
DE588234C (en) * | 1933-11-24 | Georg Stauber Dr Ing | Rotating cellular wheel work and power machine with fluid pistons and flat slides, which are carried by roller rings | |
US2052492A (en) * | 1930-08-16 | 1936-08-25 | Voith Gmbh J M | Rotary engine |
GB679329A (en) * | 1949-10-31 | 1952-09-17 | Hans Ungemach | Rotary piston machine |
US2771860A (en) * | 1950-08-22 | 1956-11-27 | Werner P Falk | Hydraulic machine |
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1969
- 1969-12-18 US US886421A patent/US3595018A/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
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DE588234C (en) * | 1933-11-24 | Georg Stauber Dr Ing | Rotating cellular wheel work and power machine with fluid pistons and flat slides, which are carried by roller rings | |
US1094919A (en) * | 1905-05-09 | 1914-04-28 | Nash Engineering Co | Turbo-displacement engine. |
US1603613A (en) * | 1924-08-16 | 1926-10-19 | F J Cunningham | Rotary engine |
US2052492A (en) * | 1930-08-16 | 1936-08-25 | Voith Gmbh J M | Rotary engine |
GB679329A (en) * | 1949-10-31 | 1952-09-17 | Hans Ungemach | Rotary piston machine |
US2771860A (en) * | 1950-08-22 | 1956-11-27 | Werner P Falk | Hydraulic machine |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4867042A (en) * | 1987-07-07 | 1989-09-19 | Yasuo Kita | Casing and cover for fluid energy converter |
US20120073296A1 (en) * | 2010-09-23 | 2012-03-29 | Courson Michael W | Rotary cam radial steam engine |
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