US789586A - Rotary engine. - Google Patents
Rotary engine. Download PDFInfo
- Publication number
- US789586A US789586A US23767204A US1904237672A US789586A US 789586 A US789586 A US 789586A US 23767204 A US23767204 A US 23767204A US 1904237672 A US1904237672 A US 1904237672A US 789586 A US789586 A US 789586A
- Authority
- US
- United States
- Prior art keywords
- rotor
- chamber
- shaft
- piston
- port
- 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.)
- Expired - Lifetime
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C15/00—Component parts, details or accessories of machines, pumps or pumping installations, not provided for in groups F04C2/00 - F04C14/00
- F04C15/0057—Driving elements, brakes, couplings, transmission specially adapted for machines or pumps
- F04C15/0061—Means for transmitting movement from the prime mover to driven parts of the pump, e.g. clutches, couplings, transmissions
Definitions
- This invention relates to a form of rotary engine which may be driven by steam -hydraulic, internal-explosion, compressed-air, or other motive power or may be driven by external means and used as a pump, exhauster, compressor, or for any other purposes whatsoever.
- the body of the engine has a casing the inside of which is so shaped as to form a portion of a sphere bounded by two parallel planes placed diagonally to the shaft, the internal chamber thus forming in the normal form a portion of a sphere bounded by two circular plane surfaces.
- the opposite faces of the rotor may be of conical shape, the angles of the cone corresponding to one another and to that made by the planes with the shaft, so that when the rotor is mounted in position there is a 1:)ermanent line of contact between one portion of the conical or other shaped surfaces and the plane on each side of the disk.
- the rotor is provided with a long slot extending across same in the direction of a diameter and placed centrally, or the rotor may consist of two separate halves so mounted or formed as .to leave a slot or space between them.
- axle on which the rotor is mounted is also so formed or fitted that a slot is made corresponding in position with the slot in the rotor and in the same plane therewith.
- a flat piece of metal which is free to swing on its pivot and is so shaped that its edges are always in contact with some portion of the inclined surfaces and with some portion of the spherical surfaces of the interior chamber in order to divide each of the chambers formed betaveen the rotor and the plane and the interior of the chamber into steam-tight chambers at constantly-varying capacity as the shaft rotates.
- Suitable inlet and outlet ports are provided for admission and egress of steam.
- Figure 1 shows a sectional elevation of an engine constructed according to my invention.
- Fig. 2 is an end view with one side of the casing removed.
- Fig. 3 shows a sectional elevation of a second form of engine.
- Fig. 4C is a section of Fig. 3, taken through the line A l) looking in the direction of the arrow.
- Figs. 5 to 9 show details hereinafter referred to.
- land 3 the whole of the parts connected with the casing are shown in section and the parts connected with the shaft, rotor, and piston are shown in elevation.
- a shows the casing, which is preferably cast in two pieces and bolted together.
- the interior of the casing u is of spherical formation, the surface of the sphere having its center at a point on the axis of the shaft (1, which point is also the point of intersection of the axis of the pivotf, (where a pivot is employed,.) upon which the piston is mounted with the axis of the shaft (Z.
- 71 and 0 are two plane surfaces, which, in conjunction with thespherical surface, bound the chamber of the motor. It will be seen that these surfaces are so disposed that they are parallel to one another and are consequently inclined at the same angle to the axis of the shaft (l.
- the shaft (Z is mounted in suitable bearings.
- the portion (2 of the shaft (1 is formed into a kind of frame, through Which the pivot f, carrying the plate or piston g, passes.
- the pivotf is shown mounted centrally and in Fig. 3 to one side of the frame, the position being determined, as before described, so that its axis and that of the shaft (Z intersect at the center of the spherical surface a. h is the rotor.
- a spherical surface or boss 1* which fills up a portion of the chambers left between the spherical surface a, the surfaces of the rotor /z., and the surfaces 710, while in the form shown at Fig. 3 the conical surfaces 7' extend as far as the frame 6.
- the frame 1 forms, as before stated, a slot in which the piston g is mounted on its pivot, or in some cases the pivot may be dispensed with.
- a slot in which the piston g is mounted on its pivot, or in some cases the pivot may be dispensed with.
- Corresponding to the slot in this frame is a slot extending across the diameter of the rotor 70, or the rotor 72.
- the slot does not extend entirely across the rotor, as will be seen on reference to Fig. 2, while in the case of that shown at Fig. 3 the slot divides the rotor 72/ into two halves, as seen at Fig. 4C.
- a corresponding groove is cut circumferentially around the inner surface of the chamber, into which the edge of the rotor iits.
- the piston g has a spherical portion Z formed therewith corresponding to the spherical portion is, formed or attached to the rotor it.
- edge of the piston g all round is constantly in contact with some portion of the spherical and inclined surfaces and that consequently each of the chambers on either side of the rotor 72. is divided into portions of constantly-varying capacity during the rotation of the shaft (2. Packing-s may be provided at all necessary points of contact.
- n is an inlet-port; n, an additional inlet-port for the purpose hereinafter described.
- p is an exhaust-port, and (1 another exhaust-port.
- the chamber 1 increases further in volume until the piston reaches the position shown at Fig. 8, when the end 2 has passed through two hundred and seventy degrees, the lower chamber c then having a maximum volume. After this it steadily decreases. Then the end 2 has passed through three hundred and sixty degrees, it (the chamber 1;) is again equal in volume to the chamber on the other side of the piston on the same side of the rotor. I/Vhen the position is that shown at Fig.
- the object of the additional inlet-port '12 is to enable the engine to start in the event of it being in a position with the piston r over the port m, in which case the steam would be shut off from the chambers. Should this be the case, the port a is temporarily opened by means of a suitable cock and the engine started, after which the port a may be closed, if required.
- a rotary engine provided with a chamber bounded by a zone and two plane surfaces parallel to each other and disposed diagonally to the axis of the shaft of the engine, the said chamber containing a disk or rotor mounted .)erpendicularly to the shaft and extending from one to the other of the plane surfaces, the faces of the said disk or rotor being preferably conical in form, the conical surfaces being of such angle that a continuous line of contact is formed on each side between the plane surface and the surface of the cone, the said disk or rotor being provided with a plate or piston so mounted as to rock backward and forward with its edges constantly in contact with some portion of the aforesaid eham' her, the steam being admitted by suitable inlet and outlet ports all substantially as set forth.
- a rotary engine comprising a casing provided with a chamber bounded by a zone and two parallel planes having suitable inlet and exhaust ports, a shaft passing through said chamber angularly disposed with relation to said planes, a rotor mounted to revolve with said shaft, and an oscillating piston mounted in said rotor, substantially as described.
- a rotary engine comprising a casing provided with a chamber bounded by a zone and two parallel planes having suitable inlet and exhaust ports, a longitudinally-slotted shaft passing through said chamber angularly disposed with relation to said planes, a rotor mounted to revolve with said shaft, and a piston mounted in said rotor to oscillate through said slot, substantially as described.
- a rotary engine comprising a casing provided with a chamber bounded by a zone and two parallel planes having suitable inlet and exhaust ports, a shaft passing through said chamber angularly disposed with relation to said planes, a rotor mounted to revolve with said shaft and constructed so as to form a continuous line of contact with said planes, and an oscillating piston mounted in said rotor, substantially as described.
- a rotary engine comprising a casing provided with a chamber bounded by a zone and two parallel planes having suitable inlet and exhaust ports, a shaft passing through said chamber angularly disposed with relation to said planes, a rotor mounted to revolve with said shaft each side of said rotor being in the form of a truncated cone, the apex of which would coincide with the intersection of the axis of said shaft and the adjacent bounding plane of said chamber, and an oscillating piston mounted in said rotor, substantially as described.
- a rotary engine comprising a casing provided with a chamber bounded by a zone and two parallel planes having suitable inlet and exhaust ports, a longitudinally-slotted shaft passing through said chamber angularly disposed with relation to said planes, a rotor mounted to revolve with said shaft, a piston passing through said slot and rotor symmetrically with respect to the latter, and a pivot pin passing through said shaft and piston at the point of intersection of the axis thereof and the center of the sphere formed by completing said bounding zone, substantially as described.
- a rotary engine comprising a casing provided with a chamber bounded by a zone and two parallel planes, having suitable inlet and exhaust ports, a shaft passing through said chamber angularly disposed with relation to said planes, a rotor dividing said chamber into two compartments mounted to revolve with said shaft, and an oscillating piston constructed to maintain its edges constantly in contact with some portion of said chamber mounted in said rotor, substantially as described.
- a rotary engine comprisii'ig a casing provided with a chamber bounded by a zone and two parallel planes equidistant from the center of the sphere formed by completing said zone, a longitudinally-slotted shaft passing through said chamber angularl y disposed with relation to said planes, a rotor mounted to revolve with said shaft, its center being coincident with the center of the sphere formed as aforesaid, a pivot-pin passing through said shaft and the center of said rotor, a piston mounted in said slot and rotor and on said pin, and suitable inlet and exhaust ports in said casing, substantially as described.
- a rotary engine eomprisin g a casing provided with a chamber bounded by a zone and two parallel planes equidistant from the center of the sphere formed by completing said zone, a shaft passing through said chamber angularl y disposed with relation to said planes, a sphere of less diameter than the sphere the casing substantially two hundred and seventy degrees apart, an auxiliary inlet-port substantially ninety degrees from the main inlet-port, and an auxiliary exhaust-port adjacent the main inletport, substantially as described.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Description
No. 789,586. PATENTED MAY 9, 1905. H. L. BIOKERTON.
ROTARY ENGINE.
APPLICATION FILED DEG. 20 1904.
3 SHEETS-SHEET 1.
ROTAR IIIIIII E.
IIIIIIIIIIIIIIIIIIIIIIIIII 4.
PATENTED MAY 9, 1905.
H. L. BIGKERTON.
ROTARY ENGINE.
APPLIOATION FILED DEC. 20, 1mm.
iipSHEETS-SHBET 3.
Z'KtMMM @7' f "7,
not 789,586.
UTTTTTn @TaTiss Patented May 9, 1905.
PATENT Tries.
RUTA'RY ENGlNE.
SPECIFICATION forming part of Letters Patent No. 789,586, dated May 9, 1905.
Application filed Decemher 20, 1904. Serial No. 237,672.
To (t/TZ whom, it lieu/y cone/1771.:
Be it known that 1, Hnunmrr LAWRENCE Bren nn'rox, a subject of the King of England, residing at Cross Path, Radlett, in the county of l-lertford, England, have inventedcertain new and useful .lmprovemem's in Rotary Engines; and I do hereby declare the following to be a full, clear, and exact description of the invention, such as will enable others skilled in the art to which it appertains to make and use the same.
This invention relates to a form of rotary engine which may be driven by steam -hydraulic, internal-explosion, compressed-air, or other motive power or may be driven by external means and used as a pump, exhauster, compressor, or for any other purposes whatsoever.
In order to explain the principle of the invention, I will first describe the same in its simplest form and then proceed to give simple examples illustrated by drawings, it being of course understood that the form may be modified according to requirements and to the use to which the engine is to be put.
The body of the engine has a casing the inside of which is so shaped as to form a portion of a sphere bounded by two parallel planes placed diagonally to the shaft, the internal chamber thus forming in the normal form a portion of a sphere bounded by two circular plane surfaces. In the chamber is a disk, (which l call the rotor,) n punted vertically between the two faces upon a horizontal shaft, with which it rotates. The opposite faces of the rotor may be of conical shape, the angles of the cone corresponding to one another and to that made by the planes with the shaft, so that when the rotor is mounted in position there is a 1:)ermanent line of contact between one portion of the conical or other shaped surfaces and the plane on each side of the disk. The rotor is provided with a long slot extending across same in the direction of a diameter and placed centrally, or the rotor may consist of two separate halves so mounted or formed as .to leave a slot or space between them. The
axle on which the rotor is mounted is also so formed or fitted that a slot is made corresponding in position with the slot in the rotor and in the same plane therewith. In this slot in the rotor at some convenient point at or near the middle I pivot a flat piece of metal, which is free to swing on its pivot and is so shaped that its edges are always in contact with some portion of the inclined surfaces and with some portion of the spherical surfaces of the interior chamber in order to divide each of the chambers formed betaveen the rotor and the plane and the interior of the chamber into steam-tight chambers at constantly-varying capacity as the shaft rotates. Suitable inlet and outlet ports are provided for admission and egress of steam.
Referring to the drawings accompanying this specification, Figure 1 shows a sectional elevation of an engine constructed according to my invention. Fig. 2 is an end view with one side of the casing removed. Fig. 3 shows a sectional elevation of a second form of engine. Fig. 4C is a section of Fig. 3, taken through the line A l) looking in the direction of the arrow. Figs. 5 to 9 show details hereinafter referred to. In Figs. land 3 the whole of the parts connected with the casing are shown in section and the parts connected with the shaft, rotor, and piston are shown in elevation.
The same letters of reference are employed to denote the same parts in all the views.
a shows the casing, which is preferably cast in two pieces and bolted together. The interior of the casing u is of spherical formation, the surface of the sphere having its center at a point on the axis of the shaft (1, which point is also the point of intersection of the axis of the pivotf, (where a pivot is employed,.) upon which the piston is mounted with the axis of the shaft (Z.
71 and 0 are two plane surfaces, which, in conjunction with thespherical surface, bound the chamber of the motor. It will be seen that these surfaces are so disposed that they are parallel to one another and are consequently inclined at the same angle to the axis of the shaft (l. The shaft (Z is mounted in suitable bearings. The portion (2 of the shaft (1 is formed into a kind of frame, through Which the pivot f, carrying the plate or piston g, passes. In Fig. 1 the pivotf is shown mounted centrally and in Fig. 3 to one side of the frame, the position being determined, as before described, so that its axis and that of the shaft (Z intersect at the center of the spherical surface a. h is the rotor. This is formed in one (as at Fig. 1) or mounted upon (as at 3) the frame portion 6 of the shaft (Z, each side of the rotor having a face j, forming a truncated cone, the apex of each cone being coincident with the points of intersection of the corresponding diagonal plane 7) or c with the axis of the shaft (Z. It is essential that the angles of inclination of the conical surfaces 7' of the rotor /L be similar to each other and to that made by the planes 7) c with the axis of the shaft (Z.
In the form of engine shown at Fig. 1 there is mounted upon or formed with the faces of the rotor 7i and the frame 0 a spherical surface or boss 1*, which fills up a portion of the chambers left between the spherical surface a, the surfaces of the rotor /z., and the surfaces 710, while in the form shown at Fig. 3 the conical surfaces 7' extend as far as the frame 6. The frame 1? forms, as before stated, a slot in which the piston g is mounted on its pivot, or in some cases the pivot may be dispensed with. Corresponding to the slot in this frame is a slot extending across the diameter of the rotor 70, or the rotor 72. is so made up as to leave a space corresponding with the slot in the frame In the case of the machine shown at Fig. 1 the slot does not extend entirely across the rotor, as will be seen on reference to Fig. 2, while in the case of that shown at Fig. 3 the slot divides the rotor 72/ into two halves, as seen at Fig. 4C. In the case of the machine shown at Figs. 1 and 2 a corresponding groove is cut circumferentially around the inner surface of the chamber, into which the edge of the rotor iits. In the case of the machine shown at Fig. 1 the piston g has a spherical portion Z formed therewith corresponding to the spherical portion is, formed or attached to the rotor it. It will be seen that the edge of the piston g all round is constantly in contact with some portion of the spherical and inclined surfaces and that consequently each of the chambers on either side of the rotor 72. is divided into portions of constantly-varying capacity during the rotation of the shaft (2. Packing-s may be provided at all necessary points of contact.
The inlet and outlet ports have been omitted from Figs. 1 and 3 for the sake of clearness; but their arrangement can be readily understood from reference to Fig. 2, which shows the arrangement which I find answers well in practice, it being understood that similar ports in corresponding positions are arranged in each of the plane surfaces. In the case of the engine shown at Fig. 1 for rot. tion in the direction of the arrow, Fig. 2, m
is an inlet-port; n, an additional inlet-port for the purpose hereinafter described. p is an exhaust-port, and (1 another exhaust-port.
To understand the action of the machine, it is necessary to consider the formation of the chamber to contain the steam, its increase to a maximum volume, its decrease and final disappearance. This will be readily understood from consideration of Figs. 5 to 9, where the position of the piston is shown diagrammatically at various portions of its travel in relation to the ports. In each of these figures an arrow showing the direction of rotation is kept opposite the same end .2 of the piston 0. 0 shows the permanent line of contact of the surface of the cone with the plane surface .7). It will be seen when the piston ,r is in the position 01 the space between the rotor lb, the spherical casing, and the plane on each side of the rotor is divided into two equal chambers; As the shaft (Z rotates the piston g travels round and rocking into the space between the rotor and the plane on each side forms a chamber o. This chamber is bounded by the line of permanent contact 0y, the spherical surface a, the piston g, and the plane Z), and as the rotor turns it (the chamber r) increases steadily in volume. At the position shown in Fig. 7, when the end 5 has passed through one hundred and eighty degrees, the chamber 4) and the chamber on the other side of the piston on the same side of the rotor are equal. The chamber 1) increases further in volume until the piston reaches the position shown at Fig. 8, when the end 2 has passed through two hundred and seventy degrees, the lower chamber c then having a maximum volume. After this it steadily decreases. Then the end 2 has passed through three hundred and sixty degrees, it (the chamber 1;) is again equal in volume to the chamber on the other side of the piston on the same side of the rotor. I/Vhen the position is that shown at Fig. 9 and the end .2- has passed through four hundred and fifty degrees, the chamber 9, is decreased greatly in volume, and when the end .2 has passed through five hundred and forty degrees the chamber o vanishes entirely. Now considering the action of the steam when the piston g is in the position shown at Fig. 6 steam is entering through the port m and, forcing its way into the steadily-expanding chamber a, drives the engine round until the position shown at Fig. 7 is reached, when the piston g crossing the port m the supply of steam is cut off. The steam continues to expand until the piston is in the position shown at Fig. 8. As from this moment the chamber 2' containing the steam begins to diminish in volume, an exhaust-port p is provided and the steam begins to escape, it being of course understood that steam is being fed through the port m into a new chamber being formed on the other side of the piston. The exhaust continues to take reasseplace until the end in of the piston 7 crosses the port 7). (See Fig. 9.) There is then a small volume left in the chamber w, and an exhaust-port is provided through which this is (flischarged in order to prevent any possibility of compression taking place. The cycle of operations continues in exactly the same order on each side of the rotor.
The object of the additional inlet-port '12 is to enable the engine to start in the event of it being in a position with the piston r over the port m, in which case the steam would be shut off from the chambers. Should this be the case, the port a is temporarily opened by means of a suitable cock and the engine started, after which the port a may be closed, if required.
For reversing the engine it is simply necessary to convert the inlet' into outlet ports and the outlet into inlet ports, and various methods may be devised for switching the steam into either set of ports, as required.
What I claim, and desire to secure by Letters Patent of the United States of America, is
1. A rotary engine, provided with a chamber bounded by a zone and two plane surfaces parallel to each other and disposed diagonally to the axis of the shaft of the engine, the said chamber containing a disk or rotor mounted .)erpendicularly to the shaft and extending from one to the other of the plane surfaces, the faces of the said disk or rotor being preferably conical in form, the conical surfaces being of such angle that a continuous line of contact is formed on each side between the plane surface and the surface of the cone, the said disk or rotor being provided with a plate or piston so mounted as to rock backward and forward with its edges constantly in contact with some portion of the aforesaid eham' her, the steam being admitted by suitable inlet and outlet ports all substantially as set forth.
2. A rotary engine comprisinga casing provided with a chamber bounded by a zone and two parallel planes having suitable inlet and exhaust ports, a shaft passing through said chamber angularly disposed with relation to said planes, a rotor mounted to revolve with said shaft, and an oscillating piston mounted in said rotor, substantially as described.
3. A rotary engine comprising a casing provided with a chamber bounded by a zone and two parallel planes having suitable inlet and exhaust ports, a longitudinally-slotted shaft passing through said chamber angularly disposed with relation to said planes, a rotor mounted to revolve with said shaft, and a piston mounted in said rotor to oscillate through said slot, substantially as described.
4. A rotary engine comprising a casing provided with a chamber bounded by a zone and two parallel planes having suitable inlet and exhaust ports, a shaft passing through said chamber angularly disposed with relation to said planes, a rotor mounted to revolve with said shaft and constructed so as to form a continuous line of contact with said planes, and an oscillating piston mounted in said rotor, substantially as described.
5. A rotary engine comprising a casing provided with a chamber bounded by a zone and two parallel planes having suitable inlet and exhaust ports, a shaft passing through said chamber angularly disposed with relation to said planes, a rotor mounted to revolve with said shaft each side of said rotor being in the form of a truncated cone, the apex of which would coincide with the intersection of the axis of said shaft and the adjacent bounding plane of said chamber, and an oscillating piston mounted in said rotor, substantially as described.
6. A rotary engine comprising a casing provided with a chamber bounded by a zone and two parallel planes having suitable inlet and exhaust ports, a longitudinally-slotted shaft passing through said chamber angularly disposed with relation to said planes, a rotor mounted to revolve with said shaft, a piston passing through said slot and rotor symmetrically with respect to the latter, and a pivot pin passing through said shaft and piston at the point of intersection of the axis thereof and the center of the sphere formed by completing said bounding zone, substantially as described.
7. A rotary engine comprising a casing provided with a chamber bounded by a zone and two parallel planes, having suitable inlet and exhaust ports, a shaft passing through said chamber angularly disposed with relation to said planes, a rotor dividing said chamber into two compartments mounted to revolve with said shaft, and an oscillating piston constructed to maintain its edges constantly in contact with some portion of said chamber mounted in said rotor, substantially as described.
8. A rotary engine comprisii'ig a casing provided with a chamber bounded by a zone and two parallel planes equidistant from the center of the sphere formed by completing said zone, a longitudinally-slotted shaft passing through said chamber angularl y disposed with relation to said planes, a rotor mounted to revolve with said shaft, its center being coincident with the center of the sphere formed as aforesaid, a pivot-pin passing through said shaft and the center of said rotor, a piston mounted in said slot and rotor and on said pin, and suitable inlet and exhaust ports in said casing, substantially as described.
9. A rotary engine eomprisin g a casing provided with a chamber bounded by a zone and two parallel planes equidistant from the center of the sphere formed by completing said zone, a shaft passing through said chamber angularl y disposed with relation to said planes, a sphere of less diameter than the sphere the casing substantially two hundred and seventy degrees apart, an auxiliary inlet-port substantially ninety degrees from the main inlet-port, and an auxiliary exhaust-port adjacent the main inletport, substantially as described.
In testimony whereof I aflix my signature in presence of two witnesses.
HERBERT LAWRENCE BICKERTON. iVitnesses:
A. BROWNE, A. E. VIDAL.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US23767204A US789586A (en) | 1904-12-20 | 1904-12-20 | Rotary engine. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US23767204A US789586A (en) | 1904-12-20 | 1904-12-20 | Rotary engine. |
Publications (1)
Publication Number | Publication Date |
---|---|
US789586A true US789586A (en) | 1905-05-09 |
Family
ID=2858079
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US23767204A Expired - Lifetime US789586A (en) | 1904-12-20 | 1904-12-20 | Rotary engine. |
Country Status (1)
Country | Link |
---|---|
US (1) | US789586A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3307487A (en) * | 1966-10-03 | 1967-03-07 | Steadman Paul | Rotary pump, compressor and the like |
US4354807A (en) * | 1977-12-08 | 1982-10-19 | The Rovac Corporation | Compressor-expander of the vane type having canted vane cavity |
-
1904
- 1904-12-20 US US23767204A patent/US789586A/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3307487A (en) * | 1966-10-03 | 1967-03-07 | Steadman Paul | Rotary pump, compressor and the like |
US4354807A (en) * | 1977-12-08 | 1982-10-19 | The Rovac Corporation | Compressor-expander of the vane type having canted vane cavity |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US1864699A (en) | Rotary engine, pump, and the like | |
US789586A (en) | Rotary engine. | |
US732671A (en) | Rotary engine. | |
US764465A (en) | Rotary engine. | |
US1296356A (en) | Combined motor and pump. | |
US1890612A (en) | Engine | |
US173030A (en) | Improvement in rotary engines and water-wheels | |
US4555A (en) | Botary steam-engine | |
US1026887A (en) | Rotary engine. | |
US263573A (en) | Rotary engine | |
US1198343A (en) | Rotary engine. | |
US763982A (en) | Rotary engine. | |
US1416174A (en) | Oscillating pump | |
US171704A (en) | Improvement in rotary engines | |
US268522A (en) | Half to mathew macdotigall | |
US1965976A (en) | Mechanism for pumps, compressors, and the like | |
US1185473A (en) | Air-pump. | |
US764551A (en) | Rotary engine. | |
US81009A (en) | Improvement in botary blowebs | |
US759571A (en) | Rotary steam-engine. | |
US683406A (en) | Discoidal engine. | |
US767207A (en) | Rotary motor. | |
US359906A (en) | Disk steam-engine | |
US1106617A (en) | Rotary engine. | |
US496966A (en) | Territory |