EP3587732A1 - Positive displacement machine with oscillating and rotary pistons - Google Patents
Positive displacement machine with oscillating and rotary pistons Download PDFInfo
- Publication number
- EP3587732A1 EP3587732A1 EP18180423.8A EP18180423A EP3587732A1 EP 3587732 A1 EP3587732 A1 EP 3587732A1 EP 18180423 A EP18180423 A EP 18180423A EP 3587732 A1 EP3587732 A1 EP 3587732A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- rotor
- stator
- integral
- crankshaft
- oscillating
- 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.)
- Pending
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C1/00—Rotary-piston machines or engines
- F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F01C1/40—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and having a hinged member
- F01C1/44—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and having a hinged member with vanes hinged to the inner member
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C17/00—Arrangements for drive of co-operating members, e.g. for rotary piston and casing
- F01C17/06—Arrangements for drive of co-operating members, e.g. for rotary piston and casing using cranks, universal joints or similar elements
Abstract
Description
- The present invention relates to a positive displacement machine with oscillating and rotary pistons.
- Positive displacement machines are known, constituted by a fixed element (called stator) and one or more movable organs that together make, with the stator, cavities (or chambers) whose volume varies periodically with the system's general motion.
- These variable volume chambers are placed in communication through appropriate conduits with two environments containing a fluid at different pressures. If the fluid gives energy to the movable organs of the mechanism, this mechanism constitutes an engine. If vice versa the movable organs of the mechanism give energy to the fluid, the mechanism is a fluid machine. (as a pump, a compressor, a fan or a vacuum pump).
-
DE 22 34 950 A1 describes a rotary piston machine, preferably adapted as an internal combustion engine. In this document, the element 5 ofFigures 1 and2 is a fixed pin installed integrally with the stator with eccentricity and orientation fixed with respect to the rotor center of rotation. -
US 3 373 723 A refers to an internal combustion engine having a plurality of oscillating pistons. In this document there is no crankshaft but a "fixed"shaft 26 blocked by theflanges -
US 3 320 936 A describes a rotary engine with three oscillating bodies. In this document the connecting rods' system is composed of a single crank 80 on which a body is articulated to three equiangolate radial spokes to 120°, on each of which is articulated one of the three connecting rods which in turn are articulated to one of the three oscillating organs. -
US 1 715 490 A discloses a steam driven rotary engine in which a crankshaft is not provided. - The object of the present invention is to make a positive displacement machine which has a high efficiency both as endothermic and not endothermic engine and as compressor, pump etc.
- This object is achieved according to the invention with a positive displacement machine with oscillating and rotary pistons as described in claim 1.
- The present invention is hereinafter further clarified with reference to the enclosed drawings in which:
- Figure 1
- shows in cross section the machine according to the invention
- Figure 2
- shows it in longitudinal section
- Figure 3
- shows the stator and rotor according to section III-III of
Figure 1 , - Figure 4
- shows the stator, the rotor and the system of the connecting rods and cranks according to section IV-IV of
Figure 1 , - Figures 5-17
- represent a complete four-phase cycle of the machine,
- Figures 18-30
- represent two complete two-phase cycles,
- Figure 31-32
- represent the geometry of the connecting rods and cranks system.
- As can be seen from
Figures 1 and2 , the positive displacement machine with oscillating and rotary pistons according to the invention consists substantially of afixed stator 2, arotor 12 and acrankshaft 36 both concentric to thestator 2. Thefixed stator 2 is in turn formed by acylindrical body 4 to which twoflanges 6 are applied laterally. - The
flanges 6 are connected to thecylindrical body 4 by means of thescrew rods 10. - Inside the
stator 2 is located in concentric position therotor 12 formed by two symmetrical parts and precisely twoannular flanges 14 reinforced by twodiscs 16. - Inside the two
annular flanges 14 fourshaped inserts 17 are fixed which divide the inner space of therotor 12 into four zones (or chambers) 20 inside which are housed fouroscillating bodies 22 fixed to fourpins 24 which in turn they are articulated to theannular flanges 14 of the rotor 12 (figure 3 ). - Each
oscillating bodies 22 is furthermore articulated, in a median position, by means of agudgeon pin 26 at thesmall end 28 of a connectingrod 30 whose thebig end 32 is articulated to thecrank 34 of the crankshaft 36 (Figure 4 ). - The
crankshaft 36 continues with ashaft extension 38 which is integral with agear 40 that meshes by means of one or more idler gear 42 agear 44 integral with the rotor. - The
gears idler gears 42. This assembly of gears is contained by thebox 62 integral with thestator 2. Theidler gears 42 turn around they own axis which is constrained to the box (62) by means of bearings. - In this way, the rotation in one direction of the
crankshaft 36 corresponds to a rotation in the opposite direction of therotor 12. - Since the
shaped inserts 17, theoscillating bodies 22 and theannular flanges 14 of therotor 12 have the contiguous profiles and are made gas tight between them, it follows that, during operation, the free ends of eachoscillating bodies 22 slide tightly and are gas-tight on the cylindrical surfaces of theshaped inserts 17, while the side plane faces of theoscillating bodies 22 slide tightly and are gas tight on the inner walls of theannular flanges 14 of therotor 12. - In the
cylindrical body 4 of the stator 2 (in the configuration shown inFigures 1 and2 ) there are anexhaust port 46, anintake port 48, acooling fluid inlet 50 and acooling fluid outlet 52. The cooling fluid flows inside thecooling jacket 51 formed inside thestator 4. In the case where the machine is used as an engine, there is also a threadedseat 54 provided with aspark plug 56. - The number of ports and seats provided in the body of the
stator 4, as will be seen below, may vary according to the number of phases of the cycle, type of cycle and practical use of the machine. - The space indicated in
Figure 1 between the cavity of thestator 4, which houses the electrodes of thespark plug 56, the oscillatingbody 22 positioned at the second (TDC) top dead center and theshaped insert 17, constitutes the combustion chamber (or clearance volume) 58. - The rotor is connected to a
drive shaft 60 constituting the power take-off of the machine, whichshaft 60 is contained by thebox 64 integral with thestator 2. - The operation of the machine according to the invention is as follows with reference to
Figures 5-17 in which a four phases cycle is shown. - For greater clarity, we will analyze the complete rotation of a single mechanical assembly consisting of an oscillating
body 22, a connectingrod 30 and acrank 34 and two shapedinserts 17. - In particular:
- the clockwise rotation of the
rotor 12 drags thepin 24 and thegudgeon pin 26, which are integral with the oscillatingbody 22, in clockwise rotation, - the anticlockwise rotation (synchronous with respect to the rotation of the rotor) of the
crankshaft 36 drags thecrank 34 in an anticlockwise rotation. - The connecting
rod 30 has thesmall end 28 articulated to thegudgeon pin 26 of the oscillatingbody 22 and thelarge end 32 articulated to thecrank 34 of thecrankshaft 36. - Therefore, the
crank 34, in an eccentric anticlockwise rotary motion, forces (via the connecting rod 30) theoscillating body 22 to perform, during rotation, an reciprocating rotary movement between a TDC (top dead center) and an BDC (bottom dead center) and vice versa. - This rotary oscillation has the
pin 24 as the center of rotation and it is cyclic ie, the transition from the TDC (top dead center) to the BDC (bottom dead center) happens in the firsts 90 ° of rotation of the rotor 12 (figs 5-8 ), and vice versa the transition from the BDC to the TDC happens in the successive rotation of 90° of therotor 12 according to a cycle that is repeated continuously (figs 8-11 ). Therefore the complete oscillation of the oscillatingbody 22 happens every 180 ° of rotation of the rotor 12 (Figures 5-11 ), therefore every oscillating body will have two positions at TDC (top dead center) and two positions at BDC (bottom dead center) every turn of therotor 12. - During the suction (intake) phase (
Fig. 5-8 ) the air enters the machine through theintake port 48, filling thechamber 20 whose volume cyclically increases from a minimum value to TDC (top dead center) (Fig. 5 ) to a maximum value to BDC (bottom dead center) (fig 8 ). - This phase, excluding of the friction of moving parts, does not absorb energy from the system.
- During the compression phase (
Figures 8-11 ) the air, previously aspirated, is compressed in thechamber 20 whose volume cyclically decreases from a maximum value BDC (bottom dead center) (Fig. 8 ) to a minimum value TDC (top dead center) (Fig. 11 ) and in this way the air, forced in a environment that decreases in volume, increases in pressure and temperature. - The ratio between the initial (maximum) and final (minimum) chamber volume is called the compression ratio; the final volume of the chamber is called the combustion chamber (or clearance volume) 58.
- This phase, excluding of the friction of moving parts, absorbs energy from the system.
- In the subsequent burst/expansion phase (
Figures 11-14 ), a fuel charge is dosed in the air previously compressed to forming a fuel-air mixture that burst with the spark ofignition spark plug 56, in turn commanded by a device suitably synchronized with the general motion of the system. - This combustion generates heat which further raises the temperature and pressure of the ignited mixture. The pressure applied to the walls of the
chamber 20 causes the expansion of the chamber itself (expansion which can occur only during the rotation of the rotor 12) whose volume increases from a minimum value TDC (in which the pressure is maximum) (Fig. 11 ) to a maximum value BDC (where the pressure is minimal) (Fig. 14 ). - This phase, excluding of the friction of moving parts, provides energy to the system.
- In the subsequent and final exhaust phase (
Figs 14-17 ) the residual combustion products through theexhaust port 46 are expelled from the chamber whose volume cyclically decreases from a maximum value BDCfig.14 ) to a minimum value TDC (fig 17 ). - This phase, excluding of the friction of moving parts, does not absorb energy from the system.
- Since at each rotation of 360° of the
rotor 12 corresponds to a contrary rotation of 360° of thecrankshaft 36, an angle of 720 ° is achieved between the two members for each revolution of the axis of therotor 12. - Considering that a reciprocating motion machine achieves a useful phase every 180 ° of rotation of the axis, the present machine produces for each
oscillating body 22, four useful phases (720 ° /180 ° = 4) at each revolution of therotor axis 12. - It follows that the machine described here produces a phase every 90 ° of rotation of the rotor axis. For example, each oscillating body can perform the intake / compression / burst / exhaust cycle typical of a 4-stroke endothermic engine at each revolution of the rotor as indicated in
Figures 5-17 . - By changing the configuration of the
stator 4, each oscillating body can realize the two-stroke intake / compression cycle, typical of a fluid machine, twice with each revolution of the rotor12 as indicated inFigures 18 - 30 .
the machine can be used as a engine by adopting a cycle with the four phases described above because the burst / expansion phase provides the system with the energy necessary to overcome the friction generated by the moving parts as well as the passive forces that develop during air compression phase in a balance sheet that remains positive even after deducting these losses. (Fig. 5-17 ). - In a variant embodiment, the machine can be used as an operating machine by adopting a two-stroke cycle, such as the intake phase and the compression phase, typical of a fluid machine (as a compressor or as a pump, etc.).
- In this case the energy required to overcome the frictions as well as the passive forces that develop during the phases must be provided by an external source. (Figg.18-30).
Claims (6)
- Positive displacement machine with oscillating and rotary pistons characterized by comprising- a fixed stator (2)- a rotor (12) coaxial to the stator- at least one intake port (48) housed in the stator and which puts the rotor in communication with the external environment- at least one exhaust port (46) housed in the stator and which puts the rotor in communication with the external environment- a crankshaft (36) coaxial to the stator and to the rotor- bearings integral with the rotor (12) and supporting the crankshaft (36)- bearings integral with the stator (2) and supporting the rotor (12)- an inverter of the rotation motion which engages the crankshaft (36) and the rotor (12) to have opposite and synchronous rotations- at least two shaped inserts (17), integral with the rotor that delimit a chamber (20)- at least one oscillating body (22) inside the chamber (20), this oscillating body (22) having one of the end in correspondence of the first shaped insert (17) of the rotor (12), and being integral with a pin (24) which in turn is articulated to the annular flanges (14) of the rotor (12) and having furthermore articulated, in a median position, by means of a gudgeon pin (26) at the small end (28) of a connecting rod (30) whose the big end (32) is articulated to the crank (34) of the crankshaft (36).
- A machine according to claim 1, characterized in that the rotation motion inverter consists of a gear (40) integral with the crankshaft (36) a gear (44) integral with the rotor (12), at least one idler gear (42), integral with the box (62) that turns around its own axis and meshes the gears (40) and (44) to rotate with reverse and synchronous rotative motion.
- A machine according to claim 1 characterized in that it further comprises a spark plug of ignition.
- A machine according to claim 2 characterized in that the gears (40) and (44) have the same constructive characteristics and specular shape and share the same teeth type with the idler gear (42).
- A machine according to claim 1, characterized in that, at each rotation of the rotor (12) of 90 °, a space (58) is formed between the cavity of the stator (4) which houses the electrodes of the spark plug (56), the oscillating body (22) in rotation when it reaches the second top dead center (TDC) and the shaped insert (17), said space constituting the combustion chamber and having two between the walls containing it, one in the stator (4) and one in the shaped insert (17) of the rotor (12) in the opposite positions.
- A machine according to claim 1 characterized in that it comprises at least a couple of connecting rod (30) - crank (34) for each individual oscillating body (22).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP18180423.8A EP3587732A1 (en) | 2018-06-28 | 2018-06-28 | Positive displacement machine with oscillating and rotary pistons |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP18180423.8A EP3587732A1 (en) | 2018-06-28 | 2018-06-28 | Positive displacement machine with oscillating and rotary pistons |
Publications (1)
Publication Number | Publication Date |
---|---|
EP3587732A1 true EP3587732A1 (en) | 2020-01-01 |
Family
ID=62841850
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP18180423.8A Pending EP3587732A1 (en) | 2018-06-28 | 2018-06-28 | Positive displacement machine with oscillating and rotary pistons |
Country Status (1)
Country | Link |
---|---|
EP (1) | EP3587732A1 (en) |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1715490A (en) | 1924-05-20 | 1929-06-04 | William D Ballerstedt | Rotary steam engine |
US3320936A (en) | 1964-12-23 | 1967-05-23 | Edward R Phalen | Bi-rotary engine with oscillating vanes |
US3373723A (en) | 1966-08-01 | 1968-03-19 | Donald N. Blosser | Internal combustion engine |
DE2234950A1 (en) | 1972-07-15 | 1974-01-31 | Karl Speidel | CENTER-AXIS ROTARY PISTON MACHINE WITH A CIRCULAR HOUSING CONTOUR, PREFERRED AS A COMBUSTION MACHINE ACCORDING TO THE GASOLINE OR DIESEL PRINCIPLE |
US4149833A (en) * | 1975-06-16 | 1979-04-17 | Idram Engineering Company Est. | Rotary machine with pistons pivotally mounted on the rotor |
FR2666377A1 (en) * | 1990-09-03 | 1992-03-06 | Ducrot Gilbert | Rotary internal combustion engine |
FR2738285A1 (en) * | 1995-08-30 | 1997-03-07 | Paris Laurent Guy | Rotary internal combustion engine |
-
2018
- 2018-06-28 EP EP18180423.8A patent/EP3587732A1/en active Pending
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1715490A (en) | 1924-05-20 | 1929-06-04 | William D Ballerstedt | Rotary steam engine |
US3320936A (en) | 1964-12-23 | 1967-05-23 | Edward R Phalen | Bi-rotary engine with oscillating vanes |
US3373723A (en) | 1966-08-01 | 1968-03-19 | Donald N. Blosser | Internal combustion engine |
DE2234950A1 (en) | 1972-07-15 | 1974-01-31 | Karl Speidel | CENTER-AXIS ROTARY PISTON MACHINE WITH A CIRCULAR HOUSING CONTOUR, PREFERRED AS A COMBUSTION MACHINE ACCORDING TO THE GASOLINE OR DIESEL PRINCIPLE |
US4149833A (en) * | 1975-06-16 | 1979-04-17 | Idram Engineering Company Est. | Rotary machine with pistons pivotally mounted on the rotor |
FR2666377A1 (en) * | 1990-09-03 | 1992-03-06 | Ducrot Gilbert | Rotary internal combustion engine |
FR2738285A1 (en) * | 1995-08-30 | 1997-03-07 | Paris Laurent Guy | Rotary internal combustion engine |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
RU2439333C1 (en) | Rotary piston machine of volumetric expansion | |
RU2627487C2 (en) | Rotary piston engine | |
US7827956B2 (en) | Revolving piston internal combustion engine | |
US6401686B1 (en) | Apparatus using oscillating rotating pistons | |
US20110048370A1 (en) | Revolving piston internal combustion engine | |
JPH05503334A (en) | rotary internal combustion engine | |
JPS6147967B2 (en) | ||
US20070062469A1 (en) | Rotary radial internal combustion piston engine | |
EP0422082B1 (en) | Radial cylinder machine | |
US9528585B2 (en) | Piston engine | |
JPS6147966B2 (en) | ||
EP3587732A1 (en) | Positive displacement machine with oscillating and rotary pistons | |
US6357397B1 (en) | Axially controlled rotary energy converters for engines and pumps | |
RU2593858C1 (en) | Combined rotary piston internal combustion engine | |
WO2009040733A2 (en) | Device for converting energy | |
US3381670A (en) | Rotary internal combustion engine | |
US5259739A (en) | Non-reciprocating multi-piston engine | |
RU2699864C1 (en) | Volumetric type rotary machine | |
RU2054122C1 (en) | Rotor-vane engine | |
EP2826954B1 (en) | Rotary piston mechanism assembly | |
EP1956188A1 (en) | Hypocycloid rotary internal combustion engine | |
US8684714B2 (en) | Internal orbital engine | |
AU621650B2 (en) | Radial cylinder machine | |
US3332613A (en) | Divergent cam expansible chamber device | |
RU2067187C1 (en) | Torus-ring piston machine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION HAS BEEN PUBLISHED |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
AX | Request for extension of the european patent |
Extension state: BA ME |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE |
|
17P | Request for examination filed |
Effective date: 20200630 |
|
RBV | Designated contracting states (corrected) |
Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
|
17Q | First examination report despatched |
Effective date: 20211006 |