WO2006030255A1 - Four-stroke endothermic engine with rotating drum - Google Patents

Four-stroke endothermic engine with rotating drum Download PDF

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Publication number
WO2006030255A1
WO2006030255A1 PCT/IB2004/004333 IB2004004333W WO2006030255A1 WO 2006030255 A1 WO2006030255 A1 WO 2006030255A1 IB 2004004333 W IB2004004333 W IB 2004004333W WO 2006030255 A1 WO2006030255 A1 WO 2006030255A1
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WO
WIPO (PCT)
Prior art keywords
drum
engine
drive shaft
chamber
mixture
Prior art date
Application number
PCT/IB2004/004333
Other languages
French (fr)
Inventor
Antioco Lampis
Original Assignee
Antioco Lampis
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Antioco Lampis filed Critical Antioco Lampis
Publication of WO2006030255A1 publication Critical patent/WO2006030255A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/14Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F02C3/16Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C5/00Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/02Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant
    • F02C5/04Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant the combustion chambers being formed at least partly in the turbine rotor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C5/00Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/06Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid being generated in an internal-combustion gas generated of the positive-displacement type having essentially no mechanical power output

Definitions

  • the present invention relates to a four-stroke endothermic engine with rotating drum, having pistons spreading apart with a reciprocating motion.
  • the design of an endothermic engine with a rotating drum i. e. an engine that does not use a crankshaft for the reciprocating motion of the pistons, like in conventional engines, has always been a fixed idea. It has been pursued through different, more or less successful solutions, which had scarce or short applications, apart from one case, the Wankel engine, produced and patented in the sixties. Many of the patents intended for this aim have proved more suitable to the construction of pumps rather than of actual endothermic engines.
  • Said internal combustion engine comprises a drive shaft onto which a cylindrical drum equipped with fixed radial blades is fitted, said shaft being rotatable inside a stationary body, the engine being characterised in that said drum internally defines a cylindrical compression chamber within which two pistons are arranged, which pistons perform a reciprocating rotary motion around the drive shaft to provide for the compression of the combustible mixture; said mixture being introduced into the hollow space defined between the drum and the stationary body, into the cell defined by two subsequent radial blades, and being dragged by the rotary motion of the drum to the burst chamber, the mixture explosion causing rotation of the drum and hence generating the driving force for the whole system.
  • - Fig. 1 is an elevational side view of a longitudinal section of the engine of the invention
  • i - Fig. 2 is a front view of a front section of the engine of the invention
  • FIG. 3 is a detailed view of the device actuating the drive cams of the admission gate.
  • Fig. 4 is a schematic view, similar to Fig. 2, of a variant embodiment including lightened pistons.
  • the engine of the invention essentially comprises: a drive shaft 1; a distribution box 3; a supporting wall 5; a compression chamber 7; a rotating drum 9; a central body 11; and a closing cap 13.
  • Drive shat 1 is a cylindrical linear axle, having fitted thereon a central gear 15 and, on the opposite side, the aforementioned rotating drum 9 which will be disclosed further on.
  • Distribution box 3 froming the external portion of the engine and the end support for drive shaft 1, internally contains:
  • Such cams are integrally formed at both sides of a central wheel 31 acting as a support, and they have different tasks: one of them provides for opening admission port 33, the other for closing same by actuating gate 29;
  • the distribution box also acts as a sump for collecting lubricating oil.
  • Support wall 5 besides performing its support function, includes admission ports 33 through which the gaseous mixture will be sucked. As said, opening and closing are controlled by gate 29, through cams 25, 27.
  • Compression chamber 7 is a cylindrical, hat-shaped chamber, which is to be fastened as shown.
  • Two ejection ports 43, 45 are formed along its side, in diametrically opposite points, and the compressed gaseous mixture will pass to burst chamber 47 through said ports.
  • Two pistons 49, 51 are located within compression chamber 7. The pistons are hinged on drive shaft 1 and their movements are driven by expansion keys 21, 23. Here, drive shaft 1 only acts as a pivot.
  • Each piston 49, 51 has a particular lobe 53, 55, having only safety functions for protecting admission gate 29 from the high pressure due to compression. It is to be appreciated that such lobe will assist in closing admission port 33, but it will not hinder the passage of the compressed mixture though ej ection ports 43, 45.
  • a plurality of curved blades 61 is provided onto the drum periphery, and they have such a height that said drum is allowed to rotate inside the central body.
  • a small cell 63 with side walls 65, 67 is formed between two consecutive blades, and opening port 69 thereof allows the compressed mixture to pass into burst chamber 47, of which said cell is part together with a small recess of the central body, where ignition plug 71 is arranged.
  • a second cell wholly similar to the cell described above, is provided on the opposite side and is spaced apart by 180° with respect to the cell described above. The description of that second cell is obviously omitted.
  • Drum 9 is also integral with the impeller (not shown) of a centrifugal pump for the lubricating oil.
  • Central body 11 is the central portion of the system, and it is shown in cross-sectional view in Fig. 2. It acts as a housing and is equipped with the actual burst chambers 47 and with exhaust manifolds 73, 75.
  • pistons 49, 51 In the opening phase, pistons 49, 51 will generate a gap of about 45° into which the gaseous mixture will be sucked through admission port 33. At the same time, on the opposite side, the same pistons 49, 51, in the closing phase, will compress the previously sucked mixture and will send it towards burst chamber 47 through ejection ports 43, 45. Now rotating drum 9 is made to intervene. The drum, by rotating in counterclockwise direction and at a speed twice that of expansion keys 21, 23, will transfer the compressed mixture, through opening port 69, into burst chamber 47, where plug 71 will cause explosion thereof.
  • Fig. 4 shows a variant embodiment of the engine of the invention, where pistons 49, 51 are lightened, i. e. they have a hollow interior.
  • ducts 81 belonging to the lubrication circuit can pass through the internal cavities of the pistons.
  • keys 21, 23 could be secured onto the respective shafts 17, 19 through strengthening members.
  • a longitudinal partition could be provided within the suction duct for the gaseous mixture, in order to protect gate 29 from the high pressure during the burst phase.

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

Abstract

A four-stroke endothermic engine with a rotating drum, essentially consisting of a drive shaft (1) onto which a cylindrical drum (9) equipped with fixed radial blades is fitted, said shaft (1) being rotatable inside a stationary body (11), characterised in that said drum (9) internally defines a cylindrical compression chamber within which two pistons (49, 51) are arranged, which perform a reciprocating rotary motion around the drive shaft (1) to provide for the compression of the combustible mixture; said mixture being introduced into the hollow space defined between the drum (9) and the stationary body (11), into the cell (63) defined by two subsequent radial blades, and being dragged by the rotary motion of the drum to the burst chamber (47), the mixture explosion causing rotation of the drum (9) and hence generating the driving force for the whole system.

Description

FOUR-STROKE ENDOTHERMIC ENGINE WITH ROTATING DRUM Description
The present invention relates to a four-stroke endothermic engine with rotating drum, having pistons spreading apart with a reciprocating motion. The design of an endothermic engine with a rotating drum, i. e. an engine that does not use a crankshaft for the reciprocating motion of the pistons, like in conventional engines, has always been a fixed idea. It has been pursued through different, more or less successful solutions, which had scarce or short applications, apart from one case, the Wankel engine, produced and patented in the sixties. Many of the patents intended for this aim have proved more suitable to the construction of pumps rather than of actual endothermic engines. Other patents directly solve the problem, yet with rather complex solutions, using either a drum eccentrically positioned relative to the stationary body where it rotates, or a drum rotating within a stationary body having an external cavity acting as a combustion chamber. The present Applicant is already the owner of some solutions in this field, which are not mentioned here to avoid making the specification too heavy. Even though those solutions were valid, they remained in the project state and they have not been produced or applied on a car by a big company in the field. The present invention provides another solution, different from the above-mentioned solutions of the same Applicant.
Said internal combustion engine comprises a drive shaft onto which a cylindrical drum equipped with fixed radial blades is fitted, said shaft being rotatable inside a stationary body, the engine being characterised in that said drum internally defines a cylindrical compression chamber within which two pistons are arranged, which pistons perform a reciprocating rotary motion around the drive shaft to provide for the compression of the combustible mixture; said mixture being introduced into the hollow space defined between the drum and the stationary body, into the cell defined by two subsequent radial blades, and being dragged by the rotary motion of the drum to the burst chamber, the mixture explosion causing rotation of the drum and hence generating the driving force for the whole system.
The invention will now be described in detail with particular reference to the accompanying drawings, in which:
- Fig. 1 is an elevational side view of a longitudinal section of the engine of the invention; i - Fig. 2 is a front view of a front section of the engine of the invention;
- Fig. 3 is a detailed view of the device actuating the drive cams of the admission gate; and
- Fig. 4 is a schematic view, similar to Fig. 2, of a variant embodiment including lightened pistons.
As it is apparent from the drawings, the engine of the invention essentially comprises: a drive shaft 1; a distribution box 3; a supporting wall 5; a compression chamber 7; a rotating drum 9; a central body 11; and a closing cap 13.
Drive shat 1 is a cylindrical linear axle, having fitted thereon a central gear 15 and, on the opposite side, the aforementioned rotating drum 9 which will be disclosed further on.
Distribution box 3, froming the external portion of the engine and the end support for drive shaft 1, internally contains:
- two distribution shafts 17 and 19, integrally formed with expansion keys 21, 23, better shown in Fig. 2. As shown, said keys 21, 23 have a peculiar, lobed shape. Each shaft has a particular shape in three different regions to perform its tasks. The hatched regions of said shafts 17, 19 have a square cross-sectional shape since drive cams 25, 27, shown in Fig. 3, are to be mounted thereon.
- drive cams 25, 27 for admission gate 29. Such cams are integrally formed at both sides of a central wheel 31 acting as a support, and they have different tasks: one of them provides for opening admission port 33, the other for closing same by actuating gate 29;
- drive gears 35, 37 (only gear 35 is shown), which are fitted on shafts 17, 19, have a diameter twice that of central gear 15 fitted on drive shaft 1, and are in constant mesh with the central gear. The distribution box also acts as a sump for collecting lubricating oil.
Support wall 5, besides performing its support function, includes admission ports 33 through which the gaseous mixture will be sucked. As said, opening and closing are controlled by gate 29, through cams 25, 27. Compression chamber 7 is a cylindrical, hat-shaped chamber, which is to be fastened as shown. Two ejection ports 43, 45 are formed along its side, in diametrically opposite points, and the compressed gaseous mixture will pass to burst chamber 47 through said ports. Two pistons 49, 51, with circular-sector shape, are located within compression chamber 7. The pistons are hinged on drive shaft 1 and their movements are driven by expansion keys 21, 23. Here, drive shaft 1 only acts as a pivot. Each piston 49, 51 has a particular lobe 53, 55, having only safety functions for protecting admission gate 29 from the high pressure due to compression. It is to be appreciated that such lobe will assist in closing admission port 33, but it will not hinder the passage of the compressed mixture though ej ection ports 43, 45.
Rotating drum 9, better shown in Fig. 2 that, as said, is a front sectional view of the whole central body 11, is the member imparting the motive power to the whole system. It is directly fitted onto drive shaft 1. A plurality of curved blades 61 is provided onto the drum periphery, and they have such a height that said drum is allowed to rotate inside the central body. A small cell 63 with side walls 65, 67 is formed between two consecutive blades, and opening port 69 thereof allows the compressed mixture to pass into burst chamber 47, of which said cell is part together with a small recess of the central body, where ignition plug 71 is arranged. A second cell, wholly similar to the cell described above, is provided on the opposite side and is spaced apart by 180° with respect to the cell described above. The description of that second cell is obviously omitted.
Drum 9 is also integral with the impeller (not shown) of a centrifugal pump for the lubricating oil. Central body 11 is the central portion of the system, and it is shown in cross-sectional view in Fig. 2. It acts as a housing and is equipped with the actual burst chambers 47 and with exhaust manifolds 73, 75.
Closing cap 13 closes the assembly and forms the natural support for the drive shaft. A short description of the operation is now necessary. In cylindrical chamber 7, both peculiar pistons 49, 51 are compelled to perform a reciprocating rotary motion about drive shaft 1 onto which they are hinged. Said motion is determined by the clockwise rotation of expansion keys 21, 23, which in turn are driven by respective gears 35, 37, integral with respective shafts 17, 19. Said gears have a diameter twice the diameter of central gear 15 fitted onto drive shaft 1, and they are in constant mesh with said central gear. Both keys 21, 23 alternatively perform an active and a stand-by function. They are in phase opposition since their angular positions are shifted by 180°, so it is evident that while one key is performing the active function, the other will take the stand-by function and vice versa. During the active period, the key concerned will provide for spacing apart pistons 49, 51 on the one side, and for making them contact on the other side, while the opening and closing movement will be constantly controlled.
In the opening phase, pistons 49, 51 will generate a gap of about 45° into which the gaseous mixture will be sucked through admission port 33. At the same time, on the opposite side, the same pistons 49, 51, in the closing phase, will compress the previously sucked mixture and will send it towards burst chamber 47 through ejection ports 43, 45. Now rotating drum 9 is made to intervene. The drum, by rotating in counterclockwise direction and at a speed twice that of expansion keys 21, 23, will transfer the compressed mixture, through opening port 69, into burst chamber 47, where plug 71 will cause explosion thereof.
The explosion, because of the reaction between the drum and the central body, will cause rotation of drum 9 and hence will generate the motive power for the whole system. After explosion, the gases will expand through blades 61 of drum 9, until they reach exhaust manifold 73, 75, to which combusted gases will be sent. Since the drum, while operating, activates only one burst chamber of the two chambers it is equipped with, and since the drum rotates in opposite direction and at twice the speed of keys 21, 23, each burst chamber will be activated every 180° of rotation, thereby ensuring two active phases at each revolution. The movement of gate 29 is ensured by a drawer 79 sliding on ball guides (see Fig. 3) to reduce friction as much as possible. The opening of the admission port during the suction phase takes place thanks to the operation of cam 25, whereas the fast closing of the same port takes place through return springs 77, without awaiting intervention of the subsequent cam 27. Fig. 4, as stated, shows a variant embodiment of the engine of the invention, where pistons 49, 51 are lightened, i. e. they have a hollow interior. In such a variant embodiment, ducts 81 belonging to the lubrication circuit can pass through the internal cavities of the pistons. It is evident that the above description has been given only by way of non-limiting example, and that changes and modifications are possible without departing from the scope of the invention. For instance, keys 21, 23 could be secured onto the respective shafts 17, 19 through strengthening members. Moreover, in the alternative or in addition to lobes 53, 55 of pistons 49, 51, a longitudinal partition could be provided within the suction duct for the gaseous mixture, in order to protect gate 29 from the high pressure during the burst phase.

Claims

Patent claims
LA four-stroke endothermic engine with rotating drum, essentially comprising a drive shaft (1) onto which a cylindrical drum (9) equipped with fixed radial blades (61) is fitted, said shaft (1) being rotatable inside a stationary body (11), the engine being characterised in that said drum (9) internally defines a cylindrical compression chamber within which two pistons (49, 51) are arranged, which pistons perform a reciprocating rotary motion around the drive shaft (1) to provide for the compression of the combustible mixture; said mixture being introduced into the hollow space defined between the drum (9) and the stationary body (11), into the cell (63) defined by two subsequent radial blades (61 - 61), and being dragged by the rotary motion of the drum (9) to the burst chamber (43, 45), the mixture explosion causing rotation of the drum (9) and hence generating the driving force for the whole system.
2.The endothermic engine as claimed in claim 1, characterised in that said engine essentially comprises: a drive shaft (1); a distribution box (3); a supporting wall (5); a compression chamber (7); a rotating drum (9); a central body (11); and a closing cap (13). 3.The endothermic engine as claimed in claim 2, characterised in that the drive shaft (1) has linear cylindrical axis and has fitted thereon a central gear (15) and, on the opposite side, a rotating drum (9). 4.The endothermic engine as claimed in claim 2, characterised in that the distribution box (3), forming the external portion of the engine and the end support for the drive shaft (1), internally contains:
- two distribution shafts (17, 19), integrally formed with the expansion keys (21, 23), said keys (21, 23) having a peculiar, lobed shape;
- drive cams (25, 27) for the admission gate (29), which cams are integrally formed at both sides of a central wheel (31) acting as support, one cam providing for opening the admission port (33) and the other providing for closing same by actuating the gate (29);
- drive gears (35, 37), which are fitted on the shafts (17, 19), have a diameter twice the diameter of the central gear (15) fitted on the drive shaft (1), and are in constant mesh with the central gear.
5. The endothermic engine as claimed in the preceding claims, characterised in that the support wall (5) includes the admission ports (33) through which the gaseous mixture will be sucked, the opening and closing of those ports being controlled by the gate (29), through the cams (25, 27). ό.The endothermic engine as claimed in the preceding claims, characterised in that the compression chamber (7) is a cylindrical, hat-shaped chamber; two ejection ports (43, 45) being formed along the chamber side, in diametrically opposite points, through which ports the compressed gaseous mixture will pass to the burst chamber (47); two pistons (49, 51), with circular-sector shape, being located within said compression chamber (7) and being hinged on the drive shaft (1), the piston movements being driven by the expansion keys (21, 23), each piston (49, 51) being equipped with a particular lobe (53, 55), having only safety functions for protecting the admission gate (29) from the high pressure due to compression. 7.The endothermic engine as claimed in the preceding claims, characterised in that the rotating drum (9), which imparts the motive power to the whole system, is directly fitted onto the drive shaft (1) and is equipped onto its external peripheral portion with a plurality of curved blades (61) having such an height that said drum is allowed to move within the central body housing it. 8. The endothermic engine as claimed in the preceding claims, characterised in that a small cell (63) with side walls (65, 67) is formed between two consecutive blades (61 - 61) at the top of the engine in the drawing, the opening port (69) of the cell allowing the compressed mixture to pass into the burst chamber (47), of which the cell is part together with a small recess in the central body, where ignition plug (71) is arranged, the same arrangement being provided at the opposite side with respect to said first cell (63), where the second burst chamber is formed.
9.The endothermic engine as claimed in the preceding claims, characterised in that two burst chambers (47) are provided, which operate one at a time when the pistons (49, 51) are in the proper positions, whereby an ignition of the compressed mixture is obtained every half revolution of the rotating drum (9). lO.The endothermic engine as claimed in the preceding claims, characterised in that the pistons (49, 51) are internally lightened and both have a wide, hollow circular sector.
PCT/IB2004/004333 2004-09-16 2004-12-29 Four-stroke endothermic engine with rotating drum WO2006030255A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ITTO20040622 ITTO20040622A1 (en) 2004-09-16 2004-09-16 ENGINE ENDOTHERMIC FOUR-STROKE ROTARY DRUM
ITTO2004A000622 2004-09-16

Publications (1)

Publication Number Publication Date
WO2006030255A1 true WO2006030255A1 (en) 2006-03-23

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Application Number Title Priority Date Filing Date
PCT/IB2004/004333 WO2006030255A1 (en) 2004-09-16 2004-12-29 Four-stroke endothermic engine with rotating drum

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IT (1) ITTO20040622A1 (en)
WO (1) WO2006030255A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2023104225A1 (en) * 2021-12-09 2023-06-15 Jan Novotny Rotary combustion engine

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB122755A (en) * 1918-04-18 1919-02-06 Tom Gordon Greenwood Internal Combustion Turbine.
DE562453C (en) * 1930-01-14 1932-10-26 Sauer Hans Internal combustion turbine with compressor cylinders arranged in the impeller
GB635663A (en) * 1948-01-22 1950-04-12 Dennis Craft An internal combustion-turbine engine
GB730383A (en) * 1952-02-07 1955-05-25 Malachi Joseph Mccarty Improvements in or relating to gas turbines

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB122755A (en) * 1918-04-18 1919-02-06 Tom Gordon Greenwood Internal Combustion Turbine.
DE562453C (en) * 1930-01-14 1932-10-26 Sauer Hans Internal combustion turbine with compressor cylinders arranged in the impeller
GB635663A (en) * 1948-01-22 1950-04-12 Dennis Craft An internal combustion-turbine engine
GB730383A (en) * 1952-02-07 1955-05-25 Malachi Joseph Mccarty Improvements in or relating to gas turbines

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2023104225A1 (en) * 2021-12-09 2023-06-15 Jan Novotny Rotary combustion engine

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