Rotating cylinder internal combustion engine

• US 5,375,564 A
• Filed: 12/10/1991
• Issued: 12/27/1994
• Est. Priority Date: 06/12/1989
• Status: Expired due to Fees

• Current Assignee: Josef Gail
• Original Assignee: Josef Gail
• Inventors: Gail, Josef
• Primary Examiner(s): Koczo, Jr., Michael
• Application Number:
  US07/793,431
• Time in Patent Office: 1,113 Days
• Field of Search: 91/493, 123/44 R, 123/44 D, 123/44 C, 60/39.6
• US Class Current: 123/44.00C
• CPC Class Codes: F01B 13/068 the connection of the pistons with an actuated or actuating element being at the inner ends of the cylinders
• CPC Class Codes: F01B 2009/045 Planetary gearings
• CPC Class Codes: F02B 2075/1824 six
• CPC Class Codes: F02B 57/08 Engines with star-shaped cylinder arrangements

Abstract

The reciprocating engine which is particularly useful as an internal combustion engine, comprises a housing (1) with, mounted to rotate about a first axis of rotation (7), a cylinder rotor (5) having three pairs of cylinders (15) which are angularly offset in respect of one another by 120° about the first axis of rotation (7). Disposed in the cylinders (15) are pistons (17) which are rigidly connected to one another in pairs by piston rods (19). Also mounted in the housing is a crank shaft (23) which is rotatable about a second axis of rotation (25) which is axially parallel with and offset by a predetermined eccentricity (e) in relation to the first axis of rotation (7). The piston rods (19) of the pairs of pistons are guided on the crank shaft (23) by means of eccentric bearings (27, 31). The eccentric bearings (27, 31) define in relation to the crank shaft (23) fixed axes of rotation (33) which, are angularly offset by 120° in respect of one another. The cylinder rotor (25) is torsionally rigidly coupled to the crank shaft (23) solely via the piston rods (19) and their eccentric bearings (27, 31) which are fixed in relation to the crank shaft. The fresh air compressed by a waste gas supercharger (37, 39) is fed to the internal combustion engine via a heat exchanger (45) in order to increase the efficiency.

Claims

1. An internal combustion reciprocating engine, comprising:

a housing;

a cylinder rotor supported in said housing for rotation about a first axis of rotation, wherein said cylinder rotor includes at least three pairs of cylinders angularly offset relative to each other about the first axis of rotation by 120°

, wherein cylinders of each pair are arranged on opposite sides of the first axis of rotation and have a common axis extending perpendicular to the first axis of rotation, wherein a piston is arranged in each cylinder for displacement therein, and wherein a piston rod rigidly connects the pistons of each of the pairs of cylinders;

a crankshaft supported in said housing for rotation about a second axis of rotation extending parallel to the first axis of rotation and offset relative thereto by a predetermined eccentricity;

eccentric bearings supported on said crank shaft for guiding the piston rods of the pairs of cylinders, wherein said eccentric bearings define third axes of rotation which are offset relative to each other about a second axis of rotation by 120°

, wherein the third axes of rotation extend parallel to the second axis of rotation and are spaced from the second axis of rotation by the predetermined eccentricity, and further wherein each of said eccentric bearings comprises a cam disc fixedly supported on said crankshaft and is received in a bearing opening of a respective piston rod, and wherein the axes of said cam discs define the third axes of rotation;

wherein said cam disc has a bearing radius which is greater than the predetermined eccentricity, and wherein the ratio of the bearing radius to the predetermined eccentricity is approximately between 2.5 and 3.

2. The internal combustion reciprocating engine of claim 1, wherein said housing has at least one inlet aperture and at least one outlet aperture, wherein each of said cylinders has opening means communicating with said inlet and outlet apertures during rotation of said cylinder rotor, wherein said engine further comprises a compressor communicating with said gas inlet aperture for introducing fresh gas into a respective cylinder when it passes said gas inlet aperture, and wherein the piston which is displaceable in the respective cylinder has a radially outer dead center position, and further wherein the respective cylinder has a dead space volume and said gas inlet aperture is so arranged that the dead space volume of the respective cylinder is charged with fresh gas before the piston reaches the radially outer dead center position thereof.

3. The internal combustion reciprocating engine of claim 2, wherein the piston has a crown having at least one depression defining the dead space volume of the respective cylinder.

4. The internal combustion reciprocating engine of claim 1, wherein said housing has at least one inlet aperture and at least one outlet aperture, wherein each of said cylinders has opening means communicating with said inlet and outlet apertures during rotation of said cylinder rotor,

wherein said gas outlet aperture comprises separate first and second outlets arranged one after another in a rotational direction of said cylinder rotor, and wherein said engine further comprises a waste gas turbine communicating with said first outlet.

5. The internal combustion reciprocating engine of claim 4, wherein said housing has a wall portion which separates said first and second outlets and which has a width greater than a width of an open end of the cylinder.

6. The internal combustion reciprocating engine of claim 1, wherein said piston has an axial dimension which is greater than a circumferential dimension thereof.

7. The internal combustion reciprocating engine of claim 6, wherein said piston has flat axial sides and peripheral sides which are one of flat and semi-cylindrical.

8. The internal combustion reciprocating engine of claim 7, wherein the axial and peripheral sides of said piston have grooves therein for receiving sealing strips overlapping each other in transitional regions between grooves of the axial and peripheral sides.

9. The internal combustion reciprocating engine of claim 2, further comprising:

a waste gas turbine for driving said compressor; and

fuel feed means for supplying fuel into a stream of fresh gas flowing from said compressor to said gas inlet aperture; and

a heat exchanger communicating with said gas outlet aperture for heating one of the fresh gas and a mixture of fresh gas and fuel.

10. The internal combustion reciprocating engine of claim 9, wherein said heat exchanger forms a part of a wall of said housing in a region of said gas outlet aperture.

11. The internal combustion reciprocating engine of claim 9, wherein said heat exchanger has a body, first passages which are formed in said body and which extend substantially perpendicular to the first axis of rotation, and which are open in a vicinity of said gas outlet aperture, and wherein said heat exchanger has second passages extending, in a tangential direction with respect to said cylinder rotor, in a flowing path of the fresh gas from said compressor to said gas inlet aperture.

12. The reciprocating combustion engine of claim 1, wherein at least one of the end faces of said cylinder rotor and an inner surface of a wall of said housing which faces said at least one end face have cooling fins thereon which extend one of parallel to the first axis of rotation and interengage with each other to form a labyrinth.

13. The internal combustion reciprocating engine of claim 12, wherein said labyrinth has inner and outer peripheries connected with an oil circuit, wherein said housing has a peripheral chamber for closing said labyrinth at one side thereof, and wherein said cylinder rotor has a splash disc extending into said peripheral chamber to form a labyrinth seal adjacent an axial end wall of said housing.

14. An internal combustion reciprocating engine comprising:

a housing;

a cylinder rotor supported in said housing for rotation about a first axis of rotation, wherein said cylinder rotor includes at least three pairs of cylinders angularly offset relative to each other about the first axis of rotation by 120°

, wherein cylinders of each pair are arranged on opposite sides of the first axis of rotation and have a common axis extending perpendicular to the first axis of rotation, wherein a piston is arranged in each cylinder for displacement therein, and further wherein a piston rod rigidly connects pistons of each of the pairs of cylinders;

a crankshaft supported in said housing for rotation about a second axis of rotation wherein said crankshaft extends parallel to the first axis of rotation and is offset relative thereto by a predetermined eccentricity;

eccentric bearings supported on said crankshaft for guiding piston rods of the pairs of cylinders, wherein said eccentric bearings defined third axes of rotation which are offset relative to each other about a second axis of rotation by 120°

, wherein the third axes of rotation extend parallel to the second axis of rotation, and are spaced from the second axis of rotation by the predetermined eccentricity, wherein each of said eccentric bearings comprises a cam disc fixedly supported on said crankshaft and are received in a bearing opening of a respective piston rod, wherein axes of said circular cam discs define the third axes of rotation;

wherein said housing has at least one inlet port and at least one outlet port, wherein each of said cylinders has radially outer and inner chambers, which are defined by the piston, and wherein said radially inner chamber communicates with said inlet and outlet ports during rotation of said cylinder rotor.

15. The internal combustion reciprocating engine of claim 14, wherein said radially outer chamber has a gas inlet aperture, and wherein said outlet port communicates with said gas inlet aperture.

16. The internal combustion reciprocating engine of claim 15, wherein said radially outer chamber has a gas outlet aperture, said engine further comprising a waste gas turbine communicating with said gas outlet aperture, and a fresh gas compressor, which is driven from said waste gas turbine, communicating with said gas inlet aperture.

17. The internal combustion reciprocating engine of claim 14, wherein said cylinder rotor has a tapering outer peripheral surface, and wherein said housing has an inner tapering peripheral surface complementary to said outer peripheral surface of said cylinder rotor.