Internal combustion engine, particularly, a free-piston engine

• US 4,803,960 A
• Filed: 06/01/1987
• Issued: 02/14/1989
• Est. Priority Date: 06/01/1987
• Status: Expired due to Fees

• Current Assignee: Detlef Koppen
• Original Assignee: Detlef Koppen
• Inventors: Koppen, Detlef
• Primary Examiner(s): Myhre, Charles J.
• Assistant Examiner(s): Okonsky, David A.
• Application Number:
  US07/056,425
• Time in Patent Office: 624 Days
• Field of Search: 123/46 R, 123/46 A, 123/47 R, 60/595
• US Class Current: 123/46.00A
• CPC Class Codes: F02B 71/00 Free-piston engines; Engines without rotary main shaft
• CPC Class Codes: F02B 75/04 Engines with variable distances between pistons at top dead-centre positions and cylinder heads
• CPC Class Codes: F02F 3/22 the fluid being liquid

Abstract

An internal combustion engine comprises a cylinder and a piston axially movable within the cylinder and formed with cylindrical projections extending axially outwardly from the piston and being of a smaller diameter than that of the piston. The piston and its projections are formed with ducts which are connectable with inlet ports formed in the wall of the cylinder for admitting air and/or air/fuel mixture into combustion chambers of the engine and outlet ports for expelling exhaust gases from the combustion chambers, upon the movement of the piston. The ducts are formed one each within one of two longitudinal piston halves. The inlet ports, outlet ports and ducts are assigned to two longitudinal halves of the piston and its projections and arranged in the engine so that the admission of air and/or air/fuel mixture into the combustion chambers and the removal of exhaust gases therefrom via short, low-turbulence paths are controlled only by the position of the piston and its projections within the cylinder.

Claims

1. An internal combustion engine, more specifically a free-piston engine, having at least one cylinder (1) comprising one piston (4) therein arranged and guided to be movable and sealed, which piston may perform axial stroke elements within a cylinder chamber (9), and featuring cylindrical projections (7,8) extending axially away from said piston (4) to either side and having at least over part of their length of diameter smaller than the diameter of the piston (4), said projections (7,8) being guided at least over some part of their length within axial cylinder bores (12,13) and therein partially sealed;

and having combustion chambers (10,11) within the cylinder (1), said combustion chambers being formed and delimited by certain parts of an inside cylinder wall defining the cylinder chamber (9) and by certain surface parts of the piston (4) and its projections (7,8), the surfaces defining said combustion chambers (10,11) being formed more particularly by end faces (5 and 26, or 6 and

     27); and

having inlet ports (2) arranged in a longitudinal cylinder wall (100) to admit air, and outlet ports (3) arranged within the longitudinal cylinder wall (100) so as to permit exhaust gases to be expelled, said inlet ports (2) and outlet ports (3) being opened and closed depending upon the axial position of the piston (4) and its projections (7,

     8); and

having ducts (18,19) within said piston (4) and its projections (7,8), wherein said ducts permit the controlled passage of gases such as air and fuel/air mixtures by forming flow path connections linked to bores (20,21) located in lateral surfaces (101,102) of the projections (7,8), and said ducts may be brought into open flow connection and blocked with respect to said inlet ports (2) depending upon the axial position of said piston (4) and its projections (7,8) relative to the cylinder (1), said ducts may also be brought into open flow connection with said combustion chambers (10,11) via said bores (20,21) and blocked by means of said axial cylinder bores (12,13) at approximately identical axial piston positions relative to said cylinder (1); and

wherein said ducts (18 and

     19) are arranged separately from each other, one each within one of two longitudinal piston halves (401 and

     402) and their respective projection (7 or

     8), located to either side of a symmetry plane (K) arranged perpendicularly with respect to the longitudinal axis (A-A) of the piston (4);

each of said ducts (18 or

     19) being connected with a corresponding orifice (90 or

     91) located within a peripheral surface (80) of the piston (4), said orifices (90 or

     91) being arranged in an area of radial planes (K1 or K2) located parallel to and at a distance (a) from said symmetry plane (K) of the piston (4);

all ports (2) located in the longitudinal cylinder wall (100) being arranged in the area of the symmetry plane (Z) of the cylinder (1);

said outlet ports (3) for the combustion chambers (10 or

     11) being separate from each other in areas located in radial planes (Z1 or Z2) in parallel to and at a second distance (b) from the symmetry plane (Z) of the cylinder (1);

the first distance (a) of the orifices (90 or

     91) at either side of the symmetry plane (K) of the piston (4) and the second distance (b) of said outlet ports (3) at either side of the symmetry plane (Z) of the cylinder (1) being defined so that all the inlet ports (2) may be in open flow path connection with the orifices (90 or

     91), the ducts (18 or

     19), the bores (20 or

     21) and the combustion chamber (10 or

     11) associated with one of said longitudinal halves (401 or

     402) of said piston whenever the end face (6 or

     5) of the opposite longitudinal half of the piston (402 or

     401) is near the respective end face (27 or

     26) of the cylinder chamber (9).

2. Internal combustion engine according to claim 1, wherein the end faces of said projections may act upon a fluid to increase its pressure, wherein said fluid consists of a gas or a hydraulic fluid actuating a system operated by a pressure fluid, which system is directly driven by said internal combustion engine.

3. Internal combustion engine according to claim 1, wherein said combustion chambers (10, 11) both feature toroid-like recesses (83,84) in their end faces (5,6 or 26,27) arranged coaxially with respect to said projections (7,8).

4. Internal combustion engine according to claim 3, wherein said toroid-like recesses (83,84) are formed within the end faces (26,27) of the cylinder chamber (9).

5. Internal combustion engine according to claim 4, wherein said toroid-like recesses (83,84) are formed into the end faces (5,6) of the piston (4).

6. Internal cmbustion engine according to claim 1, having injection nozzles and spark electrodes acting into the combustion chambers and arranged within the cylinder end faces delimiting said combustion chambers, wherein said injection nozzles (28,29) and spark electrodes (128,129) are located in a ring-shaped arrangement surrounding the longitudinal axis (A-A).

7. Internal combustion engine according to claim 3, wherein said injection nozzles (28,29) and spark electrodes (128,129) end at said toroidike recesses (82,84).

8. Internal combustion engine according to claim 1, wherein said bores (20,21) on the periphery of the projections (7,8), and inlet ports (2) on the periphery of the longitudinal cylinder wall (100), and the outlet ports (3) on the periphery of said longitudinal cylinder wall (100) are arranged in a ring-like pattern.

9. Internal combustion engine according to claim 1, wherein in order to control injection and ignition timing, displacement transducers (30,31) are located within said cylinder wall and are arranged with the cylinder (1) in order to capture the axial position of the piston (4).

10. Internal combustion engine according to claim 9, wherein said displacement transducers (30,31) are magnetic field sensors operating electrically and delivering a voltage depending upon the piston position, said voltage, upon processing by electrically operated components, being used to correlate injection and ignition timing with the axial position of the piston (4) within the cylinder (1).

11. Internal combustion engine according to claim 1, wherein within the longitudinal cylinder wall (100), axes of the inlet ports (2) are spaced, relative to the longitudinal axis (A--A), so that a rotational movement around the longitudinal axis (A--A) is superimposed upon the axial travel of the piston (4) and its projections (7,8).

12. Internal combustion engine according to claim 1, wherein said ducts (18,19) are each configured as at least a single individual duct.

13. Internal combustion engine according to claim 12, wherein said ducts (18, 19) are formed to have substantially constant flow crosssections.

14. Internal combustion engine according to claim 1, wherein said projections (7,8) exhibit axially juxtaposed longitudinal sections (121 through 126) formed by cylindrical lateral surfaces, said longitudinal sections having differing diameters relative to adjoining longitudinal sections, so that end faces spaced axially and pointed towards and away from said piston (4) are formed along said projections (7,8) said cylindrical lateral surfaces being movably and slidingly guided within corresponding axial cylinder bores (12 and 13, 133 through 136) of respective diameters and so that suitable sealing means (14,15) are provided between said cylindrical lateral surfaces and the corresponding axial cylinder bores (12 and 13, 133 through 136) therewith associated.

15. Internal combustion engine according to claim 14, wherein said projections (7,8) each have, axially side by side and in a direction away from the piston (4) at least a first longitudinal section (121,122) having a cylindrical lateral surface and a diameter smaller than the diameter of the piston (4) and a second longitudinal section (123,124) having a cylindrical lateral surface the diameter of which is greater than the diameter of said first longitudinal section (121,122).

16. Internal combustion engine according to claim 15, wherein said projections (7,8) each have, axially side by side and in a direction away from said piston (4), three sequential longitudinal sections (121 through 126) each having a cylindrical lateral surface, a diameter of either terminal longitudinal section (125,126) formed at the free end of each of said projections (7,8) being smaller than the diameter of each adjacent longitudinal section 123,124).

17. Internal combustion engine according to claim 1, wherein free ends of said projections are plunged and radially sealed into an axial cylinder bore delimited at an end thereof by a face formed by the cylinder, the plunging depth depending upon axial piston positions without allowing any of free end faces of said projections reach the face terminating said axial cylinder bore so that, within said cylinder bore, a variable-volume chamber is formed between said end faces positioned opposite to each other, the free face of the corresponding projection acting within said variable-volume chamber acting to increase pressure of a given volume of fluid, and wherein valve-controlled supply and removal, controlled via valves of the pressure fluid actuating a system operated by such pressure fluid into and out of said variable-volume chamber within said axial cylinder bores (12,13,135,136) is performed in such a manner that, by the stroke movements of the piston (4) and its projects (7,8), a pressure fluid pump is formed, which pump has two pressure generating chambers and is integrated, together with the internal combustion engine, into said cylinder (1) as a power source actuating the system operated by a pressure fluid.

18. Internal combustion engine according to claim 15, wherein said axial cylinder bores (133,,134) designed to receive two second longitudinal sections (123,124) of the projections (7,8) have an axial length at least sufficient to permit either of said second longitudinal sections (123,124) of the projections (7,8) to perform, depending upon the stroke of the piston (4), an axial stroke as a disk-shaped piston, which stroke is equal to a maximal possible stroke of the piston (4) within the cylinder chamber (9).

19. Internal combustion engine according to claim 18, wherein bores (151 through 158) piercing the wall of the cylinder (1) are provided at the ends of said axial cylinder bores (133, 134) provided for the second longitudinal sections (123,124) of the projections (7,8), which bores (151 through 158) have associated with them controlling valves, some of said bores (151,153,155 and 157) serving as outlets and some of said bores (152,154,156 and a58) serving as inlets for a fluid, and each pair of one inlet and one outlet bore (151,152 or 153,154 or 155,156 or 157, 158) extending perpendicularly into the cylinder bores (133,134) of said second longitudinal sections (123,124) and being assigned to one variable-volume chamber formed within the cylinder bores (133,134), said one chamber being hermetically sealed with respect to chambers formed within the cylinder (1) for other pairs of the inlet bores and the outlet bores, each of said cylinder bores (133,134) being subdivided into two axially adjacent chambers of negatively correlated, variable capacity by said second longitudinal sections (123,124) forming separating, disk-shaped pistons.

20. Internal combustion engine according to claim 19, wherein supply and removal of pressure fluid to and from said variable-volume chamber within axially outermost cylinder bores (12,13 or 135,136) is caused by said end faces (87,88) formed by the cylinder (1), the controlling valves (22,23,24 and 25) for controlling said supply and removal of pressure fluid being integrated into said end faces (87,88) of the cylinder wall.

21. Internal combustion engine according to claim, 20 wherein pressure fluid has a subsidiary function of cooling the cylinder (1) in the area of walls around the cylinder chamber (9).

22. Internal chamber engine according to claim 21, wherein pressure fluid is fed, at low pressure into the cylinder (1) on its suction sides at both ends of said cylinder (1), said pressure fluid being led at either end face area of the cylinder (1) to pressure fluid ducts (81,82), said ducts being large-surface ducts and each axially running towards an opposite end of the cylinder through the longitudinal cylinder wall (100), at which opposite ends said pressure fluid may enter, under valve control, via bores and valves into axially outermost variable-volume chambers located within the terminal cylinder bores (12,13 or 135,136) and the pressure fluid may leave, at increased pressure, the variable-volume chambers located within the outermost cylinder bores (12,13 or 135,136) via a corresponding outlet valve (22,24) and exit from the cylinder (1) in a directly axial direction at the same end face of the cylinder via one of the outlets (85 or 86).

23. Internal combustion engine according to claim 22, wherein the end faces (87,86) formed by the cylinder wall are formed of at least two wall areas located parallel to each other and consisting of sealed cylinder wall components arranged adjacent to each other, and wherein an exterior terminal wall area comprises pressure fluid connections leading to a system operated by said pressure fluid and an adjacent wall area parallel to the exterior terminal wall area but located axially further towards an interior to transfer suction-side supplies into the pressure fluid ducts (81,82) comprising an inlet valve (23,24) and to direct suction-side supplies arriving from another end of the cylinder through the pressure fluid ducts (81,82) via the corresponding inlet valve (23,25) into the axially exterior, variable-volume chamber of the corresponding cylinder bore (12,13 or 135,136).

24. Internal combustion engine according to claim 1 wherein precompressed air and fuel/air mixture are supplied to the internal combustion engine via a separate compressor unit (50) through the inlet ports (2).

25. Internal combustion engine according to claim 23, wherein the end faces of said projections alternatingly act to compress a temporarily enclosed volume of air before said air is supplied to the corresponding combustion chamber of said internal combustion engine, and wherein any air and fuel/air mixture intended to fill the combustion chambers (10,11) of said engine through inlet ports (152,154,156,158) may be introduced into the corresponding axial cylinder bore (133 or 134) of the second longitudinal section (123 or 124) of the corresponding projection (7 or 8) for precompression, within one of said cylinder bores (133 or 134), by the stroke of one of said second longitudinal sections (123 or 124) depending upon the movements of the piston (4), and for transfer to the inlet ports (2) via the outlet ports (151,153,155,157) and connecting ducts.

26. Internal combustion engine according to claim 23, the piston acting to precompress air and fuel/air mixture via the end faces of its projections, the precompressed fluid being supplied to the combustion chambers via ducts within the piston, and wherein at least two variable-volume chambers within the cylinder bores (133,134) of said second longitudinal sections (123,124) of the projections (7,8) are used for precompression purposes, and their outlet ports (151, 153,155,157) may be in connection with the inlet ports (2) within the longitudinal cylinder wall (100).

27. Internal combustion engine according to claim 26, wherein during any stroke of the piston (4) and said second longitudinal section (123 or 124) of each of the projections (7,8), two outlet ports (151 and 157 or 153 and 155) located at either side of the symmetry plane (Z) and assigned to the corresponding variable-volume chamber of the cylinder bores (133 or 134) are reduced in size and are jointly linked to the corresponding inlet ports (2).

28. Internal combustion engine according to claim 19, wherein control valves are assigned to said bores (151 through 158), which valves are built into said bores (151 through 158), at least some of the valves assigned to the bores (151 through 158) being used for a control of the volume of gas filling the corresponding combustion chamber, and said control valves being fitted with an exhaust air connection and automatic control means.

29. Internal combustion engine according to claim 25, wherein a corresponding, axially outermost variable-volume chamber within the respective cylinder bore (133 or 134) is used to increase the pressure of pressure fluid actuating a system operated by such pressure fluid, said outermost chamber being linked up to pressure fluid connections (81,82,85,86) and valves (22 through 25), and axially outermost free end face at each of the projections (7,8) simultaneously constituting a large-size end face of said second longitudinal section (123 or 124), acting to increase pressure of said fluid contained within the corresponding outermost chamber, while a smaller end of said second longitudinal section (123, or 124) facing the piston (4) is used, within an adjacent, negatively-correlated variable-volume chamber formed within said axial cylinder bore (133 or 134), to precompress the air and the fuel/air mixture to be fed into said combustion chambers (10, 11).

30. Internal combustion engine according to claim 18, wherein said axially terminal cylinder bores are used to precompress air and fuel/air mixture intended to fill the combustion chambers of the engine, and wherein said axial cylinder bore (133 or 134) is configured to be fitted with valve-controlled pressure-fluid inlets and outlets, and constitutes, together with said second, larger-diameter longitudinal section (123 or 124) of the corresponding projection (7,8) an alternating piston pump for a system operated by pressure fluid.

31. Internal combustion engine according to claim 2, wherein said internal combustion engine (33) is used, within a system actuated by a hydraulic pressure fluid, together with a hydraulic drive unit (46) switchable from a motor to a pump operation and vice-versa, said drive unit (46) being coupled to an electrically driven unit (47) switchable from a starter to a dynamo operation and viceversa, and including a battery (48), said unit, in order to crank the internal combustion engine (33), may be switched to its starter operation, and in its dynamo operation (45) linked up to a hydraulic motor (36) and an accumulator (40).

32. Internal combustion engine according to claim 1, wherein said piston (4) is configured as a free piston without any direct mechanical driving link in the form of a directly articulated connection to mechanical transmission members.

33. Internal combustion engine according to claim 1, said engine having a direct mechanical drive connection acting axially via an articulated, directly linked mechanical transmission member, wherein said internal combustion engine has axial, mechanical driving links at either side thereof via articulated mechanical transmission members.