Piston Internal Combustion Engine With Generator

Abstract

A piston internal combustion engine with generator has two cylinders and cylinder heads and pistons with connecting rods and two crankshafts which are connected by gears with a ratio of 1:1 (with opposite direction of rotation). The first crankshaft with the gear is mounted parallel to the second crankshaft with the second gear in one engine case such, that the gears engage. The first crankshaft is coupled to the first generator rotor and the second crankshaft is coupled to the second generator rotor or the flywheel. The moment of inertia of the first crankshaft assembly with the first gear and the first generator rotor is equal to the moment of inertia of the second crankshaft assembly with the second gear and the second generator rotor or flywheel. The cylinders with the pistons and are positioned perpendicularly to the plane of symmetry between the crankshafts, with the axes of the pair of cylinders lying in a plane with the both pistons being at the top dead center simultaneously.

Claims

1-6. (canceled)

7. A piston internal combustion engine with a generator comprising at least two cylinders with cylinder heads and pistons with connecting rods and two crankshafts connected by gears having an opposite direction of rotation with a ratio of 1:1, wherein, a first one of the two crankshafts with a first one of the gears is mounted parallel to a second one of the crankshafts with a second one of the gears in an engine case such that the gears with the 1:1 ratio are engaged, and the first crankshaft is coupled to a first generator rotor and the second crankshaft is coupled to at least one of a second generator rotor and a flywheel, such that the moment of inertia of the first crankshaft assembly with the first gear and the first generator rotor is equal to the moment of inertia of the second crankshaft assembly with the second gear and the at least one of a second generator rotor and a flywheel, wherein further the cylinders with the pistons are positioned perpendicularly to the plane of symmetry between the crankshafts, with the axes of the pair of cylinders lying in a plane with the pistons being simultaneously centered at a top position.

8. The piston internal combustion engine of claim 7, further comprising: a plurality of balance weights associated with respective crankshafts for balancing unbalanced rotating masses of the crankshafts, the weights canceling centrifugal forces, wherein the inertia forces Fs from reciprocating masses of the crankshafts eliminate each other due to symmetrically opposite movement of identical reciprocating masses of the two crankshafts in one plane.

9. The piston internal combustion engine of claim 7, wherein the engine uses a two-stroke cycle.

10. The piston internal combustion engine of claim 7, wherein the engine uses a four-stroke cycle.

11. The piston internal combustion engine of claim 7, wherein the two cylinders are an opposed pair; and the pistons and connecting rods are located symmetrically relative to a plane of symmetry between the two crankshafts for phase shifting working cycles of the opposing cylinders.

12. The piston internal combustion engine of claim 11, wherein a working cycle of the opposed pair is shifted by one revolution.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0010] The piston internal combustion engine of the present invention will be described in more detail with reference to the attached drawings.

[0011] FIG. 1 is a cross-sectional view of a piston internal combustion engine with two cylinders with cylinder heads and pistons with connecting rods and two crankshafts connected by gears with a ratio of 1:1, which means with the opposite direction of rotation. The first crankshaft with the gear is mounted parallel to the second crankshaft with the second gear in one engine case such that the 1:1 gears are engaged. The first crankshaft is coupled to the first generator rotor and the second crankshaft is coupled to the second generator rotor. The cylinders with the pistons are positioned perpendicularly to the plane of symmetry between the crankshafts, and the axes of the pair of cylinders are lying in the plane. Both pistons are at the top dead center simultaneously. The engine has a two-stroke cycle.

[0012] FIG. 2 is a cross-sectional view of a piston internal combustion engine having a generator similar to FIG. 1 but with a four-stroke cycle.

[0013] FIG. 3 is an axonometric view with partial cross-section of a piston internal combustion engine with a generator similar to that of FIG. 1. The difference is that the engine has only one generator rotor on one crankshaft and the other crankshaft has a flywheel. Due to the larger generator rotor and flywheel diameters than the distance between crankshafts, the generator rotor is axially displaced relative to the flywheel rotor.

[0014] FIG. 4 is an axonometric view with partial cross-section of a piston internal combustion engine with a generator similar to that of FIG. 1. The difference is that one generator rotor is located at the front end of the first crankshaft and the other generator rotor is located at the rear end of the second crankshaft. The rotors have large external diameters, but they do not interfere with each other in this arrangement.

[0015] FIG. 5 is an axonometric view with partial cross-section of a piston internal combustion engine with a generator, with a two-stroke cycle and two pairs of opposed cylinders. The front pair of opposed cylinders has a working cycle shifted 180 from the rear pair of opposed cylinders. The crankshafts are fitted with the same generators on the front end.

DETAILED DESCRIPTION OF THE INVENTION

[0016] The model piston internal combustion engine of FIG. 1 consists of the two cylinders 9 and 10 with the cylinder heads 13 and 14 and the pistons 11 and 12 with the connecting rods 7 and 8 and two crankshafts 1 and 2, which are connected by the gears 3 and 4 with 1:1 ratio, which means with the opposite direction of rotation. The first crankshaft 1 with the gear 3 is mounted parallel to the second crankshaft 2 with the second gear 4 in one engine case 17 such that the gears are engaged. The first crankshaft 1 is coupled to the first generator rotor 5 and the second crankshaft 2 is coupled to the second generator rotor 6. The moment of inertia of the first crankshaft assembly 1 with the first gear 3 and the first generator rotor 5 corresponds to the moment of inertia of the second crankshaft assembly 2 with the second gear 4 and the second generator rotor 6. The cylinders 9 and 10 with the pistons 11 and 12 are positioned perpendicular to the plane of symmetry 20 between the crankshafts, with the axes of the pair of cylinders lying in the plane and both pistons 11 and 12 located in the top dead center simultaneously. The engine has a two-stroke cycle.

[0017] The model piston internal combustion engine with the generator of FIG. 2 is based on the embodiment of FIG. 1. However, the engine has a four-stroke cycle. The pistons 11 and 12 are located at the top dead center simultaneously and the ignitions occur in both cylinders at the time.

[0018] The model piston internal combustion engine with the generator of FIG. 3 is based on the embodiment of FIG. 1. A larger first generator rotor 5 is mounted on the first crankshaft 1 and a flywheel 18 is mounted on the second crankshaft 2. To avoid colliding, they are axially offset.

[0019] The model piston internal combustion engine with the generator of FIG. 4 is based on the embodiment of FIG. 1. The first generator rotor 5 is mounted on the front of the first crankshaft 1 and the second generator rotor 6 is mounted on the rear of the second crankshaft 2. The generator rotors 5 and 6 have large outer diameters, but they do not interfere with each other in this arrangement.

[0020] The model piston internal combustion engine of the generator of FIG. 5 is based on the embodiment of FIG. 1. The engine differs in having two pairs of opposed cylinders 9 and 10. The front pair of opposed cylinders has a working cycle shifted 180 from the rear pair of opposed cylinders.

[0021] For the piston internal combustion engine with the generator, the operation is following. In the engine case 17, the first crankshaft 1 with the first gear 3 and the first generator rotor 5 rotates to the opposite side than the second crankshaft 2 with the second gear 4 and the second generator rotor 6 with the same speed due to the gears 3 and 4 with the gear ratio 1:1. The first piston 11 and the second piston 12 move symmetrically with respect to the plane of symmetry 20 of the engine, so that they are always at the top dead center simultaneously. Thus, the acceleration of the reciprocating masses of the first piston 11 is identical, but in the opposite direction to the acceleration of the reciprocating masses of the second piston 12, and at the same masses, the inertia forces Fs are completely eliminating each other. When replacing the connecting rod with two mass points, the additional inertia moment of the first connecting rod 7 and the second connecting rod 8 must also be considered. If the connecting rods are identical, these moments will also be identical but opposite and thus eliminated completely. Since the axes of the first cylinder 9 and the second cylinder 10 are in the same plane, no moment is generated from the inertia forces. The balancing of the rotating masses on the first crankshaft 1 as well as on the second crankshaft 2 is done in such a way that the unbalanced rotational masses are 100% balanced by balance weights 15 and 16 and the centrifugal forces FO thus also cancel each other. The ignition in the first cylinder 9 and the ignition in the second cylinder 10 transmit torque to the generator rotors 5 and 6. Since the crankshafts 1 and 2 are synchronized by the gears 3 and 4, their angular accelerations are exactly the same but opposite. Since the moment of inertia of the first crankshaft assembly 1 with the first gear 3 and the first generator rotor 5 is equal to the moment of inertia of the second crankshaft assembly 2 with the second gear 4 and the second generator rotor 6, the reaction moments has the same magnitude but opposite sense and so the resulting reaction to the engine block is completely eliminated. Thus, the piston internal combustion engine does not transmit any forces or moments except its weight to its mounts during operation. In a two-stroke engine, simultaneous ignition occurs in the first cylinder 9 and the second cylinder 10. Moreover, if the resistance of the rotors of the generators 5 and 6 is equal, the load between the first gear 3 and the second gear 4 is minimal. The function of the gears 3 and 4 will only be to synchronize. Only slight differences will be compensated due to the different course of combustion in the first cylinder 9 and the second cylinder 10.

[0022] In a four-stroke cycle engine, a common ignition in the first cylinder 9 and the second cylinder 10 or alternating ignition is possible when the working cycles are shifted 360. In the case of alternating ignition, the operation of the generators 5 and 6 is smoother, but the gear loading of the gears 3 and 4 is significant, because the active crankshaft 1 must accelerate the second idle crankshaft 2 and vice versa.

[0023] In an embodiment of the engine, wherein the first generator rotor 5 is on the first crankshaft 1 and there is a flywheel 18 on the second crankshaft 2, the gears 3 and 4 will transmit power from the second crankshaft 2 to the crankshaft 1. In the case of common ignition in cylinders 9 and 10, however, the loading of the gears 3 and 4 is relatively favorable. The advantage may be the use of only one generator.

[0024] If the engine has several pairs of opposed cylinders 9 and 10, its operation is similar to that of a two-cylinder version. Working cycles of the different pairs of cylinders 9 and 10 can be phase shifted, and then the operation of the generator rotors 5 and 6 will be smoother and the power output will be higher.

INDUSTRIAL APPLICABILITY

[0025] The piston internal combustion engine of the present invention finds application as a range extender generator type for modern electric vehicles and aircrafts.