Combustion engine without compression and method

Abstract

A none-compression internal combustion rotor motor and method to eliminate all of the disadvantages of the presently available internal combustion engines. By eliminating the compression stroke, increasing the efficiency. By replacing the crank shaft, the valve train and the cast iron parts with the main rotor, the combustion pressure can be converted into much higher rotational power and torque and efficiency. By having less parts, and by manufacturing from aluminum, eliminating all of the cast iron parts, reducing the manufacturing energy consumption. By having only balanced rotating parts that rotate on bearings without touching each other, greatly increasing the lifetime of the motor. The none-compression internal combustion rotor motor is air cooled needing no coolant, making it environmentally friendly.

Claims

1. A non-compressive internal combustion rotor-motor, comprising: a main rotor having a central tubular main shaft and a drum spaced apart from the tubular main shaft by a plurality of spacers, the drum surrounding the tubular main shaft in an axial direction; a plurality of holes for venting located between the tubular main shaft and the drum; two opposing blades arranged on the drum, configured to rotate with the tubular main shaft; at least three c-shaped timing rotors; a front side disk and a rear side disk, the front side disk and the rear side disk each comprising a plurality of bearings configured to engage respective ones of the main rotor and the at least three c-shaped timing rotors, wherein each of the plurality of bearings for the at least three c-shaped timing rotors are inserted into respective edges of the front side disk and the rear side disk, and wherein the tubular main shaft engages at least one of the plurality of bearings; a main timing gear affixed to the main shaft proximal the front side disk and in engagement with the at least three c-shaped timing rotors, wherein the main timing gear is configured to synchronize rotation of the at least three c-shaped timing rotors in a manner allowing the two opposing blades to pass through spaces occupied by the c-shaped timing rotors as the two opposing blades rotate with the tubular main shaft; wherein the c-shaped timing rotors individually enclose a space between a combustion chamber cover and the drum to form a plurality of enclosed combustion chambers bounded by the front side disk and the rear side disk; and three combustion chamber covers, each combustion chamber cover comprising at least one fuel injector port and at least one spark plug port, the ports arranged to be temporarily coverable by each of the at least three c-shaped timing rotors, and wherein each of the two opposing blades, when passing through the space, are configured to provide a distance between each of the two opposing blades and an associated one of the at least three c-shaped timing rotors.

2. The non-compressive internal combustion rotor-motor of claim 1 wherein the main rotor and each of the c-shaped timing rotors are balanced relative to each other.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 illustrates a cross-section of a non-compressive internal combustion rotor-motor in a first position;

(2) FIG. 2 illustrates the cross-section in a second position;

(3) FIG. 3 illustrates the cross-section in a third position;

(4) FIG. 4 illustrates the cross-section in a fourth position;

(5) FIG. 5 illustrates the cross-section in a fifth position;

(6) FIG. 6 illustrates the cross section in a sixth position;

(7) FIG. 7 illustrates the cross-section, showing the rotation of a cover drum relative to a combustion chamber;

(8) FIG. 8 illustrates a side disc of the non-compressive internal combustion rotor-motor;

(9) FIG. 9 illustrates a top view of a timing rotor of the non-compressive internal combustion rotor-motor;

(10) FIG. 10 illustrates a cut-away view of the timing rotor;

(11) FIG. 11 illustrates a side elevation view of the timing rotor;

(12) FIG. 12 illustrates a perspective view of the timing rotor;

(13) FIG. 13 illustrates a cut-away side view of a main rotor of the non-compressive internal combustion rotor-motor;

(14) FIG. 14 illustrates a front view of the main rotor;

(15) FIG. 15 illustrates a side view of the main rotor with timing gears; and

(16) FIG. 16 illustrates a front view of the non-compressive internal combustion rotor-motor with timing gears.

DESCRIPTION

(17) The non-compressive internal combustion rotor motor and method according to the present invention comprises a plurality of side disks 40 shown in FIG. 8. The side disks 40, which may be a front disk 40 and a rear disk 40, have bearings inserted in the center for the main rotor shown in FIGS. 13 and 14, and bearings inserted in for the three timing rotors 33 (creating combustion chambers A, B, and C in FIGS. 1-6 at the edges of each side disk 40.

(18) The main rotor shown in FIGS. 13 and 14, and in cross-section in FIG. 7, has a tubular main shaft 39, with multiple spacers between the main shaft 39 and the drum 38, with a first blade 35, and a second blade 36, inserted into the bearings of the front disk 40 and rear disk 40. The main timing gear 41 is placed on the main shaft 39 at the front side of the main rotor as shown in FIG. 15.

(19) The three timing rotors 33 are preferably C shaped as shown in FIG. 9 and are inserted between the front side disk 40 and the rear side disk 40. Timing gears 41 are placed on the font side FIG. 15 and FIG. 16. to synchronize the rotation of the timing rotors 33 positions allowing the blades 35 and 36, to rotate freely while enclosing the space between the combustion chamber cover 30 (FIG. 7) and the drum 38 of the main shaft, to create an enclosed combustion chamber.

(20) In a preferred embodiment according to the present invention, the non-compressive internal combustion rotor motor has three combustion chamber covers 30 as shown in FIG. 7 containing multiple exhaust ports 32, multiple fuel injector ports 37 and spark plug ports 31. The combustion chamber covers 30 are placed on the top edges of the two side disks 40 as shown in FIG. 15 and FIG. 16 to cover the timing rotors 33, and the side disks 40 in forming each combustion chamber.

(21) In the working method of the present invention, the non-compressive internal combustion rotor motor, in the preferred embodiment, there are has three C shape timing rotors 33 in positions A, B, and C as shown in FIG. 7 and FIGS. 3-6, and three combustion chamber covers 30. The direction of rotation of the timing rotors 33 are preferably counter clockwise, and the main rotor shown in FIGS. 13 and 14 has two blades 35, 36, wherein the direction of rotation of the main rotor is clockwise.

(22) When blade 36 is in ignition position in combustion chamber A (shown in FIG. 1) the timing rotor 33 in position A encloses the space between the combustion chamber cover 30 and the main drum 38 and fuel is injected and ignited. Before blade 36 gets to the rear exhaust port 32 of combustion chamber A to let the exhaust out as shown in FIG. 2, the timing rotor 33 in the A position opens to the front exhaust port 32 of combustion chamber A with the rear edge of blade 35 in position in chamber C as shown in FIG. 2 prior to ignition.

(23) Before blade 35 reaches the rear exhaust port 32 of combustion chamber C, as shown in FIG. 3, blade 36 gets into position near chamber B for ignition. Before blade 36 reaches the rear exhaust port 32 of combustion chamber B as shown in FIG. 4, blade 35 reaches a position in chamber A for ignition. Before blade 35 get to the rear exhaust port 32 of combustion chamber A FIG. 5, blade 36 in position in chamber C FIG. 5, to get ignited. Before blade 36 reaches the rear exhaust port 32 of combustion chamber C as shown in FIG. 6, blade 35 reaches the position shown in chamber A as shown in FIG. 1.

(24) The cycle repeats itself, with six combustions per revolution, which converts the combustion pressure to pure rotational high torque turning power. Additionally, the diameter of the motor can be made in any size, the timing rotor diameter and main rotor diameter ratio can be 1-to-1, 1-to-2, 1-to-3, 1-to-4 or greater.