PISTON ENGINE

Technical field

The present invention relates to a piston engine that performs a rotational movement of the potential energy in the gasses pressurized into the steel tank without chemical reaction.

Background

In current engine technologies, the conversion of linear force into rotational motion was achieved with Otto engine and another technology, Wankel engines. Both of these technologies and the like are technologies that use fossil fuels to generate energy by rotational motion. These fuels are very harmful to the ecosystem of our world. The piston engine, which provides the production of renewable energy with its rotational motion without chemically reacting the pressurized gasses in the technology tank, is an environmentally friendly technology that supports the ecosystem.

Object of the Invention

This technology, which aims to meet the need for portable energy with a piston engine that can produce edible energy by the rotational motion created by the pressurized gasses without chemical reaction and to protect the ecological balance of nature, is intended for mobile or fixed use in aircrafts, marine vehicles, land vehicles, spacecraft and lighting and heating in an oxygenated or oxygen-free environment.

Brief Description of the Invention

The main body of the invention is pressure resistant and is the low-pressure reservoir of the technology. While the gasses entering into the cylinder blocks in the lateral cylinder boxes through the bypass groove extending to this tank are filled through the groove at the level of the lower dead center of the pistons and the compression process is continuing, the desired pressure intensity is fixed with the valve at the upper inlet of the bypass groove and the system, which is increased to the desired pressure level with the addition of the high-pressure gas taken from the steel gas tank in accordance with the operating program and the data of the sensor, remains under pressure for approximately ninety degrees of rotation time, while towards the end of this time, this technology, which sends a volume of these pressurized gasses to the upper cylinder boxes and then back to the steel gas tank, is aimed at correlating the values obtained when circulated and pressurized in volumes designed to be able to perform four jobs in reverse symmetry within a rotation period of time. By using various connection tubes and pressure regulating mechanical or electromechanical elements, the pistons provided in said cylinder box are moved and said movement is transferred to an outlet, preferably to the flywheel.

The description of the Figures:

The piston engine for achieving the object of the present invention is shown in the accompanying figures.

Figure- 1— Perspective view of the piston engine subject to the invention.

Figure— 2 — Cross Section (A-A) view.

Figure— 3— Cross Section (B-B) view.

Figure— 4— Cross Section (C-C) view.

Figure-5— Cross Section (D-D) view.

Figure-6— Cross Section (E-E) view.

Figure-7— Cross Section (F-F) view.

Figure-8— Perspective view of main rod element.

Figure-9— Perspective view of hammer element.

Figure- 10— Perspective view of shuttle element.

Figure-11— View of gear assembly.

Figure- 12— Perspective view of crankshaft element.

Figure-13— View of connection rod element.

Figure- 14— View of piston element with ring.

Figure-15— View of cylinder element.

Figure- 16— Bulk perspective view of internal and external parts of the main body. Figure-17— Section perspective view of Main body upper half cylinder.

Figure- 18— Perspective view of steel gas tank Figure- 19— Perspective view of lateral cylinder box.

Figure-20— Perspective view of upper cylinder box.

Figure-21— Cross section and view of front cover.

Figure-22— Cross section and view of rear cover.

Figure-23— Determination of virtual planes and oscillating arcs.

Figure-24- Determination of upper and lateral surface holes.

Figure-25— Schematic view of the right-angle position of the refractive angle.

Figure-26— Schematic view of the narrow angle position of the fracture angle.

Figure-27— The technology is at the starting position when the refraction angle is again at the right-angle position and has taken the path of 80 degrees of rotation.

Description of the references in Figures;

I) Piston engine

10) Hammer element

I I) Connection rod element

12) Piston element with ring

13) Cylinder element

14) Shuttle element

15) Main rod element

16) Crankshaft element

17) Gear assembly

18) Flywheel element

19) Shaft element

100) Main body

101) Lateral surface hole

102) Gasket groove

103) Screw slot

104) Upper surface hole

105) Secondary gasket groove

106) Mounting slot

107) Pressure detection groove

108) Second screw slot

109) Detection groove ) Third screw slot ) Mounting screw ) Pressure sensor ) Fourth screw slot ) Drain valve ) Fifth screw slot ) Half cylinder slot ) Intermediate tube groove ) Sixth screw slot ) Pressurized tube groove ) Semicircular indentation ) Friction bearing ) Mounting clamp ) Screw hole ) Second mounting screw ) Seventh screw slot ) Second semicircle indentation) Multi clamp ) Third semicircle indentation) Second friction bearing ) Screw groove ) Third mounting screw ) Eighth screw slot ) Fourth semicircle indentation) Third friction bearing ) Fifth semicircle indentation) Second screw groove ) Fourth mounting screw ) Ninth screw slot ) Tertiary gasket groove ) Gasket ) Third screw groove ) Tenth screw slot ) Fifth mounting screw ) Gasket groove ) Eleventh screw slot ) Steel gas tank ) Pressure balancing tube ) Multipurpose pedestal ) Gas outlet record ) Steel belt ) Second screw hole ) Sixth mounting screw ) Manual valve ) Seventh mounting screw ) Second pressure sensor ) Lateral cylinder box ) Twelfth screw slot ) Pressure detection hole ) Eighth mounting screw ) Third pressure sensor ) Contact hole ) Ninth mounting screw ) Thirteenth screw slot ) Bypass groove ) Electric regulator ) Tenth mounting screw ) Fourteenth screw slot ) Gas inlet tube groove ) Pressurized gas inlet tube ) Pressurized gas inlet valve) Joint intermediate tube groove) Intermediate tube ) Second contact hole ) Eleventh mounting screw ) Fifteenth screw slot ) Pressurized gas outlet valve) Cylinder slot 22) Sixteenth screw slot 23) Check valve 24) Second gasket 25) Fourth screw groove 26) Twelfth mounting screw 00) Upper cylinder box 01) Joint intermediate tube groove 02) Internal groove 03) Second cylinder slot 04) Gas inlet check valve 05) Gas outlet check valve 06) Second pressure tube groove 07) Pressurized gas return tube 08) Second internal groove 09) High pressure regulator 10) Third contact hole 11) Thirteenth mounting screw 12) Seventeenth screw slot 13) Fifth screw groove 14) Sixth screw groove

415) Fourteenth mounting screw

500) Front cover

501) Shaft element hole

502) Ceramic seal

503) Revolution counter

504) Sixteenth mounting screw

505) Eighteenth screw slot

506) Seventeenth mounting screw

507) Seventh screw groove

508) Third gasket

600) Rear cover

601) Third screw hole

602) Eighteenth mounting screw

A) Main center dbd) Low pressure tank

Detailed Description of the Invention

Referring to Figure 1-7, in an embodiment, the piston engine (1) of the invention comprises the following:

- A main body (100) having two lateral cylinder boxes (300) as a double set on at least two side surfaces and two double upper cylinder boxes (400) positioned on the upper surface between the lateral cylinder boxes (300) and half cylinder slots (116) between this upper cylinder box (400) and each lateral cylinder boxes (300),

- pressure-resistant steel gas tanks (200) arranged in half cylinder slots (116) on both sides,

- a hammer element (10) arranged at its fixed center in the main body (100) and making two-way oscillating movements

- within the oscillation angle is a whole with inversely symmetrical three-center coupling apparatus on both sides of the cylinder mass that does not overlap with the central oscillation center.

- connection rod elements (11), which are connected to the centers of the three-center connection apparatus in an articulated manner,

- cylinder elements (13) in which piston elements with ring (12) are articulated from the ends of the connection rod elements (11) in order to move within the lateral cylinder boxes (300) and the upper cylinder box (400),

- the main rod elements (15) where the center of the cylinder mass of the hammer element (10) coincides with the inner rotation center and the center of the external circle of the eccentric shuttle element (14) that makes the two-way swing movements in the opposite direction, and the crankshaft elements (16) where these main rod elements (15) are connected,

- a shaft element (19) on which the rotational movements of the crankshaft elements (16) are ensured to be in opposite directions and on which the rotational movement in the desired direction is received from the gear assembly (17) and which transmits this rotational movement to the flywheel element (18),

- intermediate tubes (316) connecting said lateral cylinder boxes (300) to the upper cylinder boxes (400) in such a way as to allow fluid to pass through, - the pressure balancing tube (201) connecting said steel gas tanks (200) to each other and the pressurized gas return tube (407) connecting the multipurpose pedestal (202) and the multipurpose pedestal (202) to the upper cylinder box (400) on the pressure balancing tube (201),

- this engine, which includes pressure sensors on the multipurpose pedestal (202) and check valves that control the fluid passage between the lateral cylinder box (300) and the upper cylinder box (400), and the steel gas tanks (200) according to the data obtained from said pressure sensors, is designed with a rotation time interval of 90 degrees. This engine technology is suitable for production at 360°fully divisible angles, and this industrial design can also be revised and implemented for internal combustion piston engines.

A preferred embodiment of the invention comprises the following:

The intersection line of the virtual planes perpendicular to the oblique lateral surfaces of the upper half cylinder structure from the two joint half cylinder structures and at an angle of about (+7.1929°) with the horizontal plane is on the vertical virtual plane dividing the upper horizontal surface into two longitudinal, and this intersection line is the oscillation center of the hammer element (10) and has at least one lateral surface hole (101) perpendicular to the planes and intersection line on the lateral surface plane of the circular virtual planes of the determined dimensions, and at least one gasket groove (102) at its edge and at least one screw slot (103) and at least one upper surface hole (104) which is central to the intersection line where these virtual planes intersect on the upper surface plane, and at least one mounting slot (106) at the point of intersection with the pressurized gas outlet tube (407) of the pressure balancing tube (201) between this pair of groups with at least one secondary gasket groove (105) at its edge and connecting the two steel gas tanks (200) and on at least one multipurpose pedestal (202) fixed above the main body (100) at the point of intersection with the pressurized gas outlet tube (407)) and at least one electronic drain valve (114) fixed to at least one fourth screw slot (113) next to at least one third screw slot (110) and at least one pressure sensor (112) fixed with at least one mounting screw (111) around the at least one second screw slot (108) and at least one third screw slot (110) near the at least one detection groove (109), and at least one half cylinder slot (116) of the at least one steel gas tank (200) on the inclined surface between the upper surface having at least one fifth screw slot (115) around the upper surface holes (104) and the lateral surface. at least one mounting clamp (122) within at least one friction bearing (121) in the semicircular indentation (120) in the middle of the belt and above the circumferential gap of the mounting belt, which has a joint intermediate tube groove (117) and at least one sixth screw slot (118) on the oblique surface and is parallel to this groove (117) and is perpendicular and fixed to the surfaces joining the ends of the front and rear semicircular indentations of the upper half cylinder, which has pressurized grooves (119) located on the lateral surface side and which continues on the oblique narrow surfaces, at least one second friction bearing (129) fixed to at least one seventh screw slot (125) in the mounting belt with at least one second mounting screw (124) through at least one screw hole (123) at its ends and located in at least one third semicircular indentation (128) on both sides and at least one third semicircular indentation (130) at equal distance from the lower surface of this belt to at least one second semicircular indentation (126) on both sides and at least one screw groove on the edge thereof at least one fourth mounting screw (137) from at least one second screw groove (136) at the edge of the at least one fifth semicircular indentation (135) enclosing at least one third friction bearing (134) located in the at least one fourth semicircle indentation (133) on the parallel lower surface of the multiple clamps (127) secured to the at least one eighth screw slot (132) by a third mounting screw (131) and at least one tertiary gasket groove (139) on the long rods to which the mounting belt is perpendicular before being secured to the at least one ninth screw slot (138), and at least one gasket (140) in the at least one main body (100) fixed to the at least one tenth screw slot (142) from the at least one third screw groove (141)

At least one gas tank (200) with at least one manual valve (207) and at least one seventh mounting screw (208) fixed to the mounting slot (106) on which the at least one pressure balancing tube (201) has been inserted into at least one fixed multipurpose pedestal (202) on the main body (100) and which carries at least one gas outlet record (203) on its side and is fixed to the pressure detection groove (107) by at least one sixth mounting screw (206) through at least one second screw hole (205) on the at least one steel belt (204) on the main body (100) and is fixed to the mounting slot (106) on the fixed multipurpose pedestal (202 ) of this tank (200) at least one third pressure sensor (304) fixed with at least one eighth mounting screw (303) dependent on at least one pressure detection hole (302) from at least one twelfth screw slot (301) on its upper surface and at least one electric regulator (309) fixed with at least one ninth mounting screw (306) to at least one connection hole (305) from at least one thirteenth screw slot (307) and controlling the flow and direction of gas flow in at least one bypass groove (308) extending to the internal space of the main body (100), and at least one pressurized gas inlet valve (314) in which at least one pressurized gas inlet tube (313) is fixed in at least one pressurized gas inlet tube groove (312) fixed in at least one fourteenth screw slot (311) with at least one tenth mounting screw (310) and at least one intermediate tube (316) in at least one joint intermediate tube groove (315) and at least one eleventh mounting screw (318) in at least one second connection hole (317) through at least one fifteenth screw slot (319), the at least one check valve (323) fixed to the at least one pressurized gas outlet valve (320) and the at least one sixteenth screw slot (322) in the upper middle of the at least one cylinder slot (321) extending from the bottom to the top, and the at least one lateral cylinder box (300) in the form of a rectangular prism fixed to the screw slot (103) with at least one twelfth mounting screw (326) from the at least one fourth screw groove (325) after sealing with at least one second gasket (324) in the fixed at least one gasket groove (102) on the edge of the cylinder slot (321). at least one gas inlet check valve (404) on at least one second cylinder slot (403) connected with at least one inner groove (402) in which at least one intermediate tube (316) in at least one joint intermediate tube groove (401) in its wide edge and at least one high-pressure regulator (409) located between at least one pressurized gas outlet tube (407) in at least one second pressure tube groove (406) and at least one second inner groove (408) in its narrow edge of at least one gas outlet check valve (405) in its middle and at least one seventeenth screw slot (412) with a thirteenth mounting screw (411) in the outlet of at least one second inner groove (408) in the third connection hole (410) and at least one high pressure regulator (413) fixed from the at least one fifth screw groove (409) and at least one sixth groove (414) in the form of at least one screw (415) in the upper fixed cylinder (400) at least one revolution counter (503), which closes the circular open space on the front face of the main body (100) similar to the cylinder and reads at least one shaft element (19) and at least one ceramic seal (502) in at least one shaft hole (501) slightly below the middle and the flywheel element (18) in a slightly upper part, is fixed to at least one sixteenth mounting screw (504) and at least one eighteenth screw slot (505) and is fixed to the eleventh screw slot (145) on the main body (100) through at least one seventeenth mounting screw (506) and at least one seventh screw groove (507) and has at least one third gasket (508) for sealing. at least one rear cover (600) convex in structure with at least one third gasket (508) and secured with at least one eighteenth mounting screw (602) to the at least one eleventh screw slot (145) on the main body (100) from the at least one third screw hole (601) around and covering the circular open area on the back side of the main body (100) similar to the cylinder.

Referring to Figures 1-5 and 8-15; the main body (100) will be produced from alloyed aluminum material, and according to this art, the intersection of the virtual planes, which are perpendicular to the oblique lateral surfaces of the upper half cylinder structure and make an angle of approximately (+7.1929°) with the horizontal plane from the two half cylinder structures joined to the cylinder box forming the low pressure reservoir (dbd), is on the vertical virtual plane, which is perpendicular to the upper horizontal surface and divides it longitudinally, and this intersection line is the oscillation center of the hammer element (10), is perpendicular to these planes, and the intersection line of the circular virtual planes of the determined dimensions as can be seen in Figure 23-26, on the lateral surface plane is in the lateral cylinder box (300), which is fixed to the screw slot (103) with the twelfth mounting screw (326) after the central lateral surface hole (101) and its second gasket (324) are inserted into the gasket groove (102) at its edge, the cylinder element (13) has the piston element (12) with piston rings and the connection rod elements (11) connected with joints, and the secondary gasket groove (105) at the edge of the upper surface holes (104) and the second gasket (324) placed in it, which is the intersection line of the intersection of these virtual planes on the upper surface plane, the fixed manual valve (207) in the mounting slot (106), which carries out the process of discharging and filling the pressurized gases inside the steel gas tank (200), when necessary, above the stationary multipurpose pedestal (202) at the intersection point with the pressurized gas outlet tube (407) of the pressure balancing tube (201) between the fourteenth mounting screw (415) and the upper cylinder boxes (400) fixed in the fifth screw slot (115), and the second pressure fixed from the second screw slot (108) with the seventh mounting screw (208) in the pressure detection groove (107), which transmits the data of the pressure intensity of the gases inside the steel gas tank (200) to the main center (A) second screw on the inclined surfaces on the steel belts (204) around these upper surface holes (104), which have a drain valve (114) in a fourth screw slot (113) near the pressure sensor (112), which is fixed with a mounting screw (111) to the third screw slot (110) around a detection groove (109) near the sensor (209) and transmits the low pressure reservoir (dbd) data of the cylinder structure to the main center (A), adapts to the half cylinder slot (116) on the inclined surface between the upper surface and the lateral surface the gas outlet record (203) of the steel gas tank (200) in the pressurized tube grooves (119) parallel on both sides of the intermediate tube groove (117) and located on the side of the lateral surface, in which the gas outlet record (203) of the steel gas tank (200) is fixed to the sixth screw slot (118) of the lateral cylinder box, joins with the pressurized gas inlet tube (313) in the gas inlet tube groove (312) above the lateral cylinder box, and joins the ends of the front and rear half circular part of the upper half cylinder head with the extension of the bypass groove (308) descending from the lateral cylinder box (300) and is perpendicular to the lateral surfaces and the piston element with ring (12) at the end of the connection rod elements (11) hingedly connected to the slots of the fixed connection rod elements (15) on the eccentric cylinder mass in the middle of the shaft of the hammer element (10), which makes the two-way oscillation movement in at least one friction bearing (121) in the semicircular indentation (120) above the surface facing the gap in the circle direction of the fixed mounting belt and in the middle of the belt, reverse symmetrical and opposite directional movements in the cylinder element (13) present in the lateral cylinder box (300), and the third hinged slots of the two connection apparatus of this hammer the oscillation diameters of the single center on the upper side of the horizontal plane passing through the center of the shaft element (10) and the slot in the middle of the triple group are short, and the second friction bearings of this parallel mechanical technology, which have a ninety-degree rotation time interval between the simultaneous tidal movement of the piston element with ring (12) at the end of the connection rod element (11) in the upper cylinder boxes (400) and the tidal movement of the piston element with ring (12) making reverse symmetrical and opposite tidal movements in the lateral cylinder box (300), starting to draw the infinity diagram drawn by the slot of the main rod element (15) surrounding the shuttle element (14) of the mechanical technology complemented by the main rod element (15), in which the eccentric rods of the crankshaft elements (16), which will rotate in opposite directions, are connected in the horizontal position in the same direction, within a central rotation time interval, and the oscillating center of the hammer element (10) of the triple mechanical device and the ring element with ring (12) on a central line with articulation of the joint apparatus are in balance and while each of the crankshaft elements (16) performs a rotational movement of 45° in opposite directions to each other while rotating approximately 140° about the center of the hammer element (10) of the triple mechanical device, whose balance is disturbed in the direction of rotation by the pressure force of the gases pressurized by the piston ring element (12) in the continuing rotational movement, and as can be seen in Figure 26, the right angle turns into a narrow angle, and during this rotation cycle time interval, in which the angle of refraction of the triple mechanical assembly coming to the equilibrium position coincides with its position in the initial sequential position again, takes the path of a total of eighty degrees of rotation as shown in Figure 27, and is the combined leverage method, which is the sanction feature of the triple mechanical assembly performing the first and third ninety degrees parabolic drawings of the infinity diagram, and symmetrical with these features on both sides of the gear assembly (17), which makes the opposite rotational movement of the crankshaft elements (16) fixed from the third mounting screw (131) and an eighth screw slot (132) through a screw groove (130) and mechanical groups make their rotational movements within the ninetydegree rotational lap time interval, and externalizing this rotational movement is a fourth mounting from the second screw groove (136) on the side of a fifth semicircular indentation (135) located in at least a fourth semicircular indentation (133) on the parallel lower surface of the multi clamp (127) element and receiving the rotational movement from the gear assembly (17) on the crankshaft element (16) and insulated with the ceramic seal (502) on the front cover (500) and carrying the flywheel element (18) at its end, grasping the third friction bearing (134) of the shaft element (19) the tertiary gasket groove (139) on the long rods to which the mounting belt is perpendicular prior to mounting the screw (137) to the ninth screw slot (138) to the front surface of the cylindrical box formed by joining with a fifth mounting screw (143) from a third screw groove (141) to the tenth screw slot (142) after the sealing process with a gasket (140) through the seventh screw groove (507) on the edge of the at least one front cover (500) to the third screw slot (508) in the gasket groove (144) the body acting as a low pressure reservoir (dbd) consisting of at least one front cover fixed to the at least one front cover and at least one rear cover fixed to the eleventh screw slot (145) through a third gasket (508) in the gasket groove (144) through at least one eighteenth mounting screw (602) through the third screw hole (601) at the edge of the rear surface thereof, as shown in Figures 16, 17.

The steel gas tank (200) is made of two cylindrical stainless steel materials and has a gas outlet record (203) on the side edges of the multipurpose pedestal (202), where the pressure balancing tube (201) and the pressurized gas return tube (407) intersect, and it has a high pressure tank that is fixed to the sixth screw slot (118) with the sixth mounting screw (206) on the second screw hole (205) on the steel belts (204) and that has a manual valve (207) in the mounting slot (106) on the multipurpose pedestal (202) and a seventh mounting screw (208), where the pressure force of the pressurized gas in the second screw slot (108) is measured and this data is transmitted to the main center (A) with the second pressure sensor (209). The respective steel gas tank (200) can be seen in Figure 1 and 18.

The lateral cylinder box (300) shall be made of aluminum alloy material and the third pressure sensor (304) fixed with the eighth mounting screw (303) from the twelfth screw slot (301) to the pressure detection hole (302) in order to maintain and control the rotational movement to be produced by this technology in order to ensure the compatible movements and continuity of the fixed and moving elements in this box (300) and the ninth mounting screw (305) from the contact hole (305) in accordance with the main center (A) program, which receives the pressure force of the gases in the cylinder element (13) and the variable pressure information in the rotational time interval of the constant revolution counter (503) and the flywheel element (18), to the electrical regulator (309), which is fixed to the thirteenth screw slot (307) and has the ability to fix the gas flow rate that should come from the bypass groove (308) from the main body (100), which is a low pressure reservoir (dbd), and the pressure intensity of the gases to be pressurized in the fixed at least one cylinder element (13) in the main body (100) according to the incoming data, and also to the pressurized gas inlet tube (313) belonging to this cylinder element (13) and fixed to the fourteenth screw slot (311) with the tenth mounting screw (310) and in the gas inlet tube groove (312) with the steel in line with the information coming from the gas tank (200), the process of transmitting the amount of high-pressure gas required from the main center to the pressurized gas inlet valve (314), which gives the amount of high-pressure gas into the cylinder element (13) according to the lap time interval, and the amount of pressurized gases in the cylinder element (13) specified in the data coming from the main center and the upper cylinder box (400) during the rotation lap time, through the eleventh mounting screw (318) and the fifteenth screw slot

(319) in the second connection hole (317) with the pressurized gas intermediate tube groove (316) in the joint intermediate tube groove (315), in accordance with the data of the main center (A), which is fixed and analyzes the data detected by the third pressure sensor (304), the amount of gasses to be discharged and the time interval is realized by the pressurized gas outlet valve (320), and in the sixteenth screw slot (322) in the middle of the cylinder slot (321) extending from the bottom to the top, when the gas vacuuming process is to be performed from the outside with the fixed check valve (323), the electric regulator (309), the timing of when and how long the pressurized gas inlet valve (314) and the pressurized gas outlet valve (320) will be single or multiple deactivated, and the time is determined by the main center (A), and the gas vacuuming process from the external environment takes place with the check valve (323) and is in the form of a rectangular prism fixed to the screw slot (103) by the twelfth mounting screw (326) from the fourth screw slot (325) after the second gasket (324) is inserted into the gasket groove (102) pressed by the edge of the cylinder slot (321). Relevant embodiments can be seen in Figure 1, 16 and 19.

Referring to Figures 1, 16 and 20; the upper cylinder box (400) will be produced from aluminum alloy material; pressurized gases coming from the pressurized gas outlet valve

(320) in the lateral cylinder box (300) to the internal groove (402) where the intermediate tube (316) in the joint intermediate tube groove (401) on its wide edge are joined by the gas inlet check valve (404) on the upper surface of the second cylinder slot (403), the pressurized gases will be pressurized by the piston element with ring (12) starting the compression process in the cylinder element (13) until the upper dead point, and the pressurized gases will be pressurized by the pressure force of the steel gas tank (200) passes the high pressure regulator

(409) in the fixed and open position between the outlet of the pressurized gas return tube (407) in the second pressurized tube groove (406) of the pressurized gas outlet check valve (405) and the outlet of the joint second internal groove (408), and the third connection hole

(410) between the filling into the steel gas tank (200) and this connection finishing the recirculation process is fixed to the outlet of the second internal groove (408) and fixed to the fifth screw groove (413) through the thirteenth mounting screw (411) and the seventeenth screw slot (412) is in the form of a rectangular prism fixed to the fifth screw slot (115) by the fourteenth mounting screw (415) from the sixth screw groove (414), which reflects the compressive force of the gas pressurized by the piston element (12) when it reaches the closed position as an acceleration plus the rotational movement. Referring to Figures 1, 6, 7 and 21, the front cover (500) is externally bent with a revolution counter (503) fixed to the sixteenth mounting screw (504) and the eighteenth screw slot (505), which closes the circular open space on the front face of the main body (100) that resembles the cylinder and encapsulates the shaft element (19) that comes out of a shaft hole (501) just below the middle thereof, and which transmits the lap time angle values of the flywheel element (18) on the upper part of the main body (100) to the main center (A), and which is fixed to the eleventh screw slot (145) on the main body (100) through the seventh mounting screw groove (506) and the seventh screw groove (507), and which has a third gasket (508) to ensure its tightness.

Referring to Figure 6, 7, and 22, the rear cover (600) is convex with a third gasket (508) that closes the circular open space on the back side of the main body (100) that resembles the cylinder and has a third gasket (508) to seal it before it is fixed into the eleventh screw slot (145) on the main body (100) through the third screw hole (601) around it.

The symmetry of the triple mechanical assembly of this preferred piston engine (1) and the angle difference of rotation, which is ninety degrees between them, have been examined, and although this technology, which is possible to design methods with different rotation time angles, is similar to the mechanical structure and working feature of internal combustion piston engines, the crankshaft rotating in the opposite direction of the mechanical technology that turns the changing pressure forces of the gasses circulated by the gasses from the steel gas tank (200) and, when necessary, from the external environment between the mechanical assembly in the main body (100) and in the attachment elements into the rotational movement. The eccentric rods of the elements (16) are the hammer element (10), which are the elements of the triple mechanical mechanism, which is indispensable for the method assembled sequentially on a line in the same direction, and the main rod element (15), which surrounds the shuttle element (14), which makes two-way motion on the eccentric centered cylinder element in the middle, and the starting points of the infinity diagram to be drawn by the center of this element (15) are also the starting points of the parabolic curves and the tangent from the middle point of the lines connecting the starting and ending points of the parabolic curves drawn in the ninety-degree rotation time interval to the convex of the parabolic curve, center of the circle is the oscillation center (121) of the central hammer element (10) of the circle passing through the point where the vertical line, which is lowered from the center of the same circle drawn by centering the intersection point of the lines drawn in the second and fourth periods, and the middle of the cylinder in the middle of the shaft of the hammer element (10) is the oscillation center (121) of the central hammer element (10) of the circle passing from the point where the circle intersects the ends of the parabolic curve, and the lines connecting the midpoint of the lines between the ends of the parabolic curve and the oscillation center in each hundred and eighty degree rotation time interval are the leverage of the combined leverage method is the end axial lines of the rod and the starting point of drawing the center method infinity diagram of the circle drawn from the middle of the line connecting the ends of the parabolic curve of this method is the axial line forming the equilibrium position of the combined rod method and the alignment position on a line of the fixed oscillating center (121) and connection rod element (11) articulated centers of the hammer element (10) with the point where the oscillating spring of the circle drawn centrally and the angle between the rod axis and the end oscillating line is approximately (14.4) degrees and the ring piston element (12) at the end of the connection rod element (11) is at the level of the upper dead point of the mechanism that surrounds the eccentric spherical element (14) of the main rod element (15) the eccentric rods of the center of the junction force of the crankshaft elements (16) disrupt the balance of the pressure force falling in the middle of the horizontal line joining the centers of the crankshaft elements (16) lined up on a line in the same direction, and the simultaneous movements triggering each other with the sliding movement in the direction of rotation are translated into this pressure force rotational movement transmitted to the eccentric rods of the crankshaft element (16) through the main rod element (15) of the mechanism, and the hammer element (10) makes a rotational movement of about (14.4) degrees around the stationery center, and the connection rod part of the rod (11) the angle of refraction of one hundred and eighty degrees at the center of the hinge of the connecting apparatus to which the center of the hinge is connected is reduced, and the center of the cylinder in the center of the hammer element (10) and the eccentric center of the shuttle element (14) are coincident, and complete the rotational movement on the roller element in the center of the hammer element (10), and the shuttle element (14) starts the return movement, and the angle of refraction also begins to expand again, and when the crankshaft element (16) takes its initial straight angle position, the gasses under pressure pressurized in the cylinder element (13) before starting the yaw movement after the accelerated rotational movement under high pressure for a period of about eighty degrees of rotation opens the gas outlet valve (320) and passes through the pressurized gas intermediate tube (316) and passes through the element of the gas inlet check valve (404) at the end of the internal passage (402) in the upper cylinder box (400) and because the compressive force of the pressurized gases with the piston element with ring (12) in the cylinder element (13) will be greater than the compressive force of the pressurized gases in the steel gas tank (200), it passes the open high-pressure regulator (409) and this recirculation process made to the pressurized gases pushed back into the steel gas tank (200) is repeated and the pressurized gas inlet tube (313) and the pressurized gas inlet valve (314) are opened and the piston element with ring (12) in the lateral cylinder box (300) with its reversed symmetrical and opposite direction movements, it compresses until it reaches the time interval of the rotation round in which the skidding movement will start from the upper dead center, or it passes the check valve (323) that opens in the vacuuming process, which starts with the movement of the piston ring element (12) moving backwards until the lower dead point after all the equipment on the lateral cylinder box (300) has closed, and after repetitive recirculation processes, it lowers the pressure of the low pressure tank (dbd) to increase or equalize the pressure of the pressurized gas volume in the steel gas tank (200) with its reversed symmetrical and opposite direction movements, which performs four jobs in a rotation time interval with the drain valve (114).

Industrial application of the invention

Applications that can produce rotational motion from the potential energy in springs and magnetic waves are feasible with the "piston engine" technology that serves the above- mentioned purposes and can be applied in renewable energy production in various branches of industry and in air, sea, land, and space vehicles, and is ideal for mobile or stationary energy production accompanied by generators that support the ecological structure.