MX2013007979A - Inner combustion radial engine. - Google Patents

Abstract

The present invention refers to a pump-compressor of fluids and inner combustion engine of a novel type in the industry, which is known as Radial engine, its name evokes its mechanical principle, the form in which it is displaced and the form in which the chambers thereof are supplied, which are highly efficient in terms of compression capacity, thermodynamic efficiency, fuel consumption and power development with a low manufacturing, operation, weight and maintenance cost; the Radial Engine is based on a Single Rotor or a Twin Rotor, the pump-compressor being based on one or a plurality of rotors, in addition, these elements are able to be coupled to further engines and compressors of the same Radial type for optimally solving needs of the industry. The purpose of the invention is to provide a novel type of inner combustion engine and pump-compressor of fluids, which is totally different from those currently available on the market, which main characteristic is its design that transf orms the energy in an efficient manner.

Description

Radiano internal combustion engine FIELD OF THE INVENTION.

This invention relates to internal combustion engines of the rotary type that transform the chemical energy of the gases in a combustion chamber in mechanical movement. Its name is due to the fact that said combustion takes place inside the machine itself, unlike, for example, the steam engine. These engines are universally used for countless applications in all branches of human activity such as the transportation of people animals or things through land, water or air, for the operation of light and heavy machinery, in the development of heavy tasks for man and for the generation of electrical energy, hydraulics, pneumatics among many others, so that their efficiency depends on these processes are carried out in the best way possible for the benefit of humanity. Also this invention also relates to apparatuses that using a positive rotary movement are used for the displacement of materials such as fluid pumps and air compressors.

BACKGROUND OF THE INVENTION The invention of internal combustion engines is attributed to two Italian characters: Father Eugenio Barsanti, an Aesculapius priest, and Felice Matteucci, hydraulic and mechanical engineer who in 1853 filed several patents in Europe. The reciprocating engine as we know it today was developed by the German Nikolaus Otto, who in 1886 patented the design of a four-stroke internal combustion engine, based on the studies of the French inventor Alphonse Beau de Rochas of 1862, which in turn It was based on the internal combustion model of Barsanti and Matteucci.

The main types of these engines are Reciprocating or Alternative, the Rotary engine and the gas turbine. The former are classified as two-stroke and four-stroke engines, the most representative being Otto cycle engines, whose name comes from the German technician who developed it, Nikolaus Augusto Otto, is the conventional gasoline engine, it is also known as the Beau de Rochas cycle engine due to the French inventor who patented it in 1862 and the Diesel engine, named after the German-born German engineer Rudolf Diesel, works with a different principle and initially used diesel fuel .

In general, the structure and operation of Reciprocating or Alternative motors (which are the type of motor most commonly produced today) uses the Otto cycle and an eccentric rotor. Other engines called Rotary use a complete arrangement of planetary gears and levers to operate interconnected arms or a system of multiple arrows. Most designs of internal combustion engines are directly based or have small variants of either the Ericsson, Sterling, Otto or Diesel cycle.

The thermodynamic analysis of the cycle of these engines reveal that it is the Ericsson cycle that performs the most work, however the need for high volumes of hot gas is required to maintain constant pressure increasing the size of the engine and limiting the use of this cycle to the vast majority of applications.

The Otto and Diesel cycle are more typical in the use of engines where the combustion of the fuel is done inside the internal chamber itself. The efficiency of the Otto cycle in the internal combustion engines is limited due to the air temperature of the incoming combustion, this can not rise too much but at a certain temperature to prevent detonations by pre ignition that when they occur severely deteriorate the development of these engines However, this does not happen in the diesel cycle where the fuel requires higher temperatures.

In particular, a Reciprocating internal combustion engine is one in which the shaft rotates due to the action of the pistons in their movement from top to bottom. Commonly in the automotive industry, reciprocating four-stroke engines are used where an explosive mixture of air and fuel is thrown into a cylinder in the first cycle and this is compressed and ignited in the second cycle, the work is carried out in the third work cycle, and the products of combustion are exhaled in the fourth cycle.

An internal combustion rotary engine is one that the force is transmitted directly to the rotating shaft. A good example of this type of engine is the Wankel produced currently by MAZDA, in other words a rotary internal combustion engine has combustion chambers with pistons that are generally triangular in shape which oscillate while rotating.

In general, a turbine is any machine in which the energy of a fluid in motion is converted into mechanical force by the impulse or reaction of the fluid passing through a series of vanes or vanes placed in an array around the circumference of a wheel or cylinder. A turbine engine is one in which the energy of a fluid in motion is converted into mechanical energy by the action that is exerted on the blades of the engine to turn. A typical turbine engine will have a series of blades mounted on a rotor that assimilate and compress air, fuel is added and the mixture ignited. The expansion of hot combustion gases is accelerated by passing through a series of turbine blades and finally driving the blades of the turbine rotors as they pass through them, rotating the blades of the rotor promote the entrance of the turbine. more fresh air closing the cycle.

Reciprocating-type motors are universally used, mainly because they convert the reciprocating movement of the pistons to a rotary movement of an axis, but reciprocating internal combustion engines have a limitation in achieving high levels of efficiency in the fuel consumption due mainly to the negligible use of the force of the expansion of the combustion gases as well as the deficient transmission of the force to the crankshaft as well as the reduced time in the use of the force of expansion of the gases by the premature expulsion of very high potential energy of gases at high temperature to the environment without being used, additionally to this and as we have said before, the energy that is consumed by the friction of a number of characteristic moving parts in these motors is very high. This is why the thermal efficiency of reciprocating internal combustion engines is reduced, limitations start in the same design, the materials used, the way they operate and the use of a part of the same cylinder for all phases of the cycle. Even more so since these motors provide power for the transformation of reciprocating movement of the pistons in rotary motion in the arrow, when the fuel air mixture within a cycle in a combustion engine internal explodes or consumes the position of the piston is in the dead center (PMS), at this point the lever arm in which the connecting rod transmits force to the crankshaft the very close to zero. Therefore, at the moment of maximum energy released by the combustion gases, the piston exerts a minimum torque on the crankshaft. When the piston moves from the top dead center, the lever arm through which the piston transfers force increases, but at the same time the combustion gases expand and lose propulsive force so the maximum torque that the piston exerts. piston exerts on the arrow or crankshaft will always be very lower compared to the torque that the piston could transfer to the arrow or crankshaft if the piston could transfer this force with the lever arm to the maximum, as this is not what happens, the reality is that unfortunately reciprocating engines deliver very poor results in terms of the conversion of the potential energy of combustion gases into mechanical energy, but it turns out that in these engines the gases are released from the combustion chamber when they still have a high potential energy (90%), if we add to these two big issues that the combustible air mixture is not always lit in its total d, that the intake is sometimes affected by the exhaust valve as it sometimes releases part of the intake gases, decreasing the potential of the reciprocating engine, this and that a large part of the energy developed by the combustion gases is absorbed to counteract the internal friction of the engine the result is that the efficiency of these engines is low.

In general, current internal combustion engines both Reciprocating and Rotary suffer from several deficiencies, one of them is that their thermal efficiency are much less than their theoretical efficiencies according to the second law of thermodynamics, it has been calculated that it is up to 25 % of the heat developed by the combustion of the fuel is absorbed by the cooling system itself, another 25% is dedicated to the operations of the engine itself such as air compression, up to 10% of the available energy must be discarded by combustion incomplete hydrocarbon fuels. As a result, these engines perform poorly. Another deficiency is also the fact that we find toxic substances in the exhaust pipes like coal particles and carcinogenic hydrocarbons due to incomplete combustion as well as nitrous oxides formed at the highest combustion temperatures (1800 to 2000 degrees Celsius). Reciprocating internal combustion engines exist but are highly complex and highly deficient in terms of energy utilization.

On the other hand, the Wankel rotary engine, although it has had an acceptable performance in the industry, the problems of high oil consumption and poor performance have prevented it from replacing the reciprocating engines in the industry.

Other forms of rotary motors have been proposed, in which Toroidal motors are included where there is a toroidal piston that runs in a chamber in the same way forming a rotor that is connected to an axis where the Toroidal pistons move. in a cyclical way approaching and separating from each other forming compression and expansion chambers, the air and fuel inputs and outputs and combustion gases are located in the contour of the toroidal casing. Some of these designs use an internal mechanism that affects the cyclic movement of the pistons to get them to perform the different phases of the cycle.

There are many engine designs that have been patented and manufactured in the past. Most have been proposed as a way to reduce the large disadvantages associated with engines, especially reciprocating pistons or as a way to provide compact and light engines that are economical to manufacture and efficient in fuel consumption, however to date the only internal combustion engines that are mass produced are the Wankel Rotary engine and conventional reciprocating piston engines. With the objective of mass production, it has been considered that all new proposals and designs have disadvantages either due to an inefficient design in terms of operation or due to their low performance under normal load conditions such as maintaining an optimum power in a constant manner. Many of these proposals require sophisticated manufacturing and assembly processes, are difficult to seal, very complex, or operate inefficiently.

Making an analysis the internal combustion engines of each of the types described above have particular advantages and disadvantages, in short an engine Reciprocating has a mature design but with many moving parts (10 times more parts than a rotary engine), relatively low manufacturing cost and a moderate weight-to-power ratio, moderate size and very low efficiency in the chemical energy transformation of the gases in mechanical energy. A rotary engine has a less mature design, a high cost of production, a moderate weight-power coefficient, a moderate size and a poor coefficient of efficiency in fuel consumption, at a glance none of them in terms of efficiency manages to solve the problem , and on the other hand the turbine engines are very complex and for very particular applications where a very high power is required, to achieve this these engines reach speeds of rotation higher than 30, 000 PM. Patents such as US 4035111, US 4753073, US5203307, US6071098, US6132197, US6250277, US6293775, US6371743 propose novel changes and designs of rotary engines, however these changes do not solve the problems that reciprocating and rotary engines currently have. The invention of a completely new type of internal combustion engine that is designed from a new and different approach and whose main objectives are: 1. The maximization of the transformation of the energy of the combustion gases into mechanical energy, minimizing in the exhaust gases toxic byproducts such as carbon (CO), nitrous oxide (NOX) or hydrocarbons. 2. That is compact, lightweight, economical and easy to manufacture, '··' || 3. That its design allows its sealing and lubrication efficiently and effectively,. . 4. And, that is easily scalable (or reduced) in its dimensions with the aim of satisfying with precision the wide needs required for these engines and can be applied to new uses that currently conventional engines for the reasons previously exposed have not been able to satisfy .

The present invention relates to a "Radiano" internal combustion engine, which has advantages of both rotary and turbine engines and which solves many of the problems and disadvantages of reciprocating and rotary engines today, as a result of this new engine named "Radiano" (its name refers to the way it moves and feeds), offers much more operational advantages and is often simpler and more efficient than those known so far.

DESCRIPTION OF THE INVENTION It presents a new design of "Radiano" internal combustion engine, its name evokes its mechanical principle, the way it moves and the compression and combustion chambers of the engine are fed, it is a circular design engine that follows a bipartisan 4-stroke cycle (Admission, Compression, Combustion and Exhaust) in it, the air intake and compression is performed in a first stage of the engine as in turbine engines and is transferred to the combustion chamber that is locates in the second stage of the engine and there in combination with the fuel intake causes the mixture to ignite either by the firing of a spark, hot element or by the high temperature of the pressurized air causing the combustion gases at high pressure to drive to the rotor.

The Radiano Engine is a new type of internal combustion engine that uses radial blades called "RADIANS" that move axially and that owe their synchronous movement to hermetic displacement supported on the circular tracks of the rotor and that in these are a determined number of ridges that serve as a cam to achieve this harmonic and synchronic axial movement at all times, in the Radiano engine the rotor is also compression or combustion chamber, and this performs with great efficiency the four phases of the thermodynamic cycle. Each of these engines may contain one or more sets (or sets) of Radians, (each set or set of Radians is composed of one or more Radians of Compression and a Radial of Combustion), which will be distributed evenly and equidistantly in circles concentric to the motor, the same applies to the crests or cams on the rotors, these should be distributed similarly, the amount of ridges (or cams) in the circular tracks on the rotors must be the product of a multiple of the sum of all Radians, that is to say it is possible to have "X" number of Radians (sets of compression and combustion radians) and "nX" number of cams in rotors where "n" is a positive integer equal to or greater than 1, always respecting in the design the equidistant distribution rule, and that within a same engine the rotors must have the same number of cams; The length and axial displacement of the Radians will determine the amount of air that will be admitted to the combustion chamber. The Radiano Motor design allows compression of the intake air in one or more phases, this achieves a high compression ratio of the intake gases. Between these rotors or between the compression and combustion phases there may be a small lag (delay) on the part of the compression that guarantees the high pressure and complete expulsion of all the pressurized admission gases and lodged in the compression tank at the moment that begins phase # 3 of the cycle (combustion). These motors can have one or several units that fulfill the thermodynamic cycle within the same motor coupled axially and placed with each other with or without degrees of rotation between themAlso, these Radian engines can be coupled axially or polarly to each other in two or more arrangements with the possibility of installing them also with degrees of rotation between them to smooth the march and homologate the torque at all times. The design of the Radiano Motor makes it possible to take advantage of a large amount of the potential energy of the combustion gases and this transmits it directly to the arrow in a constant manner throughout the cycle. The design of the thermodynamic cycle of the Radiano Engine allows to have cleaner exhaust gases due mainly to the prolongation of the combustion time of the mixture in the combustion chamber, to the efficient homogenization of the stoichiometric mixture, to the preheating of the fuel and to the optimal regulation of a high temperature of the combustion chamber. The geometric design of the Radiano engine allows the combustion chambers to be kept at high temperatures without exceeding it, thus avoiding the generation of toxic particles such as nitrous oxides (NOX). Also this geometry facilitates the sealing, lubrication (liquid and solid) and cooling of the motor which is easy to obtain and maintain, therefore the loss of energy by friction is small. The Radiano engine is composed of very few parts, with the important moving parts: Rotors and Locks and the fixed parts the o-shell of the rotors and the 3 fixed discs placed in the central part of the engine. The fuel supply can be mechanical or electronic, the air intake can be natural at atmospheric pressure or with turbo charger, and the exhaust gases exit through a port at low pressure and temperature. Finally, in terms of the number of Rotors, the Radian Motors can work with one rotor (Single Rotor) or two rotors (Twin Rotor). The Single Rotor is a Motor with a single Compression and Combustion rotor called a "Compresstion" rotor, while in the Twin Rotor it has two rotors and each rotor fulfills a function of compression or combustion. Each offers important advantages.

The design and mechanical principle of this Radiano engine allows it to have a lot of flexibility since it can be adapted and scaled to cover any need or application, with information such as the diameter of the engine, position and length of the Radians, axial displacement, number of Radians of compression and combustion in the engine, number of rotors and number of cams in the circular tracks in the rotors, volume of air intake and fuel allows to obtain efficient engines covering ranges of high and low revolutions with infinite possibilities of torque of output having an efficient fuel consumption, a low weight and a low cost of manufacturing and maintenance. By separating the spaces where the compression of the intake air is made with that of the combustion of the mixture allows us to optimize the performance of the engine, adapting it precisely to the characteristics of power and fuel consumption required, thus, the mass volume of the admitted air and the compression ratio of these gases can be determined and precisely defined, on the other hand the elongated combustion chamber allows you to achieve a complete burning of the fuel and a high use of the energy of expansion of the combustion gases. With information such as the required output torque, the maximum and minimum diameter of the motor, the maximum variation of the speed, the number of motors to be coupled, we obtain data such as the volume and compression ratio of the intake gases (air). , fuel consumption, length of the Radiano, distance from the center of the Radiano to the center of rotation of the engine, axial stroke of the Radiano, number of engines coupled with rotating angle of coupling between them and performance, can calculate and design the optimal Radiano engine Radiano Single Rotor engine operation: (It has a single rotor called Compressor Rotor) The air is admitted to the compression chamber that is located in the Compression Rotor, a lock called Radiano Compression when closing against the Compression Rotor forms a wall and it is through it that the gases of admission They are highly pressurized. Air compression can be done through one or more concentric chambers that will form a highly efficient compressor with high compression capacity, this is because the air admitted by the first compression Radian once pressurized will feed the next adjacent chamber and concentrically Inside and this will compress and feed the next adjacent inner concentric chamber until it is the last compression chamber when the pressurized air is transferred to the compression tank in the combustion radiana and with it the combustion chamber will be fed. As mentioned, the transfer of the pressurized air to the combustion chamber is carried out through the interior of the two radians (the first called Radiano of Compression and the second radiant of combustion) these move axially because they rest in the circular planes of the rotors and having one or several crests or cams _on one of its faces, this rotor is mounted on an arrow (in this rotor the parts near the arrow are in turn the compression chambers of the intake air and the furthest away the combustion chamber), as we mentioned the rotors have on their front face one or more ridges in the circular tracks that serve as cam to the Radians, that is to say that the Radians rise and fall by the action of the crests of the rotors, the Radiano Compression forms the wall that makes the compression section of the Compresstion Rotor to rotate compresses the intake air and will be by a conduit located inside this Radiano that this air is transferred to the next compression chamber or finally to a pressurized air tank, this tank will release the pressurized air that is inside it to the internal part of the combustion chamber located in the combustion section of the Compresstion rotor by the axial displacement of the combustion radiano that acts as a releasing and dosing valve of both the air pressurized that was located in the pressurized air tank as well as the fuel, and that when combined these will form in a homogeneous way the stoichiometric mixture (ideal mixture of air and fuel where the correct mass of air and fuel exists to realize a complete combustion without than on any of the two initial components) to be consumed in the combustion chamber and what will give impulse to the rotor, the ignition of the mixture is carried out automatically by the almost simultaneous and instantaneous release of pressurized air at high temperature and pressure and fuel to Inside the combustion chamber, however, it can also be carried out by electric or electronic ignition, the combustion gases are expelled through localized ports when the cycle ends. This process is repeated immediately and naturally by the inertia of the rotors that also function as the motor masses.

The rotor rotates inside a housing, this. when joining together with three central discs they form the body of the engine.

Operation of the Radiano Twin Rotor engine: (It has two rotors the first the Compression Rotor and the second the Combustion Rotor both rotate with their respective circular tracks pointing to the central part of the engine.) The air is admitted to the compression chamber that is located in the compression rotor , a lock called Radiano (Radiano of compression) to close against the Compression Rotor forms a wall and is through it that the intake gases are highly pressurized. Compression of the air can be done through one or more concentric chambers that form a highly efficient compressor with high compression capacity, this is because the air admitted by the first compression Radian once pressurized will feed the next adjacent chamber and concentrically inside and this compressed feed the next adjacent inner concentric chamber until it is the last compression chamber will deliver this pressurized air to the compression tank in the combustion Radiano which will feed with this air to the combustion chamber. As mentioned, the transfer of the pressurized air to the combustion chamber is carried out through the interior of two radians (the first called Radiano of Compression and the second Radial of combustion) these move axially because they rest in the circular plane they have for This end the Compression Rotors, and Combustion in one of its faces and these have a certain number of ridges that work as cams, the mentioned rotors are mounted on the same arrow (the first rotor is in turn the camera or the ) of compression of the air of admission and the second rotor is in turn the combustion chamber),], as already mentioned the rotors have in their frontal face one or more crests that serve as a cam to the Radians, that is to say that the Radians rise and fall by the action of the crests of the circular planes of the rotors, the Radiano Compression forms the wall that causes the compression rotor to rotate compresses the intake air and will be through a (d) ducts located inside this same Radiano that this air is transferred to the next compression chamber of air or finally to a pressurized air tank, this tank will release the pressurized air that is inside it to the internal part of the combustion chamber located in the combustion rotor by the axial displacement of the combustion radiator that acts as a valve releasing and dosing both the pressurized air that was located in the pressurized air tank as well as the fuel, and that when combined these will form in a homogeneous way the stoichiometric mixture (ideal mixture of air and fuel) to be consumed in the combustion chamber and that will give impulse to the rotor, the ignition of the mixture is carried out automatically by the almost simultaneous release Anea and snapshot of pressurized air at high temperature and pressure and fuel inside the combustion chamber however can also be carried out by electric or electronic ignition. The combustion gases are expelled through localized ports when the cycle ends. This process is repeated immediately and naturally by the inertia of the rotors that also function as the motor masses.

The two rotors rotate inside the same number of casing, these when joining together with three central disks form the body of the engine.

In both cases the arrow of the motor drives the gasoline pumps, lubricant and cooling system, and other devices more like the generators of current for the ignition and operation.

The engine start can be carried out by electric motors (gears) connected to the arrow and stopped by the eventual cut in the supply of fuel or air-fuel. The main advantages of this innovative Radiano internal combustion engine are the following: 1. The Radiano engine has a novel highly efficient phase air compression system that achieves high air pressurization in order to increase the efficiency of the thermodynamic cycle.

The Radiano Engine is efficient in the transmission of the force to the arrow of the motor since this one acts on a constant lever arm and that could be as big as it is designed.

This Radiano engine takes advantage of almost all the potential chemical force of the combustion gases, due to the precise dosage of the air-fuel mixture and the design of the elongated combustion chamber, thereby benefiting the potential energy of the gases for more weather.

In the Radiano engine, the expansion of combustion gases can be exploited almost entirely In the Radiano engine the compression and combustion chambers are fed taking as a reference the radial dimension that is to say the great length of the locks called "Radians" allows to have multiple inputs and outputs of pressurized air and fuel that optimizes the exit or dosage of the pressurized air and the fuel in the combustion chamber doing it in a fast and homogeneous way.

The Radiano engine is multi-fuel, that is, it can receive a wide range of fuels.

This Radiano engine can generate high compression ratios of the intake air due to the wide seal provided by the circular tracks of the rotor and the contact surface of the Radians.

The high temperatures of the pressurized intake air allow to have or not the presence of a spark or hot element for the start of combustion due to the high temperature of the gases.

This Radiano engine can have one or more rotors with one or more crests (cams) in its circular tracks as well as one or more sets of Radians, this makes it very flexible when selecting the right motor to cover every need.

The Radiano engine is composed of very few parts, is compact, lightweight and easy to manufacture.

This Radiano engine has the possibility of having areas at different temperatures, that is to say and as an example it can maintain the combustion chamber at a high temperature, thereby producing a greater efficiency in the thermodynamic cycle. This Radiano engine is autonomous since the cycle is regulated by itself without the need for sequencers or a distribution chain as in the case of reciprocating engines.

A Radiano engine can be scaled or reduced in its diameters and dimensions (without changing design or mechanical principle) in order to optimally solve any need, also in the engine the radians can be multiplied, or the number of ridges (cams) in the tracks circular in the rotors of choice, moreover can be coupled axially or polarly two or more engines together easily, reliably and safely # 21 and # 22 Fig. 1, 15. If we consider the force generated by the combustion of an air mixture -combustible as a constant average value, the moment or torque increases with the increase of the distance of the application of the force on an axis, more powerful motors can be produced with the same energy consumption when increasing the position or distance of the Radians to shaft # 8 Fig. 2,3,4,5,6,7,8, 13,16,17,18,19,20,21,22,23,24,25 of the engine.

In this Radiano engine cooling, sealing and lubrication is done through air, water and pressurized oil, using metal and non-metallic seals in an easy and reliable way since it has large areas destined for it.

To increase its efficiency in terms of fuel consumption the Radiano engine can be of constant speed (constant torque), also arrangements of several engines placed in series or parallel will make the whole can achieve very high efficiencies by only turning on the engines that were required .

This engine can have sensors that automatically manage their performance to achieve the desired development.

This Radiano engine has a great angular moment of gyroscopic effect that can be very profitable, as an example this force can greatly increase measure the stability of a vehicle when it is conveniently installed for this purpose. 18. This Radiano engine has applications to perform mechanical, pneumatic, hydraulic or electrical work (generators) among others. 19. This Radiano engine can be manufactured with materials such as Steel, Titanium, Tungsten or Aluminum and for its manufactures are used machines and tools that can be CNC numerical control type.

Having described the nature of the present invention, three particular examples will be described with references to the accompanying drawings. However, those skilled in the art will appreciate that many variations and modifications can be devised without departing from the scope of the invention as described above.

In particular and only to exemplify this design we select for its description and analysis three motors with radians of design or rectangular shape (the Radiano can have any other geometric contour as long as it meets the condition of hermeticity with the circular tracks of the rotors). first it is a Radiano Twin Rotor Engine composed of two sets of Radians and two cams on the Compression Rotor and the Combustion Rotor, the compression is done in one step as shown in Fig. # 6, the second will be an Engine Radiano Single Rotor composed of 2 sets of Radians and two cams on the Compresstion Rotor, compression is done in one step as shown in Fig. # 17. The third will be a Single Rotor Motor composed of 2 sets of Radians and two cams, the compression is done in 3 cameras or steps.

Numbering and general description of Parts contained in the figures. 1. -Disco Central # 1, 2. -Disco central # 2 3.-Central disk # 3, 4.-Conchade Rotor, 5.-Conchade Rotor, 6.-Rotor of compression, 7. -Rotor of combustion, 8.- Arrow, 9. Radiano of Compression, 10.-Radiano of Combustion, 11. -Belards or bearings, 12. -Leven Plan (Step), 13.-Cold oil (admission to Rotors), 14.-Hot oil (Exhaust) , fifteen.- Ring separator for motor mounting. 16. -Sellos del rotor, 17. -Empaquetadura of thermo resistant material and lubrication (such as those made with graphite), 18.- Cold oil (admission Radianos), 19.-Cooling turbine. 20.-Auxiliary system (fuel pumps, oil, water, gear generator) 21.- Base for anchoring 22. -Ring for adjustment of degrees of rotation of the engine 23.-lnjector of fuel 24. -Resorts 25.-Admission of Air 26.- Fuel admission 27. - Guide cavity for air transport capsules in central disks 28. - Solid lubrication (admission) 29. - Air intake holes to intake chamber 30.-Screw holes for assembly of screws 31.- Outlets of pressurized air in the Radiano to the combustion chamber 32. - assembly lining 33 - Oil passage ducts 34.-Radian guide box in central discs 35. -Lighting escape 36.-Ducts of power or escape 37.- Crest 38.- Inclined plane of the rotor to climb to the ridge 39. -Fuel injector nozzle 40.-Air and fuel outlet chamber inside the combustion chamber. 41.-Embolo pressurized air reservoir 42. -Barra and fuel injection plunger base 43. -Compression reservoir 44.- Space for springs in Radians 45. -German guide springs in Radians 46. -Output exit fuel and air to the combustion chamber 47.-Pressurized air transport duct 48.-Compression tank cylinder bar 49.-Pressurized air outlet piston 50.-Compresstion rotor 51.-Positioning of the spark or hot body 52.-Exit of pressurized fluid in Radiano Compressor 53.- Circular tracks in Compresstion Rotor for Combustion 54. - Compresstion Rotary Plane for Compression 55.- Capsule to transport pressurized air inside the compression Radians. 56.-Deposit of pressurized air in Single-Rotor 57.-Pressurized air communication bridges between compression chambers in Radian Compressors. 58.- Fuel Spreader 59.- Radiano Combustion reaction shell for Radiano closure 60. - Compression chambers in Radiano Pump-Compressor Description of Figures: Fig. 1: Shows the external image of the two-rotor Radiano motor (Twin Rotor) in isometric view Fig. 2: It shows the external image of the Radiano motor of two rotors (Twin Rotor) in isometric view having withdrawn auxiliary systems such as cooling, fuel pumps, lubrication and gear among others.

Fig. 3: They show a cross section H.H 'of the motor indicated in figure # 2 Fig. 4: They show a cross section H.H 'of the motor indicated in figure # 2 in explosion. Fig. 5: Shows the view of the cut J-J 'indicated in figure # 2 and that shows the operation of the Radians in a two-rotor Radial motor system (Twin Rotor).

Fig. 5 ': Shows the view of the cut J-J' indicated in figure # 16 and that shows the operation of the Radians in a Radian Motor system of a rotor (Single Rotor).

Fig. 6: Shows a complete isometric view of the exploded Radiano Twin Rotor engine. The Radiano Air Intake Compressor is composed of the first section of this O - O 'diagram Fig. 7: Shows the view of the cut A.A 'indicated in figure # 3 and that is the image of the compression rotor # 6 Fig8: Shows the view of the cut B-B 'indicated in figure # 3 and that is the image of the compression rotor # 6 and the plate # 1 of Fig. # 6 as well as the Compression Radians # 9 Fig. 9: Shows the view of the cut D-D 'indicated in figure # 3 and that is the image of the piece # 2 in Fig. # 6 Fig. 10: Shows the view of the cut C-C indicated in figure # 3 and that is the image of the piece # 1 in Fig. 6 Fig. 11: Shows the view of the cut E-E 'indicated in figure # 3 and that is the image of the piece # 3 in Fig. 6 Fig. 2: Shows the view of the F-F cut 'indicated in figure # 3 and that is the image of the combustion rotor # 7 and the plate # 3 of Fig. # 6 as well as the combustion radians # 10.

Fig. 13: Shows the view of the cut G-G 'indicated in figure # 3 and that is the image of the combustion rotor # 7.

Fig. 14 Shows the axial or polar arrangement in which these motors can be coupled.

Fig. 15 Shows the external image of the Radiano motor of a rotor (Single Rotor) in isometric view Fig. 16: It shows the external image of the Radiano motor of a rotor (Single Rotor) in isometric view having withdrawn auxiliary systems such as cooling, fuel pumps, lubrication and gear among others.

Fig. 17: Shows a cross section of the Radiano motor of a rotor (Single Rotor).

Fig. 18 Shows a cross section of the Radiano motor of a rotor (Single Rotor) in explosion.

Fig. 19 Shows an isometric view of the Radiano motor of a rotor (Single Rotor) in an explosion. This diagram also shows the high pressure air compressor (section O-O ') which may have one or more compression phases (shown with a phase) the combustion section is the track furthest from the axis and the compression the closest Fig. 20 Shows the view of the cut L-L 'of Fig. # 18 and that is the piece # 3 of Fig. # 17.

Fig. 21 Shows the view of the M-M 'cut of Fig. # 18 and that is the piece # 2 of Fig. # 17.

Fig. 22. Shows the view of the cut K-K 'indicated in Fig. # 17 and that is the Rotor of Compesstion # 50 and the Radians # 10 and # 9 of the same figl7.

Fig23 It shows the cross section of an example of Radiano Single Rotor motor with 3 compression phases.

Fig24 It shows the cross section of an example of a Radiano Compressor with more than one compression phase at the height of the cut K-K 'of figure 17, in this case three compression phases are shown as an example.

Fig25 It shows a complete isometric view of the Radiano compressor. In this case, 3 compression phases are shown as an example.

Example 1: Radial motor with two rotors (Twin Rotor) Note: A rectangular-shaped Radian is shown, with a single compression chamber in the Compression Rotor: Figures 1,2,3,4,5,6,7,8,9,10,11,12,13,14 .

The air that was admitted in a previous step to the interior of the compression chamber (this through the holes # 25 Fig. 2, located in the central disc # 1 Fig.2,3,4,5,6,10, (The volume and initial pressure of intake air can be naturally atmospheric or increased through a turbo blower), will be pressurized by the action of the lock or Radial Compression # 9 Fig. 3, 4, 5, 6,8 and by the Compression Rotor # 6 Fig. 3, 4, 5, 6, 7, 8 that when rotating will reduce the size of the compression chamber producing the pressurization of the air, this pressurized air will travel through the interior duct # 47 Fig. 5 of the Radiano of Compression # 9 Fig.3,4,5,6,8 to the Compression Tank # 43 Fig. 5, The Radiano of Compression # 9 Fig. 3, 4 , 5, 6,8 when rising by the action of the inclined plane of the ridge # 37 Fig 5 of the Compression Rotor # 6 Fig. 3, 4, 5, 6, 7,8 helps the pressurization of the air entered in the Tank of Compression # 43 Fig. 5; When the inclined plane of the ridge or cam # 37 Fig. 5 of the Combustion Rotor # 7 Fig.3,4,5,6,12,13 coincides with the Burning Radial # 10 Fig. 3, 4, 5, 6 , 12 this rises and transfers the pressurized air to the other end of this tank, also preloads the spring and plunger # 49 that will help extract all the air from the compression tank # 43, also preloads the spring and plunger # 39 that will will help to extract all the pressurized fuel, immediately after passing the cam this is shot and low at high speed at the bottom of the inclined plane of this rotor by the action of a series of high capacity springs # 24 Fig6 housed in boxes for spring # 45 Fig. 5 located throughout the upper perimeters of the same, this movement allows it to be through a large number of ducts # 31 Fig. 6 that connect the Compression Tank # 43 Fig. 5 with the combustion chamber of the rotor and that are made to coincide at this precise moment, release the pressurized air directly inside the combustion chamber to the shell-shaped recess # 40 Fig5 almost simultaneously and by the same action of this Radiano of Combustion # 10 fig. 3, 4, 5, 6, 12 through a large number of injectors of mechanical or electronic type # 23 Fig6 located along the length of the Radiano by matching the outlet ducts releases the fuel at high pressure to the same recess # 40 fig. 5 which facilitates the instantaneous homologation of the stoichiometric mixture, the high temperature of the pressurized air or if the presence of the spark of a spark plug is desired, will initiate the combustion of the mixture that will give the impulse to the same rotor, as has been said compression rotor # 6 Fig. 3,4,5,6,7,8 may be out of phase (delayed) with respect to the Combustion Rotor # 7 Fig3,4,5,6,12,13 so that for a few moments after At the start of the combustion the Radiano of Compression # 9 Fig.3,4,5,6,8 (supported on the Compression Rotor # 6 Fig. 3, 4, 5, 6, 7,8) will continue sending to the Deposit of Compression # 43 Fig. 5 pressurized air and this in turn to the combustion chamber in order to exhaust the volume of pressurized air contained in it, the mixture burns and the force of expansion of these gases drives the Rotor. The elevation of the Radiant of Combustion # 10 Fig.3, 4, 5, 6.12 by the action of the inclined plane # 13 Fig.5 of the Combustion Rotor # 7 Fig.3, 4, 5, 6, 12, 13, eclipses the exit ducts # 46 Fig5 from the Compression Reservoir # 43 Fig.5 and the fuel injectors # 23 Fig.5, 6, check valves in these points will double ensure that the combustion gases are not channeled into these elements. When the ridge # 37 Fig.5 of the Compression Rotor # 6 Fig. 3, 4, 5, 6, 7,8 coincide with the Radian of Compression # 9 Fig. 3, 4, 5, 6,8, this will shoot at the bottom of the inclined plane of the Compression Rotor by the action of a series of springs 24 Fig. 6, housed in a high-capacity spring box # 45 Fig. 5 located in the upper perimeter of the same, starting again the pressurization cycle of the intake air. The air intake is made by Compression Rotor # 6 Fig.3, 4.5, 6, 7.8 in an anterior compartment at the same time that the air pressurization is carried out. The combustion gases are released through the ports # 35 Fig2, 5; 6, 11,12 located on disk # 3 these can be used to boost the intake gases through a turbo blower.

Example 2 Radial motor of a rotor (Single Rotor) Note: A rectangular rectangular Radian is shown, with only one compression chamber in the Compression Rotor: Figures 15, 16, 17, 18, 19, 20, 21,22 The air that was admitted in a previous step to the inside of the compression chamber (this through the holes located in the central disc # 3 Fig.16, 17, 18,19, (the volume and initial pressure of intake air can to be naturally atmospheric or increased through a turbo blower), it will be pressurized by the action of a lock called Radiano of Compression # 9 Fig. 17, 18, 19 and by the Rotor of Compression # 50 Fig. 17, 18,19 that when turning it will reduce the size of the compression chamber # 54 fig.19 producing the pressurization of the air, this pressurized air will travel through the inner conduit # 47 Fig. 18,20 located in the central plate # 2 Fig. 16 from the Radiano Compression # 9 Fig.17, 18,19 to Compression Tank # 56 Fig. 5 '., The air compression process could continue even beyond the start of the process by the placement of a phase shift (delay) of Compresstion Rotor Ridges # 50 Fig.17, 18,19 in its circular track # 54 Fig.19 with respect to the ridges of the Compresstion Rotor # 50 Fig.17, 18,19 in its outer circular track # 53 Fig. 19 in order to completely transfer the pressurized air of the Compression Tank # 56 Fig. 5 'to the combustion chamber, Additionally the plunger # 49 Fig. 5' which is driven by springs will help to expel all the air from this reservoir, the spring is also preloaded and plunger # 39 that will help you extract all the pressurized fuel. The Radian of Compression # 9 Figl6, 17, 18,19 when rising by the action of the inclined plane of the ridge # 54 Fig. 5 'of the Rotor of Compresstion # 50 Fig.17, 18, 19, will contribute to the pressurization of the air entered in Compression Reservoir # 56 Fig. 5 ', when the # 37 Fig.5' ridge of the Combustion Rotor # 7 Fig. 3, 4, 5, 6, 11, 12, 13 coincides with the Burning Radial # 10 Fig. 3, 4, 5, 6, 12 this is triggered and low at high speed at the bottom of the inclined plane of this rotor by the action of a series of high capacity springs # 24 Figl9 located around the upper perimeters of the same, this movement allows through a large number of ducts # 31 Fig.17 that connect the Compression Tank # 56 fig. 5 'with the combustion chamber of the rotor and which are made to coincide at this precise moment release the pressurized air directly into the combustion chamber to the shell-shaped recess # 40 Fig. 5', at the same time and for the same This Radiano de Combustion # 10 Fig. 17, 18,19 action through a large number of mechanical or electronic injectors # 23 Fig. 5 'located all along the Radiano by matching these exit ducts release the high pressure fuel to the shell-shaped recess # 40 Fig. 5 'inside the combustion chamber facilitating the instantaneous homologation of the stoichiometric mixture, the high temperature of the pressurized air or if the presence of the spark of a spark plug is desired or incandescent body, will initiate the combustion of the mixture and the expanding gases will give the impulse to the rotor. As has been said Compresstion Rotor Compression Phase # 50 Fig. 17, 18,19 could be out of phase (delayed) with respect to the combustion phase so that for a few instants after the start of combustion the Radiano Compression # 9 Fig. 17, 18, 19 (supported on the rotor) will continue to send compressed air to the Compression Tank # 56 Fig. 5 'and pressurized air to the combustion chamber to exhaust the volume of pressurized air contained in it. East. The elevation of the Radiano of Combustion # 10 fig. 17, 18,19 by the action of the inclined plane # 13 Fig. 5 'in the Rotor track will eclipse the exit ducts coming from the Compression Tank # 56 Fig. 16 and from the fuel injectors, "check" valves in these points will double ensure that the combustion gases are not channeled into these elements. When a crest of the circular compression track of the Rotor coincides with the Radiano of Compression # 9 Fig. 17, 18, 19, this will be fired at the bottom of the circular track by the action of a series of high capacity springs # 24 fig.19 located in the upper perimeter of the same beginning again the pressurization cycle of the intake air. The air intake is carried out by the Rotor in a previous compartment at the same time as the air pressurization is carried out. The combustion gases are released through the ports # 35 Fig. 17.18, 19.20 located on disk # 3 these can be used to boost the intake gases through a turbo blower.

Example 3 Radial motor of a rotor (Single Rotor) Note: Radiano of rectangular outline, with three compression chambers in the Rotor of Compression: Figure. 2. 3 The operation is exactly the same as the one described above for the single-rotor Radiano motor (Single Rotor) only the increase in the pressure of the intake gases is carried out in several steps through concentric chambers # 60 Fig. 23 starting in the chamber of compression more distant to the axis to conclude in the closest to the axis this process elevates to very high pressure the gases of admission achieving to elevate significantly the efficiency of the thermodynamic cycle of this engine.

For all types of Radian Motors (Single and Twin Rotor) with one or more steps or compression phases the following applies: 1. The volume of pressurized admission air that enters the combustion chamber is calculated according to the percentage of expansion that you want to obtain from them at the time of combustion, therefore for this calculation you must select the lengths of Radians, their axial displacement, its position or distance with respect to the axis and with it calculate the volumes of air displaced by the tracks of the rotor ie the mass and the level of air pressurization that will be supplied to the combustion chamber must be selected (initially the number of steps or compression phases is also defined).

The fuel injectors can be of the electronic, electromechanical or mechanical type since the combustion radiano in its axial movement can supply them and release them from the fuel mechanically inside the combustion chamber, in both cases a fuel pump should be the element that feed # 26 Fig. 5, 5'a these injectors, in the case of mechanical injection the increase in the pressure of the fuel line will produce an increase in the volume of fuel dosed to the combustion chamber by accelerating the engine and vice versa. In the case of electronic fuel injectors, an electronic brain will be required to govern them. An example of a mechanical injector is the one illustrated with # 23 in Fig. 5, this injector consists of a single action plunger # 39 Fig. 5 and a spring that are driven by the elevation of the Radiano by Combustion # 10 Fig 3, 4, 5, 6, 12, when the plunger is raised, this allows the fuel fed to the cylinder to pass, which will vary depending on the gasoline pressure, the higher the pressure, the greater the fuel that enters, this can be finely calibrated with a jet # 58fig. 5., when the Radiano of Combustion # 10 Fig. 3, 4, 5, 6,12 is fired at the bottom of the Combustion Rotor # 7 Fig. 3, 4, 5, 6, 12,13 the spring of this injector previously Pressurized by it will be triggered by pushing the fuel into the combustion chamber through holes # 46 Fig5 that it has for this purpose in the Radiano. The injection pressures can be very high because the fuel outlet can be very small thanks to the fact that several of these injectors are available all along the Radiano (as explained above) that allow a distribution to be made fast and homogeneous.

The pressurized oil # 18 Fig. 5,5 'coming from a cooling system # 19 and # 20 Fig. 1, 15 is injected into the motor through the holes # 13 Fig. 5 and this runs from the base of the rotor Compression to the opposite side at the base of the Rotor Combustion with branches (veins) to the key points for cooling and lubrication of the motor as well as for the arrow.

The geometrical shape of the parts in the design of this engine allows the sealing of the compression and combustion chambers easily, as well as the sealing and lubrication of the rotors, arrows and locks, as an example Compression and Combustion Rotors they can have graphite packing material or some other solid lubricant in point # 17 Fig. 7, 8 where they impact the radians in order to cushion the blow and apply lubricant to the bottom of them, also the sealing can be carry out with metallic rings # 16 Fig. 7, 8,12 and non-metallic arranged concentrically as well as rings with the geometric shape of the cameras, the same happens for the sealing of Radians # 9and # 10 and of the deposit of compression # 43 Fig. 5.

The supply of pressurized oil # 18 Fig. 5,5 'will allow the lubrication and cooling of the same in the most convenient points, additionally this motor can receive solid lubrication pressurized of high capacity and thermal resistance # 12, Fig. 2, 16 and # 28 Fig. 8, 10, 11, 12, which will allow constant lubrication and sealing as well as reserving high temperature areas in the combustion chambers, this in order to increase the efficiency of the thermodynamic cycle eliminating toxic elements such as hydrocarbons in the exhaust gases to the environment. Moving parts such as rotors are supported with different bearings and bearings # 11 Fig. 3,4 that allow a silent and frictionless operation minimizing the energy wasted by this issue.

The mass of the rotors can be optimized because it is also useful to accumulate a moment of inertia that allows the engine to continue running once it is turned on.

Claims (1)

CLAIMS Having sufficiently described my invention, I consider as a novelty and therefore claim as my exclusive property contained in the following 2 clauses:

1. INTERNAL COMBUSTION RADIANO ENGINE that evokes its name to its mechanical principle, the way in which it moves and the way in which the compression and combustion chambers of the engine are fed, which is characterized by being a circular design engine that feeds its cameras of compression and combustion using the length of a set of radial locks called RADIANS, which follows a bipartisan 4-stroke cycle (Admission, Compression-Transportation, Combustion, Exhaust), that throughout the thermodynamic cycle a constant lever arm is maintained on the motor shaft, which has one or more sets of radial locks called RADIANS that also function as valves, and that they owe their movement to a hermetic displacement on the circular tracks of the rotor where they are supported and that contain a certain number of ridges that serve as a cam to achieve in them a harmonic and synchronic axial movement at all times, that the admission and compression of air is carried out in one part of the engine and combustion and exhaust in another, that the high compression of the intake gases can be carried out in one or more stages through concentric circular tracks, which is through the interior of the Radians that the pressurized air is transported between compression chambers as well as from one end of the engine to the interior of the combustion chamber, which happens In the same way with the fuel, the axial movement and the geometric shape of the Radians is used to efficiently dose the fuel and air inside the combustion chamber since these are able to accommodate a large number of fuel and air injectors Throughout them, with the help of the Radians, these rotors become the combustion and compression chambers of the engine, and that respecting the mechanical principle indicated, these motors may be a rotor called Single Rotor or two Rotors Twin Rotor that also serve as masses, which can receive multiple types of fuel (multi-fuel), that the air-fuel mixture can be ignited with spark, hot body or by the elevated temperature of the exhaust gases of compression, which has a great angular moment of usable gyroscopic effect, that its design can be scaled dimensionally to house one or more sets of Radians and likewise include one or more ridges (cams) in the tracks circular in the rotors, which has very few fixed and mobile parts and therefore its weight is reduced, which can be coupled to other Radian engines axially or polar and with this flexibility in its design resolves precisely needs in the industry. HIGH PRESSURE RADIAL FLUID COMPRESSOR PUMP that evokes its name to its mechanical principle, the way it moves and the way its cameras are powered, which is characterized by being a circular pump-compressor with one or more rotors in its interior, which feeds and unloads its compression chambers through one or more radial locks called RADIANS, that these must their movement to a hermetic displacement on the circular tracks of the rotor where they are supported and that contain a determined number of crests that serve as a cam to achieve in them a harmonic and synchronous axial movement at all times, that by means of these locks called Radians that also serve as outlet conduits for pressurized fluids, the rotor tracks become the chambers of admission and compression, and that is to drive the arrow on which the rotor (s) is mounted that kinetic or potential energy (impulse or compression) n) is added to the fluids that are fed to it, that these can be designed with one or more rotors as well as with one or more consecutive compression chambers (or steps) through their concentric circular tracks as well as having one or more Radian games, and with this flexibility in its design, it solves precise needs in the industry.