• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    Circular impulse motor with ceramic and omnidirectional propellant in the application for the patent of addition of the main patent p201301160 and of the motor title of celestial impulse, comprising a main axis of rotation to which mechanical arms are attached in solidarity at the ends of which there are fixed spheres steel, hollow and its interior covered with refractory ceramic. In these spheres fuel and comburent are injected at high pressure and in the combustión the gases leave by a propeller coupled to the spheres, creating a torque and giving available power in the axis of rotation. The spheres can change the output direction of the propellant gases and pass from the tangential direction to the radial upward-downward, left-right direction. (Machine-translation by Google Translate, not legally binding)
    公开号:ES2544572A1
    申请号:ES201400068
    申请日:2014-01-27
    公开日:2015-09-01
    发明作者:Diego ORELLANA HURTADO
    申请人:Diego ORELLANA HURTADO；
    IPC主号:
    专利说明:

    DESCRIPTION

    Addition to patent P20131160 Celestial impulse motor: Circular impulse motor with ceramic and omnidirectional propeller.
     5
    Technical sector

    The research, production, transformation and use of thermal energy that comes from any fuel in liquid or gas phase. The sectors of the technique involved are those of the machines for the generation of electrical energy and that of the 10 motors for the drive of vehicles of any nature.

    State of the art

    The jet propellant technique is varied in unidirectional impulse but in circular impulse and with omnidirectional capacity there is no library, nor published documentation or patents, except P201301160, pending.

    Explanation of the addition patent
     twenty
    It is a variant of the combustion system.

    Technical issues raised

    Increase yields for what is necessary high temperatures in the combustion chamber 25.

    Get a propulsion engine to drive a vehicle in any direction.
     30
    Solutions to the problems

    To achieve high temperature in the combustion chamber, it is made of steel and internally coated with refractory ceramics. To achieve impulse capacity in any direction, several thrusters are placed rotating and capable of directing the combustion gases in accordance with a predetermined steering vector. If the vehicle is aerial, it will be necessary to install two propeller wheels on the same axle, supporting the rotation of one on the other. In this case, a rack-and-pinion system is also installed that allows the vertical axis of the wheels to be modified, in relation to the horizontal plane of symmetry of the engine. 40

    Advantages of the proposed solutions

    In piston and crankshaft engines the ceramic cannot be used because it is hard but fragile and its machining is very difficult. The same thing happens in jet engines for aviation. With the proposed solution, the piston and crankshaft engines and the unidirectional aviation engines can be replaced by ceramic sphere motors.

    By arranging them in a circle and constant rotation, an additional advantage is achieved by being able to orient the output of the propulsion gases in any direction 50

    Description of the drawings. Figure 1

    (1) Engine base or cylinder head.

    (2) Circular motor body. It has vents. 5

    (3) Top cover of the motor body.

    (4) Starter motor coupling and power output.
     10
    (5) Main axis of rotation. Torsion works. When used as a directional impulse, it works with torsion and flexion (not the case drawn).

    (6) Horizontal arms where they support the spheres.
     fifteen
    (7) Spheres with ceramic interior coating.

    (8) Seat base with vibration damping supports.

    (9) Control of fuel injection and oxidizer to the spheres. twenty

    (10) Engine that controls the direction of the output of the propellant gases.

    (11) Shaft base bearing.
     25
    (12) Shaft head bearing.

    (13) Power output.

    (14) Shaft gear for starting. 30

    (15) Starter motor pinion.

    (16) Engine at start and alternator in normal operation for power supplies. It can be an asynchronous motor of c.a. 35

    (17) Air cooling system fans. Depending on the power this system can incorporate water in a conventional cooling circuit.

    (18) Coupling of the oxidizer to the design pressure by means of a rotary system 40 sealed.

    (19) Coupling for fuel at design pressure.

    (20) Power supply of the positioning motors to the spheres. Four. Five

    (21) Power supply to the fuel injection and combustion control valves.

    (22) Friction ring system for power supply and control of the rotating elements.
    (23) Propellers of ceramic walls and steel body.

    Brief explanation of the drawings

    Figure 1 represents an elevational section of the circular pulse motor and Figure 2 is a plan section. By means of the external electric power supply, the starter motor (16) is started, which through the gear train (15) and (14) rotates the central axis (5) at the angular design speed. The horizontal arms (6) jointly joined to the aforementioned axis, transmit this rotation to the spheres (7), the rotating assembly storing the electrical energy consumed in the start-up, in kinetic energy 10, because its configuration is that of a steering wheel inertia.

    The circular impulse motor has the technical characteristic of operating with constant angular velocity, which may be variable for different motors or even for the same motor, but it must always have a preset speed for a given operating regime. (low load, medium or high). Once this preset speed has been reached, a control computer gives the signal for the fuel injection that is supplied by means of the rotary coupling (19) and injection of oxidizer (air normally), at very high pressure, by means of the rotary coupling (18). The injection of both components is controlled by a device of electromagnetic valves 20 and injectors (9), similar to that used in internal combustion engines. It must be said that the jet propellant can only achieve adequate thermal performance if the injection pressure of the oxidizer (air) is very high, so that its mechanical impulse (m. V) is as high as possible, in relation to the heat supplied. Fuel and oxidizer are mixed inside the sphere (7) and its ignition produces a rapid expansion of the gases that are expelled by the propeller (23) and by the third principle of Newton's mechanics to the increase of the linear momentum of The mass of gas that leaves the propeller in the opposite direction to the rotation of the spheres, corresponds to an equal and opposite reaction in the direction of the spheres of the spheres, this means that the central axis tends to increase its revolutions, which makes the Asynchronous motor 30 (16) is automatically transformed into an asynchronous generator of alternating current and also, this increase in revolutions, as an increase in the power of the rotating assembly, can be used, by coupling a mechanical load to the power shaft (13). The circulating impulse motor has the property of operating automatically as a hybrid motor, because when the revolutions of the central axis are reduced below the established limit, the electric alternator automatically transforms into an engine and supports maintaining the revolutions and in the On the contrary, if a drop in the load tends to accelerate the revolutions of the shaft, the electric alternator, by increasing its sliding range, automatically increases its power generation, acting as an electric brake. 40

    The gases when they leave the propeller (23), have two velocity components, one radial by centrifugal force and another tangential by thermal energy, a function of temperature, which decays very quickly.
     Four. Five
    The radial is a function of the revolutions and the mass, so it does not decay and the aforementioned gases tend to continue turning inside the engine enclosure, where by a cooling system, represented by the extractors (17), they are cooled and taken out of the aforementioned enclosure. At their exit, these gases will pass through the catalyst, silencer and exhaust ducts, not shown. fifty

    Detailed presentation of an embodiment

    The spheres (7) are manufactured in refractory ceramics, broken molds and with the necessary holes for the injection of fuel and oxidizer and the exit of the propulsion gases. They are covered with rolled steel plates, welded together and of sufficient thickness to withstand the expansion efforts of combustion gases. The central axis (5) is machined with three support points for bearings and, holes in its center, for feeding the fuel and oxidizer (6) at high pressure, whose ducting pipes, are coupled at their upper and lower ends by rotating pressure fittings (18) and (19). The engine chassis is manufactured in three pieces, 10 base (1), body (2) and cover (3).

    The base is fixed by means of anchor bolts to a support (8) that dampens vibrations. The motor assembly begins by placing the base in place and fixing it to its support. Then the shaft bearing is attached to the base and the shaft itself. Next, the arms that support the spheres, made of steel of sufficient mechanical strength to support their weight and centrifugal efforts of rotation, must be fixed. The arms channel to the spheres, by means of concentric conduits, the fuel and the oxidizer that increase their pressure, due to the centrifugal force and have injection mechanisms (9), consisting of electromagnetic valves 20 that open and close by means of control pulses . The aforementioned valves and their electrical connection (20) are installed, which connects to the control (computer) by means of a ring (22) at the top of the shaft and electrically isolated from the shaft itself. The ignition of the mixture will depend on the type of fuel and can be carried out by means of spark or resistance heating or spraying and injection of hot oxidizer. Next, and on the spheres, the motors (10) that can modify the direction of the output of the propellant gases, stepper electric motors and anchorage, controlled by the ceramic motor computer, are coupled. Once this is done, the circular body of the motor is attached to the base of the motor. This body has vents in all its contour and some extractors (17) located circularly to evacuate the heat of the gases once they have left the nozzle of the propeller. The fans are coupled to their shafts and the motor can now be closed with its cover that has the shaft bearing (12) attached. Next, the gear (14) and the auxiliary starter motor (16) coupled to said gear by means of the pinion (15) are fitted. With the coupling of the upper bearing, the motor is closed and 35 is ready for the functional tests.

    Industrial application of the addition patent

    In the generation of electrical energy, coupling the shaft of an electric generator 40 to the outlet (13). As a motor for moving land vehicles by coupling the corresponding vehicle drive or gearbox input shaft to the axle (13). As an engine for marine ships, coupling the propeller shaft of the ship or submarine to the shaft (13). Placing two wheels of spheres coupled in its turn and allowing to swing to the common axis can be used as an impulse engine for aviation or for ships. Four. Five

    Justification of the patent of addition

    The addition is an alternative to high pressure flooded chamber combustion of the main patent. The inventor has considered that the new technology that involves the combustion under liquid can delay the practical application of the celestial impulse engine
    Therefore, the present addition patent is proposed, which with elements of existing and proven technology, adapted to the celestial impulse motor procedure, will allow to verify the advantages of the main patent.
    权利要求:
    Claims (3)
    [1]

    1. Circular impulse motor, with ceramic and omnidirectional propeller, which by means of a circular set of propellers (23) with spherical geometry combustion chambers (7) generates a tangential impulse at the turning radius and the resulting resulting moment 5 on an axis of rotation (5). This impulse is a consequence of the expansion and high-speed output of the very hot gases from the combustion chambers, by the ejectors thereof, as a consequence of the combustion of the fuel and oxidizer inside and the consequent violent expansion of the gases produced by this combustion causing the effect of action and reaction of a jet or 10 jet propeller. The circular impulse motor with ceramic and omnidirectional propeller is characterized by having a central axis (5), supported by axial and radial bearings (11) and (12), on a support structure (1), (2) and (3) . The aforementioned shaft is perforated longitudinally, by means of concentric tubes through which the fuel (19) and the pressurized fuel (18) are injected, combustion regulation injectors (9) and spheroidal combustion chambers 15 (7), internally covered with ceramics refractory and supported by mechanical arms (6) or rotating platforms, integral to the central axis of rotation. It comprises a system for addressing the ejectors of combustion gases, by means of electric positioning motors (10) and comprises a cooling system by means of air extractors (17) which, 20 according to the design power, can be replaced by water cooling systems. It comprises a starter motor (16), normally electric from AC, and which can work as an electric generator during the operation of the thermal motor.
    A mechanical transmission system (14) and (15) from the rotation of the motor to the central axis. An ignition system that can be by means of an electric spark or spark plug, hot spot by ceramic resistance or injection of very hot oxidizer (air) and electric power supply (20) and (21), by friction rings (22) in the central axis and electrically isolated from it, for control of the injection valves (9) directional motors (10) and ignition system. 30

    [2]
    2. Circular impulse motor with ceramic and omnidirectional propeller, according to claim 1, which has the ability to make a directional impulse according to a predetermined direction vector, forward in acceleration or deceleration, to the right or to the left and for this it is characterized by installing two circular sets 35 of wheels of propeller spheres (7), located one above the other in the same central axis of rotation (5), supporting the rotation of one of them on the other, so they have to turn in in the opposite direction to keep the angular momentum equal to zero and to be able to orient the combustion gases output by means of the motors (10) of the spheres of one of the spheres wheels radially, during the course of a determined arc of circumference 40 .

    [3]
    3. Circular impulse motor with ceramic and omnidirectional propeller, according to claims 1 and 2, which has the ability to make a directional impulse according to a predetermined direction vector, which can be ascending or descending in acceleration or deceleration and for this it is characterized by arranging in the central axle (5) that supports the two spheres wheels turning in opposite directions and in one of its ends or in both, the support bearings of said axle, being the supports of these bearings, joined in solidarity with some helical gear zippers. These zippers form arcs of circumferences whose geometric centers coincide 50 with the geometric center of symmetry of the central axis and are coupled to screws without
    Finally, which, by means of electric motors that can make them turn both ways, displace the aforementioned zippers. In its displacement the zippers drag the axle support bearings so that it loses its verticality in relation to the horizontal plane of symmetry of the motor, and the same happens to the plane of rotation of the spheres so that the propellers of the spheres that are in a radial position during a given arc of rotation, they will make directional impulses, the direction vectors of these impulses being contained in the inclined plane of the rotating circle of the spheres.
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    同族专利:
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    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US2404334A|1939-12-09|1946-07-16|Power Jets Res & Dev Ltd|Aircraft propulsion system and power unit|
    ES2007844A6|1988-05-13|1989-07-01|Cortizo Garrido Manuel|Transforming motor of centrifugal energy in mechanical energy. |
    EP1548364A2|2003-12-24|2005-06-29|C.R.F. Società Consortile per Azioni|A rotary combustor, and electrical generator comprising a combustor of this type|
    WO2006137723A1|2005-06-23|2006-12-28|Eduardo Lopez Sandoval|Radial flow gas turbine|
    WO2013057351A1|2011-10-17|2013-04-25|Lopez Heras Jose Maria|Machine for the transmission of kinetic energy to other machines and electricity generators|WO2015092088A1|2013-12-17|2015-06-25|Diego Orellana Hurtado|Circular propulsion jet compressor-engine|
    法律状态:
    2016-06-09| FG2A| Definitive protection|Ref document number: 2544572 Country of ref document: ES Kind code of ref document: B1 Effective date: 20160609 |
    优先权:
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