ES2545972A1 - Circular drive motor with combustión gas neutralization system (Machine-translation by Google Translate, not legally binding) - Google Patents
Circular drive motor with combustión gas neutralization system (Machine-translation by Google Translate, not legally binding) Download PDFInfo
- Publication number
- ES2545972A1 ES2545972A1 ES201400114A ES201400114A ES2545972A1 ES 2545972 A1 ES2545972 A1 ES 2545972A1 ES 201400114 A ES201400114 A ES 201400114A ES 201400114 A ES201400114 A ES 201400114A ES 2545972 A1 ES2545972 A1 ES 2545972A1
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- Prior art keywords
- engine
- combustión
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/08—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
Description
sobre la superficie interior de las mismas), y el compresor de aire (16). La base sirve de apoyo a los rodamientos (23) para el eje de giro del motor. La base se fija mediante pernos de anclaje a un soporte que está sujeto a una bancada amortiguada para absorber las vibraciones. El chasis exterior del motor tiene la forma de dos platos, el inferior colocado en posición normal (hacia arriba), constituye el soporte y bancada de la base del motor y, en su parte más baja (fondo del plato), aloja un depósito (17) que recoge los productos resultantes de la combustión (condensados y sales neutras). Una vez instalado la parte inferior del chasis y acoplada la toma de aire exterior (15) para la combustión, se fija a esta parte inferior, la base del motor (26) y los rodamientos (23) que han de soportar al eje de giro y la rueda de esferas. Todo el material del motor se puede fabricar en acero. Mecanizado el eje (25), se acopla a los rodamientos de la base (23), quedando en posición vertical sobre la misma. Todo el montaje hay que realizarlo desde abajo hacia arriba. Este eje (25) está perforado en su parte inferior para alojar el compresor de aire (16) y en el centro del mismo la canalización (18) del sistema de refrigeración primario y en su parte superior, longitudinalmente aloja la canalización de la carga de combustible (30) y la canalización del sistema de señales y de control eléctrico (33). Sobre el eje se acopla el soporte inferior de la rueda de esferas que contiene los depósitos de aire comprimido (19) y agua (20) del sistema primario de refrigeración. En el perímetro exterior este soporte lleva mecanizados los huecos necesarios para la fijación de las esferas (1) previstas en el diseño del motor. Cada uno de estos huecos aloja una cavidad mecanizada y un rodamiento acoplado a la misma en el que encajará el eje de la esfera correspondiente. on the inner surface thereof), and the air compressor (16). The base supports the bearings (23) for the motor's axis of rotation. The base is fixed by means of anchor bolts to a support that is attached to a dampened bench to absorb vibrations. The outer chassis of the engine has the form of two plates, the lower one placed in normal position (upwards), constitutes the support and bed of the base of the engine and, in its lower part (bottom of the plate), houses a tank ( 17) which collects the products resulting from combustion (condensates and neutral salts). Once the lower part of the chassis is installed and the external air intake (15) for combustion is attached, the base of the engine (26) and the bearings (23) to support the rotation axis are fixed to this lower part and the spheres wheel. All engine material can be made of steel. Machining the shaft (25), it is coupled to the bearings of the base (23), being upright on it. All assembly must be done from the bottom up. This shaft (25) is perforated in its lower part to house the air compressor (16) and in the center of it the pipe (18) of the primary cooling system and in its upper part, longitudinally it houses the pipeline of the load of fuel (30) and the channeling of the signal and electrical control system (33). The lower support of the ball of spheres containing the compressed air tanks (19) and water (20) of the primary cooling system is coupled on the shaft. In the outer perimeter this support has machined the holes necessary for fixing the spheres (1) provided in the engine design. Each of these holes houses a mechanized cavity and a bearing coupled to it in which the axis of the corresponding sphere will fit.
El montaje ha de seguir instalando cada una de las esferas en sus respectivos alojamientos y realizando sobre las mismas las conexiones para la alimentación de combustible (4) comburente (5) agua de refrigeración (6) y circuito eléctrico de inicio de la combustión (7), alimentación del motor eléctrico de la esfera (34) y señales de control. Igualmente este soporte inferior lleva mecanizado el hueco necesario para poder acoplar el propulsor (8) asimétrico a la esfera. Una vez instalada cada esfera en su lugar, se acopla sobre el eje, el soporte superior de las esferas. Quedan cerrados los depósitos de aire a presión (19) y agua del sistema primario de refrigeración (20) y las esferas quedan rígidamente acopladas a la rueda. Esto se produce por el acoplamiento del eje superior de las esferas (25), en los rodamientos (24) que el soporte superior de las esferas, lleva alojados en sus correspondientes huecos, previamente mecanizados. El eje superior de las esferas, sobresale por encima del soporte superior y en este eje se acoplan los motores (34), paso a paso que orientarán, en su caso, la salida de los gases de propulsión. Alojados en el soporte superior, se instalan los inyectores de combustible y comburente (14), válvulas de control del circuito de refrigeración, bombas de presión del combustible (13), que descargan este sobre un distribuidor anular común (12), al que se conectan los inyectores de combustible y el propio depósito de combustible (21). El depósito (21), se ha de construir de las características adecuadas para el tipo de combustible a utilizar y proteger en toda su superficie con material aislante a la atmósfera interior del motor, caliente y ligeramente ácida. La morfología del depósito es toroidal. Situado el depósito en su lugar, se acopla al mismo la alimentación de combustible (30), a través de la canalización del eje central y la señal eléctrica de control de nivel (37) que está igualmente canalizada por el eje central. A continuación se acoplan los propulsores asimétricos (8) por las dos componentes de la velocidad que tienen los gases en expansión y se acoplan los rodamientos de la parte superior del eje central al propio eje. Fijado a la parte superior del chasis del motor y perimetralmente al mismo, se instalan los tubos de metal y tratamiento antiácido del sistema secundario de refrigeración (10), para enfriar y condensar en lo posible, los gases de la combustión, produciendo en la The assembly must continue installing each of the spheres in their respective housings and making on them the connections for the fuel supply (4) oxidizer (5) cooling water (6) and electrical combustion start circuit (7 ), electric motor supply of the sphere (34) and control signals. Likewise, this lower support has the necessary hole machined to be able to attach the impeller (8) asymmetric to the sphere. Once each sphere is installed in its place, the upper support of the spheres is coupled on the shaft. The pressurized air tanks (19) and water of the primary cooling system (20) are closed and the spheres are rigidly coupled to the wheel. This is produced by the coupling of the upper axis of the spheres (25), in the bearings (24) that the upper support of the spheres, is housed in their corresponding holes, previously machined. The upper axis of the spheres, protrudes above the upper support and in this axis the motors (34) are coupled, step by step that will guide, where appropriate, the output of the propulsion gases. Housed in the upper support, the fuel and oxidizer injectors (14), refrigeration circuit control valves, fuel pressure pumps (13) are installed, which discharge this onto a common annular distributor (12), to which connect the fuel injectors and the fuel tank itself (21). The tank (21) must be constructed of the characteristics suitable for the type of fuel to be used and protected on its entire surface with insulating material to the interior atmosphere of the engine, hot and slightly acidic. The morphology of the deposit is toroidal. With the tank in place, the fuel supply (30) is coupled to it, through the central axis channeling and the electrical level control signal (37) which is also channeled through the central axis. The asymmetric thrusters (8) are then coupled by the two velocity components that the expanding gases have and the bearings of the upper part of the central axis are coupled to the axis itself. Fixed to the top of the engine chassis and perimeter to it, the metal pipes and antacid treatment of the secondary cooling system (10) are installed, to cool and condense as much as possible, the combustion gases, producing in the
7 7
Claims (1)
Priority Applications (10)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES201400114A ES2545972B1 (en) | 2014-02-17 | 2014-02-17 | Circular impulse motor with combustion gas neutralization system |
BR112016014299A BR112016014299A2 (en) | 2013-12-17 | 2014-12-15 | CIRCULAR JET PROPULSION ENGINE-COMPRESSOR |
MX2016007888A MX366492B (en) | 2013-12-17 | 2014-12-15 | Circular propulsion jet compressor-engine. |
PCT/ES2014/000211 WO2015092088A1 (en) | 2013-12-17 | 2014-12-15 | Circular propulsion jet compressor-engine |
EP14871207.8A EP3085922A4 (en) | 2013-12-17 | 2014-12-15 | Circular propulsion jet compressor-engine |
JP2016541646A JP6377163B2 (en) | 2013-12-17 | 2014-12-15 | Circular propulsion jet compressor engine |
EA201691026A EA033334B1 (en) | 2013-12-17 | 2014-12-15 | Circular propulsion jet compressor |
US15/105,700 US10273879B2 (en) | 2013-12-17 | 2014-12-15 | Circular propulsion jet compressor-engine |
CN201480073320.8A CN107076022B (en) | 2013-12-17 | 2014-12-15 | Circular propelling jet type compression engine |
AP2016009283A AP2016009283A0 (en) | 2013-12-17 | 2014-12-15 | Circular propulsion jet compressor-engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES201400114A ES2545972B1 (en) | 2014-02-17 | 2014-02-17 | Circular impulse motor with combustion gas neutralization system |
Publications (2)
Publication Number | Publication Date |
---|---|
ES2545972A1 true ES2545972A1 (en) | 2015-09-17 |
ES2545972B1 ES2545972B1 (en) | 2016-06-28 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES201400114A Expired - Fee Related ES2545972B1 (en) | 2013-12-17 | 2014-02-17 | Circular impulse motor with combustion gas neutralization system |
Country Status (1)
Country | Link |
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ES (1) | ES2545972B1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2015092088A1 (en) | 2013-12-17 | 2015-06-25 | Diego Orellana Hurtado | Circular propulsion jet compressor-engine |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2404334A (en) * | 1939-12-09 | 1946-07-16 | Power Jets Res & Dev Ltd | Aircraft propulsion system and power unit |
WO2006137723A1 (en) * | 2005-06-23 | 2006-12-28 | Eduardo Lopez Sandoval | Radial flow gas turbine |
FR2905982A1 (en) * | 2006-09-19 | 2008-03-21 | Branislav Stefanovic | Silencer turbine engine for e.g. terrestrial vehicle, has reduction gear-inverter arranging reducing and inverting unit to reduce or invert number of rotations transmitted by driving shaft from energy produced by turbine |
WO2012030311A1 (en) * | 2010-08-31 | 2012-03-08 | Bondarenko Vladimir Petrovich | Propulsion system |
-
2014
- 2014-02-17 ES ES201400114A patent/ES2545972B1/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2404334A (en) * | 1939-12-09 | 1946-07-16 | Power Jets Res & Dev Ltd | Aircraft propulsion system and power unit |
WO2006137723A1 (en) * | 2005-06-23 | 2006-12-28 | Eduardo Lopez Sandoval | Radial flow gas turbine |
FR2905982A1 (en) * | 2006-09-19 | 2008-03-21 | Branislav Stefanovic | Silencer turbine engine for e.g. terrestrial vehicle, has reduction gear-inverter arranging reducing and inverting unit to reduce or invert number of rotations transmitted by driving shaft from energy produced by turbine |
WO2012030311A1 (en) * | 2010-08-31 | 2012-03-08 | Bondarenko Vladimir Petrovich | Propulsion system |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2015092088A1 (en) | 2013-12-17 | 2015-06-25 | Diego Orellana Hurtado | Circular propulsion jet compressor-engine |
US10273879B2 (en) | 2013-12-17 | 2019-04-30 | Diego ORELLANA HURTADO | Circular propulsion jet compressor-engine |
Also Published As
Publication number | Publication date |
---|---|
ES2545972B1 (en) | 2016-06-28 |
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