• 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 combustión gas neutralization system, patent of addition to the main patent p201301160 title celestial impulse engine. This addition patent aims to avoid atmospheric pollution of the engine, when it works by consuming fossil fuels, petroleum derivatives. It includes a secondary cooling system that condenses the water vapor of combustión, using this condensation to wash the gases of the aforementioned combustión and to retain the micro-particles, which cause pollution, inside the engine, while the water liquid, produced by condensation inside the engine, partially dissolves part of the co2 produced, expelling it from the bottom of the engine to the ground, as carbonated water harmless to the environment. With what is achieved, to the same amount of fuel consumed, cancel the micro-particle contamination and reduce the co2 emissions. (Machine-translation by Google Translate, not legally binding)
    公开号:ES2545972A1
    申请号:ES201400114
    申请日:2014-02-17
    公开日:2015-09-17
    发明作者:Diego ORELLANA HURTADO
    申请人:Diego ORELLANA HURTADO；
    IPC主号:
    专利说明:

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    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.
    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
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    权利要求:
    Claims (1)
    [1]
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    类似技术:
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    同族专利:
    公开号 | 公开日
    ES2545972B1|2016-06-28|
    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|
    WO2006137723A1|2005-06-23|2006-12-28|Eduardo Lopez Sandoval|Radial flow gas turbine|
    FR2905982A1|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|2010-08-31|2012-03-08|Bondarenko Vladimir Petrovich|Propulsion system|WO2015092088A1|2013-12-17|2015-06-25|Diego Orellana Hurtado|Circular propulsion jet compressor-engine|
    法律状态:
    2016-06-28| FG2A| Definitive protection|Ref document number: 2545972 Country of ref document: ES Kind code of ref document: B1 Effective date: 20160628 |
    优先权:
    申请号 | 申请日 | 专利标题
    ES201400114A|ES2545972B1|2014-02-17|2014-02-17|Circular impulse motor with combustion gas neutralization system|ES201400114A| ES2545972B1|2014-02-17|2014-02-17|Circular impulse motor with combustion gas neutralization system|
    CN201480073320.8A| CN107076022B|2013-12-17|2014-12-15|Circular propelling jet type compression engine|
    PCT/ES2014/000211| WO2015092088A1|2013-12-17|2014-12-15|Circular propulsion jet compressor-engine|
    AP2016009283A| AP2016009283A0|2013-12-17|2014-12-15|Circular propulsion jet compressor-engine|
    US15/105,700| US10273879B2|2013-12-17|2014-12-15|Circular propulsion jet compressor-engine|
    MX2016007888A| MX366492B|2013-12-17|2014-12-15|Circular propulsion jet compressor-engine.|
    EP14871207.8A| EP3085922A4|2013-12-17|2014-12-15|Circular propulsion jet compressor-engine|
    JP2016541646A| JP6377163B2|2013-12-17|2014-12-15|Circular propulsion jet compressor engine|
    EA201691026A| EA033334B1|2013-12-17|2014-12-15|Circular propulsion jet compressor|
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