Configuración para sistema de despegue y aterrizaje verticales para vehículos aéreos

    公开(公告)号:ES2906820T3

    公开(公告)日:2022-04-20

    申请号:ES17807144

    申请日:2017-03-10

    Applicant: JETOPTERA INC

    Inventor: EVULET ANDREI

    Abstract: Un vehículo (400), que comprende: un cuerpo (101) principal que tiene una parte (102) de frente, una parte (103) de cola, un lado de estribor y un lado de babor; un generador (104) de fluido acoplado al cuerpo (101) principal y que produce una corriente de fluido; al menos un conducto (111) de frente acoplado de forma fluida al generador (104); al menos un conducto (112) de cola acoplado de forma fluida al generador (104); eyectores (105,106) de frente primero y segundo acoplados de forma fluida al, al menos, un conducto (111) de frente, acoplados a la parte (102) de frente y acoplados respectivamente al lado de estribor y al lado de babor, los eyectores de frente (105,106) que comprenden respectivamente una estructura de salida fuera de la cual fluye fluido desde el al menos un conducto (111) de frente a una velocidad ajustable predeterminada; al menos un eyector (109,110) de cola acoplado de forma fluida al, al menos, un conducto (112) de cola y acoplado a la parte (103) de cola, el al menos un eyector (109,110) de cola que comprende una estructura de salida de la cual fluye fluido del al menos un conducto (112) de cola a una velocidad ajustable predeterminada; y un elemento (115) de perfil aerodinámico principal que tiene una superficie, el elemento (115) de perfil aerodinámico principal acoplado a la parte (103) de cola, la superficie del elemento (115) de perfil aerodinámico principal está ubicada directamente en sentido descendente del primer y segundo eyectores (105,106) de frente de manera que el fluido de los eyectores (105,106) de frente primero y segundo fluya sobre la superficie del elemento (115) de perfil aerodinámico principal; caracterizado por que el elemento (115) de perfil aerodinámico principal comprende un ala (409) cerrada que tiene un borde de ataque y un borde de salida, los bordes de ataque y de salida del ala (409) cerrada que definen una región interior.

    Ejector and airfoil configurations
    43.
    发明专利

    公开(公告)号:AU2016338382B2

    公开(公告)日:2021-04-01

    申请号:AU2016338382

    申请日:2016-07-27

    Applicant: JETOPTERA INC

    Inventor: EVULET ANDREI

    Abstract: A propulsion system coupled to a vehicle. The system includes an ejector having an outlet structure out of which propulsive fluid flows at a predetermined adjustable velocity. A control surface having a leading edge is located directly downstream of the outlet structure such that propulsive fluid from the ejector flows over the control surface.

    INTERNAL COMBUSTION ENGINE EXHAUST PIPE FLUIDIC PURGER SYSTEM

    公开(公告)号:SG11201900875SA

    公开(公告)日:2019-02-27

    申请号:SG11201900875S

    申请日:2017-08-07

    Applicant: JETOPTERA INC

    Inventor: EVULET ANDREI

    Abstract: An internal combustion engine includes an exhaust conduit having an exhaust port fluidically coupled to ambient fluid and having an internal cross-sectional area and an engine cylinder fluidically coupled to the exhaust conduit. A fluidic amplifier is disposed within the exhaust conduit and is fluidically coupled to the engine cylinder. The amplifier is further fluidically coupled to a source of primary fluid and is configured to introduce the primary fluid and at least a portion of fluid from the engine cylinder to the exhaust port.

    Internal combustion engine intake power booster system

    公开(公告)号:AU2017305160A1

    公开(公告)日:2019-02-21

    申请号:AU2017305160

    申请日:2017-07-19

    Applicant: JETOPTERA INC

    Abstract: An internal combustion engine includes an intake conduit fluidically coupled to ambient fluid and having an internal cross-sectional area and an engine cylinder fluidically coupled to the intake conduit. A fluidic amplifier is disposed within the intake conduit and is fluidically coupled to the ambient fluid and engine cylinder. The amplifier is further fluidically coupled to a source of primary fluid and is configured to introduce the primary fluid and at least a portion of the ambient fluid to the engine cylinder.

    Configuration for vertical take-off and landing system for aerial vehicles

    公开(公告)号:AU2017274156A1

    公开(公告)日:2018-09-27

    申请号:AU2017274156

    申请日:2017-03-10

    Applicant: JETOPTERA INC

    Inventor: EVULET ANDREI

    Abstract: A vehicle, includes a main body. A fluid generator is coupled to the main body and produces a fluid stream.. At least one fore conduit and at least one tail conduit are fluidly coupled to the generator. First and second fore ejectors are fluidly coupled to the fore conduit, coupled to the main body and respectively coupled to a starboard side and port side of the vehicle. The fore ejectors respectively comprise an outlet structure out of which fluid flows. At least one tail ejector is fluidly coupled to the tail conduit. The tail ejector comprises an outlet structure out of which fluid flows. A primary airfoil element is coupled to the tail portion. A surface of the primary airfoil element is located directly downstream of the first and second fore ejectors such that the fluid from the first and second fore ejectors flows over the such surface.

    Fluidic propulsive system
    47.
    发明专利

    公开(公告)号:AU2016338383A1

    公开(公告)日:2018-03-22

    申请号:AU2016338383

    申请日:2016-07-27

    Applicant: JETOPTERA INC

    Inventor: EVULET ANDREI

    Abstract: A propulsion system coupled to a vehicle. The system includes a convex surface, a diffusing structure coupled to the convex surface, and at least one conduit coupled to the convex surface. The conduit is configured to introduce to the convex surface a primary fluid produced by the vehicle. The system further includes an intake structure coupled to the convex surface and configured to introduce to the diffusing structure a secondary fluid accessible to the vehicle. The diffusing structure comprises a terminal end configured to provide egress from the system for the introduced primary fluid and secondary fluid.

    CONFIGURATION FOR VERTICAL TAKE-OFF AND LANDING SYSTEM FOR AERIAL VEHICLES

    公开(公告)号:CA3017263A1

    公开(公告)日:2017-12-07

    申请号:CA3017263

    申请日:2017-03-10

    Applicant: JETOPTERA INC

    Inventor: EVULET ANDREI

    Abstract: A vehicle, includes a main body. A fluid generator is coupled to the main body and produces a fluid stream.. At least one fore conduit and at least one tail conduit are fluidly coupled to the generator. First and second fore ejectors are fluidly coupled to the fore conduit, coupled to the main body and respectively coupled to a starboard side and port side of the vehicle. The fore ejectors respectively comprise an outlet structure out of which fluid flows. At least one tail ejector is fluidly coupled to the tail conduit. The tail ejector comprises an outlet structure out of which fluid flows. A primary airfoil element is coupled to the tail portion. A surface of the primary airfoil element is located directly downstream of the first and second fore ejectors such that the fluid from the first and second fore ejectors flows over the such surface.

    Propulsion system and applications thereof

    公开(公告)号:IL319090A

    公开(公告)日:2025-04-01

    申请号:IL31909025

    申请日:2025-02-18

    Inventor: EVULET ANDREI

    Abstract: A propulsion system coupled to an aft portion of a hull of a water-borne vehicle includes a convex surface, a pump configured to impel a liquid, a diffusing structure coupled to the convex surface, at least one conduit coupled to the convex surface and configured to introduce to the convex surface a primary liquid provided by the pump, and an intake structure coupled to the convex surface and configured to introduce to the diffusing structure a secondary liquid accessible to the vehicle, wherein the diffusing structure comprises a terminal end configured to provide egress from the system for the introduced primary liquid and secondary liquid.

    Configuration for vertical take-off and landing system for aerial vehicles

    公开(公告)号:AU2017274156B2

    公开(公告)日:2022-10-13

    申请号:AU2017274156

    申请日:2017-03-10

    Applicant: JETOPTERA INC

    Inventor: EVULET ANDREI

    Abstract: A vehicle, includes a main body. A fluid generator is coupled to the main body and produces a fluid stream.. At least one fore conduit and at least one tail conduit are fluidly coupled to the generator. First and second fore ejectors are fluidly coupled to the fore conduit, coupled to the main body and respectively coupled to a starboard side and port side of the vehicle. The fore ejectors respectively comprise an outlet structure out of which fluid flows. At least one tail ejector is fluidly coupled to the tail conduit. The tail ejector comprises an outlet structure out of which fluid flows. A primary airfoil element is coupled to the tail portion. A surface of the primary airfoil element is located directly downstream of the first and second fore ejectors such that the fluid from the first and second fore ejectors flows over the such surface.

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