公开(公告)号：AU2020268690A1

公开(公告)日：2021-09-02

申请号：AU2020268690

申请日：2020-01-21

Applicant: JETOPTERA INC

Inventor： EVULET ANDREI

IPC: B64C21/02 ,  B64C3/10 ,  B64C15/00 ,  B64C15/12 ,  B64C15/14 ,  B64C21/00 ,  B64C21/04 ,  B64C21/06 ,  B64C21/08 ,  B64C23/00 ,  B64C29/04 ,  B64D27/10 ,  B64D27/14 ,  B64D27/18 ,  B64D33/04 ,  F02C6/04 ,  F02K1/36 ,  F23L17/16

Abstract: An aircraft includes a fuselage and at least one primary wing having an upper surface, at least one recess in the upper surface and at least one conduit in fluid communication with the at least one recess. At least one ejector is disposed within the at least one recess and is configured to receive compressed air via the at least one conduit.

公开(公告)号：CA3126943A1

公开(公告)日：2020-11-12

申请号：CA3126943

申请日：2020-01-21

Applicant: JETOPTERA INC

Inventor： EVULET ANDREI

IPC: B64C21/02 ,  B64C3/10 ,  B64C15/00 ,  B64C15/12 ,  B64C15/14 ,  B64C21/00 ,  B64C21/04 ,  B64C21/06 ,  B64C21/08 ,  B64C23/00 ,  B64C29/04 ,  B64D27/10 ,  B64D27/14 ,  B64D27/18 ,  B64D33/04 ,  F02C6/04 ,  F02K1/36 ,  F23L17/16

Abstract: An aircraft includes a fuselage and at least one primary wing having an upper surface, at least one recess in the upper surface and at least one conduit in fluid communication with the at least one recess. At least one ejector is disposed within the at least one recess and is configured to receive compressed air via the at least one conduit.

公开(公告)号：HK1257209A1

公开(公告)日：2019-10-18

申请号：HK18116212

申请日：2018-12-18

Applicant: JETOPTERA INC

Inventor： EVULET ANDREI

IPC: B64D20060101 ,  B64C20060101 ,  F02C20060101 ,  F02K20060101

公开(公告)号：CA3068569A1

公开(公告)日：2019-01-03

申请号：CA3068569

申请日：2018-06-27

Applicant: JETOPTERA INC

Inventor： EVULET ANDREI

IPC: F02K1/36

Abstract: A vehicle, includes a main body. A fluid generator is coupled to the main body and produces a fluid stream. At least one tail conduit is fluidly coupled to the generator. First and second fore ejectors are 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 includes a closed wing having a leading edge and a trailing edge. The leading and trailing edges of the closed wing define an interior region. The at least one propulsion device is at least partially disposed within the interior region.

公开(公告)号：AU2016382619A1

公开(公告)日：2018-06-14

申请号：AU2016382619

申请日：2016-12-02

Applicant: JETOPTERA INC

Inventor： EVULET ANDREI

IPC: F02C3/04 ,  F02C7/08

Abstract: A propulsion system includes a first compressor in fluid communication with a fluid source. A first conduit is coupled to the first compressor, and a heat exchanger is in fluid communication with the first compressor via the first conduit. A second conduit is positioned proximal to the heat exchanger. A combustor is in fluid communication with the heat exchanger via the second conduit and is configured to generate a high-temperature gas stream. A third conduit is coupled to the combustor, and a first thrust augmentation device is in fluid communication with the combustor via the third conduit. The heat exchanger is positioned within the gas stream generated by the combustor.

公开(公告)号：AU2023233073B2

公开(公告)日：2025-04-10

申请号：AU2023233073

申请日：2023-09-19

Applicant: JETOPTERA INC

Inventor： EVULET ANDREI

IPC: F02K1/36 ,  F02K1/00 ,  F02K1/06 ,  F02K1/08 ,  F02K1/09 ,  F02K1/11 ,  F02K1/28

Abstract: A propulsion system coupled to a vehicle. The system includes a diffusing structure and a conduit portion configured to introduce to the diffusing structure through a passage a primary fluid produced by the vehicle. The passage is defined by a wall, and the diffusing structure comprises a terminal end configured to provide egress from the system for the introduced primary fluid. A constricting element is disposed adjacent the wall. An actuating apparatus is coupled to the constricting element and is configured to urge the constricting element toward the wall, thereby reducing the cross-sectional area of the passage.

公开(公告)号：AU2025201014A1

公开(公告)日：2025-03-06

申请号：AU2025201014

申请日：2025-02-13

Applicant: JETOPTERA INC

Inventor： EVULET ANDREI

IPC: B64C29/04 ,  B64C29/00 ,  B64C39/12 ,  B64D33/04

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.

公开(公告)号：AU2019279873B2

公开(公告)日：2025-02-27

申请号：AU2019279873

申请日：2019-05-29

Applicant: JETOPTERA INC

Inventor： EVULET ANDREI

IPC: B64D33/02 ,  B64C29/04 ,  B64C39/12 ,  F01N13/10 ,  F02C6/08 ,  F02K1/38

Abstract: A vehicle includes a main body and at least one wing coupled to the main body. A source of compressed fluid is coupled to the main body. The vehicle further includes first and second thrusters, each said first and second thruster having an intake structure and each said first and second thruster in fluid communication with the source. The first thruster is coupled to the main body and the second thruster is coupled to the at least one wing. The first and second thrusters are positioned, when in a first configuration, such that at least a portion of a boundary layer produced due to motion of the vehicle is ingested by the intake structures of the first and second thrusters. The vehicle further includes a system for selectively providing the compressed fluid to the first and second thrusters.

公开(公告)号：AU2023330901A1

公开(公告)日：2025-02-06

申请号：AU2023330901

申请日：2023-08-21

Applicant: JETOPTERA INC

Inventor： EVULET ANDREI

IPC: B63H11/10 ,  B63H11/04 ,  F04F5/02

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.

公开(公告)号：IL316931A

公开(公告)日：2025-01-01

申请号：IL31693124

申请日：2024-11-10

Applicant: JETOPTERA INC ,  EVULET ANDREI

Inventor： EVULET ANDREI

IPC: B64C15/14 ,  B64C29/00 ,  B64D33/04

Abstract: An ejector system is constructed of a soft yet strong material such as silicone-based material which can be pressed to conform within a small space and stowed when inactive and can be expanded or stretched by mechanical, pneumatic or hydraulic means when in operation. One or more embodiments of the present invention disclosed in this application relate to an adaptive propulsive system that specifically operates in conjunction with an air compressor or fan.