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公开(公告)号：AU2021245108A1
公开(公告)日：2021-10-28
申请号：AU2021245108
申请日：2021-10-05
Applicant: JETOPTERA INC
Inventor： EVULET ANDREI
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.
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公开(公告)号：IL271678D0
公开(公告)日：2020-02-27
申请号：IL27167819
申请日：2019-12-24
Applicant: JETOPTERA INC , EVULET ANDREI
Inventor： EVULET ANDREI
IPC: B64C20060101
Abstract: A vehicle, includes a main body. A fluid generator is coupled to the main body and produces a fluid stream. At least one tad 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.
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公开(公告)号：CA3102088A1
公开(公告)日：2019-12-05
申请号：CA3102088
申请日：2019-05-29
Applicant: JETOPTERA INC
Inventor： EVULET ANDREI
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.
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公开(公告)号：CA3100545A1
公开(公告)日：2019-11-21
申请号：CA3100545
申请日：2019-05-17
Applicant: JETOPTERA INC
Inventor： EVULET ANDREI
Abstract: A propulsion system includes a source of compressed fluid, at least one thruster in fluid communication with the source, at least one turbine in fluid communication with the source and coupled to a propeller, and an apparatus for selectively providing the compressed fluid to one or both of the at least one thruster and the at least one turbine.
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公开(公告)号：HK1256699A1
公开(公告)日：2019-10-04
申请号：HK18115684
申请日：2018-12-07
Applicant: JETOPTERA INC
Inventor： EVULET ANDREI
IPC: F02K20060101 , B64C20060101
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Patent Agency Ranking
公开(公告)号：AU2017315790A1
公开(公告)日：2019-03-14
申请号：AU2017315790
申请日：2017-08-24
Applicant: JETOPTERA INC
Inventor： EVULET ANDREI
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.
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公开(公告)号：SG11201900823VA
公开(公告)日：2019-02-27
申请号：SG11201900823V
申请日：2017-07-19
Applicant: JETOPTERA INC
Inventor： EVULET ANDREI , HAWKINS JOHN
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.
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公开(公告)号：CA3067346A1
公开(公告)日：2018-12-20
申请号：CA3067346
申请日：2018-06-15
Applicant: JETOPTERA INC
Inventor： EVULET ANDREI
IPC: B64D33/04
Abstract: An ejector system for propelling a vehicle. The system includes a diffusing structure and a duct coupled to the diffusing structure. The duct includes a wall having openings formed therethrough and configured to introduce to the diffusing structure a primary fluid produced by the vehicle. An airfoil is positioned within the flow of the primary fluid through the openings to the diffusing structure.
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公开(公告)号：AU2016315450A1
公开(公告)日：2018-03-22
申请号：AU2016315450
申请日：2016-09-02
Applicant: JETOPTERA INC
Inventor： EVULET ANDREI
Abstract: A vehicle includes a main body and a gas generator producing a gas stream. At least one fore conduit and tail conduit are fluidly coupled to the generator. First and second fore ejectors are fluidly coupled to the at least one fore conduit. At least one tail ejector is fluidly coupled to the at least one tail conduit. The fore ejectors respectively include an outlet structure out of which gas from the at least one fore conduit flows. The at least one tail ejector includes an outlet structure out of which gas from the at least one tail conduit flows. First and second primary airfoil elements have leading edges respectively located directly downstream of the first and second fore ejectors. At least one secondary airfoil element has a leading edge located directly downstream of the outlet structure of the at least one tail ejector.
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公开(公告)号：CA3032950A1
公开(公告)日：2018-02-08
申请号：CA3032950
申请日：2017-07-19
Applicant: JETOPTERA INC
Inventor： EVULET ANDREI , HAWKINS JOHN
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.
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