| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 61 | 비행접시 | KR1020040079998 | 2004-10-07 | KR1020060031105A | 2006-04-12 | 김이섭 |
| 본 고안발명은 팬을 이용해 공기를 흡입하며 비행체의 지붕 곡면을 따라 흐르는 공기흐름에 의해 발생하는 저압에 의해발생하는 부양력을 이용해 비행하는 비행법시에 관한 발명이다. 비행접시,팬, 공기흡입구, 공기배출구 | ||||||
| 62 | 원반 비행접시 | KR1020010009394 | 2001-02-21 | KR1020020069061A | 2002-08-29 | 서민호 |
| PURPOSE: A disk flying saucer is provided to make the movement fast, to make flying simple, to reduce noise and fuel, to make a runway not required, and to make taking off and landing simple. CONSTITUTION: A vertical ascent is performed by rotating a middle vertical propeller(1) and circular wings(2), and rotation of a fuselage is controlled by rotating powerfully and softly. Flying right and left is performed by controlling both inlet ports(4) in front of a horizontal propeller and flying up and down is performed by moving an outlet port(3) up and down. The flying angle is controlled quickly and smoothly by using a fuselage-directional apparatus installed on the outlet port. The inside of the fuselage comprises the first floor(5) and the second floor(6). The middle propeller and horizontal propeller can be those of a jet engine. Air resistance of the flying saucer is low, the speed is fast, and the noise is low. Moreover, a runway is not required because vertical taking off and landing is performed. | ||||||
| 63 | UNMANNED AERIAL VEHICLE HAVING DUCT STRUCTURE | EP18161233.4 | 2018-03-12 | EP3375711A1 | 2018-09-19 | Baek, Sangin; Kang, Jaeho; Baek, Seungchul; Kim, Jongkeun; Yoon, Yeonggyu; Choi, Wonhee; Kim, Hyungil; Hwang, Seunghyun; Yoo, Minwoo; Yoon, Byounguk; Choi, Jongchul |
An unmanned aerial vehicle (100) is disclosed. The unmanned aerial vehicle includes a frame (105) configured to fix a motor (172). The unmanned aerial vehicle also includes a housing (101) configured to enclose the frame. The housing includes a top mesh (101a) corresponding to an upper surface of the housing and a bottom mesh (101b) that covers a portion of a bottom surface of the housing. The housing also includes middle part (101c) coupled to the top mesh and the bottom mesh. The housing also includes a plurality of duct areas (102) that penetrate each of the top mesh, the bottom mesh, and the middle part. The motor and a propeller (173) connected to the motor and for rotating are positioned within the duct area.
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| 64 | VERTICAL TAKE-OFF AND LANDING AIRCRAFT | EP15819516.4 | 2015-08-14 | EP3168147A1 | 2017-05-17 | Noroian, Gevorg Serezhaevich |
The invention relates to aviation technology, specifically to vertical take-off and landing aircraft. The vertical take-off and landing aircraft comprises two turbines, the lower of which is of plate-like shape, and the upper is of flat or plate-like shape. Each turbine comprises a reactive power plant. The body of each turbine is mounted on a metallic disc connected to a vertical shaft of the aircraft, and is equipped with vanes. The vanes are mounted such that the position thereof can be changed. The aircraft can comprise intermediate turbines which are mounted between the upper and lower turbine and are flat or plate-like. The reactive power plant of each turbine comprises an air engine and receivers which are connected to a compressor. The body of each turbine is metallic and comprises two rings, one of which is connected to the disc, and also radial struts which are mounted along the perimeter of the turbine body and are connected to the rings and vanes. The vanes are mounted in a single row along the perimeter of the body or are arranged in a single tier. The result is an increase in the reliability and economy of the aircraft, and the possibility of the latter moving vertically, horizontally or at any inclination. |
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| 65 | AIR-THRUST VEHICLE | EP13841102 | 2013-09-19 | EP2900550A4 | 2016-06-22 | MAHAJAN MAHESH DATTATRAY |
| 66 | AIR-THRUST VEHICLE | EP13841102.0 | 2013-09-19 | EP2900550A1 | 2015-08-05 | Mahajan Mahesh Dattatray |
| An air-thrust vehicle (100) includes a base (130) and an inverted saucer shaped body (132) mounted on the base (130). A plurality of sets of apertures (114, 115, 116, 117, 118, 119, 120, 121) is defined at a plurality of pre-determined locations on the base (130) and the saucer shaped body (132). A plurality of air-displacement mechanisms (105) is configured to draw air via pre-determined sets of apertures and force air via other pre-determined sets of apertures for providing lift for forward and backward movement and for providing horizontal pivoting of the vehicle (100) on the base. A plurality of ducts (122) is adapted to operatively connect the air-displacement mechanisms (105) to each aperture of the sets of apertures (114, 115, 116, 117, 118, 119, 120, 121) and an engine (106) is coupled to operate the air-displacement mechanisms (105). | ||||||
| 67 | ELECTRODYNAMIC DISH-SHAPED FLYING GENERATOR | EP13835159.8 | 2013-03-07 | EP2894097A1 | 2015-07-15 | LIANG, Xiqiu |
An electrodynamic dish-shaped power-generating flying machine comprises a body, a power plant, and a control system. The power plant includes a plurality of annular ferromagnetic guide rails for generating magnetic levitation, a plurality of rising force generation vehicles for generating a rising force and a plurality of forward force generation vehicles for generating a forward force. Both wings of the annular ferromagnetic guide rails are provided with induction coils used for power generation and generator assemblies used for power generation. The control system controls the circling of each vehicle along the annular ferromagnetic guide rails to generate the rising force and the forward force for flying of the electrodynamic dish-shaped power-generating flying machine. At the same time, the vehicles circle make magnetic lines that pass through the induction coils change, so that the induction coils can generate an electromotive force for power generation. The generated power can serve as an electrodynamic force for generation of magnetic levitation forces and driving forces between the annular ferromagnetic guide rails and the vehicles, and the recovered power can be stored in a storage battery for standby use. When rotating around the annular ferromagnetic guide rails, each vehicle operates stably and is easy to realize automatic control, and energy can be recovered to regenerate power for flying when the electrodynamic force is adopted for flying and transportation. |
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| 68 | A flying saucer | EP12160197.5 | 2012-03-19 | EP2502826B1 | 2015-01-21 | Madonia, Mauro; Anzilotti, Stefano; Trancossi, Michele; Dumas, Antonio; Giuliani, Ilaria |
| 69 | KREISFLÜGEL - AKTINISCHER FLUIDANTRIEB (AF) | EP08858729.0 | 2008-12-02 | EP2252796A1 | 2010-11-24 | Papageorgiou, Nikolaos |
| Disclosed is an actinic (radial) fluid drive (AF) which can replace any propeller used, e.g. for fans, ventilators, pumps, hydraulic power plants and wind power plants (repeller), watercraft and aircraft (boats, helicopters, etc.) and can also reduce form drag (in tips of rockets, etc.) or wave-making resistance (in bulbous bows of ships, etc.). Said actinic (radial) fluid drive (AF) is at least characterized by: a) a ring wing (11) (annular wing) - like a truncated cone -, the leading edge and trailing edge of which (corresponding to the periphery of the top surface and base of a truncated cone) determine the chord of the ring wing (11) (rectilinear length of the side), said chord forming the angle of inclination (φ) of the ring wing along with the plane of the top surface; and b) an actinic main flow (15), the direction (plane) of which forms the angle of attack (θ) along with the chord on the leading edge of the ring wing (11), said angle of attack (θ) being greater than 0° and smaller than 90°, especially greater than 8°, and the actinic main flow (15) is inclined (thrust is generated) analogous to the angle of attack (θ) (as a result of the Coanda effect). | ||||||
| 70 | DISCOIDAL FLYING CRAFT | EP06849201 | 2006-02-21 | EP1917189A4 | 2010-07-28 | BOJIUC DUMITRU |
| 71 | RADIOMETRIC PROPULSION SYSTEM | EP05810307.8 | 2005-01-31 | EP1728093A2 | 2006-12-06 | KREMEN, Stanley H.; Scandurra, Marco Dr. |
| A highly efficient propulsion system for flying, floating, and ground vehicles that operates in an atmosphere under standard conditions according to radiometric principles. The propulsion system comprises specially fabricated plates that exhibit large linear thrust forces upon application of a temperature gradient across edge surfaces. Several embodiments are presented. The propulsion system has no moving parts, does not use working fluids, and does not burn hydrocarbon fuels. | ||||||
| 72 | THRUST LEVITATION | EP97949538.9 | 1997-11-18 | EP0939726B1 | 2005-05-11 | SMITH, Boyd, E.; VINCENT, Mervin, C. |
| 73 | CIRCULAR VERTICAL TAKE-OFF AND LANDING AIRCRAFT | EP02703709.2 | 2002-02-26 | EP1370460A1 | 2003-12-17 | Walmsley, Eric Ronald |
| A circular VTOL aircraft with a central vertically mounted turboprop engine (14), driving contra-rotating co-axial propellers (24), above a central jet engine, or engines (12), horizontally mounted on a turntable (11) and steerable through 360 degrees. The turboprop provides vertical thrust from propellers compressing air from an upper circular intake (5) downward through a circular funnel-shaped rotor-chamber (6), to a circular vent (10) at the base of the aircraft. The resulting column of compressed air gives lift for VTOL operations and a cushion of air in flight. The horizontally mounted turbine provides acceleration, retro-thrust and directional control for horizontal flight and vectored thrust for VTOL. An alternative engine configuration (Figure 9), replaces the turboprop and propellers with a vertical turbojet or rocket-engine system providing direct vertical thrust via four control vents (12/14), with an optional horizontal vectored thrust vent (15/37). he aircraft. Fuel-tanks are installed around the central engines. The flight-deck is at the top-centre of the craft above the engines, which are detachable for maintenance. | ||||||
| 74 | Lift generating means for aircraft | EP02250423.7 | 2002-01-22 | EP1247737A3 | 2003-01-22 | Sanders, Albert Owen |
The aircraft or flying vessel has a lifting body 1 which includes one (or more) discs 6 of soft iron and silicon. The rim of the disc is encircled by the windings 7 of an induction motor. Application of power to the motor causes the disc 6 to rotate about a central vertical axle 5 and generate a magnetic field which interacts with the Earth's magnetic field to generate lift by magnetic repulsion. |
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| 75 | Lift generating means for aircraft | EP02250423.7 | 2002-01-22 | EP1247737A2 | 2002-10-09 | Sanders, Albert Owen |
The aircraft or flying vessel has a lifting body 1 which includes one (or more) discs 6 of soft iron and silicon. The rim of the disc is encircled by the windings 7 of an induction motor. Application of power to the motor causes the disc 6 to rotate about a central vertical axle 5 and generate a magnetic field which interacts with the Earth's magnetic field to generate lift by magnetic repulsion. |
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| 76 | FLYING SAUCER AND PROCESS OF BUILDING AND OPERATING IT | EP01930345.2 | 2001-02-14 | EP1226071A2 | 2002-07-31 | Nica, Grigore |
| The invention refers to flying saucers as well as the processes of building and operating them, characterised by having an original propulsion system of a new type, respectively two special turbo reactor engines capable of propulsion in any direction (including zig-zag movements), and ensuring by centrifugal motion both the annulment of the earth gravity, a sustentation in the air due to the permanent depressurisation from the upper exterior side and changing at every moment the ways of working of the propulsion system from the combustion under constant pressure to the combustion overfeed by statoreactor or by rocket engine used at movement in the outer space. | ||||||
| 77 | AIRSHIP/SPACECRAFT | EP00953628.5 | 2000-04-11 | EP1175332A2 | 2002-01-30 | Provitola, Anthony I. |
| An airship/spacecraft, which, in a preferred embodiment, uses its lifting gas (64) as fuel for thrusters, which may be of the turbo-type or rocket type, or both, to achieve transition to space flight. The airship aspect has gas retaining structures (61) that can withstand internal and external pressure and can change in volume and shape. The gas retaining structures (61) may be compartmentalized with a folded diaphragm membrane (63) and also configured as pressure vessels. The spacecraft aspect provides control, power, services, and space for missions of the airship/spacecraft. The best mode includes a turbo-rocket thruster in which the turbine compressor is used to intake and compress a gaseous fuel for combustion with a stored oxidizer injected into the compressed gaseous fuel stream. The compressor stage (6) is driven by the turbine stage (7), which is driven by burning gaseous fuel passing across the turbine blades (13). The burned gases are then expanded through an exhaust nozzle and thereby ejected to produce reaction thrust. | ||||||
| 78 | Fluggerät | EP92122020.8 | 1992-12-25 | EP0553490B1 | 1997-04-23 | Bucher, Franz |
| 79 | Flügelrand-Düsen-VSL-Flugzeug | EP91100127.9 | 1991-01-03 | EP0439014A2 | 1991-07-31 | Teinzer, Harald; Teinzer, Bernd |
Es wird ein Flügelrand-Düsen-Flugzeug vorgeschlagen, welches ein Nur-Flügelflugzeug (1) ist. Mittels einer Radialturbine (5,6) wird ein Gas/Luft-Strom (8,9) erzeugt, der über einen Luftkanal (11) den Randdüsen (4) zugeführt wird. Mit den Randdüsen wird der Gas/Luft-Strom so eingestellt, daß das Flugzeug vertikal starten und Landen, aber auch horizontal fliegen kann. |
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| 80 | Senkrecht startender und landender Flugkörper | EP88111582.8 | 1988-07-19 | EP0304614A3 | 1990-04-25 | von Kozierowski, Joachim |
Senkrecht startender und landender und in jede Richtung steuerbarer Fliehkraftring in torusähnlicher Form mit mittiger Aufnahme von Transportkapseln für die Fortbewegung in einem beliebigen Medium, bestehend aus übereinander oder ineinander angeordneten Kreisringschalen, die in einem Abstand konzentrisch um eine Mittelachse rotieren, wobei jede Kreisringschale für sich aus, auf einem Kreisring nebeneinander angeordneten, über Separatorring (4) und Lagerringe miteinander verbundenen, Verdichter- (1) und Turbinenschaufeln (2) besteht. und die ein oder mehrere Energieaggregate haben, die die Kreisringschalen antreiben, so daß das umgebende Medium von den Kreisringschalen aufgenommen, beschleunigt und über Düsen (10) ausgestoßen wird, wobei der Fliehkraftring selbst gegenüber der Mittelachse mittels einer elektronisch gesteuerten Bremsanlage (14) an den gegenläufigen Schalen oder über Düsen oder über eine ausladende Drehmomentstütze drehstabil gehalten wird. |
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