ES2119603B1 - PROPULSION AND STABILIZATION SYSTEM FOR VERTICAL TAKEOFF AIRCRAFT. - Google Patents
PROPULSION AND STABILIZATION SYSTEM FOR VERTICAL TAKEOFF AIRCRAFT.Info
- Publication number
- ES2119603B1 ES2119603B1 ES9402265A ES9402265A ES2119603B1 ES 2119603 B1 ES2119603 B1 ES 2119603B1 ES 9402265 A ES9402265 A ES 9402265A ES 9402265 A ES9402265 A ES 9402265A ES 2119603 B1 ES2119603 B1 ES 2119603B1
- Authority
- ES
- Spain
- Prior art keywords
- propulsion
- stabilization system
- vertical takeoff
- aircraft
- center
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
SISTEMA DE PROPULSION Y ESTABILIZACION PARA AVIONES DE DESPEQUE VERTICAL QUE COMPRENDE UNOS MOTORES TURBOPROPULSORES GIRATORIOS ALREDEDOR DE EJES PARALELOS AL EJE TRANSVERSAL DEL AVION MEDIANTE UNOS BRAZOS DE SUJECCION Y DISPUESTOS SOBRE EL CENTRO DE GRAVEDAD DEL AVION Y DE UN GRAN ORIFICIO EN ZONA CENTRAL, PRESENTANDO DICHOS MOTORES CUATRO ALETAS PENDULARES Y TANGENCIALES A 90 ENTRE SI Y DISPUESTAS EN EL CHORROS DE AIRE DEL FAN, ESTAS ALETAS PUEDEN SER ACTUADAS MEDIANTE UNOS SERVOMANDOS Y UNOS GIROSCOPOS. (FIGURA 1).PROPULSION AND STABILIZATION SYSTEM FOR VERTICAL CLEARING AIRCRAFT INCLUDING SOME TURBO-PROPELLING GEARS AROUND A PARALLEL AXLES TO THE AIRCRAFT AXIS BY SOME ARMS OF GRIP AND AVAILABLE IN THE CENTER OF GRAVE AND ARAVIOS IN THE CENTER OF GRAVIO, ARAZOS ENGINES FOUR PENDULAR AND TANGENTIAL FINS AT 90 BETWEEN THEM AND ARRANGED IN THE FAN AIR JETS, THESE FINS MAY BE OPERATED BY SINGLE SERVO CONTROLS AND GYROSCOPES. (FIGURE 1).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES9402265A ES2119603B1 (en) | 1994-11-03 | 1994-11-03 | PROPULSION AND STABILIZATION SYSTEM FOR VERTICAL TAKEOFF AIRCRAFT. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES9402265A ES2119603B1 (en) | 1994-11-03 | 1994-11-03 | PROPULSION AND STABILIZATION SYSTEM FOR VERTICAL TAKEOFF AIRCRAFT. |
Publications (2)
Publication Number | Publication Date |
---|---|
ES2119603A1 ES2119603A1 (en) | 1998-10-01 |
ES2119603B1 true ES2119603B1 (en) | 1999-05-01 |
Family
ID=8287872
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES9402265A Expired - Lifetime ES2119603B1 (en) | 1994-11-03 | 1994-11-03 | PROPULSION AND STABILIZATION SYSTEM FOR VERTICAL TAKEOFF AIRCRAFT. |
Country Status (1)
Country | Link |
---|---|
ES (1) | ES2119603B1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2293818B1 (en) * | 2006-02-09 | 2009-02-16 | Manuel Muñoz Saiz | SUSTAINER AND PROPULSOR SYSTEM FOR AIRCRAFT AND VERTICAL LANDING AIRCRAFT. |
ES2288083B1 (en) * | 2005-07-20 | 2008-10-16 | Manuel Muñoz Saiz | SUSTAINING PROVISION FOR AIRCRAFT AIRCRAFT AND VERTICAL LANDING. |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2508018A1 (en) * | 1975-02-25 | 1976-09-02 | Messerschmitt Boelkow Blohm | Variable geometry jet engines for stol aircraft - has engines pivoted above main wing and directed at wing flaps |
US4116405A (en) * | 1977-03-28 | 1978-09-26 | Grumman Aerospace Corporation | Airplane |
US4296896A (en) * | 1979-08-27 | 1981-10-27 | Grumman Aerospace Corporation | VTOL Airplane |
ES8500836A1 (en) * | 1984-01-03 | 1984-12-01 | Munoz Saiz Manuel | Improvements in vertical tuna aircraft (Machine-translation by Google Translate, not legally binding) |
ES2008200A6 (en) * | 1987-09-02 | 1989-07-16 | Munoz Saiz Manuel | Lifting arrangement by direct thrust of the engine flow to vertical take-off aircraft |
EP0356601A1 (en) * | 1988-08-30 | 1990-03-07 | AERITALIA - Società Aerospaziale Italiana - p.A. | Improvements in jet-propelled aircraft |
US5131605A (en) * | 1991-06-12 | 1992-07-21 | Grumman Aerospace Corporation | Four engine VTOL aircraft |
-
1994
- 1994-11-03 ES ES9402265A patent/ES2119603B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
ES2119603A1 (en) | 1998-10-01 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
ES2030062T3 (en) | APPARATUS AND METHOD FOR PROVIDING A MULTIPLICITY OF AIR DRAGGED FIBER CURRENTS. | |
SE400903B (en) | DEVICE FOR REMOVING ACID AND HARMFUL GASES, AS SUBSTANT SULFUR DIOXIDE GAS, A WHEAT SULFID GAS OR AN ACID MIST INTO THE AIR | |
NO773719L (en) | PROPULSION NOZZLE FOR AIR OR WATER TRANSPORT Means | |
IT7926822A0 (en) | SEALS FOR THE COOLING AIR OF GAS TURBO ENGINES. | |
ES2125457T3 (en) | MOVABLE DEVICE. | |
IT1118722B (en) | MOTOR VEHICLE ENGINE COOLING AIR FLOW PARTITIALIZER | |
IT8020488A0 (en) | PROCEDURE FOR ACTIVATING AND CONTROLLING THE BY-PASS AIR FLOW IN A SUPERCHARGED INTERNAL ICE ENGINE AND ICE ENGINE FOR THE IMPLEMENTATION OF THE PROCEDURE. | |
IT8721065A0 (en) | PRESSURE REGULATING VALVE CONTROLLER IN AN AIRCRAFT CABIN AIR CONDITIONING SYSTEM. | |
IT8121454A1 (en) | ANTI-VORTICE DEVICE FOR THE COOLING AIR OF A GAS TURBINE | |
ES2119603B1 (en) | PROPULSION AND STABILIZATION SYSTEM FOR VERTICAL TAKEOFF AIRCRAFT. | |
SE9202801D0 (en) | PROCEDURE AND ESTABLISHMENT FOR TREATMENT OF AIR IN THE AREA OF A TRAFFIC DRIVE FOR MOTOR VEHICLES | |
IT1158460B (en) | WORKING DEVICE WITH NATURAL EVAPORATION, PARTICULARLY SUITABLE FOR AIR CONDITIONING OF PASSENGERS OF MOTOR VEHICLES, WHEELWHEELS, AND SIMILAR | |
FR2511339B1 (en) | ADJUSTABLE AIR INTAKE, IN PARTICULAR TWO-DIMENSIONAL DIFFUSER WITH OBLIQUE SHOCK FOR HIGH-POWER AIRCRAFT DRIVE TURBOREACTORS | |
RU2005669C1 (en) | Method of landing aircraft and device for its realization | |
IT8368106A0 (en) | FILTERING DEVICE FOR THE INTAKE AIR OF AIRCRAFT ENGINES IN PARTICULAR HELICOPTERS | |
SE7807499L (en) | HEAT EXCHANGER FOR GAS / AIR OR AIR / AIR | |
AR248364A1 (en) | Apparatus for dressing of blow-molded articles in a strand | |
IT1146223B (en) | IMPROVEMENT IN HELICOPTERS EQUIPPED WITH MEANS FOR THE ABSORPTION OF VIBRATIONS ON THE MAIN ROTOR | |
JPH0414919U (en) | ||
SU875283A1 (en) | Pneumatic anemometer | |
IT1126985B (en) | IMPROVEMENT IN FLUID FLOW REGULATION SYSTEMS, IN PARTICULAR FOR THE PRODUCTION OF AIR AND FUEL MIXTURES | |
SU580414A1 (en) | Device for suction of contaminated air | |
RU96123008A (en) | AIR RESCUE | |
IT7926496A0 (en) | LIGHTING, HEATING, HIGH EFFICIENCY MOTOR FOR REFRIGERATION AND SIMILAR. APPLICATIONS IN LAND, SEA AND AIR ENGINES, AS WELL AS FOR USE OF | |
Golovkin et al. | Optical flow visualization in a hydraulic tunnel |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
EC2A | Search report published |
Date of ref document: 19981001 Kind code of ref document: A1 Effective date: 19981001 |
|
FA2A | Application withdrawn |
Effective date: 19991117 |