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
Application number
ES9402265A
Other languages
Spanish (es)
Other versions
ES2119603A1 (en
Inventor
Oz Saiz Manuel Mu
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to ES9402265A priority Critical patent/ES2119603B1/en
Publication of ES2119603A1 publication Critical patent/ES2119603A1/en
Application granted granted Critical
Publication of ES2119603B1 publication Critical patent/ES2119603B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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  • 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).

ES9402265A 1994-11-03 1994-11-03 PROPULSION AND STABILIZATION SYSTEM FOR VERTICAL TAKEOFF AIRCRAFT. Expired - Lifetime ES2119603B1 (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
ES2119603A1 (en) 1998-10-01

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