ES2119603A1 - Propulsion and stabilization system for vertical-take-off aircraft - Google Patents

Propulsion and stabilization system for vertical-take-off aircraft

Info

Publication number
ES2119603A1
ES2119603A1 ES09402265A ES9402265A ES2119603A1 ES 2119603 A1 ES2119603 A1 ES 2119603A1 ES 09402265 A ES09402265 A ES 09402265A ES 9402265 A ES9402265 A ES 9402265A ES 2119603 A1 ES2119603 A1 ES 2119603A1
Authority
ES
Spain
Prior art keywords
aircraft
propulsion
take
vertical
stabilization system
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.)
Granted
Application number
ES09402265A
Other languages
Spanish (es)
Other versions
ES2119603B1 (en
Inventor
Saiz Manuel Munoz
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

Links

Landscapes

  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

System which comprises turboprop engines rotating about axes (shafts) parallel to the transverse axis of the aircraft by means of securing arms, arranged on the centre of gravity of the aircraft, and a large port in the central zone, said engines having four pendular fins in a 90 degree tangential position with respect to one another and arranged in the air stream of the FAN, which fins may be actuated by means of servo controls and gyroscopes.
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 true ES2119603A1 (en) 1998-10-01
ES2119603B1 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)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2288083A1 (en) * 2005-07-20 2007-12-16 Manuel Muñoz Saiz Lifting and propulsion system for aircraft, has stabilizing propellers, turbines or fans on wing tips, nose and tail of aircraft, activated by motor
ES2293818A1 (en) * 2006-02-09 2008-03-16 Manuel Muñoz Saiz Lifting and propulsion system for aircraft, has stabilizing propellers, turbines or fans on wing tips, nose and tail of aircraft, activated by motor

Citations (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

Patent Citations (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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2288083A1 (en) * 2005-07-20 2007-12-16 Manuel Muñoz Saiz Lifting and propulsion system for aircraft, has stabilizing propellers, turbines or fans on wing tips, nose and tail of aircraft, activated by motor
ES2293818A1 (en) * 2006-02-09 2008-03-16 Manuel Muñoz Saiz Lifting and propulsion system for aircraft, has stabilizing propellers, turbines or fans on wing tips, nose and tail of aircraft, activated by motor

Also Published As

Publication number Publication date
ES2119603B1 (en) 1999-05-01

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