WO2011018559A3 - Stabilized safety gyroplane - Google Patents

Stabilized safety gyroplane Download PDF

Info

Publication number
WO2011018559A3
WO2011018559A3 PCT/FR2009/001017 FR2009001017W WO2011018559A3 WO 2011018559 A3 WO2011018559 A3 WO 2011018559A3 FR 2009001017 W FR2009001017 W FR 2009001017W WO 2011018559 A3 WO2011018559 A3 WO 2011018559A3
Authority
WO
WIPO (PCT)
Prior art keywords
ecrt
gyroplane
fluctuating
rotating wing
time
Prior art date
Application number
PCT/FR2009/001017
Other languages
French (fr)
Other versions
WO2011018559A2 (en
Inventor
Claude Annie Perrichon
Francois Giry
Pierre Piccaluga
Jose Buendia
Original Assignee
Claude Annie Perrichon
Francois Giry
Pierre Piccaluga
Jose Buendia
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
Priority claimed from PCT/FR2009/001006 external-priority patent/WO2010103194A2/en
Priority to CN2009801608717A priority Critical patent/CN102811904A/en
Priority to US13/390,276 priority patent/US20120138730A1/en
Priority to EP09740163A priority patent/EP2464566A2/en
Priority to BR112012003387A priority patent/BR112012003387A2/en
Priority to JP2012524256A priority patent/JP2013501675A/en
Application filed by Claude Annie Perrichon, Francois Giry, Pierre Piccaluga, Jose Buendia filed Critical Claude Annie Perrichon
Priority to CA2770944A priority patent/CA2770944A1/en
Priority to RU2012109561/11A priority patent/RU2012109561A/en
Priority to PCT/FR2010/000572 priority patent/WO2011020955A2/en
Priority to EP10765468A priority patent/EP2467298A2/en
Publication of WO2011018559A2 publication Critical patent/WO2011018559A2/en
Publication of WO2011018559A3 publication Critical patent/WO2011018559A3/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/02—Gyroplanes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/02—Gyroplanes
    • B64C27/021—Rotor or rotor head construction
    • B64C27/025—Rotor drives, in particular for taking off; Combination of autorotation rotors and driven rotors

Abstract

The present application takes various known processes and assembles the latter in a particular manner, said application relating to the integration of a double rotating wing which is in turn coupled to a launching engine, which dispenses with a counter-torque propeller, which can be dangerous. The device is arranged such that the time for the natural effect of self-containment is sufficient. A specific compilation introduces novel technologies brought together for the first time with the principle of gyroplane technology, which is the eCRT technology providing additional safety. An aircraft with a rotating wing is assisted by "radio controlled" eCRT performed by eCRT sensors which impede the effects of fluctuating electromagnetic incompatibilities generated by the mechanical parts under stress, thus increasing flight performances, and freeing the available power from stresses, parasites or fluctuating counterforces.
PCT/FR2009/001017 2009-05-25 2009-08-20 Stabilized safety gyroplane WO2011018559A2 (en)

Priority Applications (9)

Application Number Priority Date Filing Date Title
RU2012109561/11A RU2012109561A (en) 2009-08-14 2009-08-20 SAFE AND SUSTAINABLE FAT
US13/390,276 US20120138730A1 (en) 2009-05-25 2009-08-20 Stabilized safety gyroplane
EP09740163A EP2464566A2 (en) 2009-08-14 2009-08-20 Stabilized safety gyroplane
BR112012003387A BR112012003387A2 (en) 2009-08-14 2009-08-20 A process that makes a self-turning and rotary-wing flight device safe and stable.
JP2012524256A JP2013501675A (en) 2009-08-14 2009-08-20 Stabilized and safe gyroplane
CN2009801608717A CN102811904A (en) 2009-08-14 2009-08-20 Stabilized Safety Gyroplane
CA2770944A CA2770944A1 (en) 2009-08-14 2009-08-20 Stabilized safety gyroplane
PCT/FR2010/000572 WO2011020955A2 (en) 2009-08-20 2010-08-16 Variable parameter rotary wing
EP10765468A EP2467298A2 (en) 2009-08-20 2010-08-16 Variable parameter rotary wing

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FRPCT/FR2009/001006 2009-08-14
PCT/FR2009/001006 WO2010103194A2 (en) 2009-03-12 2009-08-14 Mechanical movements adjusted by electromagnetic probe

Publications (2)

Publication Number Publication Date
WO2011018559A2 WO2011018559A2 (en) 2011-02-17
WO2011018559A3 true WO2011018559A3 (en) 2012-08-23

Family

ID=43587046

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2009/001017 WO2011018559A2 (en) 2009-05-25 2009-08-20 Stabilized safety gyroplane

Country Status (8)

Country Link
EP (1) EP2464566A2 (en)
JP (1) JP2013501675A (en)
KR (1) KR20120040713A (en)
CN (1) CN102811904A (en)
BR (1) BR112012003387A2 (en)
CA (1) CA2770944A1 (en)
RU (1) RU2012109561A (en)
WO (1) WO2011018559A2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2015123961A (en) * 2013-12-26 2015-07-06 郁徳 新原 Helicopter of body of rotation type
US9776713B2 (en) 2015-01-21 2017-10-03 Jaime G. Sada-Salinas Off-board gyrocopter take-off systems and associated methods

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1339650A (en) * 1962-08-30 1963-10-11 Device for rotating rotors of rotorcraft such as gyroplanes
CH666664A5 (en) * 1985-10-09 1988-08-15 Hans Berger High speed helicopter fitted with propeller - has clutch to uncouple main rotor at speed of 150 kilometres an hour
EP0378302A2 (en) * 1989-01-09 1990-07-18 Westland Helicopters Limited Helicopters
FR2869754A1 (en) * 2004-04-29 2005-11-04 Francois Giry Sound reproducing method, for use with e.g. television set, involves generating sound by magnetic field that induces variable electric current which mechanically vibrates silica or silica compound structures e.g. molded plaster
EP1724192A1 (en) * 2005-05-04 2006-11-22 Mauro Achille Nostrini Structure and control system of an aircraft equipped with rotors for lift and vertical flight, and with a pusher-propeller for horizontal thrust
WO2007141395A1 (en) * 2006-06-02 2007-12-13 Claude Annie Perrichon Management of active electrons
WO2007147640A1 (en) * 2006-06-23 2007-12-27 Alessandro Quercetti & C. - Fabbrica Giocattoli Formativi - S.P.A. A flying aircraft supported by a birotor having dihedral blades
WO2009019326A1 (en) * 2007-08-08 2009-02-12 Picy Gestion S.A.S. Reducing the boundary layer of aerodynamic effects

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS52135200A (en) * 1976-05-04 1977-11-11 Satoru Nakagome Helicopter autogyro convertible plane
US7967239B2 (en) * 2005-05-31 2011-06-28 Sikorsky Aircraft Corporation Rotor drive and control system for a high speed rotary wing aircraft
CN101244762A (en) * 2008-03-21 2008-08-20 周公平 Power-driven system of aerial vehicle

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1339650A (en) * 1962-08-30 1963-10-11 Device for rotating rotors of rotorcraft such as gyroplanes
CH666664A5 (en) * 1985-10-09 1988-08-15 Hans Berger High speed helicopter fitted with propeller - has clutch to uncouple main rotor at speed of 150 kilometres an hour
EP0378302A2 (en) * 1989-01-09 1990-07-18 Westland Helicopters Limited Helicopters
FR2869754A1 (en) * 2004-04-29 2005-11-04 Francois Giry Sound reproducing method, for use with e.g. television set, involves generating sound by magnetic field that induces variable electric current which mechanically vibrates silica or silica compound structures e.g. molded plaster
EP1724192A1 (en) * 2005-05-04 2006-11-22 Mauro Achille Nostrini Structure and control system of an aircraft equipped with rotors for lift and vertical flight, and with a pusher-propeller for horizontal thrust
WO2007141395A1 (en) * 2006-06-02 2007-12-13 Claude Annie Perrichon Management of active electrons
WO2007147640A1 (en) * 2006-06-23 2007-12-27 Alessandro Quercetti & C. - Fabbrica Giocattoli Formativi - S.P.A. A flying aircraft supported by a birotor having dihedral blades
WO2009019326A1 (en) * 2007-08-08 2009-02-12 Picy Gestion S.A.S. Reducing the boundary layer of aerodynamic effects

Also Published As

Publication number Publication date
BR112012003387A2 (en) 2016-02-16
JP2013501675A (en) 2013-01-17
CA2770944A1 (en) 2011-02-17
KR20120040713A (en) 2012-04-27
RU2012109561A (en) 2013-09-20
WO2011018559A2 (en) 2011-02-17
CN102811904A (en) 2012-12-05
EP2464566A2 (en) 2012-06-20

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