FR1331306A - Individual helicopter - Google Patents

Individual helicopter

Info

Publication number
FR1331306A
FR1331306A FR732663A FR732663A FR1331306A FR 1331306 A FR1331306 A FR 1331306A FR 732663 A FR732663 A FR 732663A FR 732663 A FR732663 A FR 732663A FR 1331306 A FR1331306 A FR 1331306A
Authority
FR
France
Prior art keywords
helicopter
individual
individual helicopter
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
Application number
FR732663A
Other languages
French (fr)
Inventor
Georges Albert Sablier
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 filed Critical
Priority to FR732663A priority Critical patent/FR1331306A/en
Application granted granted Critical
Publication of FR1331306A publication Critical patent/FR1331306A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/02Aircraft not otherwise provided for characterised by special use
    • B64C39/026Aircraft not otherwise provided for characterised by special use for use as personal propulsion unit
FR732663A 1957-02-26 1957-02-26 Individual helicopter Expired FR1331306A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR732663A FR1331306A (en) 1957-02-26 1957-02-26 Individual helicopter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR732663A FR1331306A (en) 1957-02-26 1957-02-26 Individual helicopter

Publications (1)

Publication Number Publication Date
FR1331306A true FR1331306A (en) 1963-07-05

Family

ID=8704171

Family Applications (1)

Application Number Title Priority Date Filing Date
FR732663A Expired FR1331306A (en) 1957-02-26 1957-02-26 Individual helicopter

Country Status (1)

Country Link
FR (1) FR1331306A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2584044A1 (en) * 1985-09-27 1987-01-02 Pauchard Daniel ROTATING WING AIRCRAFT OF SIMPLIFIED AND LIGHTWEIGHT STRUCTURE
WO1994010034A1 (en) * 1992-10-27 1994-05-11 Georgette Durand Rotary wing comprising two coaxial rotors
US6488232B2 (en) * 1998-12-16 2002-12-03 Trek Aerospace, Inc. Single passenger aircraft
EP1396423A1 (en) * 2002-07-26 2004-03-10 C.R.F. Società Consortile per Azioni Vtol aircraft
DE102011082719A1 (en) * 2011-09-14 2013-03-14 Antun Sljivac Ultralight helicopter i.e. one-man helicopter, for transporting persons from traffic jam caused by motor vehicles in heavy traffic, has control unit for controlling position of coaxial rotors and rotor blades and regulating engine power

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2584044A1 (en) * 1985-09-27 1987-01-02 Pauchard Daniel ROTATING WING AIRCRAFT OF SIMPLIFIED AND LIGHTWEIGHT STRUCTURE
WO1987002004A1 (en) * 1985-09-27 1987-04-09 Daniel Pauchard Aircraft with rotary wings
US4787573A (en) * 1985-09-27 1988-11-29 Bernard Solinhac Aircraft with rotary wings
AU587073B2 (en) * 1985-09-27 1989-08-03 Solinhac, Bernard Aircraft with rotary wings
WO1994010034A1 (en) * 1992-10-27 1994-05-11 Georgette Durand Rotary wing comprising two coaxial rotors
US6488232B2 (en) * 1998-12-16 2002-12-03 Trek Aerospace, Inc. Single passenger aircraft
EP1396423A1 (en) * 2002-07-26 2004-03-10 C.R.F. Società Consortile per Azioni Vtol aircraft
US6854686B2 (en) 2002-07-26 2005-02-15 C.R.F. Societa Consortile Per Azioni VTOL aircraft
DE102011082719A1 (en) * 2011-09-14 2013-03-14 Antun Sljivac Ultralight helicopter i.e. one-man helicopter, for transporting persons from traffic jam caused by motor vehicles in heavy traffic, has control unit for controlling position of coaxial rotors and rotor blades and regulating engine power

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