FR799420A - Self-propelled device for plane or rotary lift system - Google Patents

Self-propelled device for plane or rotary lift system

Info

Publication number
FR799420A
FR799420A FR799420DA FR799420A FR 799420 A FR799420 A FR 799420A FR 799420D A FR799420D A FR 799420DA FR 799420 A FR799420 A FR 799420A
Authority
FR
France
Prior art keywords
self
plane
lift system
propelled device
rotary lift
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
Other languages
French (fr)
Inventor
Alexandre Rene Tassin De Cesar
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
Application granted granted Critical
Publication of FR799420A publication Critical patent/FR799420A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR799420D 1935-03-12 1935-03-12 Self-propelled device for plane or rotary lift system Expired FR799420A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR799420T 1935-03-12

Publications (1)

Publication Number Publication Date
FR799420A true FR799420A (en) 1936-06-12

Family

ID=9236763

Family Applications (1)

Application Number Title Priority Date Filing Date
FR799420D Expired FR799420A (en) 1935-03-12 1935-03-12 Self-propelled device for plane or rotary lift system

Country Status (1)

Country Link
FR (1) FR799420A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3343768A (en) * 1966-03-14 1967-09-26 Walter R Gartzke Aircraft
DE4017402A1 (en) * 1990-05-30 1991-12-05 Dieter Schlueter Blades of helicopter rotor - are stabilised by stabilising rods connected to swash plate
FR2840267A1 (en) 2002-05-28 2003-12-05 Faurecia Sieges Automobile Vehicle seat comprises seat part and back having lower and upper pivoted parts connected by locking mechanism belonging to bi-stable mechanical device comprising pusher which can push back upper part onto folded down position
FR2969121A1 (en) * 2010-12-16 2012-06-22 Francois Clement Gyroplane rotor launching device, has metal or composite support fixed more or less vertically at end of blades of rotor, where support includes thin portion at front part of support for fixing support on rotor blades

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3343768A (en) * 1966-03-14 1967-09-26 Walter R Gartzke Aircraft
DE4017402A1 (en) * 1990-05-30 1991-12-05 Dieter Schlueter Blades of helicopter rotor - are stabilised by stabilising rods connected to swash plate
FR2840267A1 (en) 2002-05-28 2003-12-05 Faurecia Sieges Automobile Vehicle seat comprises seat part and back having lower and upper pivoted parts connected by locking mechanism belonging to bi-stable mechanical device comprising pusher which can push back upper part onto folded down position
FR2969121A1 (en) * 2010-12-16 2012-06-22 Francois Clement Gyroplane rotor launching device, has metal or composite support fixed more or less vertically at end of blades of rotor, where support includes thin portion at front part of support for fixing support on rotor blades

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