FR1358006A - Swing-hub helicopter blade drag interconnection system with constant velocity transmission - Google Patents

Swing-hub helicopter blade drag interconnection system with constant velocity transmission

Info

Publication number
FR1358006A
FR1358006A FR935632A FR935632A FR1358006A FR 1358006 A FR1358006 A FR 1358006A FR 935632 A FR935632 A FR 935632A FR 935632 A FR935632 A FR 935632A FR 1358006 A FR1358006 A FR 1358006A
Authority
FR
France
Prior art keywords
hub
swing
constant velocity
interconnection system
helicopter blade
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
FR935632A
Other languages
French (fr)
Inventor
Jean Cantinieau
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.)
Sud Aviation Societe Nationale de Constructions Aerdnaettiques
Original Assignee
Sud Aviation Societe Nationale de Constructions Aerdnaettiques
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 Sud Aviation Societe Nationale de Constructions Aerdnaettiques filed Critical Sud Aviation Societe Nationale de Constructions Aerdnaettiques
Priority to FR935632A priority Critical patent/FR1358006A/en
Application granted granted Critical
Publication of FR1358006A publication Critical patent/FR1358006A/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
    • B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/58—Transmitting means, e.g. interrelated with initiating means or means acting on blades
    • B64C27/59—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical
    • B64C27/635—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical specially for controlling lag-lead movements of blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR935632A 1963-05-22 1963-05-22 Swing-hub helicopter blade drag interconnection system with constant velocity transmission Expired FR1358006A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR935632A FR1358006A (en) 1963-05-22 1963-05-22 Swing-hub helicopter blade drag interconnection system with constant velocity transmission

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR935632A FR1358006A (en) 1963-05-22 1963-05-22 Swing-hub helicopter blade drag interconnection system with constant velocity transmission

Publications (1)

Publication Number Publication Date
FR1358006A true FR1358006A (en) 1964-04-10

Family

ID=8804391

Family Applications (1)

Application Number Title Priority Date Filing Date
FR935632A Expired FR1358006A (en) 1963-05-22 1963-05-22 Swing-hub helicopter blade drag interconnection system with constant velocity transmission

Country Status (1)

Country Link
FR (1) FR1358006A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2392875A1 (en) * 1977-03-23 1978-12-29 Messerschmitt Boelkow Blohm ROTOR FOR ROTATING BLADE APPLIANCE
FR2427251A1 (en) * 1978-06-02 1979-12-28 Aerospatiale Helicopter rotor with rigid hub - has each blade mounted via laminated spherical bearings and strut
FR2456034A2 (en) * 1979-05-08 1980-12-05 Aerospatiale Helicopter rotor with rigid hub - has each blade mounted via laminated spherical bearings and strut
WO1988008392A1 (en) * 1987-04-27 1988-11-03 Bernard Baudrous Power-driven rotor for apparatus with rotary sails, such as helicopters

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2392875A1 (en) * 1977-03-23 1978-12-29 Messerschmitt Boelkow Blohm ROTOR FOR ROTATING BLADE APPLIANCE
FR2427251A1 (en) * 1978-06-02 1979-12-28 Aerospatiale Helicopter rotor with rigid hub - has each blade mounted via laminated spherical bearings and strut
FR2456034A2 (en) * 1979-05-08 1980-12-05 Aerospatiale Helicopter rotor with rigid hub - has each blade mounted via laminated spherical bearings and strut
WO1988008392A1 (en) * 1987-04-27 1988-11-03 Bernard Baudrous Power-driven rotor for apparatus with rotary sails, such as helicopters
FR2616411A1 (en) * 1987-04-27 1988-12-16 Roche Kerandraon Oliver MOTORIZED ROTOR FOR A TURNING WHEEL APPARATUS, FOR EXAMPLE: HELICOPTERS

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