FR1411762A - Further development of pitch control gear for helicopter tail rotors - Google Patents

Further development of pitch control gear for helicopter tail rotors

Info

Publication number
FR1411762A
FR1411762A FR983060A FR983060A FR1411762A FR 1411762 A FR1411762 A FR 1411762A FR 983060 A FR983060 A FR 983060A FR 983060 A FR983060 A FR 983060A FR 1411762 A FR1411762 A FR 1411762A
Authority
FR
France
Prior art keywords
further development
control gear
pitch control
helicopter tail
tail rotors
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
FR983060A
Other languages
French (fr)
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 FR983060A priority Critical patent/FR1411762A/en
Application granted granted Critical
Publication of FR1411762A publication Critical patent/FR1411762A/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
    • B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
FR983060A 1964-07-25 1964-07-25 Further development of pitch control gear for helicopter tail rotors Expired FR1411762A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR983060A FR1411762A (en) 1964-07-25 1964-07-25 Further development of pitch control gear for helicopter tail rotors

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR983060A FR1411762A (en) 1964-07-25 1964-07-25 Further development of pitch control gear for helicopter tail rotors

Publications (1)

Publication Number Publication Date
FR1411762A true FR1411762A (en) 1965-09-24

Family

ID=8835392

Family Applications (1)

Application Number Title Priority Date Filing Date
FR983060A Expired FR1411762A (en) 1964-07-25 1964-07-25 Further development of pitch control gear for helicopter tail rotors

Country Status (1)

Country Link
FR (1) FR1411762A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3023328A1 (en) 2014-11-20 2016-05-25 Airbus Helicopters A rotary wing aircraft having a non-ducted tail rotor with at least five blades

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3023328A1 (en) 2014-11-20 2016-05-25 Airbus Helicopters A rotary wing aircraft having a non-ducted tail rotor with at least five blades
FR3028838A1 (en) * 2014-11-20 2016-05-27 Airbus Helicopters AIRCRAFT WITH A ROTATING VESSEL WITH A NON-CARINE REAR ROTOR COMPRISING AT LEAST FIVE PALESTS
US10131425B2 (en) 2014-11-20 2018-11-20 Airbus Helicopters Rotary wing aircraft having a non-ducted tail rotor with at least five blades

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