FR2119828A1 - - Google Patents

Info

Publication number
FR2119828A1
FR2119828A1 FR7044937A FR7044937A FR2119828A1 FR 2119828 A1 FR2119828 A1 FR 2119828A1 FR 7044937 A FR7044937 A FR 7044937A FR 7044937 A FR7044937 A FR 7044937A FR 2119828 A1 FR2119828 A1 FR 2119828A1
Authority
FR
France
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.)
Granted
Application number
FR7044937A
Other versions
FR2119828B1 (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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Priority to FR707044937A priority Critical patent/FR2119828B1/fr
Priority to DE2159413A priority patent/DE2159413C3/de
Priority to GB5618371A priority patent/GB1306908A/en
Priority to US00207043A priority patent/US3734644A/en
Publication of FR2119828A1 publication Critical patent/FR2119828A1/fr
Application granted granted Critical
Publication of FR2119828B1 publication Critical patent/FR2119828B1/fr
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
    • B64C27/605—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical including swash plate, spider or cam mechanisms
FR707044937A 1970-12-14 1970-12-14 Expired FR2119828B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR707044937A FR2119828B1 (fr) 1970-12-14 1970-12-14
DE2159413A DE2159413C3 (de) 1970-12-14 1971-11-30 Einrichtung zur zyklischen und kollektiven Blattverstellung eines Drehflügelflugzeugs
GB5618371A GB1306908A (en) 1970-12-14 1971-12-03 Helicopter rotor assembly
US00207043A US3734644A (en) 1970-12-14 1971-12-13 Helicopter rotor pitch control system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR707044937A FR2119828B1 (fr) 1970-12-14 1970-12-14

Publications (2)

Publication Number Publication Date
FR2119828A1 true FR2119828A1 (fr) 1972-08-11
FR2119828B1 FR2119828B1 (fr) 1974-02-15

Family

ID=9065723

Family Applications (1)

Application Number Title Priority Date Filing Date
FR707044937A Expired FR2119828B1 (fr) 1970-12-14 1970-12-14

Country Status (4)

Country Link
US (1) US3734644A (fr)
DE (1) DE2159413C3 (fr)
FR (1) FR2119828B1 (fr)
GB (1) GB1306908A (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4630998A (en) * 1984-05-14 1986-12-23 Aerospatiale Societe Nationale Industrielle Apparatus for control of collective and cyclic pitch of the blades of a rotor
EP0706936A1 (fr) 1994-10-11 1996-04-17 Eurocopter France Perfectionnements aux dispositifs de commande de pas pour rotors sans articulation
EP0718188A1 (fr) 1994-12-22 1996-06-26 Eurocopter France Rotor sans articulation à anneaux intermédiaires de commande de pas
FR2770828A1 (fr) * 1997-11-13 1999-05-14 Eurocopter France Dispositif a plateaux cycliques de commande du pas des pales d'un rotor avec plateau non-tournant articule sur une rotule centrale
FR2770827A1 (fr) * 1997-11-13 1999-05-14 Eurocopter France Dispositif a plateaux cycliques de commande du pas des pales d'un rotor avec plateau non-tournant articule par clavettes sur une rotule centrale

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2525391C3 (de) * 1975-06-06 1986-10-23 Peddinghaus, Rolf, Dipl.-Ing., 5828 Ennepetal Druckmittelbetätigte Schere, Lochstanze o.dgl. Maschine
US4326834A (en) * 1979-06-05 1982-04-27 Stanislaw Ostrowski Helicopter rotor assembly and blade pitch control
DE2925368A1 (de) * 1979-06-22 1981-01-15 Alfred Dipl Ing Vogt Einrichtung zur zyklischen und kollektiven rotorblattverstellung fuer drehfluegelfluggeraete
US4445421A (en) * 1981-11-06 1984-05-01 The Charles Stark Draper Laboratory, Inc. Helicopter swashplate controller
FR2570673B1 (fr) * 1984-09-26 1987-01-09 Aerospatiale Dispositif a plateaux cycliques entraines par lames souples, pour la commande d'un rotor d'helicoptere
US4804315A (en) * 1987-07-30 1989-02-14 United Technologies Corporation Composite helicopter swashplate
US5071319A (en) * 1987-09-30 1991-12-10 The Boeing Company Low maintenance, advanced technology swashplate
FR2768996B1 (fr) * 1997-09-30 1999-12-03 Eurocopter France Dispositif a plateaux cycliques de commande du pas des pales d'un rotor avec entraineur de plateau tournant
FR2771707B1 (fr) * 1997-11-28 2000-02-04 Eurocopter France Dispositif a plateaux cycliques de commande du pas des pales d'un rotor avec patins cylindriques glissant sur colonnes non-tournantes
US10994840B1 (en) 2017-08-16 2021-05-04 United States Of America As Represented By The Secretary Of The Air Force Thrust vectoring control of a cyclorotor
EP3467608B1 (fr) 2017-10-05 2019-12-04 LEONARDO S.p.A. Système d'augmentation de stabilité et de manoeuvrabilité pour un aéronef

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2448073A (en) * 1944-06-27 1948-08-31 Helicopters Inc Mechanism for controlling helicopters with coaxial rotors
US3135335A (en) * 1962-12-31 1964-06-02 Lockheed Aircraft Corp Helicopter rotor system
US3207228A (en) * 1962-10-30 1965-09-21 James F Spielman Helicopter rotors and controls
US3426982A (en) * 1967-02-03 1969-02-11 Ronald L Markwood Vertiplane vtol aircraft

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB632606A (en) * 1945-05-15 1949-11-28 Sperry Gyroscope Co Inc Improvements in or relating to control systems for rotary wing aircraft
US2753004A (en) * 1952-03-15 1956-07-03 Mcculloch Motors Corp Pitch control means for aircraft sustaining rotors
US2861640A (en) * 1956-12-27 1958-11-25 Doman Helicopters Inc Helicopter rotor head combination with mechanism to fly rotor level
US2978038A (en) * 1958-03-11 1961-04-04 Doman Helicopters Inc Swash plate operating mechanism and combination with swash plate
US3134444A (en) * 1961-08-23 1964-05-26 Kaman Aircraft Corp Aircraft rotor-propeller

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2448073A (en) * 1944-06-27 1948-08-31 Helicopters Inc Mechanism for controlling helicopters with coaxial rotors
US3207228A (en) * 1962-10-30 1965-09-21 James F Spielman Helicopter rotors and controls
US3135335A (en) * 1962-12-31 1964-06-02 Lockheed Aircraft Corp Helicopter rotor system
US3426982A (en) * 1967-02-03 1969-02-11 Ronald L Markwood Vertiplane vtol aircraft

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4630998A (en) * 1984-05-14 1986-12-23 Aerospatiale Societe Nationale Industrielle Apparatus for control of collective and cyclic pitch of the blades of a rotor
EP0706936A1 (fr) 1994-10-11 1996-04-17 Eurocopter France Perfectionnements aux dispositifs de commande de pas pour rotors sans articulation
US5562415A (en) * 1994-10-11 1996-10-08 Eurocopter France Pitch-control devices for hingeless rotors
EP0718188A1 (fr) 1994-12-22 1996-06-26 Eurocopter France Rotor sans articulation à anneaux intermédiaires de commande de pas
FR2770828A1 (fr) * 1997-11-13 1999-05-14 Eurocopter France Dispositif a plateaux cycliques de commande du pas des pales d'un rotor avec plateau non-tournant articule sur une rotule centrale
FR2770827A1 (fr) * 1997-11-13 1999-05-14 Eurocopter France Dispositif a plateaux cycliques de commande du pas des pales d'un rotor avec plateau non-tournant articule par clavettes sur une rotule centrale

Also Published As

Publication number Publication date
GB1306908A (en) 1973-02-14
DE2159413B2 (de) 1974-02-07
DE2159413C3 (de) 1974-09-05
US3734644A (en) 1973-05-22
DE2159413A1 (de) 1972-06-29
FR2119828B1 (fr) 1974-02-15

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Legal Events

Date Code Title Description
ST Notification of lapse