IT1142357B - Apparecchiatura per la trattenuta di pale in una testa di rotore di aeroplani ad ala rotante - Google Patents

Apparecchiatura per la trattenuta di pale in una testa di rotore di aeroplani ad ala rotante

Info

Publication number
IT1142357B
IT1142357B IT48066/81A IT4806681A IT1142357B IT 1142357 B IT1142357 B IT 1142357B IT 48066/81 A IT48066/81 A IT 48066/81A IT 4806681 A IT4806681 A IT 4806681A IT 1142357 B IT1142357 B IT 1142357B
Authority
IT
Italy
Prior art keywords
rotor head
rotating wing
head equipment
wing airplane
airplane rotor
Prior art date
Application number
IT48066/81A
Other languages
English (en)
Other versions
IT8148066A0 (it
Inventor
Robert R Peterson
Original Assignee
Wright Barry Corp
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 Wright Barry Corp filed Critical Wright Barry Corp
Publication of IT8148066A0 publication Critical patent/IT8148066A0/it
Application granted granted Critical
Publication of IT1142357B publication Critical patent/IT1142357B/it

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/35Rotors having elastomeric joints
IT48066/81A 1980-03-24 1981-03-20 Apparecchiatura per la trattenuta di pale in una testa di rotore di aeroplani ad ala rotante IT1142357B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/133,015 US4341499A (en) 1980-03-24 1980-03-24 Blade retention system

Publications (2)

Publication Number Publication Date
IT8148066A0 IT8148066A0 (it) 1981-03-20
IT1142357B true IT1142357B (it) 1986-10-08

Family

ID=22456629

Family Applications (1)

Application Number Title Priority Date Filing Date
IT48066/81A IT1142357B (it) 1980-03-24 1981-03-20 Apparecchiatura per la trattenuta di pale in una testa di rotore di aeroplani ad ala rotante

Country Status (7)

Country Link
US (1) US4341499A (it)
JP (1) JPS56146498A (it)
CA (1) CA1158622A (it)
DE (1) DE3111016A1 (it)
FR (1) FR2478574A1 (it)
GB (1) GB2072114B (it)
IT (1) IT1142357B (it)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT1157122B (it) * 1982-12-06 1987-02-11 Agusta Aeronaut Costr Rotore per elicottero
DE4444256C2 (de) * 1994-12-13 1999-03-04 Gerhard Benker Rotorblattaufbau für einen Hubschrauber
DE19713591C2 (de) * 1997-04-02 2001-01-04 Karl Mayer Rotor für ein Drehflügelflugzeug mit Schlagflügelantrieb
US6860015B2 (en) 2001-10-10 2005-03-01 The Boeing Company Method of forming opposing internally preloaded conical elastomeric bearing assembly
US6889965B2 (en) 2001-10-10 2005-05-10 The Boeing Company Opposing conical preloaded elastomeric bearing assembly
DE202007018524U1 (de) * 2007-07-27 2008-11-06 Mendoza, Adrián C. González de Schlagflügelanordnung
DE102007035760B4 (de) * 2007-07-27 2010-02-04 González de Mendoza, Adrián C. Schlagflügelanordnung
FR2925015B1 (fr) * 2007-12-14 2010-06-04 Eurocopter France Pale de giravion, rotor de giravion muni de ladite pale, et procede de fabrication de cette pale
US9796469B2 (en) * 2014-04-04 2017-10-24 The Boeing Company Modular rotor craft rotor hub system
US10457380B2 (en) * 2017-06-28 2019-10-29 Bell Textron Inc. Articulated rotor systems with pitch independent damping
FR3078315B1 (fr) * 2018-02-28 2022-03-04 Airbus Helicopters Butee lamifiee, rotor muni d'une telle butee et aeronef
US10597150B2 (en) 2018-04-24 2020-03-24 Textron Innovations Inc. Articulated rotor systems with blade-to-blade damping
JP2021049081A (ja) 2019-09-24 2021-04-01 株式会社スクウェア・エニックス ゲームプログラム、コンピュータ装置、及び、ゲームの進行方法
US11105381B2 (en) * 2020-02-04 2021-08-31 Aktiebolaget Skf Rotor assembly bearing with centrifugal clutch mechanism

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2169849A (en) * 1938-01-08 1939-08-15 Autogiro Co Of America Aircraft with rotative sustaining blades
FR934336A (fr) * 1946-09-25 1948-05-19 Const Aeronautiques Du Ct Soc Perfectionnements apportés aux articulations des pales des voilures sustentatrices tournantes et des hélices propulsives d'aéronefs
DE1048155B (de) * 1957-09-02 1958-12-31 Ruhr Storch G M B H Einrichtung zur Daempfung der Schlag- und Schwenkbewegungen eines gelenkig aufgehaengten Drehfluegelblattes
FR1471622A (fr) * 1966-03-17 1967-03-03 Lord Corp Joint d'articulation et son application à un rotor d'hélicoptère
FR1585533A (it) * 1967-10-04 1970-01-23
US3556673A (en) * 1968-10-11 1971-01-19 Bolkow Gmbh Rotor mounting
US3700352A (en) * 1971-03-05 1972-10-24 Lord Corp Rotor system
US3790302A (en) * 1972-10-10 1974-02-05 Textron Inc Tail rotor mounting for coning relief
US3862812A (en) * 1973-07-18 1975-01-28 Lord Corp Rotor blade retention system
DE2643166A1 (de) * 1975-11-03 1977-05-12 United Technologies Corp Elastomeres lager fuer hubschrauberrotor
GB1539200A (en) * 1976-12-08 1979-01-31 Westland Aircraft Ltd Helicopter rotors
US4135856A (en) * 1977-02-03 1979-01-23 Lord Corporation Rotor blade retention system
US4232563A (en) * 1978-03-16 1980-11-11 Barry Wright Corporation Laminated elastomeric end bearings for articulating links

Also Published As

Publication number Publication date
DE3111016A1 (de) 1982-01-28
FR2478574A1 (fr) 1981-09-25
IT8148066A0 (it) 1981-03-20
CA1158622A (en) 1983-12-13
JPS56146498A (en) 1981-11-13
US4341499A (en) 1982-07-27
GB2072114B (en) 1984-02-08
FR2478574B1 (it) 1983-07-22
GB2072114A (en) 1981-09-30
JPS6328839B2 (it) 1988-06-09

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