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FR2660620B1 - Rotor principal d'helicoptere du type spherique. - Google Patents

Rotor principal d'helicoptere du type spherique.

Info

Publication number
FR2660620B1
FR2660620B1 FR9104205A FR9104205A FR2660620B1 FR 2660620 B1 FR2660620 B1 FR 2660620B1 FR 9104205 A FR9104205 A FR 9104205A FR 9104205 A FR9104205 A FR 9104205A FR 2660620 B1 FR2660620 B1 FR 2660620B1
Authority
FR
France
Prior art keywords
helicopter
main rotor
spherical type
spherical
type
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 - Lifetime
Application number
FR9104205A
Other languages
English (en)
Other versions
FR2660620A1 (fr
Inventor
Pancotti Santino
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.)
Agusta SpA
Original Assignee
Agusta SpA
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 Agusta SpA filed Critical Agusta SpA
Publication of FR2660620A1 publication Critical patent/FR2660620A1/fr
Application granted granted Critical
Publication of FR2660620B1 publication Critical patent/FR2660620B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/35Rotors having elastomeric joints
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/37Rotors having articulated joints
    • B64C27/41Rotors having articulated joints with flapping hinge or universal joint, common to the blades
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00Fluid reaction surfaces, i.e. impellers
    • Y10S416/50Vibration damping features

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Support Of The Bearing (AREA)
  • Toys (AREA)
  • Jellies, Jams, And Syrups (AREA)
  • Friction Gearing (AREA)
FR9104205A 1990-04-06 1991-04-05 Rotor principal d'helicoptere du type spherique. Expired - Lifetime FR2660620B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT67262A IT1240177B (it) 1990-04-06 1990-04-06 Rotore principale per elicotteri

Publications (2)

Publication Number Publication Date
FR2660620A1 FR2660620A1 (fr) 1991-10-11
FR2660620B1 true FR2660620B1 (fr) 1993-02-12

Family

ID=11300951

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9104205A Expired - Lifetime FR2660620B1 (fr) 1990-04-06 1991-04-05 Rotor principal d'helicoptere du type spherique.

Country Status (6)

Country Link
US (1) US5165853A (fr)
JP (1) JP2612110B2 (fr)
DE (1) DE4111324C2 (fr)
FR (1) FR2660620B1 (fr)
GB (1) GB2243590B (fr)
IT (1) IT1240177B (fr)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5620305A (en) * 1995-03-20 1997-04-15 The Boeing Company Hub for rotary wing aircraft
US5826822A (en) * 1996-04-19 1998-10-27 Rehm; Rehm N. System and method for providing cyclic and collective pitch control in a rotary wing aircraft
DE19960198A1 (de) * 1999-12-14 2001-06-28 Pfisterer Kontaktsyst Gmbh Mittel zum Festlegen eines Gegenstandes, insbesondere Klemmschraube, Distanzierelement für ein solches Mittel und Schraubverbindungsklemme mit einem solchen Mittel
DE10100872A1 (de) * 2001-01-11 2002-07-18 Ltn Servotechnik Gmbh Vorrichtung zum Drehen eines Körpers um zwei Achsen
FR2837462B1 (fr) 2002-03-20 2004-05-28 Eurocopter France Rotor de giravion a entrainement homocinetique
US7083142B2 (en) * 2004-04-21 2006-08-01 Sikorsky Aircraft Corporation Compact co-axial rotor system for a rotary wing aircraft and a control system thereof
US7097169B2 (en) * 2004-08-04 2006-08-29 Skf Usa Inc. Elastomeric bearing with modified cylindrical core
MX2007015457A (es) * 2005-06-07 2008-02-25 Bell Helicopter Textron Inc Junta de velocidad constante mejorada para ejes de convertiplano.
CA2592947C (fr) * 2005-11-30 2011-10-11 Bell Helicopter Textron Inc. Dispositif de transmission de couple pour aeronef a voilure tournante
BRPI0620973A2 (pt) * 2006-01-13 2011-11-29 Bell Helicopter Textron Inc cubo de rotor inclinável com articulação cardan rìgido no plano de rotação
US8360721B2 (en) * 2008-01-08 2013-01-29 The Boeing Company Low maintenance stiff in plane gimbaled rotor head
EP2274203A4 (fr) * 2008-04-23 2014-10-15 Abe Karem Systèmes de moyeu de rotor et procédés associés
US9555881B2 (en) * 2014-04-02 2017-01-31 The Boeing Company Propeller/rotor control apparatus and method
US9796469B2 (en) * 2014-04-04 2017-10-24 The Boeing Company Modular rotor craft rotor hub system
US11292587B2 (en) 2019-08-13 2022-04-05 Lockheed Martin Corporation Hingeless helicopter rotor with high stiffness and low drag configuration
US12060148B2 (en) 2022-08-16 2024-08-13 Honeywell International Inc. Ground resonance detection and warning system and method

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE653402C (de) * 1933-04-05 1937-11-23 Anton Flettner Steilschrauber
US2216164A (en) * 1936-03-13 1940-10-01 Autogiro Co Of America Rotary-wing aircraft
US2639776A (en) * 1942-05-14 1953-05-26 Autogiro Co Of America Aircraft rotor with tilting hub and damper control of blade swinging
US3087690A (en) * 1961-01-30 1963-04-30 Doman Helicopters Inc Rotor with two joints in drive shaft
US3080002A (en) * 1961-06-29 1963-03-05 Doman Helicopters Inc Rotor with fixed pylon
US3700352A (en) * 1971-03-05 1972-10-24 Lord Corp Rotor system
GB2007176B (en) * 1977-09-07 1982-01-06 Westland Aircraft Ltd Helicopters
US4297078A (en) * 1978-05-17 1981-10-27 Westland Aircraft Limited Helicopter rotors
US4306836A (en) * 1978-05-25 1981-12-22 Kaman Aerospace Corporation Hub assembly
FR2430354A1 (fr) * 1978-07-07 1980-02-01 Aerospatiale Helice multipale a pas variable d'un type simplifie
FR2458457A1 (fr) * 1979-06-05 1981-01-02 Aerospatiale Rotor de giravion a moyeu articule compact
US4323332A (en) * 1979-12-21 1982-04-06 United Technologies Corporation Hingeless helicopter rotor with elastic gimbal hub
DE3006088A1 (de) * 1980-02-19 1981-08-20 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Rotor eines drehfluegelflugzeugs
DE176466T1 (de) * 1984-09-27 1986-09-04 United Technologies Corp., Hartford, Conn. Hubschrauberrotor mit einem fuer alle blaetter gemeinsamen gelenk.
US4566856A (en) * 1984-09-27 1986-01-28 United Technologies Corporation Helicopter gimbal rotor

Also Published As

Publication number Publication date
IT9067262A1 (it) 1991-10-06
FR2660620A1 (fr) 1991-10-11
IT1240177B (it) 1993-11-27
JPH06234396A (ja) 1994-08-23
GB9107159D0 (en) 1991-05-22
US5165853A (en) 1992-11-24
JP2612110B2 (ja) 1997-05-21
DE4111324C2 (de) 2003-01-02
IT9067262A0 (it) 1990-04-06
GB2243590B (en) 1994-01-05
DE4111324A1 (de) 1992-04-02
GB2243590A (en) 1991-11-06

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Legal Events

Date Code Title Description
CL Concession to grant licences
TP Transmission of property