IT9067262A0 - Rotore principale per elicotteri - Google Patents

Rotore principale per elicotteri

Info

Publication number
IT9067262A0
IT9067262A0 IT67262A IT6726290A IT9067262A0 IT 9067262 A0 IT9067262 A0 IT 9067262A0 IT 67262 A IT67262 A IT 67262A IT 6726290 A IT6726290 A IT 6726290A IT 9067262 A0 IT9067262 A0 IT 9067262A0
Authority
IT
Italy
Prior art keywords
helicopters
main rotor
rotor
main
Prior art date
Application number
IT67262A
Other languages
English (en)
Other versions
IT9067262A1 (it
IT1240177B (it
Inventor
Santino Pancotti
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
Priority to IT67262A priority Critical patent/IT1240177B/it
Publication of IT9067262A0 publication Critical patent/IT9067262A0/it
Priority to US07/681,137 priority patent/US5165853A/en
Priority to JP3154176A priority patent/JP2612110B2/ja
Priority to FR9104205A priority patent/FR2660620B1/fr
Priority to GB9107159A priority patent/GB2243590B/en
Priority to DE4111324A priority patent/DE4111324C2/de
Publication of IT9067262A1 publication Critical patent/IT9067262A1/it
Application granted granted Critical
Publication of IT1240177B publication Critical patent/IT1240177B/it

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)
  • Friction Gearing (AREA)
  • Jellies, Jams, And Syrups (AREA)
IT67262A 1990-04-06 1990-04-06 Rotore principale per elicotteri IT1240177B (it)

Priority Applications (6)

Application Number Priority Date Filing Date Title
IT67262A IT1240177B (it) 1990-04-06 1990-04-06 Rotore principale per elicotteri
US07/681,137 US5165853A (en) 1990-04-06 1991-04-05 Main helicopter rotor
JP3154176A JP2612110B2 (ja) 1990-04-06 1991-04-05 ヘリコプタのメインロータ
FR9104205A FR2660620B1 (fr) 1990-04-06 1991-04-05 Rotor principal d'helicoptere du type spherique.
GB9107159A GB2243590B (en) 1990-04-06 1991-04-05 Main helicopter rotor
DE4111324A DE4111324C2 (de) 1990-04-06 1991-04-08 Hubschrauber-Hauptrotor

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 (3)

Publication Number Publication Date
IT9067262A0 true IT9067262A0 (it) 1990-04-06
IT9067262A1 IT9067262A1 (it) 1991-10-06
IT1240177B IT1240177B (it) 1993-11-27

Family

ID=11300951

Family Applications (1)

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

Country Status (6)

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

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
JP2008542668A (ja) * 2005-06-07 2008-11-27 ベル ヘリコプター テクストロン インコーポレイテッド ティルトロータハブのための改良された等速ジョイント
DE06750638T1 (de) * 2005-11-30 2009-02-26 Bell Helicopter Textron, Inc., Fort Worth Drehmomentkupplung für einen drehflügler
CA2635672C (en) * 2006-01-13 2012-06-12 Bell Helicopter Textron Inc. Stiff-in-plane gimbaled tiltrotor hub
US8360721B2 (en) * 2008-01-08 2013-01-29 The Boeing Company Low maintenance stiff in plane gimbaled rotor head
WO2009132090A1 (en) * 2008-04-23 2009-10-29 Abe Karem Rotor hub systems and methods
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
DE3563833D1 (en) * 1984-09-27 1988-08-25 United Technologies Corp Helicopter gimbal rotor
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
DE4111324A1 (de) 1992-04-02
IT1240177B (it) 1993-11-27
JPH06234396A (ja) 1994-08-23
JP2612110B2 (ja) 1997-05-21
GB2243590B (en) 1994-01-05
GB2243590A (en) 1991-11-06
FR2660620B1 (fr) 1993-02-12
FR2660620A1 (fr) 1991-10-11
GB9107159D0 (en) 1991-05-22
DE4111324C2 (de) 2003-01-02
US5165853A (en) 1992-11-24

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Legal Events

Date Code Title Description
0001 Granted
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19990429