IT1111887B - Pala di rotore,specialmente per aeromobili ad ali rotanti - Google Patents

Pala di rotore,specialmente per aeromobili ad ali rotanti

Info

Publication number
IT1111887B
IT1111887B IT7920713A IT2071379A IT1111887B IT 1111887 B IT1111887 B IT 1111887B IT 7920713 A IT7920713 A IT 7920713A IT 2071379 A IT2071379 A IT 2071379A IT 1111887 B IT1111887 B IT 1111887B
Authority
IT
Italy
Prior art keywords
rotating wing
wing aircrafts
shovel
rotor
rotor shovel
Prior art date
Application number
IT7920713A
Other languages
English (en)
Other versions
IT7920713A0 (it
Original Assignee
Messerschmitt Boelkow Blohm
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 Messerschmitt Boelkow Blohm filed Critical Messerschmitt Boelkow Blohm
Publication of IT7920713A0 publication Critical patent/IT7920713A0/it
Application granted granted Critical
Publication of IT1111887B publication Critical patent/IT1111887B/it

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/001—Vibration damping devices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/46—Blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/51—Damping of blade movements

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
IT7920713A 1978-03-10 1979-03-02 Pala di rotore,specialmente per aeromobili ad ali rotanti IT1111887B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19782810334 DE2810334A1 (de) 1978-03-10 1978-03-10 Rotorblatt, insbesondere fuer drehfluegelflugzeuge

Publications (2)

Publication Number Publication Date
IT7920713A0 IT7920713A0 (it) 1979-03-02
IT1111887B true IT1111887B (it) 1986-01-13

Family

ID=6034020

Family Applications (1)

Application Number Title Priority Date Filing Date
IT7920713A IT1111887B (it) 1978-03-10 1979-03-02 Pala di rotore,specialmente per aeromobili ad ali rotanti

Country Status (6)

Country Link
US (1) US4252503A (it)
JP (1) JPS54126398A (it)
DE (1) DE2810334A1 (it)
FR (1) FR2419215A1 (it)
GB (1) GB2015956B (it)
IT (1) IT1111887B (it)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3004451C2 (de) * 1980-02-07 1985-04-04 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Elastomere Dämpfungseinrichtung
DE3401737A1 (de) * 1984-01-19 1985-07-25 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Rotor, insbesondere eines drehfluegelflugzeuges
DE3526470C1 (de) * 1985-07-24 1987-01-02 Messerschmitt Boelkow Blohm Rotor,insbesondere eines Drehfluegelflugzeugs
JP5113734B2 (ja) * 2008-12-19 2013-01-09 川崎重工業株式会社 フレックスビームの断面決定方法およびフレックスビーム
US9150305B2 (en) 2012-02-29 2015-10-06 Sikorsky Aircraft Corporation Vibration absorbing device for flexbeams
EP2653383B1 (en) * 2012-04-18 2016-04-13 AIRBUS HELICOPTERS DEUTSCHLAND GmbH An airfoil blade of a bearingless rotor of a helicopter
US10442531B2 (en) * 2015-08-18 2019-10-15 Sikorsky Aircraft Corporation Rotor damping

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2949967A (en) * 1959-05-25 1960-08-23 Hughes Tool Co Blade-to-hub connector for thrust producing rotor
FR1334446A (fr) * 1961-06-28 1963-08-09 Bolkow Entwicklungen Kg Articulation sans frottement
US3231222A (en) * 1964-05-20 1966-01-25 Scheutzow Helicopter Corp Rotary wing aircraft
US3261407A (en) * 1964-08-05 1966-07-19 Lockheed Aircraft Corp Helicopter rotor system
US3330362A (en) * 1966-05-31 1967-07-11 Lockheed Aircraft Corp Helicopter rotor
FR2041747A1 (it) * 1969-05-20 1971-02-05 Sud Aviation
FR2285298A1 (fr) * 1974-09-19 1976-04-16 Aerospatiale Agencement de rotor de queue pour giravions
US3999886A (en) * 1974-10-10 1976-12-28 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Hingeless helicopter rotor with improved stability
US4037988A (en) * 1974-11-25 1977-07-26 The Boeing Company Flexure having pitch flap coupling
FR2310920A1 (fr) * 1975-05-14 1976-12-10 Aerospatiale Agencement de rotor pour aeronef a voilure tournante
US4008980A (en) * 1975-06-26 1977-02-22 United Technologies Corporation Composite helicopter spar and means to alleviate stress concentration
US4093400A (en) * 1976-12-15 1978-06-06 United Technologies Corporation Cross beam rotor
FR2397325A1 (fr) * 1977-07-13 1979-02-09 Aerospatiale Moyeu de rotor, en particulier pour le rotor principal d'un helicoptere

Also Published As

Publication number Publication date
FR2419215A1 (fr) 1979-10-05
IT7920713A0 (it) 1979-03-02
FR2419215B1 (it) 1984-04-27
JPS54126398A (en) 1979-10-01
GB2015956A (en) 1979-09-19
GB2015956B (en) 1982-07-21
DE2810334A1 (de) 1979-09-13
US4252503A (en) 1981-02-24

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