IT1170333B - Dispositivo di controllo del passo delle pale per sistemi a pala rotante per veicoli tipo elicottero - Google Patents

Dispositivo di controllo del passo delle pale per sistemi a pala rotante per veicoli tipo elicottero

Info

Publication number
IT1170333B
IT1170333B IT47913/83A IT4791383A IT1170333B IT 1170333 B IT1170333 B IT 1170333B IT 47913/83 A IT47913/83 A IT 47913/83A IT 4791383 A IT4791383 A IT 4791383A IT 1170333 B IT1170333 B IT 1170333B
Authority
IT
Italy
Prior art keywords
control device
pitch control
type vehicles
helicopter type
blades pitch
Prior art date
Application number
IT47913/83A
Other languages
English (en)
Other versions
IT8347913A0 (it
Inventor
Stephan Roman
Original Assignee
Stephan Roman
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 Stephan Roman filed Critical Stephan Roman
Publication of IT8347913A0 publication Critical patent/IT8347913A0/it
Application granted granted Critical
Publication of IT1170333B publication Critical patent/IT1170333B/it

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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/33—Rotors having flexing arms

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Road Repair (AREA)
  • Working-Up Tar And Pitch (AREA)
  • Transmission Devices (AREA)
IT47913/83A 1982-03-19 1983-03-15 Dispositivo di controllo del passo delle pale per sistemi a pala rotante per veicoli tipo elicottero IT1170333B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/360,072 US4502840A (en) 1982-03-19 1982-03-19 Blade pitch control in rotatable bladed devices for vehicles

Publications (2)

Publication Number Publication Date
IT8347913A0 IT8347913A0 (it) 1983-03-15
IT1170333B true IT1170333B (it) 1987-06-03

Family

ID=23416468

Family Applications (1)

Application Number Title Priority Date Filing Date
IT47913/83A IT1170333B (it) 1982-03-19 1983-03-15 Dispositivo di controllo del passo delle pale per sistemi a pala rotante per veicoli tipo elicottero

Country Status (7)

Country Link
US (1) US4502840A (it)
JP (1) JPS58170697A (it)
CA (1) CA1206944A (it)
DE (1) DE3309677A1 (it)
FR (1) FR2523546B1 (it)
GB (1) GB2116928B (it)
IT (1) IT1170333B (it)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4759689A (en) * 1986-01-15 1988-07-26 Stephan Roman Bladed aircraft rotor with flexible blade mountings
US4669958A (en) * 1986-03-31 1987-06-02 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Swashplate control system
JP2998943B2 (ja) * 1991-05-31 2000-01-17 株式会社キーエンス プロペラを用いた玩具におけるプロペラ回転面傾動装置
FR2725688A1 (fr) * 1994-10-13 1996-04-19 Eurocopter France Dispositif de commande de pas des pales d'un rotor de giravion
DE19841855B4 (de) * 1998-09-14 2006-10-26 Zf Luftfahrttechnik Gmbh Einzelblatt-Steuerungsvorrichtung für einen Hubschrauberhauptrotor
FR2923210A1 (fr) * 2007-11-02 2009-05-08 Gaudeffroy Michel Guilhot Plateau cyclique sur rotor.
GB2501145A (en) * 2012-04-12 2013-10-16 Supercell Oy Rendering and modifying objects on a graphical user interface
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
CN111392031B (zh) * 2020-02-24 2022-05-06 深圳联合飞机科技有限公司 一种旋翼变距装置

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB595987A (en) * 1945-07-12 1947-12-24 Fairey Aviat Co Ltd Improvements in or relating to helicopters
DE156921C (it) *
US2439089A (en) * 1944-05-22 1948-04-06 Fairey Aviat Co Ltd Control of rotating wing aircraft
US2677429A (en) * 1947-02-07 1954-05-04 Const Aeronautiques Du Sud Que Stabilizing device for helicopters and the like flying machines
US3199601A (en) * 1962-02-02 1965-08-10 United Aircraft Corp Flight control system
US3144908A (en) * 1962-12-28 1964-08-18 Bell Aerospace Selective second harmonic control
US4111605A (en) * 1976-12-16 1978-09-05 The Boeing Company Composite hingeless rotor hub for rotary wing aircraft
US4227856A (en) * 1978-07-12 1980-10-14 The United States Of Ameria As Represented By The Secretary Of The Navy Reverse velocity rotor system for rotorcraft
US4266912A (en) * 1978-10-06 1981-05-12 Stephan Roman Rotor blade support setup for rotary wing aircraft
DE2932441C2 (de) * 1979-08-10 1983-10-06 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Dämpfungseinrichtung für ein Rotorblatt
US4297080A (en) * 1979-12-17 1981-10-27 United Technologies Corporation Rotor blade pitch control linkage
US4340335A (en) * 1979-12-17 1982-07-20 United Technologies Corporation Helicopter tail rotor with pitch control mechanism

Also Published As

Publication number Publication date
GB2116928B (en) 1985-06-12
DE3309677C2 (it) 1987-01-15
FR2523546A1 (fr) 1983-09-23
IT8347913A0 (it) 1983-03-15
DE3309677A1 (de) 1983-10-06
FR2523546B1 (fr) 1986-09-19
GB2116928A (en) 1983-10-05
US4502840A (en) 1985-03-05
GB8302983D0 (en) 1983-03-09
JPS58170697A (ja) 1983-10-07
CA1206944A (en) 1986-07-02

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