HK1110048A1 - Helicopter with horizontal control - Google Patents

Helicopter with horizontal control

Info

Publication number
HK1110048A1
HK1110048A1 HK08100494A HK08100494A HK1110048A1 HK 1110048 A1 HK1110048 A1 HK 1110048A1 HK 08100494 A HK08100494 A HK 08100494A HK 08100494 A HK08100494 A HK 08100494A HK 1110048 A1 HK1110048 A1 HK 1110048A1
Authority
HK
Hong Kong
Prior art keywords
helicopter
horizontal control
horizontal
control
Prior art date
Application number
HK08100494A
Inventor
Alexander Jozef Magdalena Van De Rostyne
Chi Pok Billy Wai
Original Assignee
Silverlit Toys Manufactory Ltd
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
Priority claimed from US11/462,177 external-priority patent/US20070164148A1/en
Priority claimed from US11/465,781 external-priority patent/US7815482B2/en
Priority claimed from US11/627,919 external-priority patent/US7662013B2/en
Application filed by Silverlit Toys Manufactory Ltd filed Critical Silverlit Toys Manufactory Ltd
Publication of HK1110048A1 publication Critical patent/HK1110048A1/en

Links

Classifications

    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
    • A63H27/00—Toy aircraft; Other flying toys
    • A63H27/12—Helicopters ; Flying tops
    • 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
    • B64C27/605—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical including swash plate, spider or cam mechanisms
    • 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
    • B64C27/625—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical including rotating masses or servo rotors
    • 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
    • B64C27/72—Means acting on blades
    • 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
    • B64C27/78—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement in association with pitch adjustment of blades of anti-torque rotor
    • 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
    • B64C27/80—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement for differential adjustment of blade pitch between two or more lifting rotors

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
HK08100494A 2006-08-03 2008-01-15 Helicopter with horizontal control HK1110048A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US11/462,177 US20070164148A1 (en) 2006-01-19 2006-08-03 Helicopter
US11/465,781 US7815482B2 (en) 2006-01-19 2006-08-18 Helicopter
US11/627,919 US7662013B2 (en) 2006-01-19 2007-01-26 Helicopter with horizontal control

Publications (1)

Publication Number Publication Date
HK1110048A1 true HK1110048A1 (en) 2008-07-04

Family

ID=40429885

Family Applications (2)

Application Number Title Priority Date Filing Date
HK08100494A HK1110048A1 (en) 2006-08-03 2008-01-15 Helicopter with horizontal control
HK08105541.5A HK1116454A1 (en) 2006-08-03 2008-05-20 Helicopter with horizontal control

Family Applications After (1)

Application Number Title Priority Date Filing Date
HK08105541.5A HK1116454A1 (en) 2006-08-03 2008-05-20 Helicopter with horizontal control

Country Status (3)

Country Link
DE (1) DE102007016701B4 (en)
GB (2) GB2442146B (en)
HK (2) HK1110048A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113884268B (en) * 2021-12-08 2022-02-22 中国空气动力研究与发展中心低速空气动力研究所 Longitudinal aerodynamic characteristic test and analysis method for full-dynamic horizontal tail helicopter body

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2633924A (en) 1948-02-26 1953-04-07 Bell Aircraft Corp Helicopter aircraft control
US2549313A (en) * 1948-11-01 1951-04-17 Grant W Johnson Changeable pitch propeller
DE1270408B (en) 1958-09-30 1968-06-12 Bell Helicopter Corp Damping device for the rotor of a helicopter with a semi-rigid blade connection
US3031017A (en) * 1959-09-30 1962-04-24 United Aircraft Corp Cyclic pitch control
GB958536A (en) 1961-10-12 1964-05-21 Kenneth Horatio Wallis Improvements in or relating to rotary winged aircraft
DE1267096B (en) * 1964-05-22 1968-04-25 Boelkow Gmbh Device for the longitudinal stabilization of rotary wing aircraft in high-speed flight
DE1481524A1 (en) * 1967-02-25 1969-07-17 Messerschmitt Boelkow Blohm Stabilization device for fast-flying, relieved rotary wing rotor
US4118143A (en) 1977-03-29 1978-10-03 Franz Kavan Stabilizing and control device for two-bladed helicopter rotors
US4522563A (en) 1982-07-06 1985-06-11 Bell Helicopter Textron, Inc. Elastomeric system for mounting a helicopter rotor
US5255871A (en) 1990-11-29 1993-10-26 Minoru Ikeda Helicopter having rotors equipped with flaps
US5511947A (en) 1995-02-17 1996-04-30 The Boeing Company Cyclic pitch control having torsion spring system
FR2765550B1 (en) * 1997-07-07 1999-10-01 Eurocopter France DEVICE FOR PITCHING THE BLADES OF A MAIN ROTOR OF A GIRAVION
JP3723820B2 (en) * 2005-03-22 2005-12-07 ヒロボー株式会社 Coaxial inversion radio control helicopter

Also Published As

Publication number Publication date
GB0722209D0 (en) 2007-12-19
GB2442146B (en) 2010-11-10
GB0709014D0 (en) 2007-06-20
HK1116454A1 (en) 2008-12-24
GB2442146A (en) 2008-03-26
DE102007016701A1 (en) 2008-02-07
GB2439290B (en) 2008-07-23
GB2439290A (en) 2007-12-27
DE102007016701B4 (en) 2017-03-30

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Legal Events

Date Code Title Description
PC Patent ceased (i.e. patent has lapsed due to the failure to pay the renewal fee)

Effective date: 20200510