AU1646801A - Helicopter with highly stable and highly manoeuvrable pendular piloting system - Google Patents

Helicopter with highly stable and highly manoeuvrable pendular piloting system

Info

Publication number
AU1646801A
AU1646801A AU16468/01A AU1646801A AU1646801A AU 1646801 A AU1646801 A AU 1646801A AU 16468/01 A AU16468/01 A AU 16468/01A AU 1646801 A AU1646801 A AU 1646801A AU 1646801 A AU1646801 A AU 1646801A
Authority
AU
Australia
Prior art keywords
helicopter
highly
pendular
piloting system
manoeuvrable
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.)
Abandoned
Application number
AU16468/01A
Inventor
Bernard De Salaberry
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of AU1646801A publication Critical patent/AU1646801A/en
Abandoned legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/46—Blades
    • B64C27/473—Constructional features
    • B64C27/48—Root attachment to rotor head
    • 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
    • B64C27/04—Helicopters
    • B64C27/08—Helicopters with two or more rotors
    • B64C27/10—Helicopters with two or more rotors arranged coaxially
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/52—Tilting of rotor bodily relative to fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B64U30/24—Coaxial rotors

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Control And Safety Of Cranes (AREA)
  • Solid-Sorbent Or Filter-Aiding Compositions (AREA)
  • Catching Or Destruction (AREA)

Abstract

The invention concerns a helicopter with pendular piloting system and counter-rotating rotors whereof the rotor head (2) can be inclined by 20 degrees relative to the fuselage (1) and is piloted relative to the vertical independently of the movements of said fuselage. Thus, said helicopter has high manoeuvrability and stability enabling its use from steeply sloping grounds or on rolling and pitching mobile platforms such as ship decks. The invention is applicable to helicopters of all sizes, whether manned or unmanned.
AU16468/01A 1999-11-12 2000-11-10 Helicopter with highly stable and highly manoeuvrable pendular piloting system Abandoned AU1646801A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR9914229 1999-11-12
FR9914229A FR2801034B1 (en) 1999-11-12 1999-11-12 HIGH STABILITY AND HIGHLY MANEUVERABLE PENDULAR PILOT HELICOPTER
PCT/FR2000/003135 WO2001034466A1 (en) 1999-11-12 2000-11-10 Helicopter with highly stable and highly manoeuvrable pendular piloting system

Publications (1)

Publication Number Publication Date
AU1646801A true AU1646801A (en) 2001-06-06

Family

ID=9552048

Family Applications (1)

Application Number Title Priority Date Filing Date
AU16468/01A Abandoned AU1646801A (en) 1999-11-12 2000-11-10 Helicopter with highly stable and highly manoeuvrable pendular piloting system

Country Status (6)

Country Link
EP (1) EP1165369B1 (en)
AT (1) ATE316898T1 (en)
AU (1) AU1646801A (en)
DE (1) DE60025844D1 (en)
FR (1) FR2801034B1 (en)
WO (1) WO2001034466A1 (en)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE516367C2 (en) * 2000-10-23 2002-01-08 Unmanned rotor propelled aircraft, controlled by rudders actuated by air flow from rotor, and provided with articulated rotor shaft
GB2375090A (en) * 2001-01-17 2002-11-06 David Henry Foote Rotor tilting system, eg for helicopters
US7241953B2 (en) 2003-04-15 2007-07-10 Cable Components Group, Llc. Support-separators for high performance communications cable with optional hollow tubes for; blown optical fiber, coaxial, and/or twisted pair conductors
FR2860211A1 (en) * 2003-09-30 2005-04-01 Gaudeffroy Michel Char Guilhot Aircraft with multiple contrarotating rotors has automated control coupling mechanism for rotors
CN1305194C (en) * 2004-12-17 2007-03-14 华北电力大学（北京） Power circuit scanning test robot airplane and controlling system
FR2880866B1 (en) * 2005-01-14 2008-08-22 De Salaberry Bernard Lucien Ch ROTOR HEAD ORIENTATION DEVICE FOR HELICOPTER
JP2011502847A (en) 2007-11-07 2011-01-27 ヘリスカンディア アンパーツゼルスカブ Autonomous rotor system for aircraft
ES2339098B1 (en) * 2009-09-23 2011-05-27 Gometrics, S.L. POWER TRANSMISSION SYSTEM FOR COAXIAL AXLES.
WO2013026963A1 (en) * 2011-08-25 2013-02-28 Kokkelink Rene Felix Charles Helicopter rotor system, and helicopter including such a rotor system
FR2980117B1 (en) * 2011-09-16 2014-06-13 Francois Viguier FLYING AND VERTICAL LANDING ENGINE WITH CONTRAROTATIVE ROTOR
CN107117300B (en) * 2017-04-26 2019-04-16 哈尔滨工业大学 Unmanned vehicle based on coaxial more rotor pose adjustments
CN107985582B (en) * 2017-11-30 2020-11-03 哈尔滨工业大学 Mars rotor type unmanned aerial vehicle's coaxial anti-oar double-blade rotor system
WO2019117602A1 (en) * 2017-12-15 2019-06-20 서울대학교산학협력단 Flight vehicle
CN108045576A (en) * 2018-01-15 2018-05-18 缪顺文 Deformable bionical rotor flapping wing fixed-wing one aircraft
NO344927B1 (en) * 2018-10-10 2020-06-29 Vantage Dynamic As An aerial vehicle arrangement
CN112407229A (en) * 2020-10-30 2021-02-26 中国直升机设计研究所 Unmanned helicopter fuselage force transmission structure assembly

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2628683A (en) * 1947-04-01 1953-02-17 Harold H Reuther Rotor means for helicopters and the like
US5791592A (en) 1995-01-18 1998-08-11 Nolan; Herbert M. Helicopter with coaxial counter-rotating dual rotors and no tail rotor

Also Published As

Publication number Publication date
FR2801034A1 (en) 2001-05-18
DE60025844D1 (en) 2006-04-13
EP1165369A1 (en) 2002-01-02
EP1165369B1 (en) 2006-02-01
ATE316898T1 (en) 2006-02-15
WO2001034466A1 (en) 2001-05-17
FR2801034B1 (en) 2001-12-14

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Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase