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AU6763296A - System for controlling and automatically stabilizing the rotational motion of a rotary wing aircraft - Google Patents

System for controlling and automatically stabilizing the rotational motion of a rotary wing aircraft

Info

Publication number
AU6763296A
AU6763296A AU67632/96A AU6763296A AU6763296A AU 6763296 A AU6763296 A AU 6763296A AU 67632/96 A AU67632/96 A AU 67632/96A AU 6763296 A AU6763296 A AU 6763296A AU 6763296 A AU6763296 A AU 6763296A
Authority
AU
Australia
Prior art keywords
controlling
rotational motion
wing aircraft
rotary wing
automatically stabilizing
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
AU67632/96A
Inventor
Paul E. Arlton
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 AU6763296A publication Critical patent/AU6763296A/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
    • B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
AU67632/96A 1995-07-27 1996-07-26 System for controlling and automatically stabilizing the rotational motion of a rotary wing aircraft Abandoned AU6763296A (en)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US155895P 1995-07-27 1995-07-27
US001558 1995-07-27
US707995P 1995-10-24 1995-10-24
US007079 1995-10-24
PCT/US1996/012322 WO1997005017A1 (en) 1995-07-27 1996-07-26 System for controlling and automatically stabilizing the rotational motion of a rotary wing aircraft

Publications (1)

Publication Number Publication Date
AU6763296A true AU6763296A (en) 1997-02-26

Family

ID=26669193

Family Applications (1)

Application Number Title Priority Date Filing Date
AU67632/96A Abandoned AU6763296A (en) 1995-07-27 1996-07-26 System for controlling and automatically stabilizing the rotational motion of a rotary wing aircraft

Country Status (4)

Country Link
EP (1) EP0869901A4 (en)
JP (1) JPH11510127A (en)
AU (1) AU6763296A (en)
WO (1) WO1997005017A1 (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2562938C1 (en) * 2014-04-29 2015-09-10 Акционерное общество "Московский вертолетный завод им. М.Л. Миля" Single-rotor helicopter and method of its control
WO2016109004A2 (en) * 2014-12-19 2016-07-07 Sikorsky Aircraft Corporation Adjustable scissor link
US11040785B2 (en) * 2018-04-16 2021-06-22 Bell Helicopter Textron Inc. Devices and methods to verify tail rotor cross-head positioning
CN111470033B (en) * 2020-05-14 2023-05-16 芜湖丽勤光电技术有限公司 Small aircraft tail balancing device
CN112594131B (en) * 2020-11-26 2022-04-26 中国船舶重工集团海装风电股份有限公司 Method and system for controlling yaw of wind generating set during crosswind and related components
EP4086171B1 (en) * 2021-05-05 2023-11-22 AIRBUS HELICOPTERS DEUTSCHLAND GmbH A cyclic pitch angle adjustment apparatus
CN113815854B (en) * 2021-10-29 2024-06-11 湖南韬讯航空科技有限公司 Aircraft rotor system and control method

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2689099A (en) * 1951-09-20 1954-09-14 United Aircraft Corp Triangular stabilizer for rotary wing aircraft
GB751837A (en) * 1954-02-01 1956-07-04 Carlo Lualdi Gyroscopic device for stabilizing the rotors of helicopters
US3027948A (en) * 1958-01-24 1962-04-03 Kellett Aircraft Corp Stabilization of rotary wing aircraft
US3004736A (en) 1959-10-06 1961-10-17 Lockheed Aircraft Corp Tail rotor for helicopter
US3211235A (en) * 1964-02-17 1965-10-12 Enstrom Corp Control system for yaw control rotors of helicopters
US3528633A (en) * 1967-11-14 1970-09-15 Siegfried Knemeyer System for controlling and stabilizing an aircraft in yaw
JPS582706B2 (en) * 1977-09-06 1983-01-18 マブチモ−タ−株式会社 helicopter model equipment
US4759514A (en) 1986-09-30 1988-07-26 The Boeing Company Tail rotor yaw position control for a helicopter
US5609312A (en) 1991-09-30 1997-03-11 Arlton; Paul E. Model helicopter
US5628620A (en) 1991-09-30 1997-05-13 Arlton; Paul E. Main rotor system for helicopters
US5597138A (en) 1991-09-30 1997-01-28 Arlton; Paul E. Yaw control and stabilization system for helicopters
US5305968A (en) 1991-09-30 1994-04-26 Arlton Paul E Device for automatically stabilizing the yaw motion of a helicopter

Also Published As

Publication number Publication date
EP0869901A1 (en) 1998-10-14
JPH11510127A (en) 1999-09-07
WO1997005017A1 (en) 1997-02-13
EP0869901A4 (en) 2000-10-04

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