EP0869901A4 - System zur steuerung und zur automatischen stabilisierung der gierbewegung eines drehflügelflugzeuges - Google Patents

System zur steuerung und zur automatischen stabilisierung der gierbewegung eines drehflügelflugzeuges

Info

Publication number
EP0869901A4
EP0869901A4 EP96928019A EP96928019A EP0869901A4 EP 0869901 A4 EP0869901 A4 EP 0869901A4 EP 96928019 A EP96928019 A EP 96928019A EP 96928019 A EP96928019 A EP 96928019A EP 0869901 A4 EP0869901 A4 EP 0869901A4
Authority
EP
European Patent Office
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.)
Ceased
Application number
EP96928019A
Other languages
English (en)
French (fr)
Other versions
EP0869901A1 (de
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.)
ARLTON, PAUL E.
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 EP0869901A1 publication Critical patent/EP0869901A1/de
Publication of EP0869901A4 publication Critical patent/EP0869901A4/de
Ceased 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)
EP96928019A 1995-07-27 1996-07-26 System zur steuerung und zur automatischen stabilisierung der gierbewegung eines drehflügelflugzeuges Ceased EP0869901A4 (de)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US155895P 1995-07-27 1995-07-27
US707995P 1995-10-24 1995-10-24
US7079 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
US1558 1997-12-31

Publications (2)

Publication Number Publication Date
EP0869901A1 EP0869901A1 (de) 1998-10-14
EP0869901A4 true EP0869901A4 (de) 2000-10-04

Family

ID=26669193

Family Applications (1)

Application Number Title Priority Date Filing Date
EP96928019A Ceased EP0869901A4 (de) 1995-07-27 1996-07-26 System zur steuerung und zur automatischen stabilisierung der gierbewegung eines drehflügelflugzeuges

Country Status (4)

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

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2562938C1 (ru) * 2014-04-29 2015-09-10 Акционерное общество "Московский вертолетный завод им. М.Л. Миля" Одновинтовой вертолет и способ управления им
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 (zh) * 2020-05-14 2023-05-16 芜湖丽勤光电技术有限公司 一种小型飞机尾部平衡装置
CN112594131B (zh) * 2020-11-26 2022-04-26 中国船舶重工集团海装风电股份有限公司 一种风力发电机组侧风偏航控制方法、系统及相关组件
EP4089011B1 (de) * 2021-05-05 2025-03-26 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Vorrichtung zur zyklischen neigungswinkeleinstellung
CN113815854B (zh) * 2021-10-29 2024-06-11 湖南韬讯航空科技有限公司 一种飞行器旋翼系统及控制方法

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB751837A (en) * 1954-02-01 1956-07-04 Carlo Lualdi Gyroscopic device for stabilizing the rotors of helicopters
US3004736A (en) * 1959-10-06 1961-10-17 Lockheed Aircraft Corp Tail rotor for helicopter

Family Cites Families (10)

* 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
US3027948A (en) * 1958-01-24 1962-04-03 Kellett Aircraft Corp Stabilization of rotary wing aircraft
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 (ja) * 1977-09-06 1983-01-18 マブチモ−タ−株式会社 ヘリコプタ模型装置
US4759514A (en) 1986-09-30 1988-07-26 The Boeing Company Tail rotor yaw position control for a helicopter
US5597138A (en) 1991-09-30 1997-01-28 Arlton; Paul E. Yaw control and stabilization system for helicopters
US5628620A (en) 1991-09-30 1997-05-13 Arlton; Paul E. Main rotor system for helicopters
US5305968A (en) 1991-09-30 1994-04-26 Arlton Paul E Device for automatically stabilizing the yaw motion of a helicopter
US5609312A (en) 1991-09-30 1997-03-11 Arlton; Paul E. Model helicopter

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB751837A (en) * 1954-02-01 1956-07-04 Carlo Lualdi Gyroscopic device for stabilizing the rotors of helicopters
US3004736A (en) * 1959-10-06 1961-10-17 Lockheed Aircraft Corp Tail rotor for helicopter

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of WO9705017A1 *

Also Published As

Publication number Publication date
AU6763296A (en) 1997-02-26
WO1997005017A1 (en) 1997-02-13
EP0869901A1 (de) 1998-10-14
JPH11510127A (ja) 1999-09-07

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Legal Events

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PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

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Owner name: ARLTON, PAUL E.

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Inventor name: ARLTON, PAUL E.

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Effective date: 20020806

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Effective date: 20051024