ATE152062T1 - Anlage zum kontrollieren der höheren oberwellenschwingungen in den rotorblättern eines hubschraubers - Google Patents

Anlage zum kontrollieren der höheren oberwellenschwingungen in den rotorblättern eines hubschraubers

Info

Publication number
ATE152062T1
ATE152062T1 AT93119661T AT93119661T ATE152062T1 AT E152062 T1 ATE152062 T1 AT E152062T1 AT 93119661 T AT93119661 T AT 93119661T AT 93119661 T AT93119661 T AT 93119661T AT E152062 T1 ATE152062 T1 AT E152062T1
Authority
AT
Austria
Prior art keywords
cylinder
hhc
rotor blade
force
higher harmonic
Prior art date
Application number
AT93119661T
Other languages
English (en)
Inventor
Wilmer H Reed Iii
Original Assignee
Dynamic Eng Inc
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 Dynamic Eng Inc filed Critical Dynamic Eng Inc
Application granted granted Critical
Publication of ATE152062T1 publication Critical patent/ATE152062T1/de

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
    • B64C27/56—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated
    • B64C27/57—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated automatic or condition responsive, e.g. responsive to rotor speed, torque or thrust
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/46—Blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/001—Vibration damping devices
    • 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
    • B64C2027/7205—Means acting on blades on each blade individually, e.g. individual blade control [IBC]
    • B64C2027/7261—Means acting on blades on each blade individually, e.g. individual blade control [IBC] with flaps
    • B64C2027/7294—Means acting on blades on each blade individually, e.g. individual blade control [IBC] with flaps actuated mechanically, e.g. by means of linkages
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/30—Wing lift efficiency
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00—Fluid reaction surfaces, i.e. impellers
    • Y10S416/50—Vibration damping features

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Catching Or Destruction (AREA)
  • Vibration Prevention Devices (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Apparatuses For Generation Of Mechanical Vibrations (AREA)
  • Wind Motors (AREA)
AT93119661T 1992-12-11 1993-12-07 Anlage zum kontrollieren der höheren oberwellenschwingungen in den rotorblättern eines hubschraubers ATE152062T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/989,583 US5314308A (en) 1992-12-11 1992-12-11 System for controlling higher harmonic vibrations in helicopter rotor blades

Publications (1)

Publication Number Publication Date
ATE152062T1 true ATE152062T1 (de) 1997-05-15

Family

ID=25535244

Family Applications (1)

Application Number Title Priority Date Filing Date
AT93119661T ATE152062T1 (de) 1992-12-11 1993-12-07 Anlage zum kontrollieren der höheren oberwellenschwingungen in den rotorblättern eines hubschraubers

Country Status (11)

Country Link
US (1) US5314308A (de)
EP (1) EP0601527B1 (de)
JP (1) JPH072187A (de)
KR (1) KR940014085A (de)
CN (1) CN1092727A (de)
AT (1) ATE152062T1 (de)
DE (2) DE69310111T2 (de)
DK (1) DK0601527T3 (de)
ES (1) ES2060576T3 (de)
GR (2) GR940300078T1 (de)
TW (1) TW239107B (de)

Families Citing this family (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19528155C1 (de) * 1995-08-02 1996-06-27 Deutsche Forsch Luft Raumfahrt Verdrehbares Rotorblatt aus faserverstärktem Kunstharz
US5973440A (en) 1997-07-07 1999-10-26 Nitzsche; Fred Structural component having means for actively varying its stiffness to control vibrations
EP0936140A4 (de) * 1997-09-10 2002-07-10 Inst Adv Tech Helicopter Ltd Steuersystem für hubschrauberrotor
FR2770826B1 (fr) * 1997-11-07 2000-01-07 Eurocopter France Pale de rotor a volet orientable
DE10035333B4 (de) * 2000-07-20 2008-08-14 Eads Deutschland Gmbh Rotorblatt mit Steuerklappen
DE10052757A1 (de) * 2000-10-25 2002-05-08 Zf Luftfahrttechnik Gmbh Rotorblatt-Steuerungsvorrichtung
US6493689B2 (en) 2000-12-29 2002-12-10 General Dynamics Advanced Technology Systems, Inc. Neural net controller for noise and vibration reduction
US6671590B1 (en) 2001-04-30 2003-12-30 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method and system for active noise control of tiltrotor aircraft
DE60239338D1 (de) * 2001-08-02 2011-04-14 Bell Helicopter Textron Inc Ausgleichsgewichthalteanordnung für hubschrauberhauptrotorblatt
FR2871435B1 (fr) * 2004-06-10 2006-08-18 Eurocopter France Dispositif d'indication d'un niveau de battement
US8162606B2 (en) 2004-08-30 2012-04-24 Lord Corporation Helicopter hub mounted vibration control and circular force generation systems for canceling vibrations
US7722322B2 (en) 2004-08-30 2010-05-25 Lord Corporation Computer system and program product for controlling vibrations
US8267652B2 (en) 2004-08-30 2012-09-18 Lord Corporation Helicopter hub mounted vibration control and circular force generation systems for canceling vibrations
US8435002B2 (en) 2004-08-30 2013-05-07 Lord Corporation Helicopter vibration control system and rotating assembly rotary forces generators for canceling vibrations
CN101022994B (zh) 2004-08-30 2012-07-04 洛德公司 直升飞机振动控制系统和消除振动的旋转力发生器
US8090482B2 (en) 2007-10-25 2012-01-03 Lord Corporation Distributed active vibration control systems and rotary wing aircraft with suppressed vibrations
DE102005007129B4 (de) * 2005-02-17 2008-07-10 Zf Friedrichshafen Ag Einrichtung zur Steuerung von Rotorblättern eines Hubschraubers
US7648338B1 (en) 2006-09-14 2010-01-19 Sikorsky Aircraft Corporation Dual higher harmonic control (HHC) for a counter-rotating, coaxial rotor system
FR2929253B1 (fr) 2008-03-28 2013-09-13 Sartorius Stedim Biotech Sa Cadre rigide pour conteneur 3d a contenant au moins partiellement deformable
US8985068B2 (en) 2010-07-22 2015-03-24 Robert Bosch Gmbh Systems and methods for avoiding resonances excited by rotating components
KR101752645B1 (ko) 2011-02-04 2017-06-30 로오드 코포레이션 공진 관성형 액추에이터를 구비한 회전익 항공기 진동 제어 시스템
WO2013120103A1 (en) 2012-02-10 2013-08-15 Appareo Systems, Llc Frequency-adaptable structural health and usage monitoring system
US10607424B2 (en) 2012-02-10 2020-03-31 Appareo Systems, Llc Frequency-adaptable structural health and usage monitoring system (HUMS) and method with smart sensors
US9394045B2 (en) 2013-03-15 2016-07-19 Kcf Technologies, Inc. Propeller sound field modification systems and methods
US9816529B2 (en) 2013-03-15 2017-11-14 Kcf Technologies, Inc. Propeller sound field modification systems and methods
JP6469389B2 (ja) * 2014-08-29 2019-02-13 三菱航空機株式会社 航空機の加振システム、及び、航空機
CN104670492B (zh) * 2015-01-23 2016-11-16 南京航空航天大学 一种直升机桨叶嵌入式径向运动摆振阻尼器
IL240316B (en) 2015-08-03 2018-10-31 Technion Res & Dev Foundation Method and system for parametric amplification
EP3168145B1 (de) * 2015-11-10 2020-01-29 Sikorsky Aircraft Corporation Individuelles blattsteuerungssystem mit reduzierter leistung auf einem drehflügler
DE102016213720A1 (de) * 2016-07-26 2018-02-01 Zf Friedrichshafen Ag System zur Datenübermittlung und -verarbeitung zur Regelung eines Rotorblattaktuators
US11299263B2 (en) 2016-12-07 2022-04-12 Textron Innovations Inc. Automatic, active blade tracking and balance system
CN108639335B (zh) * 2018-04-04 2020-06-02 北京航空航天大学 一种面向振动与噪声控制的直升机旋翼副翼的柔性变形系统
CN113955142B (zh) * 2021-10-09 2023-09-05 中国直升机设计研究所 一种旋翼1ω谐波振动实时调整控制方法
CN115056979B (zh) * 2022-07-01 2023-05-23 南京航空航天大学 基于旋翼摆振方向周期型运动的振动主动控制方法及系统

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB219664A (de) * 1923-07-28 1925-10-27 "N.V. Instituut Voor Aero- En Hydro-Dynamiek"
US1785333A (en) * 1926-11-18 1930-12-16 Trey Serge Helicopter
FR855833A (fr) * 1939-06-07 1940-05-21 Dispositif pour la production d'une force résultant de l'écoulement d'un fluide spécialement pour des avions
US2344515A (en) * 1941-01-17 1944-03-21 Henry P Massey Means and method for increasing the magnus effect
GB616163A (en) * 1943-01-19 1949-01-18 Groupement Francais Pour Le Developpement Des Recherches Aeronautiques Means for avoid separation and turbulence in fluids moving with respect to solid surfaces
FR1104006A (fr) * 1952-04-23 1955-11-15 Perfectionnements aux surfaces portantes pour avions
GB1153137A (en) * 1965-08-31 1969-05-21 Hovercraft Dev Ltd Cycloidal Propeller
US3649132A (en) * 1970-03-02 1972-03-14 United Aircraft Corp Vibration control for rotors
US3692259A (en) * 1970-06-26 1972-09-19 Shao Wen Yuan Wing-tip vortices control
US4040578A (en) * 1973-12-17 1977-08-09 Shao Wen Yuan Rotor vortex control
US4236607A (en) * 1979-02-26 1980-12-02 Textron, Inc. Vibration suppression system
US4514143A (en) * 1983-04-28 1985-04-30 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Aircraft rotor blade with passive tuned tab
DE3534169A1 (de) * 1985-09-25 1987-03-26 Wolfgang Loesel Zirkulationsanregung fuer auftriebsprofile zur auftriebserhoehung und widerstandsverminderung
US4655685A (en) * 1985-12-16 1987-04-07 United Technologies Corporation Helicopter main rotor blade having a short span slot near the tip end
US4809553A (en) * 1987-07-16 1989-03-07 Dynamic Engineering Inc. Flutter exciter
US4965879A (en) * 1988-10-13 1990-10-23 United Technologies Corporation X-wing fly-by-wire vehicle management system
US4953098A (en) * 1988-10-13 1990-08-28 United Technologies Corporation Higher harmonic control system for X-Wing aircraft
US5099430A (en) * 1988-10-28 1992-03-24 Joseph Hirsch Method and apparatus for continuously suppressing unwanted rotational phenomena in a rotating body

Also Published As

Publication number Publication date
ES2060576T1 (es) 1994-12-01
KR940014085A (ko) 1994-07-16
EP0601527B1 (de) 1997-04-23
GR940300078T1 (en) 1994-11-30
GR3023986T3 (en) 1997-10-31
DE601527T1 (de) 1995-04-06
EP0601527A1 (de) 1994-06-15
DK0601527T3 (da) 1997-10-27
CN1092727A (zh) 1994-09-28
DE69310111T2 (de) 1997-08-07
DE69310111D1 (de) 1997-05-28
US5314308A (en) 1994-05-24
ES2060576T3 (es) 1997-06-16
JPH072187A (ja) 1995-01-06
TW239107B (de) 1995-01-21

Similar Documents

Publication Publication Date Title
ATE152062T1 (de) Anlage zum kontrollieren der höheren oberwellenschwingungen in den rotorblättern eines hubschraubers
US5903077A (en) Modular vibratory force generator, and method of operating same
US5347884A (en) Method and apparatus for cancellation of rotational unbalance
US5988063A (en) Printing machine with printing groups driven by individual electric motors
US5853144A (en) Helicopter and method for reducing vibration of a helicopter fuselage
KR970704983A (ko) 진동 보상용 장치
CA2028265A1 (en) Propeller blade position controller
WO1997020734A3 (en) Flight control system for jet powered tri-mode aircraft
US4724763A (en) Offset web-fed rotary printing machine
CA2113719A1 (en) Ducted Fan and Pitch Controls for Tail Rotor of Rotary Wing Aircraft
DE68911663T2 (de) Aktives Regelungssystem und Verfahren zur Verminderung von Motorgeräusch und -schwingung.
EP3197771B1 (de) Schwingungsdämpfendes, momenterzeugendes flugzeugbetätigungssystem
EP0776820B1 (de) Propellerantriebseinheit für Flugzeuge
ES2013879A6 (es) Un rotor de cola de helicoptero.
JPH07205897A (ja) シュラウド付回転翼
WO2000027698A1 (en) Rotor hub for rotating wing aircraft
PL124083B1 (en) Apparatus for balancing free moments caused by forces of inertia in an internal combustion engine
EP0025408A3 (de) Schwingungsgenerator mit veränderbarer Wirkrichtung
GB2387157A (en) A rotor pitch control system for a rotating wing aircraft
SU1615056A1 (ru) Способ регулировани т ги судового машущего движител
RU1787726C (ru) Приводной ролик конвейера
Nitzsche Smart-spring actuation for helicopter individual blade control- A frequency-domain analysis
Zhu The action of velocity feedback on active vibration control
SE8501816L (sv) Propelleraggregat med reglerbara blad
JPH05170189A (ja) ヘリコプタ

Legal Events

Date Code Title Description
UEP Publication of translation of european patent specification
REN Ceased due to non-payment of the annual fee