EA201190276A1 - Способ компенсации гироскопических сил несущего винта вертолета - Google Patents

Способ компенсации гироскопических сил несущего винта вертолета

Info

Publication number
EA201190276A1
EA201190276A1 EA201190276A EA201190276A EA201190276A1 EA 201190276 A1 EA201190276 A1 EA 201190276A1 EA 201190276 A EA201190276 A EA 201190276A EA 201190276 A EA201190276 A EA 201190276A EA 201190276 A1 EA201190276 A1 EA 201190276A1
Authority
EA
Eurasian Patent Office
Prior art keywords
helicopter
rotor
compensation
gyroscopic forces
fuselage
Prior art date
Application number
EA201190276A
Other languages
English (en)
Inventor
Герт Ладинг
Original Assignee
ХЕЛИСКАНДИЯ АпС
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 ХЕЛИСКАНДИЯ АпС filed Critical ХЕЛИСКАНДИЯ АпС
Publication of EA201190276A1 publication Critical patent/EA201190276A1/ru

Links

Classifications

    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Toys (AREA)

Abstract

Предложен способ компенсации гироскопических сил несущего винта вертолета. Для предотвращения возникновения прецессии при наклоне несущего винта (24, 26) вертолета относительно фюзеляжа (31), траекторию наклона дополняют поперечными составляющими. Вертолет снабжен приводным изгибаемым сочленением (34) между несущим винтом и фюзеляжем. Контроллер (2) принимает входной сигнал (4) от рулевого устройства (1) и преобразует его в выходной сигнал (7) для системы (3) исполнительных механизмов для перемещения в сочленении. На основании входного сигнала контроллер выполняет оценку дополнительных входных сигналов и до передачи выходной траектории (11) дополняет ее поперечной составляющей.
EA201190276A 2009-05-07 2010-05-05 Способ компенсации гироскопических сил несущего винта вертолета EA201190276A1 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DKPA200900596 2009-05-07
PCT/DK2010/050098 WO2010127675A2 (en) 2009-05-07 2010-05-05 Method for compensation of gyroscopic forces of a rotor in a helicopter

Publications (1)

Publication Number Publication Date
EA201190276A1 true EA201190276A1 (ru) 2012-05-30

Family

ID=43050538

Family Applications (1)

Application Number Title Priority Date Filing Date
EA201190276A EA201190276A1 (ru) 2009-05-07 2010-05-05 Способ компенсации гироскопических сил несущего винта вертолета

Country Status (6)

Country Link
US (1) US8565941B2 (ru)
EP (1) EP2427373A2 (ru)
CN (1) CN102428001A (ru)
BR (1) BRPI1011640A2 (ru)
EA (1) EA201190276A1 (ru)
WO (1) WO2010127675A2 (ru)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10065732B2 (en) * 2012-08-21 2018-09-04 Technology For Energy Corporation Systems and methods of tracking rotor blades
US9452829B2 (en) * 2013-10-08 2016-09-27 Sikorsky Aircraft Corporation Yaw control of co-axial rotor
US10259575B2 (en) 2014-09-25 2019-04-16 Sikorsky Aircraft Corporation Feed-forward compensation for gyroscopic loads in a coaxial rotor
CN110719874B (zh) * 2017-06-01 2023-07-04 罗马里斯公司 带有同步传感器网络的无人驾驶飞机
CN112363542B (zh) * 2020-11-23 2022-09-27 上海航天测控通信研究所 用于箭载相控阵天线初始相位配平的地面设备

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2418407A (en) * 1943-08-14 1947-04-01 Russell R Hays Control means for helicopters
US3228479A (en) * 1963-05-27 1966-01-11 Bruno A Nagler Rotary wing aircraft
FR1424495A (fr) 1964-12-01 1966-01-14 Aéronef à décollage et atterrissage verticaux
US3489018A (en) * 1967-04-27 1970-01-13 Hughes Aircraft Co Gyro erection system
US3576299A (en) * 1968-05-16 1971-04-27 Thomas F Hanson Direction control system
US3765622A (en) * 1972-01-17 1973-10-16 R Haines Aircraft control means
DE2209733C3 (de) 1972-02-25 1982-11-04 Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt Kollektorlose Drehstromlichtmaschine mit drei stirnseitig innerhalb eines isolierenden Tragringes montierten Gleichrichterphasensätzen
US5507453A (en) * 1993-12-21 1996-04-16 Shapery; Sandor W. Gyro stabilized vectored thrust vertical takeoff or landing aircraft
SE9800231D0 (sv) 1998-01-28 1998-01-28 Avia Adviser Hb Obemannad rotorburen flygfarkost
US6598827B2 (en) * 1998-11-16 2003-07-29 Tom Kusic Telescopic vertical take-off aircraft
US6460802B1 (en) * 2000-09-13 2002-10-08 Airscooter Corporation Helicopter propulsion and control system
GB2375090A (en) 2001-01-17 2002-11-06 David Henry Foote Rotor tilting system, eg for helicopters
AUPS330502A0 (en) * 2002-06-28 2002-07-25 Kusic, Tom Tandem powered power tilting aircraft - june 2002
US20040076518A1 (en) * 2002-10-17 2004-04-22 Drake Devon Glen Tilt stabilized / ballast controlled wind turbine
NO317612B1 (no) * 2003-05-20 2004-11-22 Proxflyer As Rotor som genererer loft og bruk av rotor
US7128293B2 (en) * 2003-12-04 2006-10-31 Reggald Emory Isley Helicopter
JP3595988B1 (ja) 2004-01-27 2004-12-02 快堂 池田 回転ダクト方式シュラウド付回転翼
FR2880866B1 (fr) 2005-01-14 2008-08-22 De Salaberry Bernard Lucien Ch Dispositif d'orientation de la tete de rotor pour helicoptere
AU2008324560B2 (en) * 2007-11-07 2012-08-30 Heliscandia Aps Autonomic rotor system for an aircraft

Also Published As

Publication number Publication date
EP2427373A2 (en) 2012-03-14
CN102428001A (zh) 2012-04-25
WO2010127675A2 (en) 2010-11-11
US20120056031A1 (en) 2012-03-08
BRPI1011640A2 (pt) 2016-03-22
US8565941B2 (en) 2013-10-22
WO2010127675A3 (en) 2011-04-21

Similar Documents

Publication Publication Date Title
EA201190276A1 (ru) Способ компенсации гироскопических сил несущего винта вертолета
WO2009124832A3 (de) Flugzeug mit kraftübertragungselement zwischen einem kabinenstrukturelement und einer primärstruktur
WO2010089072A8 (de) Modellflugkörpersteuer- und empfangseinrichtung
PL2046644T3 (pl) System wyrzucania i lądowania bezzałogowych statków powietrznych
WO2010047484A3 (ko) 클럭 신호가 임베딩된 단일 레벨 신호 전송을 이용한 디스플레이 구동 시스템
EP4534065A3 (en) Systems methods and components for transferring medical fluids
FR2948629B1 (fr) Amortissement variable de restitution haptique pour chaine cinematique de changement d'attitude de vol d'un aeronef
WO2010123636A3 (en) Method and system for controlling propulsion systems
CN104176251B (zh) 一种用于小型倾转旋翼机的发动机小角度倾转机构
WO2012036426A3 (ko) 두 개의 입력 특성을 이용한 유성 기어 시스템, 이의 기어 모듈 및 이의 제어방법
WO2012063220A3 (en) Aerial unit and method for elevating payloads
WO2013169320A3 (en) Autopilot and methods
WO2013182704A3 (en) Powertrain control system and method
WO2007127723A3 (en) Control of robots from human motion descriptors
EP2735495A3 (en) Control System
MX2009003067A (es) Sistema de control automatico de rumbo para aeronaves y helicopteros de rotor inclinable.
EP3791834A3 (en) Soft exosuit for assistance with human motion
WO2009019863A1 (ja) 絶対変位検出方法及びその方法を用いた絶対変位センサ
BRPI0715266A8 (pt) sistema de transferência de aeronaves sem comando humano e método para transferir uma aeronave
EP2012212A3 (en) Flight control backup mode with separate set of inertial signals
WO2011059815A3 (en) Methods for hybrid velocity control of at least partially resonant actuator systems and systems thereof
GB2489938B (en) A drive train apparatus
WO2007149908A3 (en) Method to control image stabilizer
WO2008154217A3 (en) Systems and methods for controlling limited rotation motor systems
FR2930758B1 (fr) Procede et dispositif pour la correction de la dissymetrie laterale d'un aeronef