ES2112609T3 - Sistema de control de guiñadas y compensador de par para helicopteros. - Google Patents

Sistema de control de guiñadas y compensador de par para helicopteros.

Info

Publication number
ES2112609T3
ES2112609T3 ES95302639T ES95302639T ES2112609T3 ES 2112609 T3 ES2112609 T3 ES 2112609T3 ES 95302639 T ES95302639 T ES 95302639T ES 95302639 T ES95302639 T ES 95302639T ES 2112609 T3 ES2112609 T3 ES 2112609T3
Authority
ES
Spain
Prior art keywords
helicopters
control system
yaw control
torque compensator
pusher
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.)
Expired - Lifetime
Application number
ES95302639T
Other languages
English (en)
Inventor
Alan Nurick
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.)
Denel Pty Ltd
Original Assignee
Denel Pty Ltd
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 Denel Pty Ltd filed Critical Denel Pty Ltd
Application granted granted Critical
Publication of ES2112609T3 publication Critical patent/ES2112609T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • 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
    • B64C2027/8245—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 using air jets

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)

Abstract

EN UN HELICOPTERO (10) QUE TIENE UN ROTOR PRINCIPAL (14), UN LARGUERO DE COLA (16) Y UNA RANURA DE CONTROL DE LA CIRCULACION (30) A LO LARGO DE UN LADO DEL LARGUERO DE COLA (16), Y UN EMPUJADOR (32) QUE SE PUEDE DIRECCIONAR SELECTIVAMENTE A CUALQUIER LADO DE LOS DOS LADOS DEL EXTREMO POSTERIOR DEL LARGUERO DE COLA (16), EL CONTROL DEL ANTIPAR Y DE LA GUIÑADA SE LLEVA A CABO GENERANDO CORRIENTES DE CIRCULACION DEL AIRE INDEPENDIENTES DE PRESIONES DIFERENTES MEDIANTE UNOS ELEMENTOS DE PRESION INDEPENDIENTES Y DIRIGIENDO DICHAS CORRIENTES DE CIRCULACION DEL AIRE A PRESIONES DIFERENTES A UNOS CONDUCTOS DE PASO INDEPENDIENTES (24,26) A LA RANURA DE CONTROL DE LA CIRCULACION (30) Y AL EMPUJADOR (32) RESPECTIVAMENTE.
ES95302639T 1994-04-20 1995-04-20 Sistema de control de guiñadas y compensador de par para helicopteros. Expired - Lifetime ES2112609T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ZA942707 1994-04-20

Publications (1)

Publication Number Publication Date
ES2112609T3 true ES2112609T3 (es) 1998-04-01

Family

ID=25583824

Family Applications (1)

Application Number Title Priority Date Filing Date
ES95302639T Expired - Lifetime ES2112609T3 (es) 1994-04-20 1995-04-20 Sistema de control de guiñadas y compensador de par para helicopteros.

Country Status (8)

Country Link
US (1) US5649678A (es)
EP (1) EP0678448B1 (es)
CN (1) CN1055444C (es)
BR (1) BR9501737A (es)
DE (1) DE69501478T2 (es)
ES (1) ES2112609T3 (es)
RU (1) RU2136543C1 (es)
ZA (1) ZA953216B (es)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ZA962567B (en) * 1995-07-25 1996-10-07 Denel Pty Ltd Operation of a helicopter
JP3051357B2 (ja) * 1997-03-26 2000-06-12 株式会社コミュータヘリコプタ先進技術研究所 主ロータトルク補正装置
DE19835385B4 (de) * 1998-08-05 2007-08-16 Uli Streich Modellhubschrauber
US6352220B1 (en) * 2000-06-02 2002-03-05 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Helicopter tail boom with venting for alleviation and control of tail boom aerodynamic loads and method thereof
US6416015B1 (en) * 2001-05-01 2002-07-09 Franklin D. Carson Anti-torque and yaw-control system for a rotary-wing aircraft
US6755374B1 (en) 2003-01-27 2004-06-29 Franklin D. Carson Anti-Torque and yaw-control system for a rotary-wing aircraft
US7255309B2 (en) * 2004-07-14 2007-08-14 The Boeing Company Vernier active flow control effector
US7032860B1 (en) 2004-11-05 2006-04-25 Eatts, Llc Emergency anti-torque thruster system
US7077358B1 (en) * 2005-01-27 2006-07-18 The United States Of America As Represented By The Secretary Of The Navy Helicopter with torque-correcting thruster device
US20090101753A1 (en) * 2007-10-20 2009-04-23 Shahin Kassai Device for compensation of the Tail rotor in a helicopter
PT2133265E (pt) * 2008-06-10 2010-10-18 Agusta Spa Helicóptero
DE102008058029B3 (de) * 2008-11-18 2010-01-07 Deutsches Zentrum für Luft- und Raumfahrt e.V. Hubschrauber
US8196855B2 (en) * 2009-11-23 2012-06-12 Balkus Jr Carl E Helicopter auxiliary anti-torque system
GB201012675D0 (en) * 2010-07-29 2010-09-15 Rolls Royce Plc Aerospace vehicle yaw generating tail section
BR112013002800A2 (pt) * 2010-09-20 2016-08-02 Bell Helicopter Textron Inc cone de cauda em forma de aerofólio
RU2514010C1 (ru) * 2012-11-29 2014-04-27 Владимир Ильич Юркин Способ компенсации реактивного момента несущего винта
RU2527602C1 (ru) * 2013-02-12 2014-09-10 Андрей Михайлович Матико Способ управления вертолетом и стабилизации реактивного момента без хвостового винта
US8882024B1 (en) * 2013-06-24 2014-11-11 Bell Helicopter Textron Inc. Rotorcraft anti-torque rotor and rudder system
PL3056423T3 (pl) * 2015-02-16 2018-04-30 Airbus Helicopters Deutschland GmbH Statek powietrzny z kadłubem, który wyznacza co najmniej obszar wewnętrzny i obszar mieszczący układ napędowy
US11584522B2 (en) * 2020-11-30 2023-02-21 Textron Innovations Inc. Rotorcraft with cooling anti-torque system

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2518697A (en) * 1944-10-30 1950-08-15 United Aircraft Corp Helicopter with antitorque tail jet
US2918232A (en) * 1956-09-24 1959-12-22 Collins Radio Co Twin shroud aerodyne
US2932468A (en) * 1957-12-06 1960-04-12 Gen Electric Vtol aircraft
US3807662A (en) * 1972-11-13 1974-04-30 Lockheed Aircraft Corp Anti-torque, propulsion, and directional control system
US3990811A (en) * 1975-02-26 1976-11-09 The United States Of America As Represented By The Secretary Of The Navy Circulation controlled rotary wing aircraft and control system therefor
US4200252A (en) * 1977-12-21 1980-04-29 Summa Corporation Helicopter antitorque system using circulation control
US4828203A (en) * 1986-12-16 1989-05-09 Vulcan Aircraft Corporation Vertical/short take-off and landing aircraft
US5067668A (en) * 1988-02-29 1991-11-26 Y&B Investment Corporation Compound helicopter with no tail rotor
US4928907A (en) * 1988-02-29 1990-05-29 Y & B Investment Corporation Compound helicopter with no tail rotor
US4948068A (en) * 1988-05-12 1990-08-14 Mcdonnell Douglas Corporation Circulation control slots in helicopter yaw control system
US5232183A (en) * 1991-03-06 1993-08-03 The Boeing Company Helicopter anti-torque control system utilizing exhaust gas
FR2679199B1 (fr) * 1991-07-16 1997-01-31 Aerospatiale Systeme anticouple pour helicoptere.
US5205512A (en) * 1991-08-19 1993-04-27 The Boeing Company Fluid control apparatus

Also Published As

Publication number Publication date
CN1114623A (zh) 1996-01-10
CN1055444C (zh) 2000-08-16
US5649678A (en) 1997-07-22
RU95106376A (ru) 1996-12-20
RU2136543C1 (ru) 1999-09-10
EP0678448B1 (en) 1998-01-21
DE69501478D1 (de) 1998-02-26
EP0678448A1 (en) 1995-10-25
DE69501478T2 (de) 1998-04-30
ZA953216B (en) 1996-01-03
BR9501737A (pt) 1995-11-14

Similar Documents

Publication Publication Date Title
ES2112609T3 (es) Sistema de control de guiñadas y compensador de par para helicopteros.
ES2093622T3 (es) Ranuras de control de la circulacion en un sistema de control de guiñada en un helicoptero.
ES2048834T3 (es) Metodo para conducir instalaciones de separacion con membranas.
ES2119983T3 (es) Sistema de defensa antiaerea y misil de defensa para un tal sistema.
ES2121306T3 (es) Sistema de impresion automatica por ambas caras de tarjetas en blanco y negro y de color, dando la vuelta a la tarjeta.
ES2122477T3 (es) Procedimiento y dispositivo para la identificacion de averias en un sistema complejo.
ES2143872T3 (es) Unidad de envase.
ES2110517T3 (es) Coordinacion de viraje a baja velocidad para helicoptero.
ES2131245T3 (es) Sistema de iluminacion por guiaondas de luz para formar un dispositivo delgado de iluminacion.
DK95287A (da) Slaamaskine
ES2118010T3 (es) Sistema para el marcado de pliegues y cortes de laminas de un material tal como carton o similar.
ES2088999T3 (es) Misiles supersonicos con pilotado en par mediante espoilers.
ES2191460T3 (es) Pulverizadores y metodo de pulverizacion.
BR9713560A (pt) Isolador ótico.
ES2134854T3 (es) Procedimiento que sirve para cortar el borde de una cinta en una maquina de fabricacion de papel.
ES2187504T3 (es) Vectores no oncovirales, basados en el vmmp, con encapsidacion defectuosa.
ES2152968T3 (es) Valvula para sistema de frenado de vehiculos.
ES2095042T3 (es) Conjunto ligero sellado de paracaidas y arnes.
ES2041895T3 (es) Cilindro estriado para una maquina productora de carton ondulado de una cara.
ES2045822T3 (es) Cable aereo de fibra optica.
AR000719A1 (es) Un metodo para abrir una bolsa y una disposion para llevar a la practica dicho metodo.
ES2084775T3 (es) Maquina aplicadora de adhesivo.
ES2112711B1 (es) Estructura para aviones.
ES2103698T1 (es) Fuelle y pasarela de embarque.
CA2134407A1 (en) Aircraft crosswind control apparatus

Legal Events

Date Code Title Description
FG2A Definitive protection

Ref document number: 678448

Country of ref document: ES