ES2093622T3 - Ranuras de control de la circulacion en un sistema de control de guiñada en un helicoptero. - Google Patents

Ranuras de control de la circulacion en un sistema de control de guiñada en un helicoptero.

Info

Publication number
ES2093622T3
ES2093622T3 ES90111370T ES90111370T ES2093622T3 ES 2093622 T3 ES2093622 T3 ES 2093622T3 ES 90111370 T ES90111370 T ES 90111370T ES 90111370 T ES90111370 T ES 90111370T ES 2093622 T3 ES2093622 T3 ES 2093622T3
Authority
ES
Spain
Prior art keywords
helicopter
wink
control system
slots
circulation
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
ES90111370T
Other languages
English (en)
Inventor
Horn James R Van
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.)
McDonnell Douglas Corp
Original Assignee
McDonnell Douglas Corp
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 McDonnell Douglas Corp filed Critical McDonnell Douglas Corp
Application granted granted Critical
Publication of ES2093622T3 publication Critical patent/ES2093622T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/82Rotorcraft; 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/82Rotorcraft; 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
    • B64C2027/8245Rotorcraft; 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

Abstract

EN UN SISTEMA NOTAR (TM) (NO-TERMINAL-ROTOR) PARA HELICOPTERO, LA ADICION DE GENERADORES VORTICES (20) EN LAS RANURAS LONGITUDINALES O TOBERAS (11) PRODUCE QUE LA PORCION DE CONTROL DE CIRCULACION DEL SISTEMA SE COMBINE CON UN IMPULSOR A CHORRO (17) Y REABASTECIMIENTO DE FLUIDO PARA REEMPLAZAR EL ROTOR TERMINAL.
ES90111370T 1988-05-12 1990-06-15 Ranuras de control de la circulacion en un sistema de control de guiñada en un helicoptero. Expired - Lifetime ES2093622T3 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US07/193,018 US4948068A (en) 1988-05-12 1988-05-12 Circulation control slots in helicopter yaw control system
HK98105342A HK1006164A1 (en) 1988-05-12 1998-06-16 Circulation control slots in helicopter yaw control system

Publications (1)

Publication Number Publication Date
ES2093622T3 true ES2093622T3 (es) 1997-01-01

Family

ID=26316725

Family Applications (1)

Application Number Title Priority Date Filing Date
ES90111370T Expired - Lifetime ES2093622T3 (es) 1988-05-12 1990-06-15 Ranuras de control de la circulacion en un sistema de control de guiñada en un helicoptero.

Country Status (6)

Country Link
US (1) US4948068A (es)
EP (1) EP0461296B1 (es)
AT (1) ATE142156T1 (es)
DE (1) DE69028391T2 (es)
ES (1) ES2093622T3 (es)
HK (1) HK1006164A1 (es)

Families Citing this family (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5232183A (en) * 1991-03-06 1993-08-03 The Boeing Company Helicopter anti-torque control system utilizing exhaust gas
US5205512A (en) * 1991-08-19 1993-04-27 The Boeing Company Fluid control apparatus
US5209430A (en) * 1991-11-07 1993-05-11 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Helicopter low-speed yaw control
US5527155A (en) * 1992-08-21 1996-06-18 Mcdonnell Douglas Corp. Injection molded fan blade
US5649678A (en) * 1994-04-20 1997-07-22 Denel (Proprietary) Limited Operation of a helicopter
US5676335A (en) * 1995-03-08 1997-10-14 Mcdonnell Douglas Helicopter Company Airflow control system for a helicopter
ZA962567B (en) * 1995-07-25 1996-10-07 Denel Pty Ltd Operation of a helicopter
US5791601A (en) * 1995-08-22 1998-08-11 Dancila; D. Stefan Apparatus and method for aerodynamic blowing control using smart materials
US5727757A (en) * 1996-01-17 1998-03-17 Mcdonnell Douglas Helicopter Co. Slotted cam control system
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
US6095428A (en) * 1999-07-07 2000-08-01 Wells; David S. Water-powered aircraft lawn sprinkler
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
EP1799544B1 (en) * 2004-09-28 2016-05-25 Bell Helicopter Textron Inc. Propulsive anti-torque system for rotorcraft
US7032860B1 (en) 2004-11-05 2006-04-25 Eatts, Llc Emergency anti-torque thruster system
US20060097105A1 (en) * 2004-11-11 2006-05-11 Stone C R Propulsion and attitude control systems for aircraft
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
DE102008058029B3 (de) * 2008-11-18 2010-01-07 Deutsches Zentrum für Luft- und Raumfahrt e.V. Hubschrauber
DE102009048778A1 (de) * 2009-10-08 2011-04-14 HERGENRÖDER, Jörn Hubschrauberbasiertes Reinigungsgerät
US8256705B2 (en) * 2009-11-04 2012-09-04 Raytheon Company Torque production vehicle and method
US8196855B2 (en) * 2009-11-23 2012-06-12 Balkus Jr Carl E Helicopter auxiliary anti-torque system
DE102010032217A1 (de) * 2010-07-26 2012-01-26 Siemens Aktiengesellschaft Drehmomentenausgleich für einen Helikopter
GB201012675D0 (en) * 2010-07-29 2010-09-15 Rolls Royce Plc Aerospace vehicle yaw generating tail section
US8960594B2 (en) * 2010-11-02 2015-02-24 Groen Brothers Aviation, Inc. Use of auxiliary rudders for yaw control at low speed
EP2511177B1 (en) * 2011-04-11 2013-06-05 Eurocopter Deutschland GmbH Helicopter with cycloidal rotor system
DE102012100102B4 (de) * 2012-01-06 2015-09-24 Deutsches Zentrum für Luft- und Raumfahrt e.V. Hubschrauberkonfiguration
CN102774496A (zh) * 2012-06-28 2012-11-14 南京航空航天大学 直升机环量控制尾梁的狭缝控制装置
US8991747B2 (en) 2012-12-18 2015-03-31 Blr Aerospace, L.L.C. Aircraft stabilization systems and methods of modifying an aircraft with the same
US8985503B2 (en) * 2013-04-26 2015-03-24 Blr Aerospace, L.L.C. Aircraft stabilization systems and methods of modifying an aircraft with the same
CN104229123A (zh) * 2013-06-24 2014-12-24 孔令全 去直升机尾桨
EP3317180B1 (en) 2015-07-02 2021-09-01 BLR Aerospace, LLC Helicopter with anti-torque system, related kit and methods
US10633086B2 (en) * 2017-03-23 2020-04-28 Bell Helicopter Textron Inc. Rotorcraft anti-torque and directional control using a centrifugal blower
US11718394B2 (en) 2019-04-16 2023-08-08 The Boeing Company Anti-torque and propulsion system for rotorcraft
US11584522B2 (en) * 2020-11-30 2023-02-21 Textron Innovations Inc. Rotorcraft with cooling anti-torque system

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR850918A (fr) * 1938-09-05 1939-12-29 Perfectionnements apportés aux engins de navigation aérienne
GB1183714A (en) * 1966-02-22 1970-03-11 Hawker Siddeley Aviation Ltd Improvements in or relating to Boundary Layer Control Systems.
US4200252A (en) * 1977-12-21 1980-04-29 Summa Corporation Helicopter antitorque system using circulation control

Also Published As

Publication number Publication date
EP0461296B1 (en) 1996-09-04
DE69028391T2 (de) 1997-04-03
EP0461296A1 (en) 1991-12-18
HK1006164A1 (en) 1999-02-12
DE69028391D1 (de) 1996-10-10
US4948068A (en) 1990-08-14
ATE142156T1 (de) 1996-09-15

Similar Documents

Publication Publication Date Title
ES2093622T3 (es) Ranuras de control de la circulacion en un sistema de control de guiñada en un helicoptero.
DE68901357D1 (de) Kombinationstriebwerk, rakete mit luftatmendem turbinenstrahltriebwerk.
IT8922684A0 (it) Controllo di velocita' di elica di aereo
DE59208399D1 (de) Fluggerät
GR3017847T3 (en) Razor head with riblets.
GB8713097D0 (en) Aerofoil/hydrofoil
DE3767324D1 (de) Laserstrahldrucker.
ATE46668T1 (de) Bodeneffekt-fahrzeug.
DE69100339T2 (de) Raketensteuerungsanlage mit seitlichem Gasstrahl.
RU95106376A (ru) Способ и устройство управления вертолетом
GB2226088B (en) Aircraft propulsion system.
EP0617348A3 (en) Control system for the propulsion of an aircraft.
FI871080A (fi) 1,1-disubstituerade cyklopropanderivat, foerfarande foer deras framstaellning samt deras anvaendning som antimykotiska medel eller mellanprodukter.
IT8423422A0 (it) Sistema di impostazione per aeromobili guidati, volanti a velocita' supersonica.
GB2188886B (en) Thrust deflectors for turbomachine propulsion nozzles
DE3750161T2 (de) Flugsteuerungssystem mit synthetischer geschwindigkeitsstabilisierung.
IT8422828A0 (it) Getto d'aria per testurizzare filati.
DE69300636D1 (de) Doppelrumpfwasserfahrzeug mit aerodynamische auftriebskraft erzeugendem aufbau.
DE69010356T2 (de) Abwerfbares aerodynamisches Ruder.
HU9203341D0 (en) System for transforming wqter energy
FR2688077B1 (fr) Procede de pilotage d'un avion en mode "maintien de vitesse par action sur la gouverne de profondeur".
DE68901756T2 (de) Zweidimensionale strahltriebsduese und deren kontrollsystem.
CA2183279A1 (en) Missile Having Non-Cylindrical Propulsion Section
FR2591187B1 (fr) Perfectionnements aux aeronefs a decollage vertical.
FI895221A0 (fi) Monteringsanordning vid ett foenster, en doerr eller liknande.

Legal Events

Date Code Title Description
FG2A Definitive protection

Ref document number: 461296

Country of ref document: ES