DE2849171C2 - Gegendrehmomenteinrichtung bei einem mechanisch angetriebenen - Google Patents

Gegendrehmomenteinrichtung bei einem mechanisch angetriebenen

Info

Publication number
DE2849171C2
DE2849171C2 DE2849171A DE2849171A DE2849171C2 DE 2849171 C2 DE2849171 C2 DE 2849171C2 DE 2849171 A DE2849171 A DE 2849171A DE 2849171 A DE2849171 A DE 2849171A DE 2849171 C2 DE2849171 C2 DE 2849171C2
Authority
DE
Germany
Prior art keywords
nozzle
counter
fuselage
rotor
torque
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
Application number
DE2849171A
Other languages
German (de)
English (en)
Other versions
DE2849171A1 (de
Inventor
Andrew Hance Rancho Palos Verdes Calif. Logan
Richard Edward Los Angeles Calif. Moore
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.)
Boeing Co
Original Assignee
Hughes Helicopters 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 Hughes Helicopters Inc filed Critical Hughes Helicopters Inc
Publication of DE2849171A1 publication Critical patent/DE2849171A1/de
Application granted granted Critical
Publication of DE2849171C2 publication Critical patent/DE2849171C2/de
Expired 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)
  • Jet Pumps And Other Pumps (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Road Paving Structures (AREA)
  • Toys (AREA)
DE2849171A 1977-12-21 1978-11-13 Gegendrehmomenteinrichtung bei einem mechanisch angetriebenen Expired DE2849171C2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/862,814 US4200252A (en) 1977-12-21 1977-12-21 Helicopter antitorque system using circulation control

Publications (2)

Publication Number Publication Date
DE2849171A1 DE2849171A1 (de) 1979-06-28
DE2849171C2 true DE2849171C2 (de) 1983-10-06

Family

ID=25339435

Family Applications (2)

Application Number Title Priority Date Filing Date
DE2849171A Expired DE2849171C2 (de) 1977-12-21 1978-11-13 Gegendrehmomenteinrichtung bei einem mechanisch angetriebenen
DE19782857901 Pending DE2857901A1 (enExample) 1977-12-21 1978-11-13

Family Applications After (1)

Application Number Title Priority Date Filing Date
DE19782857901 Pending DE2857901A1 (enExample) 1977-12-21 1978-11-13

Country Status (6)

Country Link
US (1) US4200252A (enExample)
JP (1) JPS54100098A (enExample)
DE (2) DE2849171C2 (enExample)
FR (1) FR2412462A1 (enExample)
GB (1) GB2012223B (enExample)
IT (1) IT1101191B (enExample)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE9012671U1 (de) * 1990-09-05 1990-11-08 Dornier Luftfahrt GmbH, 8031 Weßling Drehflügelfluggerät mit Mitteln zur Steuerung um die Fluggerätehochachse
DE4039027A1 (de) * 1989-12-08 1991-06-13 Westland Helicopters Verbundhubschrauber
DE4039028A1 (de) * 1989-12-08 1991-06-13 Westland Helicopters Verbundhubschrauber

Families Citing this family (69)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4632337A (en) * 1981-09-21 1986-12-30 Hughes Helicopters, Inc. Helicopter rotor transmission systems
GB2114229B (en) * 1981-11-03 1984-11-21 Rolls Royce Gas turbine engine infra-red radiation suppressor
US4648568A (en) * 1985-05-28 1987-03-10 Phillips Richard G Emergency anti-torque control system and method for helicopters
US4660785A (en) * 1985-12-16 1987-04-28 Munski Michael S Helicopter antitorque auxiliary propulsion system
US4708305A (en) * 1987-01-30 1987-11-24 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Helicopter anti-torque system using fuselage strakes
US4844385A (en) * 1987-04-03 1989-07-04 Lockheed Corporation Pneumatic aerodynamic control surface
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
GB9114085D0 (en) * 1991-06-29 1997-09-17 Rolls Royce Plc Improvements in or relating to helicopters
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
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
US5908185A (en) * 1995-10-12 1999-06-01 Pawling Corporation Handrail and bumper combination
US5727757A (en) 1996-01-17 1998-03-17 Mcdonnell Douglas Helicopter Co. Slotted cam control system
US6425553B1 (en) * 1999-08-20 2002-07-30 West Virginia University Piezoelectric actuators for circulation controlled rotorcraft
CZ289229B6 (cs) 1999-10-12 2001-12-12 Jan Ing. Csc. Námisňák Vznáąivé těleso
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
US6648269B2 (en) 2001-12-10 2003-11-18 Sikorsky Aircraft Corporation Trim augmentation system for a rotary wing aircraft
US20030201367A1 (en) * 2002-04-24 2003-10-30 Saiz Manuel Munoz Process for the recovery of the energy from the air in pressurised areas of aircraft
US6755374B1 (en) 2003-01-27 2004-06-29 Franklin D. Carson Anti-Torque and yaw-control system for a rotary-wing aircraft
WO2006036147A1 (en) * 2004-09-28 2006-04-06 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
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
FR2897040B1 (fr) * 2006-02-06 2008-04-11 Christian Claude Sellet Dispositif de controle en lacet pour helicopteres.
US7708229B1 (en) 2006-03-22 2010-05-04 West Virginia University Circulation controlled airfoil
USD548803S1 (en) * 2006-04-27 2007-08-14 Nachman Zimet Helicopter
CA118559S (en) 2006-12-06 2007-08-22 Nachman Zimet Toy helicopter
WO2008156533A2 (en) 2007-05-14 2008-12-24 Blr Aerospace L.L.C. Aircraft stabilizer system and methods of using the same
JP2009045976A (ja) * 2007-08-16 2009-03-05 Mitsubishi Heavy Ind Ltd テールブーム
US20090101753A1 (en) * 2007-10-20 2009-04-23 Shahin Kassai Device for compensation of the Tail rotor in a helicopter
FR2923456B1 (fr) * 2007-11-08 2009-12-18 Eurocopter France Aeronef muni d'un rotor carene silencieux
DE102009048778A1 (de) * 2009-10-08 2011-04-14 HERGENRÖDER, Jörn Hubschrauberbasiertes Reinigungsgerät
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
US8931731B2 (en) 2010-11-02 2015-01-13 Groen Brothers Aviation, Inc. Tail jet apparatus and method for low speed yaw control of a rotorcraft
US8844880B1 (en) 2010-09-09 2014-09-30 Groen Brothers Aviation, Inc. Two-place, collective pitch and throttle control
US8991745B1 (en) 2011-08-17 2015-03-31 Groen Brothers Aviation, Inc. Rotor-mast-tilting apparatus and method for lower flapping loads
US8950700B2 (en) 2010-11-02 2015-02-10 Groen Brothers Aviation, Inc. Rotor driven auxiliary power apparatus and method
US8960594B2 (en) 2010-11-02 2015-02-24 Groen Brothers Aviation, Inc. Use of auxiliary rudders for yaw control at low speed
US9139297B1 (en) 2010-09-09 2015-09-22 Groen Brothers Aviation, Inc. Rotor blade subsystems attachment
US8998127B2 (en) 2010-09-09 2015-04-07 Groen Brothers Aviation, Inc. Pre-landing, rotor-spin-up apparatus and method
US9038940B1 (en) 2011-05-16 2015-05-26 Groen Brothers Aviation, Inc. Rotor configuration for reaction drive rotor system
US8944366B2 (en) 2010-09-09 2015-02-03 Groen Brothers Aviation, Inc. Rotorcraft empennage mounting system
US9169009B1 (en) 2010-09-09 2015-10-27 Groen Brothers Aviation, Inc. Hub-mounted auxilliary systems for tipjets in a reaction drive rotor system
US9205913B2 (en) 2010-09-09 2015-12-08 Groen Brothers Aviation, Inc. Rotorcraft, dynamic, CG management apparatus and method
US8991748B1 (en) 2011-04-19 2015-03-31 Groen Brothers Aviation, Inc. Solid lubricated blade pitch control system for use within a compressed airstream of a reaction driven rotorcraft
US8840058B2 (en) 2010-09-20 2014-09-23 Textron Innovations Inc. Airfoil shaped tail boom
WO2012064343A1 (en) * 2010-11-12 2012-05-18 Bell Helicopter Textron Inc. Propulsive anti-torque nozzle system with external rotating sleeve for a rotorcraft
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
CN103507947A (zh) * 2012-06-29 2014-01-15 新昌县冠阳技术开发有限公司 一种旋翼飞行器扭矩自平衡的装置
RU2514010C1 (ru) * 2012-11-29 2014-04-27 Владимир Ильич Юркин Способ компенсации реактивного момента несущего винта
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
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
EP3317180B1 (en) * 2015-07-02 2021-09-01 BLR Aerospace, LLC Helicopter with anti-torque system, related kit and methods
US10556702B2 (en) 2016-07-13 2020-02-11 General Electric Company Aircraft having an airflow duct
EP3272640B1 (en) * 2016-07-21 2019-04-17 AIRBUS HELICOPTERS DEUTSCHLAND GmbH A helicopter with a fuselage and a composite tail boom
US11718394B2 (en) 2019-04-16 2023-08-08 The Boeing Company Anti-torque and propulsion system for rotorcraft
CN113968339B (zh) * 2021-11-19 2023-04-28 中国直升机设计研究所 一种可应急配平直升机旋翼反扭矩的环控系统及控制方法
CN113928554B (zh) * 2021-11-19 2023-04-28 中国直升机设计研究所 一种直升机尾部反扭矩装置及气动设计方法
US20250236386A1 (en) * 2024-01-19 2025-07-24 Pratt & Whitney Canada Corp. Rotorcraft with powerplant exhaust sound attenuation
US20250289567A1 (en) * 2024-03-15 2025-09-18 Pratt & Whitney Canada Corp. Rotorcraft with anti-torque air system and tail rotor(s)

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR883462A (fr) * 1939-01-12 1943-07-06 Hélicoptère
US2486272A (en) * 1943-12-14 1949-10-25 Gazda Antoine Helicopter with antitorque reaction jet
US3020003A (en) * 1955-07-05 1962-02-06 Avro Aircraft Ltd Disc aircraft with gas turbine and ram jet engines
FR1298518A (fr) * 1961-06-02 1962-07-13 Sud Aviation Dispositif de contrôle de l'orientation pour hélicoptère
US3059877A (en) * 1961-08-11 1962-10-23 United Aircraft Corp Helicopter anti-torque device
GB964360A (en) * 1961-12-12 1964-07-22 Power Jets Res & Dev Ltd Helicopter
FR1332300A (fr) * 1962-07-25 1963-07-12 United Aircraft Corp Mécanisme anti-couple pour hélicoptères
US3262271A (en) * 1965-07-30 1966-07-26 Gen Electric Thrust reverser
US3510087A (en) * 1968-05-06 1970-05-05 James C Strickland Air coupling system for helicopters
US3756540A (en) * 1971-08-06 1973-09-04 Us Navy Minimum drag circulation profile
US3807662A (en) * 1972-11-13 1974-04-30 Lockheed Aircraft Corp Anti-torque, propulsion, and directional control system
US3957226A (en) * 1975-01-27 1976-05-18 The Boeing Company Helicopter yaw and propulsion mechanism

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4039027A1 (de) * 1989-12-08 1991-06-13 Westland Helicopters Verbundhubschrauber
DE4039028A1 (de) * 1989-12-08 1991-06-13 Westland Helicopters Verbundhubschrauber
DE9012671U1 (de) * 1990-09-05 1990-11-08 Dornier Luftfahrt GmbH, 8031 Weßling Drehflügelfluggerät mit Mitteln zur Steuerung um die Fluggerätehochachse

Also Published As

Publication number Publication date
DE2849171A1 (de) 1979-06-28
FR2412462A1 (fr) 1979-07-20
IT1101191B (it) 1985-09-28
IT7831058A0 (it) 1978-12-20
GB2012223B (en) 1982-01-20
FR2412462B1 (enExample) 1983-11-10
DE2857901A1 (enExample) 1982-09-23
GB2012223A (en) 1979-07-25
US4200252A (en) 1980-04-29
JPS54100098A (en) 1979-08-07

Similar Documents

Publication Publication Date Title
DE2849171C2 (de) Gegendrehmomenteinrichtung bei einem mechanisch angetriebenen
DE69126132T2 (de) Antriebssystem für kurz- und senkrecht-start- und -landeflugzeug
DE69201690T2 (de) Gegendrehmomentanlage eines Hubschraubers.
DE69028391T2 (de) Schlitze für die regelbare Zirkulation bei einer Hubschrauberseitensteuerung
DE69710733T2 (de) Verbesserungen an oder bezuglich der fluiddynamische auftriebserzeugung
DE2737016C2 (de) Tragfläche mit aktiver Auftriebssteuerung
EP0667283B1 (de) Kombinations-luftfahrzeug
DE2156319C3 (enExample)
DE69801589T2 (de) Auftrieberhöhungsvorrichtung einer flügelvorderkante mit laminarer strömungkontrolle
DE69521152T2 (de) Flugzeug mit strahlantrieb der tragflächenklappen
DE3223201A1 (de) Verbundtriebwerk
DE1506810B2 (de) Vorrichtung zur steuerung und oder stabilisierung eines luft oder wasserfahrzeugs
DE1134594B (de) Schubwender fuer ein Zweikreisstrahltriebwerk
DE1285894B (de) Flugzeugtragfluegel mit Hinterkantenklappen
DE4039028A1 (de) Verbundhubschrauber
DE1481576C3 (de) Flugzeug
DE3150595C2 (enExample)
DE2012243B1 (de) Flugzeug mit Deltaflügel
DE1288924B (de) Fluggeraet zum wahlweisen Einsatz im Vollflug oder Flug mit Bodeneffekt
DE2733463A1 (de) Antriebssystem, insbesondere fuer luft-, boden- oder wasserfahrzeuge
DE1157929B (de) Flugzeug mit Strahltriebwerken, die mit Schubwendern versehen sind
DE1506569A1 (de) Duesenflugzeug mit nach unten richtbarem Schubstrahl
DE4039027A1 (de) Verbundhubschrauber
DE102023118008B3 (de) Anflugverfahren mit verteilten Antrieben
DE1286405B (de) Flugzeug mit einem Hubschrauberrotor

Legal Events

Date Code Title Description
OD Request for examination
8127 New person/name/address of the applicant

Owner name: HUGHES HELICOPTERS, INC., 90230 CULVER CITY, CALIF

8128 New person/name/address of the agent

Representative=s name: LIEBAU, G., DIPL.-ING., PAT.-ANW., 8900 AUGSBURG

8172 Supplementary division/partition in:

Ref country code: DE

Ref document number: 2857901

Format of ref document f/p: P

Q171 Divided out to:

Ref country code: DE

Ref document number: 2857901

AH Division in

Ref country code: DE

Ref document number: 2857901

Format of ref document f/p: P

D2 Grant after examination
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: MCDONNELL DOUGLAS HELICOPTER CO., CULVER CITY, CAL