DE69228246D1 - Mantelgebläse und blattverstellsteuerung eines drehflügelflugzeugheckrotors - Google Patents

Mantelgebläse und blattverstellsteuerung eines drehflügelflugzeugheckrotors

Info

Publication number
DE69228246D1
DE69228246D1 DE69228246T DE69228246T DE69228246D1 DE 69228246 D1 DE69228246 D1 DE 69228246D1 DE 69228246 T DE69228246 T DE 69228246T DE 69228246 T DE69228246 T DE 69228246T DE 69228246 D1 DE69228246 D1 DE 69228246D1
Authority
DE
Germany
Prior art keywords
rear rotor
blade adjustment
plane rear
turning plane
shell blower
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 - Fee Related
Application number
DE69228246T
Other languages
English (en)
Other versions
DE69228246T2 (de
Inventor
Rene Desjardins
Francis Mccardle
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
Boeing Co
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 Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of DE69228246D1 publication Critical patent/DE69228246D1/de
Publication of DE69228246T2 publication Critical patent/DE69228246T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • B64C27/32—Rotors
    • B64C27/37—Rotors having articulated joints
    • B64C27/45—Rotors having articulated joints with a feathering hinge only
    • 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
    • B64C2027/8254—Shrouded tail rotors, e.g. "Fenestron" fans

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)
  • Transmission Devices (AREA)
DE69228246T 1991-08-02 1992-07-31 Mantelgebläse und blattverstellsteuerung eines drehflügelflugzeugheckrotors Expired - Fee Related DE69228246T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US73949891A 1991-08-02 1991-08-02
PCT/US1992/006441 WO1993002916A1 (en) 1991-08-02 1992-07-31 Ducted fan and pitch controls for tail rotor of rotary wing aircraft

Publications (2)

Publication Number Publication Date
DE69228246D1 true DE69228246D1 (de) 1999-03-04
DE69228246T2 DE69228246T2 (de) 1999-08-19

Family

ID=24972582

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69228246T Expired - Fee Related DE69228246T2 (de) 1991-08-02 1992-07-31 Mantelgebläse und blattverstellsteuerung eines drehflügelflugzeugheckrotors

Country Status (9)

Country Link
US (1) US5478204A (de)
EP (1) EP0597038B1 (de)
JP (1) JP2768826B2 (de)
AU (1) AU2467992A (de)
CA (1) CA2113719C (de)
DE (1) DE69228246T2 (de)
ES (1) ES2126600T3 (de)
IL (1) IL102698A (de)
WO (1) WO1993002916A1 (de)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2725420B1 (fr) * 1994-10-11 1996-12-13 Eurocopter France Dispositif de commande de pas pour rotor sans articulation
US5607122A (en) * 1994-12-22 1997-03-04 Bell Helicopter Textron Inc. Tail rotor authority control for a helicopter
FR2764578B1 (fr) * 1997-06-13 1999-09-10 Eurocopter France Rotor de giravion a moyeu bi-plateau et commande de pas partiellement externe
FR2775951B1 (fr) * 1998-03-16 2001-09-07 Rene Mouille Pale de rotor, notamment pour le rotor arriere anticouple d'un helicoptere
US7194913B2 (en) 2002-08-26 2007-03-27 Shell Oil Company Apparatuses and methods for monitoring stress in steel catenary risers
WO2006050488A1 (en) 2004-11-03 2006-05-11 Shell Internationale Research Maatschappij B.V. Apparatus and method for retroactively installing sensors on marine elements
EA014651B1 (ru) * 2006-01-13 2010-12-30 Белл Хеликоптер Текстрон Инк. Жесткая в плоскости, установленная в карданном подвесе втулка несущего винта с изменяемым наклоном
US20100019082A1 (en) * 2008-07-25 2010-01-28 Tsc, Llc Composite Flight Control Cables
PT2154065E (pt) * 2008-08-14 2011-09-30 Agusta Spa Rotor de helicóptero
US8122586B2 (en) * 2008-11-18 2012-02-28 The Boeing Company Method for connecting a tension-torsion strap
EP2367719B1 (de) * 2008-12-11 2018-09-12 Sikorsky Aircraft Corporation Heckrotorblattbaugruppe mit bewegungsbegrenzer für ein elastomeres lagersystem
GB2511668A (en) * 2012-04-12 2014-09-10 Supercell Oy System and method for controlling technical processes
FR2991294B1 (fr) * 2012-06-04 2015-02-13 Etienne Jean Rampal Ensemble rotor bi-plateaux d'aeronefs avec logement interne des commandes de pas et adaptateurs de frequence
US9441495B2 (en) 2013-02-27 2016-09-13 Sikorsky Aircraft Corporation Rotary wing aircraft pitch beam attachment with anti-rotation plate design
RU2538497C1 (ru) * 2013-12-03 2015-01-10 Открытое акционерное общество "Камов" Рулевой винт вертолета, установленный в туннеле
WO2016028762A1 (en) 2014-08-20 2016-02-25 Sikorsky Aircraft Corporation Rotor blade pitch horn assembly
FR3031497B1 (fr) 2015-01-08 2017-01-06 Airbus Helicopters Rotor de giravion comportant un moyeu en materiaux composites issus de tissus de fibres de carbone poudrees d'une resine thermoplastique
US20180002002A1 (en) * 2016-02-22 2018-01-04 Sikorsky Aircraft Corporation Rotor assembly including a one piece molding rotor hub
EP3366584B1 (de) * 2017-02-27 2019-04-17 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Anstellwinkelsteuerungsvorrichtung für einen heckrotor eines drehflüglers
EP3434590B1 (de) * 2017-07-27 2019-11-27 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Steuerungsübertragungselement für eine anstellwinkelsteuerungsvorrichtung für einen heckrotor eines drehflüglers
FR3072939B1 (fr) * 2017-10-31 2021-11-26 Airbus Helicopters Rotor a pas collectif variable et aeronef
KR102153511B1 (ko) * 2019-01-08 2020-09-10 에어버스 헬리콥터스 도이칠란트 게엠베하 덕트된 회전익기 테일 로터의 피치 제어 장치용 제어 이동 부재
US11034440B2 (en) 2019-03-01 2021-06-15 Textron Innovations Inc. Tail rotor gearbox support assemblies for helicopters
US10988243B2 (en) * 2019-03-15 2021-04-27 Bell Textron Inc. Tension-torsion strap
EP3753848B1 (de) * 2019-06-17 2021-08-04 LEONARDO S.p.A. Drehmomentausgleichsrotor für einen hubschrauber
EP3753850B1 (de) * 2019-06-17 2021-08-04 LEONARDO S.p.A. Drehmomentausgleichsrotor für einen hubschrauber
CH717386A1 (de) * 2020-05-06 2021-11-15 Kopter Group Ag Lösbare Verbindung zwischen einem Blattsteuereinheitsarm und einem Blattverstellhebel.
CN114537655B (zh) * 2022-01-28 2023-07-28 南京航空航天大学 旋翼机构
CN117419885B (zh) * 2023-12-19 2024-03-19 中国空气动力研究与发展中心低速空气动力研究所 一种剪刀式尾桨风洞试验台

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2499314A (en) * 1947-09-12 1950-02-28 United Aircraft Corp Two-bladed tail rotor on common hinge
US3450208A (en) * 1967-04-07 1969-06-17 Barton R E Dual drive mechanism
US3518025A (en) * 1968-05-06 1970-06-30 Lockheed Aircraft Corp Helicopter rotor system
FR1593008A (de) * 1968-07-11 1970-05-25
US3637321A (en) * 1968-12-04 1972-01-25 Andrei Vladimirovich Nekrasov Tail rotor of a helicopter
US3768334A (en) * 1972-06-26 1973-10-30 Bendix Corp Load equalized tension torsion tie bar
US3790302A (en) * 1972-10-10 1974-02-05 Textron Inc Tail rotor mounting for coning relief
FR2397326A2 (fr) * 1977-07-13 1979-02-09 Aerospatiale Rotor sans articulations, en particulier pour un giravion
FR2430354A1 (fr) * 1978-07-07 1980-02-01 Aerospatiale Helice multipale a pas variable d'un type simplifie
FR2534222A1 (fr) * 1982-10-06 1984-04-13 Aerospatiale Agencement de rotor de queue a poussee accrue pour aeronef a voilure tournante et dispositif pour accroitre la poussee d'un tel agencement
FR2542695B1 (fr) * 1983-03-18 1985-07-26 Aerospatiale Helice multipale a pas variable a pale s en materiaux composites demontables individuellement, procede de fabrication de telles pales et pales ainsi realisees
IT1161530B (it) * 1983-10-26 1987-03-18 Agusta Aeronaut Costr Trasmissione per rotore anticoppia di elicotteri
IT1161531B (it) * 1983-10-26 1987-03-18 Agusta Aeronaut Costr Assieme di rotore anticoppia per elicotteri
SE458293B (sv) * 1987-09-15 1989-03-13 Svenning Konsult Ab S Regleranordning foer konstanthaallning av varvtalet vid turbiner

Also Published As

Publication number Publication date
IL102698A (en) 1996-11-14
ES2126600T3 (es) 1999-04-01
JPH06509765A (ja) 1994-11-02
AU2467992A (en) 1993-03-02
EP0597038B1 (de) 1999-01-20
CA2113719C (en) 1999-11-02
DE69228246T2 (de) 1999-08-19
US5478204A (en) 1995-12-26
WO1993002916A1 (en) 1993-02-18
JP2768826B2 (ja) 1998-06-25
IL102698A0 (en) 1993-02-21
EP0597038A1 (de) 1994-05-18
CA2113719A1 (en) 1993-02-18

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee