ES2089568T3 - Tubo de torsion de conjunto de rotor principal sin cojinetes. - Google Patents

Tubo de torsion de conjunto de rotor principal sin cojinetes.

Info

Publication number
ES2089568T3
ES2089568T3 ES92920438T ES92920438T ES2089568T3 ES 2089568 T3 ES2089568 T3 ES 2089568T3 ES 92920438 T ES92920438 T ES 92920438T ES 92920438 T ES92920438 T ES 92920438T ES 2089568 T3 ES2089568 T3 ES 2089568T3
Authority
ES
Spain
Prior art keywords
drive shaft
shaft tube
brm
main rotor
tube
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
ES92920438T
Other languages
English (en)
Inventor
Francis E Byrnes
I Lawrence Cullen Iii
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.)
RTX Corp
Original Assignee
United Technologies 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 United Technologies Corp filed Critical United Technologies Corp
Application granted granted Critical
Publication of ES2089568T3 publication Critical patent/ES2089568T3/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
    • B64C27/32—Rotors
    • B64C27/46—Blades
    • B64C27/473—Constructional features
    • B64C27/48—Root attachment to rotor head

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
  • Rotary Pumps (AREA)

Abstract

UN TUBO (10) COMPUESTO QUE CONTIENE EL EJE MOTOR PARA UNA JUNTA (100) PARA ROTOR PRINCIPAL SIN COJINETE (BRM) QUE ESTA OPTIMAMENTE FABRICADA PARA OBTENER RIGIDEZ TORSIONAL, RESISTENCIA A LA FATIGA, Y RESISTENCIA A DOBLARSE DISEÑADO CONSTREÑIDO AL MINIMO PESO POR UNIDAD. EL TUBO (10) DE EJE MOTOR COMPUESTO INCLUYE UNA SECCION (12) INTERIOR REFORZADA PARA ACOPLAR MECANICAMENTE EL TUBO (10) DE EJE MOTOR EN COMBINACION CON LA ESTRUCTURA (120) DEL EJE DE LA JUNTA BRM, UNA SECCION (16) EXTERIOR REFORZADA PARA ACOPLAR MECANICAMENTE EL TUBO (10) DE EJE MOTOR EN COMBINACION CON UNA HOJA DEL ROTOR PRINCIPAL CORRESPONDIENTE, Y UNA SECCION (14) INTERMEDIA QUE ES OPERATIVA PARA ACOMODAR LA CARGA TERMINAL DE PLANO Y/O DE CANTO QUE ACTUA SOBRE LA JUNTA BRM DURANTE LA OPERACION DE ELLA. LA SECCION INTERMEDIA (14) DEL TUBO (10) DE EJE MOTOR TIENE UN ESPESOR DE PARED CONSTANTE Y ESTA FORMADA DE FILAMENTOS CONTINUOS ENROLLADOS QUE TIENEN UNA ORIENTACION DE FIBRA PREDETERMINADA DENTRO DE UN AMPLIO MARGEN DE ALREDEDOR DE +/DUCIDO MARGEN DE ALREDEDOR DE +/ EL TUBO (10) DE EJE MOTOR ESTA PREFERIBLEMENTE FORMADO DE FILAMENTO CONTINUO ARROLLADO QUE TIENE UNA OPTIMA ORIENTACION DE FIBRA DE ALREDEDOR DE +/ ERMEDIA (14) QUE TIENE UN MINIMO ESPESOR DE PARED DEL TUBO DE EJE MOTOR.
ES92920438T 1991-08-28 1992-08-26 Tubo de torsion de conjunto de rotor principal sin cojinetes. Expired - Lifetime ES2089568T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US75127291A 1991-08-28 1991-08-28

Publications (1)

Publication Number Publication Date
ES2089568T3 true ES2089568T3 (es) 1996-10-01

Family

ID=25021260

Family Applications (1)

Application Number Title Priority Date Filing Date
ES92920438T Expired - Lifetime ES2089568T3 (es) 1991-08-28 1992-08-26 Tubo de torsion de conjunto de rotor principal sin cojinetes.

Country Status (10)

Country Link
US (1) US5242267A (es)
EP (1) EP0600040B1 (es)
JP (1) JP3242405B2 (es)
KR (1) KR100207361B1 (es)
AU (1) AU655504B2 (es)
CA (1) CA2115166C (es)
DE (1) DE69210028T2 (es)
ES (1) ES2089568T3 (es)
IL (1) IL102867A (es)
WO (1) WO1993004917A1 (es)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5372479A (en) * 1993-06-02 1994-12-13 United Technologies Corporation Flexbeam for a helicopter bearingless main rotor assembly
US5431538A (en) * 1993-07-01 1995-07-11 United Technologies Corporation Hybrid composite flexbeam for a helicopter bearingless main rotor assembly
DE4423115A1 (de) * 1994-07-01 1996-01-04 Wolf Hirth Gmbh Propellerflügel aus Kunststoffmaterial und Verfahren zu seiner Herstellung
FR2728540A1 (fr) * 1994-12-22 1996-06-28 Eurocopter France Rotor sans articulation a anneaux intermediaires de commande de pas
US5636969A (en) * 1995-03-28 1997-06-10 Sikorsky Aircraft Corporation Torque tube/spar assembly for variable diameter helicopter rotors
US5645400A (en) * 1996-03-18 1997-07-08 Sikorsky Aircraft Corporation Composite cuff structure for helicopter rotors
US5690474A (en) * 1996-07-18 1997-11-25 Sikorsky Aircraft Corporation Optimized composite flexbeam for helicopter tail rotors
JP3737962B2 (ja) * 2001-11-08 2006-01-25 富士重工業株式会社 フレックスビーム
US6695583B2 (en) 2002-05-30 2004-02-24 Sikorsky Aircraft Corporation Snubber-vibration damper system for a bearingless main rotor
US8720825B2 (en) * 2005-03-31 2014-05-13 The Boeing Company Composite stiffeners for aerospace vehicles
ES2274701B1 (es) * 2005-07-15 2008-05-01 GAMESA INNOVATION & TECHNOLOGY, S.L. Procedimiento de fabricacion de piezas huecas de grandes dimensiones a base de materiales compuestos.
US8142158B2 (en) 2005-12-02 2012-03-27 Sikorsky Aircraft Corporation Compact load path swashplate assembly
US8548648B2 (en) * 2007-07-02 2013-10-01 Sikorsky Aircraft Corporation Fly-by-wire flight control system with electronic lead/lag damper algorithm
US8038394B2 (en) * 2008-01-16 2011-10-18 Sikorsky Aircraft Corporation System and method of damping a 1P motion
EP2246260B1 (en) * 2009-04-29 2011-08-31 EUROCOPTER DEUTSCHLAND GmbH Rotor blade made of a fibre-reinforced composite material
US8801378B2 (en) 2010-02-24 2014-08-12 Sikorsky Aircraft Corporation Low offset hingeless rotor with pitch change bearings
CN102452477B (zh) * 2010-10-15 2015-03-25 空客直升机德国有限公司 由纤维加固复合材料制成的转子叶片及其生产方法
US9169011B2 (en) 2011-09-13 2015-10-27 Sikorsky Aircraft Corporation Rotor with blades including outer blade shell and inner structural member
US11014658B1 (en) 2015-01-02 2021-05-25 Delbert Tesar Driveline architecture for rotorcraft featuring active response actuators
US10160540B2 (en) 2015-01-09 2018-12-25 Rohr, Inc. Rotor head for a vertical takeoff and landing aircraft
EP3225542B1 (en) * 2016-03-30 2018-05-09 AIRBUS HELICOPTERS DEUTSCHLAND GmbH A method of manufacturing a control cuff for a rotor blade of a hinge- and bearingless rotor
FR3075757B1 (fr) * 2017-12-22 2019-11-15 Airbus Helicopters Enveloppes aerodynamiques epaisses pour cols de pales et carenages de manchons de pales d'un rotor d'un aeronef
CN113316886B (zh) 2018-11-21 2024-08-23 通用电气可再生能源西班牙有限公司 由风力涡轮驱动的超导发电机
CN110641734B (zh) * 2019-09-29 2022-11-04 中国直升机设计研究所 一种主桨中央件挥摆加载装置
JP7664616B2 (ja) * 2021-06-11 2025-04-18 株式会社石井鐵工所 ドローン用プロペラのブレード
US12384551B2 (en) * 2023-03-31 2025-08-12 Beta Air Llc System for controlling a propulsor assembly of an electric aircraft

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2397325A1 (fr) * 1977-07-13 1979-02-09 Aerospatiale Moyeu de rotor, en particulier pour le rotor principal d'un helicoptere
DE2758086C2 (de) * 1977-12-24 1983-12-01 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Rotor für ein Drehflügelflugzeug mit gelenklosem Blattanschluß
US4381902A (en) * 1979-12-20 1983-05-03 Hughes Helicopters, Inc. Helicopter tail rotor of the elastomerically-mounted composite flexbeam type
EP0085129B1 (de) * 1982-02-02 1985-11-06 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Rotor, insbesondere eines Drehflügelflugzeugs
GB2133499B (en) * 1982-11-16 1985-10-09 Honda Motor Co Ltd Shafts incorporating fibre-reinforced plastics
US4568246A (en) * 1983-03-22 1986-02-04 United Technologies Corporation Fiber reinforced/epoxy matrix composite helicopter rotor torque tube
US4676720A (en) * 1984-07-10 1987-06-30 Kawasaki Jukogyo Kabushiki Kaisha Bearingless hub structure for rotary-wing aircrafts
US4676853A (en) * 1985-08-30 1987-06-30 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method of making a flexible diaphragm
DE3704552C1 (en) * 1987-02-13 1988-03-17 Messerschmitt Boelkow Blohm Rotor blade, especially of a rotary wing aircraft
FR2618499B3 (fr) * 1987-07-24 1990-02-23 Matra Automobile Arbre de transmission composite et procede de fabrication d'un tel arbre
US4963215A (en) * 1987-12-07 1990-10-16 The Boeing Company Method for debulking precured thermoplastic composite laminae
US5059094A (en) * 1989-10-13 1991-10-22 Bell Helicopter Textron, Inc. Rotor redundant force retention system for vtol and vstol aircraft

Also Published As

Publication number Publication date
CA2115166C (en) 2000-06-20
AU655504B2 (en) 1994-12-22
KR100207361B1 (ko) 1999-07-15
CA2115166A1 (en) 1993-03-18
JPH06510007A (ja) 1994-11-10
DE69210028T2 (de) 1996-12-19
DE69210028D1 (de) 1996-05-23
EP0600040B1 (en) 1996-04-17
US5242267A (en) 1993-09-07
AU2664892A (en) 1993-04-05
JP3242405B2 (ja) 2001-12-25
EP0600040A1 (en) 1994-06-08
IL102867A0 (en) 1993-02-21
IL102867A (en) 1998-02-08
WO1993004917A1 (en) 1993-03-18

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