BR112014010089A2 - junta universal de velocidade constante para rotor de helicóptero - Google Patents

junta universal de velocidade constante para rotor de helicóptero

Info

Publication number
BR112014010089A2
BR112014010089A2 BR112014010089A BR112014010089A BR112014010089A2 BR 112014010089 A2 BR112014010089 A2 BR 112014010089A2 BR 112014010089 A BR112014010089 A BR 112014010089A BR 112014010089 A BR112014010089 A BR 112014010089A BR 112014010089 A2 BR112014010089 A2 BR 112014010089A2
Authority
BR
Brazil
Prior art keywords
constant speed
universal joint
helicopter rotor
speed universal
helicopter
Prior art date
Application number
BR112014010089A
Other languages
English (en)
Inventor
Lidak Vladimiro
Original Assignee
K4A S R L
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 K4A S R L filed Critical K4A S R L
Publication of BR112014010089A2 publication Critical patent/BR112014010089A2/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/37Rotors having articulated joints
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/37Rotors having articulated joints
    • B64C27/41Rotors having articulated joints with flapping hinge or universal joint, common to the blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D3/00Yielding couplings, i.e. with means permitting movement between the connected parts during the drive
    • F16D3/16Universal joints in which flexibility is produced by means of pivots or sliding or rolling connecting parts
    • F16D3/26Hooke's joints or other joints with an equivalent intermediate member to which each coupling part is pivotally or slidably connected
    • F16D3/30Hooke's joints or other joints with an equivalent intermediate member to which each coupling part is pivotally or slidably connected in which the coupling is specially adapted to constant velocity-ratio
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S464/00Rotary shafts, gudgeons, housings, and flexible couplings for rotary shafts
    • Y10S464/904Homokinetic coupling
    • Y10S464/905Torque transmitted via radially extending pin

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Transmission Devices (AREA)
  • Toys (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
BR112014010089A 2011-10-27 2012-10-23 junta universal de velocidade constante para rotor de helicóptero BR112014010089A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IT000563A ITRM20110563A1 (it) 2011-10-27 2011-10-27 "giunto cardanico omocinetico per rotori di elicottero"
PCT/IT2012/000322 WO2013061348A1 (en) 2011-10-27 2012-10-23 Constant velocity universal joint for helicopter rotor

Publications (1)

Publication Number Publication Date
BR112014010089A2 true BR112014010089A2 (pt) 2017-04-25

Family

ID=45757110

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112014010089A BR112014010089A2 (pt) 2011-10-27 2012-10-23 junta universal de velocidade constante para rotor de helicóptero

Country Status (9)

Country Link
US (1) US9388862B2 (pt)
EP (1) EP2771240B1 (pt)
CN (1) CN103917448A (pt)
BR (1) BR112014010089A2 (pt)
ES (1) ES2553214T3 (pt)
IT (1) ITRM20110563A1 (pt)
PL (1) PL2771240T3 (pt)
RU (1) RU2607717C2 (pt)
WO (1) WO2013061348A1 (pt)

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US9399513B2 (en) * 2012-11-09 2016-07-26 Bell Helicopter Textron Inc. Constant velocity joint with control mechanism
US9878783B2 (en) 2012-11-09 2018-01-30 Bell Helicopter Textron Inc. Constant velocity joint with spring rate control mechanism
US20150065259A1 (en) * 2013-08-29 2015-03-05 Flexous B.V. Compliant constant velocity constant torque universal joint
US9382001B2 (en) * 2014-07-23 2016-07-05 Bell Helicopter Textron Inc. Torque transfer system for a rotorcraft
US10432840B2 (en) * 2015-10-08 2019-10-01 L-3 Communication-Insight Technology Division Fusion night vision system
US11186363B2 (en) 2015-10-21 2021-11-30 Sikorsky Aircraft Corporation Electric propulsion system for a rotary wing aircraft
US10275565B2 (en) * 2015-11-06 2019-04-30 The Boeing Company Advanced automated process for the wing-to-body join of an aircraft with predictive surface scanning
WO2017213936A1 (en) * 2016-06-07 2017-12-14 Fpv Manuals Llc Quick disconnect coupling for a propeller
CN106168259B (zh) * 2016-07-19 2019-03-12 北京航空航天大学 一种具有常值刚度的柔性并联万向节
US10752343B2 (en) 2016-10-18 2020-08-25 Sikorsky Aircraft Corporation Electric propulsion system for a rotary wing aircraft
US10974824B2 (en) 2017-07-20 2021-04-13 Sikorsky Aircraft Corporation Electric powered direct drive rotor motor
US10676182B2 (en) * 2017-07-20 2020-06-09 Sikorsky Aircraft Corporation Tilting coaxial rotor for a rotary wing aircraft
US11114138B2 (en) 2017-09-15 2021-09-07 Groq, Inc. Data structures with multiple read ports
US11868804B1 (en) 2019-11-18 2024-01-09 Groq, Inc. Processor instruction dispatch configuration
US11243880B1 (en) 2017-09-15 2022-02-08 Groq, Inc. Processor architecture
US11360934B1 (en) 2017-09-15 2022-06-14 Groq, Inc. Tensor streaming processor architecture
US11170307B1 (en) 2017-09-21 2021-11-09 Groq, Inc. Predictive model compiler for generating a statically scheduled binary with known resource constraints
US11097837B2 (en) 2018-06-11 2021-08-24 Bell Helicopter Textron Inc. Bearingless gimbaled rotor hubs and swashplates
CN108945426B (zh) * 2018-06-27 2021-12-03 中国直升机设计研究所 一种适用于多种桨毂构型的自动倾斜器
US10712730B2 (en) 2018-10-04 2020-07-14 The Boeing Company Methods of synchronizing manufacturing of a shimless assembly
CN109466749B (zh) * 2018-11-06 2023-07-04 珠海隆华直升机科技有限公司 直升机变距驱动总成及直升机
US11537687B2 (en) 2018-11-19 2022-12-27 Groq, Inc. Spatial locality transform of matrices
RU2746024C2 (ru) * 2018-12-24 2021-04-06 Александр Александрович Горшков Втулка воздушного винта с автоматом перекоса
US11136116B2 (en) * 2019-09-05 2021-10-05 Bell Textron Inc. Elastomeric double Hooke's joint
CN112078787B (zh) * 2020-09-17 2022-01-21 中国航空制造技术研究院 一种直升机主减速器的自适应定位装置
US11691723B2 (en) * 2021-05-04 2023-07-04 Textron Innovations Inc. Rotor assembly with static mast and pivoting rotor hub
RU2763606C1 (ru) * 2021-07-08 2021-12-30 Непубличное Акционерное Общество "Гиропланы - Передовые Авиационные Технологии" Узел крепления втулки и ступицы несущего винта автожира к пилону с непосредственным управлением наклоном оси вращения для управления автожиром

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1899170A (en) * 1931-12-07 1933-02-28 Wainwright Lawrence Universal joint
US3263447A (en) * 1964-01-09 1966-08-02 Gen Motors Corp Constant velocity universal joint
US3841586A (en) * 1973-04-26 1974-10-15 Boeing Co Rotor swashplate assembly
US4232563A (en) * 1978-03-16 1980-11-11 Barry Wright Corporation Laminated elastomeric end bearings for articulating links
GB8822843D0 (en) * 1988-09-29 1988-11-02 Jaguar Cars Universal joints
RU2156208C1 (ru) * 1999-04-14 2000-09-20 Любимов Александр Александрович Колонка вертолета
CA2442323C (en) * 2001-03-26 2011-10-18 Glenn Alexander Thompson Constant velocity coupling and control system therefor
CN101583535B (zh) * 2006-01-13 2013-11-06 贝尔直升机泰克斯特龙公司 硬共面的、装有万向架的斜旋翼毂
EP2223854B8 (en) * 2009-02-25 2011-10-05 AGUSTAWESTLAND S.p.A. Helicopter rotor

Also Published As

Publication number Publication date
RU2607717C2 (ru) 2017-01-10
EP2771240A1 (en) 2014-09-03
US9388862B2 (en) 2016-07-12
ES2553214T3 (es) 2015-12-07
CN103917448A (zh) 2014-07-09
ITRM20110563A1 (it) 2013-04-28
RU2014121220A (ru) 2015-12-10
US20140302938A1 (en) 2014-10-09
EP2771240B1 (en) 2015-07-01
WO2013061348A1 (en) 2013-05-02
PL2771240T3 (pl) 2016-01-29

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B11B Dismissal acc. art. 36, par 1 of ipl - no reply within 90 days to fullfil the necessary requirements
B350 Update of information on the portal [chapter 15.35 patent gazette]