BR0309371A - Eixo mecânico de acionamento composto com adaptadores de extremidade capturados - Google Patents

Eixo mecânico de acionamento composto com adaptadores de extremidade capturados

Info

Publication number
BR0309371A
BR0309371A BR0309371-9A BR0309371A BR0309371A BR 0309371 A BR0309371 A BR 0309371A BR 0309371 A BR0309371 A BR 0309371A BR 0309371 A BR0309371 A BR 0309371A
Authority
BR
Brazil
Prior art keywords
end adapters
mechanical shaft
drive mechanical
composite drive
captured
Prior art date
Application number
BR0309371-9A
Other languages
English (en)
Inventor
Sherman S Lin
Scott D Poster
Original Assignee
Bell Helicopter Textron 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 Bell Helicopter Textron Inc filed Critical Bell Helicopter Textron Inc
Publication of BR0309371A publication Critical patent/BR0309371A/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • B29C70/462Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • B29C70/48Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/86Incorporated in coherent impregnated reinforcing layers, e.g. by winding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C29/00Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0033Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D35/00Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
    • 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
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C3/00Shafts; Axles; Cranks; Eccentrics
    • F16C3/02Shafts; Axles
    • F16C3/026Shafts made of fibre reinforced resin
    • 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
    • F16D1/00Couplings for rigidly connecting two coaxial shafts or other movable machine elements
    • F16D1/06Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end
    • F16D1/064Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end non-disconnectable
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/748Machines or parts thereof not otherwise provided for
    • B29L2031/75Shafts
    • 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
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2326/00Articles relating to transporting
    • F16C2326/43Aeroplanes; Helicopters
    • 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
    • F16D2250/00Manufacturing; Assembly

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)

Abstract

"EIXO MECâNICO DE ACIONAMENTO COMPOSTO COM ADAPTADORES DE EXTREMIDADE CAPTURADOS". Um eixo mecânico de acionamento composto, no qual os adaptadores de extremidade são capturados na porção de material composto durante o processo de manufaturamento do conjunto de eixo mecânico de acionamento composto é revelado. Os adaptadores de extremidade incluem aletas que se projetam para fora para transmitir torque, tensão e força compressiva, e momento de encurvamento para a porção de material composto e vice-versa.
BR0309371-9A 2002-04-19 2003-04-18 Eixo mecânico de acionamento composto com adaptadores de extremidade capturados BR0309371A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US37430802P 2002-04-19 2002-04-19
PCT/US2003/012423 WO2003089145A2 (en) 2002-04-19 2003-04-18 Composite drive shaft with captured end adapters

Publications (1)

Publication Number Publication Date
BR0309371A true BR0309371A (pt) 2005-02-22

Family

ID=29251172

Family Applications (1)

Application Number Title Priority Date Filing Date
BR0309371-9A BR0309371A (pt) 2002-04-19 2003-04-18 Eixo mecânico de acionamento composto com adaptadores de extremidade capturados

Country Status (7)

Country Link
US (1) US7335108B2 (pt)
EP (1) EP1499554B1 (pt)
AU (1) AU2003223688A1 (pt)
BR (1) BR0309371A (pt)
CA (1) CA2481730C (pt)
DE (2) DE60333912D1 (pt)
WO (1) WO2003089145A2 (pt)

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WO2008024108A1 (en) * 2006-08-23 2008-02-28 Gkn Driveline North America, Inc. Direct torque flow constant velocity joint face spline connector
KR100831643B1 (ko) 2007-04-10 2008-05-22 류충오 연결 조인트 및 이를 구비한 복합재료 드라이브 샤프트어셈블리
DE102008056017A1 (de) * 2008-11-05 2010-05-06 Rolls-Royce Deutschland Ltd & Co Kg Verfahren zur Herstellung einer Triebwerkswelle
EP2602496A1 (de) * 2011-12-05 2013-06-12 Magna Steyr Fahrzeugtechnik AG & Co KG Verbindung zwischen zwei Bauteilen und Verfahren zur Verbindung zweier Bauteile
FR3001656B1 (fr) * 2013-02-04 2015-06-26 Safran Procede de fabrication ameliore d'un arbre de transmission, de preference pour systeme de boite d'accessoires de turbomachine d'aeronef
US9441374B2 (en) 2014-04-08 2016-09-13 Goodrich Corporation Struts and methods utilizing a compression collar
US9726325B2 (en) 2014-05-01 2017-08-08 Goodrich Corporation Composite tube assemblies and methods
US9568040B2 (en) 2014-06-02 2017-02-14 Goodrich Corporation Struts and methods utilizing a locking collar nut
US20160137308A1 (en) * 2014-11-17 2016-05-19 Hamilton Sundstrand Corporation Ram air turbine with composite shaft
EP3081822B1 (en) 2015-04-16 2019-08-28 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Hybrid metal-composite drive shaft unit and method of manufacturing the same
US9909624B2 (en) 2015-09-22 2018-03-06 Rohr, Inc. Composite driveshaft for a rotary system
US20170082137A1 (en) * 2015-09-22 2017-03-23 Rohr, Inc. Driveshaft for a rotary system
US10508682B2 (en) * 2015-12-31 2019-12-17 Moog Inc. Composite torque tube end fitting attachment method
US9937671B2 (en) 2016-01-15 2018-04-10 Moog Inc. All-composite torque tube with metal eyelets
US10272991B2 (en) * 2016-06-23 2019-04-30 Goodrich Corporation Metallic composite joint
US20180086444A1 (en) 2016-09-23 2018-03-29 Bell Helicopter Textron Inc. Aircraft Drive System
US11255373B2 (en) 2016-09-23 2022-02-22 Textron Innovations Inc. Active thermal management for fire-tolerant drive systems
US10677261B2 (en) * 2017-04-13 2020-06-09 General Electric Company Turbine engine and containment assembly for use in a turbine engine
US10689106B2 (en) 2017-07-06 2020-06-23 Bell Helicopter Textron Inc. Fixed outboard engine tiltrotor with leading edge drive system and angled rotation spindle configuration
EP3427921B1 (en) 2017-07-14 2021-11-17 Crompton Technology Group Limited Composite ball screw
FR3075898B1 (fr) * 2017-12-22 2019-11-29 Safran Transmission Systems Arbre de transmission pour une turbomachine
US11156245B2 (en) * 2018-01-08 2021-10-26 Goodrich Corporation Hybrid metallic/composite axial tension/compression lobe joint
US11519454B2 (en) 2019-07-24 2022-12-06 Goodrich Corporation Hybrid metallic/composite tube design to transfer bending, axial, and flexural shear
US11603801B2 (en) 2021-05-24 2023-03-14 General Electric Company Midshaft rating for turbomachine engines
US12071978B2 (en) 2021-05-24 2024-08-27 General Electric Company Midshaft rating for turbomachine engines
US11808214B2 (en) 2021-05-24 2023-11-07 General Electric Company Midshaft rating for turbomachine engines
US20220373019A1 (en) * 2021-05-24 2022-11-24 General Electric Company Midshaft rating for turbomachine engines
US11724813B2 (en) 2021-05-24 2023-08-15 General Electric Company Midshaft rating for turbomachine engines

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US4561799A (en) * 1982-02-08 1985-12-31 Grumman Aerospace Corp. Torque joint
EP0474441A3 (en) * 1990-08-30 1993-06-16 Sumitomo Chemical Company, Limited Fiber-reinforced plastics drive shafts
US5342464A (en) * 1992-04-24 1994-08-30 United Technologies Corporation Bonding of thermoplastic composite structures to metal structures
US5304012A (en) * 1992-07-01 1994-04-19 Curtiss Wright Flight Systems Inc. Drive shaft fitting or coupling
DE19524903A1 (de) * 1995-07-08 1997-04-30 Inst Kraftfahrwesen Rwth Aache Wellenförmige Kraftübertragungseinrichtung in faserverstärkte Rahmenstrukturen sowie Verfahren zu ihrer Herstellung
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US6932118B2 (en) * 2002-09-24 2005-08-23 The Boeing Company Low chamfer angled torque tube end fitting metal

Also Published As

Publication number Publication date
AU2003223688A1 (en) 2003-11-03
EP1499554B1 (en) 2010-08-25
CA2481730A1 (en) 2003-10-30
US20050239562A1 (en) 2005-10-27
US7335108B2 (en) 2008-02-26
CA2481730C (en) 2010-03-23
EP1499554A4 (en) 2006-03-01
DE60333912D1 (de) 2010-10-07
WO2003089145A3 (en) 2004-08-05
WO2003089145A2 (en) 2003-10-30
EP1499554A2 (en) 2005-01-26
DE03719885T1 (de) 2005-06-23
AU2003223688A8 (en) 2003-11-03

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Legal Events

Date Code Title Description
B06A Patent application procedure suspended [chapter 6.1 patent gazette]
B11B Dismissal acc. art. 36, par 1 of ipl - no reply within 90 days to fullfil the necessary requirements