BR0309371A - Eixo mecânico de acionamento composto com adaptadores de extremidade capturados - Google Patents
Eixo mecânico de acionamento composto com adaptadores de extremidade capturadosInfo
- 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
Links
- 239000002131 composite material Substances 0.000 title abstract 5
- 238000005452 bending Methods 0.000 abstract 1
- 238000004519 manufacturing process Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/46—Shaping 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
- B29C70/462—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/46—Shaping 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
- B29C70/48—Shaping 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/68—Shaping 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
- B29C70/86—Incorporated in coherent impregnated reinforcing layers, e.g. by winding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft 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
- B64C29/0033—Aircraft 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C3/00—Shafts; Axles; Cranks; Eccentrics
- F16C3/02—Shafts; Axles
- F16C3/026—Shafts made of fibre reinforced resin
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D1/00—Couplings for rigidly connecting two coaxial shafts or other movable machine elements
- F16D1/06—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end
- F16D1/064—Couplings 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/748—Machines or parts thereof not otherwise provided for
- B29L2031/75—Shafts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2326/00—Articles relating to transporting
- F16C2326/43—Aeroplanes; Helicopters
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D2250/00—Manufacturing; 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.
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) |
Families Citing this family (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS54151677A (en) * | 1978-05-16 | 1979-11-29 | Toyo Boseki | Concentrator for polyvinylalcohol |
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 |
DE19524901A1 (de) * | 1995-07-08 | 1997-04-30 | Inst Kraftfahrwesen Rwth Aache | Kraftübertragungseinrichtung in geflochtene, faserverstärkte Rahmenstrukturen sowie Verfahren zu ihrer Herstellung |
US6336986B1 (en) * | 1997-07-14 | 2002-01-08 | Korea Advanced Institute Science Technology | Method for producing hybrid driveshaft |
DE19900449C2 (de) * | 1999-01-08 | 2003-01-23 | Daimler Chrysler Ag | Antriebswelle |
JP3420754B2 (ja) * | 2000-10-10 | 2003-06-30 | 株式会社豊田自動織機 | プロペラシャフト |
US6932118B2 (en) * | 2002-09-24 | 2005-08-23 | The Boeing Company | Low chamfer angled torque tube end fitting metal |
-
2003
- 2003-04-18 CA CA2481730A patent/CA2481730C/en not_active Expired - Lifetime
- 2003-04-18 WO PCT/US2003/012423 patent/WO2003089145A2/en not_active Application Discontinuation
- 2003-04-18 AU AU2003223688A patent/AU2003223688A1/en not_active Abandoned
- 2003-04-18 BR BR0309371-9A patent/BR0309371A/pt not_active Application Discontinuation
- 2003-04-18 US US10/511,658 patent/US7335108B2/en not_active Expired - Lifetime
- 2003-04-18 DE DE60333912T patent/DE60333912D1/de not_active Expired - Lifetime
- 2003-04-18 EP EP03719885A patent/EP1499554B1/en not_active Expired - Lifetime
- 2003-04-18 DE DE03719885T patent/DE03719885T1/de active Pending
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 |