IT8621827A0 - Struttura a filamenti avvolti con anelli di rinforzo a filamenti avvolti per l'uso come trasmissione di coppia. - Google Patents
Struttura a filamenti avvolti con anelli di rinforzo a filamenti avvolti per l'uso come trasmissione di coppia.Info
- Publication number
- IT8621827A0 IT8621827A0 IT8621827A IT2182786A IT8621827A0 IT 8621827 A0 IT8621827 A0 IT 8621827A0 IT 8621827 A IT8621827 A IT 8621827A IT 2182786 A IT2182786 A IT 2182786A IT 8621827 A0 IT8621827 A0 IT 8621827A0
- Authority
- IT
- Italy
- Prior art keywords
- filament wound
- torque transmission
- reinforcement rings
- filament
- wound structure
- Prior art date
Links
- 230000005540 biological transmission Effects 0.000 title 1
- 230000002787 reinforcement Effects 0.000 title 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
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/56—Winding and joining, e.g. winding spirally
- B29C53/564—Winding and joining, e.g. winding spirally for making non-tubular articles
-
- 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
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/56—Winding and joining, e.g. winding spirally
- B29C53/58—Winding and joining, e.g. winding spirally helically
- B29C53/60—Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels
- B29C53/602—Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels for tubular articles having closed or nearly closed ends, e.g. vessels, tanks, containers
-
- 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
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
- B29C70/347—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation combined with compressing after the winding of lay-ups having a non-circular cross-section, e.g. flat spiral windings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
-
- 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
- F16D3/00—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive
- F16D3/50—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members
- F16D3/72—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members with axially-spaced attachments to the coupling parts
- F16D3/725—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members with axially-spaced attachments to the coupling parts with an intermediate member made of fibre-reinforced resin
-
- 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
- B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
-
- 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
- F16D3/00—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive
- F16D3/50—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members
- F16D3/72—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members with axially-spaced attachments to the coupling parts
- F16D3/74—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members with axially-spaced attachments to the coupling parts the intermediate member or members being made of rubber or other rubber-like flexible material
- F16D2003/745—Tyre type coupling, i.e. bellows with only one fold
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/902—High modulus filament or fiber
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/21—Circular sheet or circular blank
- Y10T428/218—Aperture containing
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24273—Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
- Y10T428/24322—Composite web or sheet
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/30—Self-sustaining carbon mass or layer with impregnant or other layer
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/31504—Composite [nonstructural laminate]
- Y10T428/31551—Of polyamidoester [polyurethane, polyisocyanate, polycarbamate, etc.]
- Y10T428/31616—Next to polyester [e.g., alkyd]
- Y10T428/3162—Cross-linked polyester [e.g., glycerol maleate-styrene, etc.]
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- General Engineering & Computer Science (AREA)
- Moulding By Coating Moulds (AREA)
- Laminated Bodies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/781,605 US4629644A (en) | 1985-09-30 | 1985-09-30 | Filament wound structure having filament wound reinforcing rings for use as a torque drive |
Publications (3)
Publication Number | Publication Date |
---|---|
IT8621827A0 true IT8621827A0 (it) | 1986-09-26 |
IT8621827A1 IT8621827A1 (it) | 1988-03-26 |
IT1197288B IT1197288B (it) | 1988-11-30 |
Family
ID=25123309
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT2182786A IT1197288B (it) | 1985-09-30 | 1986-09-26 | Struttura a filamenti avvolti con anelli di rinforzo a filamenti avvolti per l'uso come trasmissione di coppia |
Country Status (6)
Country | Link |
---|---|
US (1) | US4629644A (it) |
JP (1) | JPH0655456B2 (it) |
DE (1) | DE3629758C2 (it) |
FR (1) | FR2587938B1 (it) |
GB (1) | GB2181107B (it) |
IT (1) | IT1197288B (it) |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4877375A (en) * | 1986-09-30 | 1989-10-31 | The Boeing Company | Drive shaft and rotor hub for helicopter flexible rotor system |
US5405560A (en) * | 1987-06-18 | 1995-04-11 | Societe Nationale Industrielle Et Aerospatiale | Process for the production of a part, particularly a carbon-carbon brake disk and to the part obtained |
US4804315A (en) * | 1987-07-30 | 1989-02-14 | United Technologies Corporation | Composite helicopter swashplate |
US5071319A (en) * | 1987-09-30 | 1991-12-10 | The Boeing Company | Low maintenance, advanced technology swashplate |
US4968286A (en) * | 1988-03-03 | 1990-11-06 | Lord Corporation | Composite coupling having hubs connectable to drive and driven members |
US4888236A (en) * | 1988-04-18 | 1989-12-19 | O & S Manufacturing Company | Torque rod of composite material |
IT1240178B (it) * | 1990-04-06 | 1993-11-27 | Agusta Spa | Rotore principale per elicotteri |
US5452625A (en) * | 1993-09-29 | 1995-09-26 | United Technologies Corporation | Energy storage flywheel device |
US5620305A (en) * | 1995-03-20 | 1997-04-15 | The Boeing Company | Hub for rotary wing aircraft |
US6365257B1 (en) | 1999-04-14 | 2002-04-02 | Bp Corporation North America Inc. | Chordal preforms for fiber-reinforced articles and method for the production thereof |
US20030186038A1 (en) * | 1999-11-18 | 2003-10-02 | Ashton Larry J. | Multi orientation composite material impregnated with non-liquid resin |
PT1261472E (pt) | 2000-02-22 | 2006-05-31 | Soplar Sa | Dispositivo e processo para a fabricacao de corpos ocos de material plastico |
AU2001228248A1 (en) * | 2000-03-03 | 2001-09-12 | Proteus Gmbh | Component consisting of a fibre-reinforced synthetic material and a method for producing same |
US7309166B2 (en) * | 2005-09-30 | 2007-12-18 | The Boeing Company | Hub joint for transferring load from a rotating shaft to a stationary body |
DE102014004994B3 (de) * | 2014-04-02 | 2015-07-23 | Airbus Ds Gmbh | Chopperscheibe sowie Vorrichtung und Verfahren zu deren Herstellung |
DE102014219046A1 (de) * | 2014-09-22 | 2016-03-24 | Mahle International Gmbh | Lüfterrad |
CN113795693A (zh) | 2019-06-04 | 2021-12-14 | 基耐迪科尔解决方案有限责任公司 | 飞轮储能装置 |
DE102021103917A1 (de) | 2021-02-18 | 2022-08-18 | Connova Deutschland GmbH | Hybridscheibenrad mit wickelfadenbedecktem Faserverbundwickelkern und Herstellverfahren für Hybridscheibenrad |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1525341A1 (de) * | 1966-03-07 | 1969-07-10 | Colmant Cuvelier | Flexible Kupplung fuer die UEbertragung von Bewegungen zwischen zwei Wellen |
DE2648343C3 (de) * | 1976-10-26 | 1981-06-19 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Schlag- und schwenkgelenkloser Rotor für Drehflügelflugzeuge |
US4168194A (en) * | 1977-08-12 | 1979-09-18 | Sea Log Corporation | Method for production of fiber reinforced resin structures |
DE3026104A1 (de) * | 1980-07-10 | 1982-02-04 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Rotor eines drehfluegelflugzeuges |
US4156583A (en) * | 1977-07-11 | 1979-05-29 | Kaman Aerospace Corporation | Hub assembly |
FR2433003A1 (fr) * | 1978-08-08 | 1980-03-07 | Commissariat Energie Atomique | Procede de fabrication d'un materiau renforce par une structure textile tridimensionnelle |
US4323332A (en) * | 1979-12-21 | 1982-04-06 | United Technologies Corporation | Hingeless helicopter rotor with elastic gimbal hub |
US4305903A (en) * | 1980-02-25 | 1981-12-15 | Norris Industries, Inc. | Composite fiber reinforced member and method |
US4341840A (en) * | 1981-03-13 | 1982-07-27 | United Technologies Corporation | Composite bearings, seals and brakes |
US4451528A (en) * | 1981-03-30 | 1984-05-29 | Ni Industries, Inc. | Composite fiber reinforced member and method |
US4455123A (en) * | 1982-06-01 | 1984-06-19 | Westland Plc | Connecting element and helicopter rotor incorporating same |
GB2121844B (en) * | 1982-06-10 | 1985-08-29 | T & N Materials Res Ltd | Met laid flexable sheet materials |
GB2138100B (en) * | 1983-03-18 | 1987-02-11 | Steven Odobasic | Laminated tubular link |
US4545837A (en) * | 1983-05-31 | 1985-10-08 | United Technologies Corporation | Molded-in composite bushings |
-
1985
- 1985-09-30 US US06/781,605 patent/US4629644A/en not_active Expired - Fee Related
-
1986
- 1986-09-01 DE DE19863629758 patent/DE3629758C2/de not_active Expired - Fee Related
- 1986-09-02 GB GB8621191A patent/GB2181107B/en not_active Expired
- 1986-09-26 IT IT2182786A patent/IT1197288B/it active
- 1986-09-30 FR FR8613609A patent/FR2587938B1/fr not_active Expired - Fee Related
- 1986-09-30 JP JP23312986A patent/JPH0655456B2/ja not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
GB2181107B (en) | 1989-09-06 |
GB8621191D0 (en) | 1986-10-08 |
US4629644A (en) | 1986-12-16 |
DE3629758C2 (de) | 1995-07-20 |
FR2587938A1 (fr) | 1987-04-03 |
FR2587938B1 (fr) | 1994-05-13 |
DE3629758A1 (de) | 1987-04-09 |
JPS6292834A (ja) | 1987-04-28 |
GB2181107A (en) | 1987-04-15 |
IT8621827A1 (it) | 1988-03-26 |
IT1197288B (it) | 1988-11-30 |
JPH0655456B2 (ja) | 1994-07-27 |
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