WO2003024662A1 - Method for controlling composite preform elements during processing - Google Patents
Method for controlling composite preform elements during processing Download PDFInfo
- Publication number
- WO2003024662A1 WO2003024662A1 PCT/US2002/030121 US0230121W WO03024662A1 WO 2003024662 A1 WO2003024662 A1 WO 2003024662A1 US 0230121 W US0230121 W US 0230121W WO 03024662 A1 WO03024662 A1 WO 03024662A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- assembly
- metal
- wire
- retaining wire
- mandrel
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P17/00—Metal-working operations, not covered by a single other subclass or another group in this subclass
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
- C22C47/20—Making alloys containing metallic or non-metallic fibres or filaments by subjecting to pressure and heat an assembly comprising at least one metal layer or sheet and one layer of fibres or filaments
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
- C22C47/02—Pretreatment of the fibres or filaments
- C22C47/06—Pretreatment of the fibres or filaments by forming the fibres or filaments into a preformed structure, e.g. using a temporary binder to form a mat-like element
- C22C47/062—Pretreatment of the fibres or filaments by forming the fibres or filaments into a preformed structure, e.g. using a temporary binder to form a mat-like element from wires or filaments only
- C22C47/064—Winding wires
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49801—Shaping fiber or fibered material
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/4981—Utilizing transitory attached element or associated separate material
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
Definitions
- the present invention relates to composite preforms used in the formation
- Composite preforms such as those used in the formation of continuous
- fiber/metal matrix composites are composed of an assembly of mono-filament
- a pre-preg sheet In the case of a rod, a pre-preg sheet
- This sheet is then rolled up onto a cylindrical
- Such processing is composed of either steel or titanium metal, neither of which
- the assembly of fibers and metal on the mandrel or substrate is
- the ends of the clamping wire may be fixed
- clamping wire overwrap is
- the spacing between the clamping wires can be
- clamping wire overwrap may be tensioned during winding, for example, to
- Figure 1 is a block diagram of a typical process flow for the formation of
- continuous fiber/metal matrix composites made up of an assembly of fibers
- Figure 2 is a side elevational view, partly in section, of a metal wire/fiber
- Figure 3 is a side elevational view similar to Figure 2 wherein the
- clamping wire is spirally wrapped over the metal wire/fiber assembly prior to
- Figure 4 is a side elevational view, partly in section, of a metal fiber pre-
- Figure 5 is a side elevational view similar to Figure 4 showing the
- Fig. 1 illustrates in block form a typical process flow for the formation of
- continuous fiber/metal matrix composites made up of an assembly of
- monofilament fibers and a matrix metal in the form of foil, powder or wire.
- the mandrel is prepared for winding. Thereafter, the fiber and metal
- Fig. 2 illustrates the method step in block 4 in Fig. 1 for a ring component
- the rolled assembly comprises a selected or
- metal wire in any desired orientation.
- the metal can be in the form of
- a foil or powder and the rolled assembly can include layers of adhesive to hold
- FIG. 3 illustrates the wire overwrap of the present invention applied to the
- a metal retaining wire 22 formed of a high temperature resistant metal is
- wire/fiber assembly to hold the wires and fibers in their desired positions during
- retaining wire 22 may be formed of titanium, molybdenum, tungsten, rhenium
- substrate 16 or are otherwise secured thereto in any suitable manner.
- the wire overwrap would be wound tight to itself
- retaining wires 22 can be spaced apart typically 20 to 50 wires per inch for the metal foil/fiber assembly the spacing between the retaining wires 22 could be
- Fig. 4 illustrates the method step in block 4 in Fig. 1 for a rod component
- a metal/fiber pre-preg sheet 30 is rolled up in a desired number of
- the pre-preg sheet 30 comprises a layer of fibers and a
- metal matrix layer may be in the form of wires, foil or powder.
- Fig. 5 is a view similar to Fig. 4 which illustrates the metal retaining wire
- the mandrel 32 in any suitable manner (not shown).
- the metal wire overwrap could be tensioned during winding to
- the metal overwrap of the present invention serves to
- present invention is simple in construction, inexpensive and easy to apply over
Landscapes
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Engineering & Computer Science (AREA)
- Organic Chemistry (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Crystallography & Structural Chemistry (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Laminated Bodies (AREA)
- Wire Processing (AREA)
- Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
- Furan Compounds (AREA)
- Saccharide Compounds (AREA)
Abstract
Description
Claims
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020047004131A KR100972409B1 (en) | 2001-09-21 | 2002-09-23 | Method for controlling composite preform elements during processing |
AT02780338T ATE435311T1 (en) | 2001-09-21 | 2002-09-23 | METHOD FOR CONTROLLING COMPOSITE PREFORM ELEMENTS DURING MACHINING |
JP2003528350A JP4452500B2 (en) | 2001-09-21 | 2002-09-23 | Method for controlling composite preform components during formation of a fiber / metal matrix composite |
DE60232806T DE60232806D1 (en) | 2001-09-21 | 2002-09-23 | METHOD FOR CONTROLLING COMPOSITE FORMULAS IN PROCESSING |
EP02780338A EP1438155B1 (en) | 2001-09-21 | 2002-09-23 | Method for controlling composite preform elements during processing |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/957,630 US6568061B2 (en) | 2001-09-21 | 2001-09-21 | Method for controlling composite preform elements during processing |
US09/957,630 | 2001-09-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2003024662A1 true WO2003024662A1 (en) | 2003-03-27 |
Family
ID=25499881
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2002/030121 WO2003024662A1 (en) | 2001-09-21 | 2002-09-23 | Method for controlling composite preform elements during processing |
Country Status (9)
Country | Link |
---|---|
US (1) | US6568061B2 (en) |
EP (1) | EP1438155B1 (en) |
JP (1) | JP4452500B2 (en) |
KR (1) | KR100972409B1 (en) |
CN (1) | CN1302893C (en) |
AT (1) | ATE435311T1 (en) |
DE (1) | DE60232806D1 (en) |
ES (1) | ES2331989T3 (en) |
WO (1) | WO2003024662A1 (en) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20040018237A1 (en) * | 2002-05-31 | 2004-01-29 | Perricone Nicholas V. | Topical drug delivery using phosphatidylcholine |
US7118063B2 (en) * | 2004-07-29 | 2006-10-10 | Sequa Corporation | Wire/fiber ring and method for manufacturing the same |
US7842375B2 (en) * | 2005-05-17 | 2010-11-30 | Rolls-Royce Corporation | Fiber retention system for metal matrix composite preform |
FR2911524B1 (en) * | 2007-01-23 | 2009-08-21 | Snecma Sa | TUBULAR PIECE COMPRISING A METALLIC MATRIX COMPOSITE INSERT. |
FR2950078B1 (en) * | 2009-09-11 | 2012-10-05 | Messier Dowty Sa | METAL PIECE PROVIDED WITH FIBROUS REINFORCEMENTS WITH BITEAUTEE END. |
CN101825218B (en) * | 2010-04-27 | 2013-07-10 | 济南大学 | Production method of double metal network-interpenetrated multiphase section |
US8871256B2 (en) | 2012-09-19 | 2014-10-28 | Transdermal Biotechnology, Inc. | Methods and systems for treatment of inflammatory diseases with nitric oxide |
US8871259B2 (en) | 2012-09-19 | 2014-10-28 | Transdermal Biotechnology, Inc. | Techniques and systems for treatment of neuropathic pain and other indications |
US8871260B2 (en) | 2012-09-19 | 2014-10-28 | Transdermal Biotechnology, Inc. | Methods and compositions for muscular and neuromuscular diseases |
US9849160B2 (en) | 2013-03-13 | 2017-12-26 | Transdermal Biotechnology, Inc. | Methods and systems for treating or preventing cancer |
US9314433B2 (en) | 2013-03-13 | 2016-04-19 | Transdermal Biotechnology, Inc. | Methods and systems for treating or preventing cancer |
US9295647B2 (en) | 2013-03-13 | 2016-03-29 | Transdermal Biotechnology, Inc. | Systems and methods for delivery of peptides |
US9314417B2 (en) | 2013-03-13 | 2016-04-19 | Transdermal Biotechnology, Inc. | Treatment of skin, including aging skin, to improve appearance |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3615277A (en) * | 1969-05-02 | 1971-10-26 | United Aircraft Corp | Method of fabricating fiber-reinforced articles and products produced thereby |
US4562951A (en) * | 1982-04-12 | 1986-01-07 | The United States Of America As Represented By The Secretary Of The Army | Method of making metallic glass-metal matrix composites |
US4761206A (en) * | 1987-02-17 | 1988-08-02 | Norman Forrest | Method for producing large reinforced seamless casings and the product obtained therefrom |
US5104460A (en) * | 1990-12-17 | 1992-04-14 | The United States Of America As Represented By The Secretary Of The Air Force | Method to manufacture titanium aluminide matrix composites |
US5440806A (en) * | 1992-03-13 | 1995-08-15 | Mtu Motoren- Und Turbinen-Union Muenchen Gmbh | Method of making blank for the manufacturing of fiber-reinforced coatings or metal components |
US5454403A (en) * | 1993-02-03 | 1995-10-03 | The United States Of America As Represented By The Secrtary Of The Air Force | Weaving method for continuous fiber composites |
US5763079A (en) * | 1995-05-23 | 1998-06-09 | Atlantic Research Corporation | Wire preforms for composite material manufacture and methods of making |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3606667A (en) * | 1968-09-27 | 1971-09-21 | United Aircraft Corp | Method of fabricating fiber-reinforced articles |
US3596344A (en) * | 1968-09-27 | 1971-08-03 | United Aircraft Corp | Method of fabricating fiber-reinforced articles |
US3571901A (en) * | 1969-06-13 | 1971-03-23 | Union Carbide Corp | Method of fabricating a carbon-fiber reinforced composite article |
US4867644A (en) * | 1987-05-15 | 1989-09-19 | Allied-Signal Inc. | Composite member, unitary rotor member including same, and method of making |
US4919594A (en) * | 1987-05-15 | 1990-04-24 | Allied-Signal Inc. | Composite member, unitary rotor member including same, and method of making |
JPH028333A (en) * | 1988-06-27 | 1990-01-11 | Agency Of Ind Science & Technol | Method for forming fiber-reinforced metal |
CN1023414C (en) * | 1989-10-27 | 1994-01-05 | 合肥工业大学 | Method for making copper-carbon fibre complex material and support electrode in power semiconductor appliances |
US5933703A (en) * | 1991-10-29 | 1999-08-03 | The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland | Process for the preparation of fibre reinforced metal matrix composites and novel preforms therefor |
US5180409A (en) * | 1992-01-30 | 1993-01-19 | Minnesota Mining And Manufacturing Company | Hot-gas-filtering fabric of spaced uncrimped support strands and crimped lofty fill yarns |
CN2217505Y (en) * | 1994-07-30 | 1996-01-17 | 金锋 | Composite bar-section |
IT1289707B1 (en) * | 1996-12-03 | 1998-10-16 | Fiatavio Spa | METHOD AND MACHINE FOR THE REALIZATION OF A CONTINUOUS WIRE DISC ELEMENT AND DISC ELEMENT MADE WITH THIS METHOD. |
-
2001
- 2001-09-21 US US09/957,630 patent/US6568061B2/en not_active Expired - Fee Related
-
2002
- 2002-09-23 DE DE60232806T patent/DE60232806D1/en not_active Expired - Lifetime
- 2002-09-23 ES ES02780338T patent/ES2331989T3/en not_active Expired - Lifetime
- 2002-09-23 EP EP02780338A patent/EP1438155B1/en not_active Expired - Lifetime
- 2002-09-23 CN CNB028184823A patent/CN1302893C/en not_active Expired - Fee Related
- 2002-09-23 WO PCT/US2002/030121 patent/WO2003024662A1/en active Application Filing
- 2002-09-23 AT AT02780338T patent/ATE435311T1/en not_active IP Right Cessation
- 2002-09-23 JP JP2003528350A patent/JP4452500B2/en not_active Expired - Fee Related
- 2002-09-23 KR KR1020047004131A patent/KR100972409B1/en not_active IP Right Cessation
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3615277A (en) * | 1969-05-02 | 1971-10-26 | United Aircraft Corp | Method of fabricating fiber-reinforced articles and products produced thereby |
US4562951A (en) * | 1982-04-12 | 1986-01-07 | The United States Of America As Represented By The Secretary Of The Army | Method of making metallic glass-metal matrix composites |
US4761206A (en) * | 1987-02-17 | 1988-08-02 | Norman Forrest | Method for producing large reinforced seamless casings and the product obtained therefrom |
US5104460A (en) * | 1990-12-17 | 1992-04-14 | The United States Of America As Represented By The Secretary Of The Air Force | Method to manufacture titanium aluminide matrix composites |
US5440806A (en) * | 1992-03-13 | 1995-08-15 | Mtu Motoren- Und Turbinen-Union Muenchen Gmbh | Method of making blank for the manufacturing of fiber-reinforced coatings or metal components |
US5454403A (en) * | 1993-02-03 | 1995-10-03 | The United States Of America As Represented By The Secrtary Of The Air Force | Weaving method for continuous fiber composites |
US5763079A (en) * | 1995-05-23 | 1998-06-09 | Atlantic Research Corporation | Wire preforms for composite material manufacture and methods of making |
Also Published As
Publication number | Publication date |
---|---|
CN1302893C (en) | 2007-03-07 |
DE60232806D1 (en) | 2009-08-13 |
JP4452500B2 (en) | 2010-04-21 |
EP1438155A4 (en) | 2006-03-15 |
KR20040035856A (en) | 2004-04-29 |
KR100972409B1 (en) | 2010-07-26 |
CN1556739A (en) | 2004-12-22 |
US6568061B2 (en) | 2003-05-27 |
JP2005523379A (en) | 2005-08-04 |
EP1438155B1 (en) | 2009-07-01 |
ES2331989T3 (en) | 2010-01-22 |
EP1438155A1 (en) | 2004-07-21 |
ATE435311T1 (en) | 2009-07-15 |
US20030056355A1 (en) | 2003-03-27 |
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