MX172931B - Metodo para unir disposiciones de fibra de ceramica a substratos metalicos - Google Patents
Metodo para unir disposiciones de fibra de ceramica a substratos metalicosInfo
- Publication number
- MX172931B MX172931B MX018819A MX1881989A MX172931B MX 172931 B MX172931 B MX 172931B MX 018819 A MX018819 A MX 018819A MX 1881989 A MX1881989 A MX 1881989A MX 172931 B MX172931 B MX 172931B
- Authority
- MX
- Mexico
- Prior art keywords
- ceramic fiber
- metal substrates
- fiber arrangements
- joining ceramic
- fibrous
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B37/00—Joining burned ceramic articles with other burned ceramic articles or other articles by heating
- C04B37/02—Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K1/00—Soldering, e.g. brazing, or unsoldering
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/02—Layer formed of wires, e.g. mesh
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
- B32B5/024—Woven fabric
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B37/00—Joining burned ceramic articles with other burned ceramic articles or other articles by heating
- C04B37/02—Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles
- C04B37/023—Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles characterised by the interlayer used
- C04B37/026—Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles characterised by the interlayer used consisting of metals or metal salts
-
- 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
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/24—Brasses; Bushes; Linings with different areas of the sliding surface consisting of different materials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/105—Ceramic fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/514—Oriented
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/02—Aspects relating to interlayers, e.g. used to join ceramic articles with other articles by heating
- C04B2237/12—Metallic interlayers
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/38—Fiber or whisker reinforced
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/40—Metallic
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/50—Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
- C04B2237/59—Aspects relating to the structure of the interlayer
- C04B2237/592—Aspects relating to the structure of the interlayer whereby the interlayer is not continuous, e.g. not the whole surface of the smallest substrate is covered by the interlayer
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Textile Engineering (AREA)
- Ceramic Products (AREA)
- Woven Fabrics (AREA)
- Laminated Bodies (AREA)
Abstract
La presente invención se refiere a un método para unir un cuerpo de cerámica fibroso a un substrato metálico que comprende: el tejido de una plurelidad de alambres a través del cuerpo fibroso con por lo menos una porción de alambres tejidos estando expuestos en una cara del cuerpo fibroso, y soldado las porciones de alambre expuestas al substrato metálico.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/286,836 US5115962A (en) | 1988-12-20 | 1988-12-20 | Method of attaching ceramic fiber arrays to metallic substrates |
Publications (1)
Publication Number | Publication Date |
---|---|
MX172931B true MX172931B (es) | 1994-01-24 |
Family
ID=23100377
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MX018819A MX172931B (es) | 1988-12-20 | 1989-12-20 | Metodo para unir disposiciones de fibra de ceramica a substratos metalicos |
Country Status (10)
Country | Link |
---|---|
US (1) | US5115962A (es) |
EP (1) | EP0375589B1 (es) |
JP (1) | JP2866411B2 (es) |
KR (1) | KR930012003B1 (es) |
CN (1) | CN1020081C (es) |
AU (1) | AU623954B2 (es) |
BR (1) | BR8906564A (es) |
DE (2) | DE375589T1 (es) |
IL (1) | IL92610A0 (es) |
MX (1) | MX172931B (es) |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2692255B1 (fr) * | 1992-06-11 | 1994-11-04 | Snecma | Procédé d'assemblage d'au moins deux pièces réalisées dans un matériau composite comprenant une matrice céramique ou vitrocéramique renforcée par des fibres céramiques. |
JP3813654B2 (ja) * | 1995-02-09 | 2006-08-23 | 日本碍子株式会社 | セラミックスの接合構造およびその製造方法 |
US5674585A (en) * | 1995-11-15 | 1997-10-07 | United Technologies Corporation | Composite thermal insulation structure |
US5862975A (en) * | 1996-03-20 | 1999-01-26 | The Boeing Company | Composite/metal structural joint with welded Z-pins |
US6748791B1 (en) | 1996-10-18 | 2004-06-15 | The Boeing Company | Damage detection device and method |
WO2000057738A2 (en) * | 1999-03-29 | 2000-10-05 | N.V. Bekaert S.A. | Heat-resistant garment |
DE10319852B3 (de) * | 2003-05-03 | 2004-12-09 | Daimlerchrysler Ag | Verbundmaterial und Verfahren zur Herstellung von Verbundmaterial |
FR2886180B1 (fr) * | 2005-05-27 | 2007-07-13 | Snecma Moteurs Sa | Procede de fabrication d'une nappe liee constituee de fils ceramiques a matrice metallique, dispositif de mise en oeuvre du procede nappe liee obtenue par le procede |
US7802799B1 (en) | 2006-09-18 | 2010-09-28 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Method of joining metallic and composite components |
US20100021716A1 (en) * | 2007-06-19 | 2010-01-28 | Strock Christopher W | Thermal barrier system and bonding method |
US7887929B2 (en) * | 2007-08-28 | 2011-02-15 | United Technologies Corporation | Oriented fiber ceramic matrix composite abradable thermal barrier coating |
DE102010025618A1 (de) * | 2010-06-30 | 2012-01-05 | Daimler Ag | Verbindungsanordnung und Verfahren zu deren Herstellung |
FR2965202B1 (fr) | 2010-09-28 | 2012-10-12 | Snecma | Procede de fabrication d'une piece et piece massive composite obtenue par ce procede |
FR2966801B1 (fr) * | 2010-10-29 | 2012-11-02 | Aircelle Sa | Structure de bord d'attaque notamment pour entree d'air de nacelle de moteur d'aeronef |
CN104228185A (zh) * | 2014-07-16 | 2014-12-24 | 华南理工大学 | 一种在金属表面牢固复合长纤维丝材的方法 |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2531782A (en) * | 1947-04-21 | 1950-11-28 | Emmett L Moore | Friction assembly and method of making the same |
GB1310355A (en) * | 1969-07-03 | 1973-03-21 | Foseco Trading Ag | Fibre containing compositions |
US4075364A (en) * | 1976-04-15 | 1978-02-21 | Brunswick Corporation | Porous ceramic seals and method of making same |
US4338380A (en) * | 1976-04-05 | 1982-07-06 | Brunswick Corporation | Method of attaching ceramics to metals for high temperature operation and laminated composite |
US4120641A (en) * | 1977-03-02 | 1978-10-17 | The Carborundum Company | Ceramic fiber module attachment system |
DE3622781A1 (de) * | 1986-07-07 | 1988-01-28 | Alfred Buck | Mehrschicht-system |
-
1988
- 1988-12-20 US US07/286,836 patent/US5115962A/en not_active Expired - Lifetime
-
1989
- 1989-12-07 AU AU46018/89A patent/AU623954B2/en not_active Ceased
- 1989-12-08 IL IL92610A patent/IL92610A0/xx not_active IP Right Cessation
- 1989-12-14 DE DE198989630220T patent/DE375589T1/de active Pending
- 1989-12-14 DE DE68913172T patent/DE68913172T2/de not_active Expired - Lifetime
- 1989-12-14 EP EP89630220A patent/EP0375589B1/en not_active Expired - Lifetime
- 1989-12-19 BR BR898906564A patent/BR8906564A/pt not_active IP Right Cessation
- 1989-12-19 KR KR1019890019119A patent/KR930012003B1/ko not_active IP Right Cessation
- 1989-12-20 MX MX018819A patent/MX172931B/es unknown
- 1989-12-20 JP JP1330963A patent/JP2866411B2/ja not_active Expired - Fee Related
- 1989-12-20 CN CN89109404A patent/CN1020081C/zh not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US5115962A (en) | 1992-05-26 |
DE375589T1 (de) | 1990-10-18 |
CN1020081C (zh) | 1993-03-17 |
AU4601889A (en) | 1990-06-28 |
AU623954B2 (en) | 1992-05-28 |
BR8906564A (pt) | 1990-09-04 |
CN1043664A (zh) | 1990-07-11 |
IL92610A0 (en) | 1990-08-31 |
KR900009506A (ko) | 1990-07-04 |
EP0375589A1 (en) | 1990-06-27 |
JP2866411B2 (ja) | 1999-03-08 |
JPH02217373A (ja) | 1990-08-30 |
EP0375589B1 (en) | 1994-02-16 |
DE68913172D1 (de) | 1994-03-24 |
KR930012003B1 (ko) | 1993-12-23 |
DE68913172T2 (de) | 1994-06-09 |
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