专利摘要:
Disclosed are manufacturing systems (100) and methods configured to facilitate the manufacture of composite articles (e.g., ceramic composite articles), particularly hollow article composite articles. The manufacturing system (100) includes a consumable core (130) for placement within an interior portion of a composite precursor, wherein the consumable core (130) is configured to transform into an infiltrant during a manufacturing process and to infiltrate the composite precursor (140).
公开号:CH706865B1
申请号:CH01394/13
申请日:2013-08-14
公开日:2017-08-31
发明作者:Curtis Taxacher Glenn;De Diego Peter;Edward Gray Paul;Harold Monaghan Phillip
申请人:Gen Electric;
IPC主号:
专利说明:

Description [0001] This invention has been made with the assistance of the US government.
Background of the Invention The invention disclosed herein relates to manufacturing systems for producing consumable-core composite articles and related methods.
Current methods of fabricating ceramic composite articles (e.g., melt infiltration processes) involve the use of a liquid phase infiltrating material (e.g., silicon, silicon alloys, etc.) which is incorporated into a volumetric material / composite precursor to form a composite article. During fabrication, this infiltrant material is taken up on the exposed surfaces of the composite precursor and penetrates into the composite precursor by wicking to form the composite article. In the fabrication of voided composite articles, the typical process is to introduce a removable core into the interior portions of the hollow composite precursor to form the cavity. Subsequently, the core is taken out exposing internal surfaces of the composite precursor. Removal of the core must occur prior to melt infiltration to prevent the infiltrant from reacting with the core, bonding it to the composite article, and preventing core removal. Some manufacturing methods include removable cores that are configured to be melted or burned out in a separate process subsequent to the formation of the composite article. Some other manufacturers construct composite articles that have constructive holes large enough to pull the removable cores out of the interior of the article. These methods may limit the design or performance of the article, require additional steps in the manufacturing process, and / or expose components and parts of the composite article to temperature extremes that may damage or destroy the article.
Brief Description of the Invention The present invention relates to a method and manufacturing system suitable for facilitating the manufacture of composite articles.
The invention provides a manufacturing system comprising a consumable core for placement in an interior portion of a composite precursor, wherein the consumable core may transform into an infiltrant during a manufacturing process and penetrate the composite precursor.
Particularly advantageous and preferred embodiments of the inventive manufacturing system have one or more of the following features:
The manufacturing system may include an external supply connected to the consumable core via a wick to promote infiltrant flow to the composite precursor.
The consumable core is preferably configured to debris free from melt infiltration into the composite precursor during the manufacturing process to substantially free the interior portion of the composite precursor during the manufacturing process.
The consumable core may comprise a casting material.
The consumable core may comprise at least one of silicon and / or boron.
The manufacturing system may further include an external block disposed proximate the composite precursor for delivering infiltrant material to the composite precursor.
[0006] According to another embodiment, the manufacturing system may further comprise: a composite precursor, wherein within an interior portion of the composite precursor is disposed the consumable core configured to transform into an infiltrant during a manufacturing process and to penetrate the composite precursor; and an external feeder connected to the consumable core via a wick, the external feeder configured to convey an infiltrant flow to the composite precursor.
Particularly advantageous and preferred embodiments of the manufacturing system according to the latter embodiment further comprise one or more of the following features:
The manufacturing system may further comprise an external block disposed substantially in proximity to the composite precursor for supplying additional infiltrant material to the composite precursor to infiltrate it.
Preferably, the composite precursor completely encloses the consumable core.
The manufacturing system may further comprise a collection container connected via a drain to the consumable core, wherein the collection container is configured to receive an infiltrant flow from the consumable core.
The consumable core may be formed of sintered powders and may comprise at least one of silicon and / or boron.
The wick preferably comprises woven carbon fibers.
The composite precursor is preferably porous and carbonated.
The invention also provides a method of making composite articles comprising: inserting a consumable core into a composite precursor; Connecting an external feeder to the composite article fabrication system to supply additional infiltrant material, forming a composite article fabrication system; Setting at least one environmental condition on the composite article fabrication system to infiltrate the composite precursor via the consumable core with a reinforcing material; Consuming the consumable core; and adjusting the environmental condition.
Particularly advantageous and preferred embodiments of the method according to the invention include the embodiments mentioned in connection with the production system according to the invention and in particular comprise one or more of the following features:
The method may further comprise connecting a collection container to the consumable core via a drain, the process configured to receive excess infiltrant material from the consumable core.
Consuming the consumable core may include transitioning (interaling) the consumable core into the composite precursor.
Adjusting the at least one environmental condition includes raising a temperature of the environment and increasing a pressure of the environment.
The consumable core may comprise at least one of the following elements: silicon, boron and / or a refractory material.
The method may further comprise disposing a set of external blocks substantially proximate to the composite precursor, the external blocks configured to promote an infiltrant flow to the composite precursor.
BRIEF DESCRIPTION OF THE DRAWINGS These and other features of this invention will be better understood by the following detailed description of the invention, taken in conjunction with the accompanying drawings, which illustrate various embodiments of the invention, wherein:
Fig. 1 shows a three-dimensional perspective view of a part of a composite article manufacturing system according to an embodiment of the invention.
Fig. 2 shows a three-dimensional perspective view of a composite article according to an embodiment of the invention.
3 shows a three-dimensional perspective view of part of a composite article manufacturing system according to one embodiment of the invention.
4 shows a process flow diagram illustrating a process according to an embodiment of the invention.
It should be noted that the drawings of the disclosure are not necessarily to scale. The drawings are merely intended to depict typical aspects of the disclosure and are therefore not to be considered as limiting the scope of the disclosure. It should be understood that elements having like reference numerals in the drawings are substantially similar. Furthermore, in embodiments illustrated and described with reference to the drawings, like reference numerals may represent the same elements. A redundant explanation of these elements has been omitted for the sake of clarity. Finally, it should be understood that the components in the drawings and their corresponding descriptions are applicable to any embodiment described herein.
DETAILED DESCRIPTION OF THE INVENTION As indicated herein, the invention provides manufacturing systems and methods adapted to facilitate the manufacture of composite articles, especially composite hollow articles. These methods and systems utilize a consumable core configured to fit into hollow components of a composite precursor, wherein the consumable core applies an infiltrant material to the interior surfaces of the composite precursor and the core itself is consumed during the manufacturing process.
Cores are often used in the prior art composite article fabrication to form internal surfaces during the manufacture of a composite precursor. In these systems, after molding the composite article, the removable core must be pulled out of the interior of the composite article. Some systems use removable cores that can be melted out or burned out of the composite article by exposure to a heat source; Some other systems require that the composite article itself have a constructive opening large enough to facilitate removal of the removable core. However, these methods may limit the construction or performance of the subject, additional
Require steps in the manufacturing process and / or expose components and parts of the composite article to temperature extremes that can damage or destroy the article.
The present invention provides manufacturing systems and methods that include the use of a consumable core in composite article manufacturing processes. The consumable core comprises precursor infiltrating materials and is configured to apply an infiltrant material to the interior surfaces of a composite hollow precursor product. During fabrication, this consumable core is incorporated into the composite precursor (e.g., by absorption and capillary action), consumes internally in the composite precursor, thereby becoming part of the composite article itself, while at the same time freeing the interior of the hollow constituent. This consumable core simplifies the manufacturing process and eliminates the need for burnouts, flashings, dissolution processes, post-assembly, structural apertures, or other core removal processes as it forms the holes of the composite articles.
With reference to the figures, embodiments of consumable cores are shown for composite articles and composite article fabrication processes in which the consumable cores can simplify manufacturing processes and increase the quality and design flexibility of composite articles. The components in the figures may each be connected by conventional means, e.g. via a common line or other means shown in Figs. 1-4. In particular, referring to FIG. 1, there is shown a three-dimensional perspective view of a composite article manufacturing system 100 that includes a consumable core 130 within a composite precursor 140 (shown in phantom) according to embodiments of the invention. The composite precursor 140 may be a porous carbonated composite precursor which, upon absorption of an infiltrating material (e.g., silicon with minor additions of secondary elements such as boron) may form a composite article 200 (shown in FIG. The consumable core 130 is positioned within the composite precursor 140 and may be connected to an external feed block 110 via a wick 112 (e.g., a permeable belt for conveying a molten mixture). The feedblock 110 may direct additional portions of infiltrant material to the consumable core 130 and may include a silicon ingot formed from solid, pressed and / or sintered particles. The consumable core 130 may also be connected to a drain 122 (e.g., a permeable ribbon for passing a molten mixture) which may include a collection container 120. During the formation of a composite article (e.g., a melt infiltration process), the composite article manufacturing system 100 may be exposed to a cycle of environmental conditions with heat and pressure variations. This cycle causes the infiltrant material (e.g., silicon) to transfer from the feedblock 110 to the consumable core 130, causing the consumable core 130 to be absorbed into the composite precursor. Excess portions of the infiltration material can flow via the outlet 122 into the collecting container 120. Material from the consumable core 130 may be incorporated into the composite precursor 140 by capillary action.
The composite precursor 140 may completely accommodate (e.g., enclose) the consumable core 130. The consumable core 130 may be pressed, cast, or machined from metals, silicon, or any currently known or yet-to-be-developed materials. Preforming may design the consumable core 130 to complement the contours of a hollow feature of the composite precursor 140. A composition of the consumable core 130 may comprise pure silicon or silicon at the same time as alloy materials. The consumable core 130 may include silicon and boron. The consumable core 130 may include sintered particles and comprise about 95% silicon and about 5% boron. The consumable core 130 may have a composition of about 20% boron (B), 20% carbon (C) or 20% refractory (e.g., Ta, Zr, Nb, etc.) and a residual amount of silicon. The consumable core 130 may be poured to a predetermined size and shape prior to internalization in the composite precursor 140. It will be understood that while the consumable core 130 is described herein with reference to certain exemplary compositions and chemical properties, these compositions and chemical properties are merely illustrative, and that any sintered materials, solid cast materials, and currently known or later developed Compositions may be included in the consumable core 130.
During fabrication, the consumable core 130 may consume itself in the composite precursor, thereby forming the composite article 200. The consumable core 130 may be completely consumed (e.g., incorporated into the composite article 200). The consumable core 130 and the feedblock 110 may comprise substantially the same material. The feed block 110 may contain pure silicon, boron, silicon at the same time as alloy materials or any other materials currently known or later to be developed.
The wick 112 and drain 122 may comprise similar materials and compositions, both configured to promote a molten mixture (e.g., molten silicon, boron). The wick 112 and the drain 122 may be interchangeable. The wick 112 and the drain 122 may include inert materials that are woven or braided to form the wick 112 and the drain 122. The wick 112 and drain 122 may include woven or braided carbon fibers.
With reference to FIG. 2, a three-dimensional perspective view of parts of a composite article 200 according to an embodiment of the invention is shown. In this embodiment, the composite article 200 may include a composite body 240 that defines an inner / hollow feature 230 (shown in phantom). The composite body 240 may have a substantially uniform material composition that forms the composite article 200. The inner / hollow feature 230 may be substantially free of the consumable core 130 (shown in FIG. 1) which clears the inner / hollow feature 230 because it is debris free during the melt infiltration process. The composite article 240 may include an upper surface 250 and a lower surface 270 that seal the inner / hollow feature 230.
With reference to FIG. 3, there is shown a three-dimensional perspective view of a composite article manufacturing system 300 having a consumable core 330 inserted within a composite precursor 340 (shown in phantom) according to one embodiment of the invention. In this embodiment, a set of external blocks 380 and 382 are disposed about the composite precursor 340 and configured to apply an infiltrant material to exterior surfaces of the composite precursor 340. The additional infiltrating material blocks 380 and 382 may have a similar composition to the consumable core 330. The use and / or inclusion of additional infiltrating material blocks 380 and 382 may depend on the volume of infiltrating material needed to completely fill the capillaries within the composite precursor 340. The composite precursor 340 is connected to a first external feed block 310 via a wick 312 and to a second external feed block 314 via a wick 316. During the manufacturing process (eg, a melt infiltration process), the composite article manufacturing system 300 may be exposed to a high temperature causing the infiltrant material (eg, a matrix) to be conveyed via the consumable core 330, external feedblock 310, external feedblock 314, external Feed block 380 and / or external feed block 382 is introduced into the composite precursor 340 (eg volumetric material). As can be seen in FIG. 3, the consumable core 330 and the composite precursor 340 can be formed to produce any shape of composite article, including complex geometries, airfoils, turbine blades, etc. The infiltrant material can be converted into the composite precursor as needed and as desired any / any of the external block 380, the external block 382, the external feed block 310, the external feed block 314, and the consumable core 330, to ensure that the infiltrant material surrounds all the fibers of the composite precursor 340 and all interstices in a ceramic composite crowded.
Referring to FIG. 4, an illustrative process flow diagram according to one embodiment of the invention is shown. In the initial process P1 (shown in phantom), the consumable core 130 is disposed within the composite precursor 140. The consumable core 130 may be taken up (internalized) within the composite precursor 140, being completely enclosed by the composite precursor. This may be done by technicians and / or machines according to a scheduled or user-initiated manufacturing process. For example, in assembling the composite precursor 140, the consumable core 130 may be inserted into the composite precursor 140 while the remaining portions of the composite precursor 140 are formed after insertion to substantially sealingly enclose the consumable core 130 therein. Following process P1, in process P2, an external feedblock 110 is connected to the consumable core 130 via a wick 112. Following process P2, in process P3, the consumable core 130 is connected via a drain 122 to a collection container 120, thereby forming a composite article manufacturing system 100. Subsequent to the process P3, in the process P4, the composite article fabrication system 100 is subjected to a series of environmental conditions settings (eg, a melt infiltration process, elevated temperature, elevated pressure, etc.) causing the consumable core 130 to transform into an infiltrant material and begins to infiltrate portions of the composite precursor 140. Subsequent to the process P4, in the process P5, the consumable core 130 is consumed during the melt infiltration process and thereby incorporated into the composite precursor 140 to clear the inner / hollow feature 230 and form the composite article 200. Following the process P5, in the process P6, the environmental conditions around the composite article manufacturing system 100 are readjusted to the environment, and the wick 112 and the process thereof are separated from the composite article 200.
The dataflow diagram and block diagrams in the figures illustrate the architecture, functionality, and operation of systems, methods, and computer program products according to various embodiments of the present invention. In this regard, each block in the flowchart or block diagrams may be a module, segment, or part of a Represent codes that include one or more executable instructions for performing the predetermined logical function (s). It should be noted that in some alternative embodiments, the functions specified in the block may occur in a different order than indicated in the figures. For example, two blocks shown in succession may in fact be executed substantially simultaneously, or the blocks may sometimes be executed in reverse order, depending on the functionality involved. It is also noted that each block of the block diagrams and / or the flowchart representation and combinations of blocks in the block diagrams and / or the flowchart representation by special hardware-based systems that perform the predetermined functions or activities, or combinations of special hardware and special computer instructions can be realized.
The consumable cores, systems, and methods of the present disclosure are not limited to any particular composite material, composite article, process, or other system, and may be used with other manufacturing processes and / or systems. The consumable cores and systems of the present invention may also be used in conjunction with other systems not described herein
权利要求:
Claims (10)
[1]
and that can benefit from the self-consumption, finishing and manufacturing benefits described here. This written description uses examples to disclose the invention, including the best mode, and also to enable one skilled in the art to practice the invention, also for the purpose of making any devices or systems and carrying out any methods incorporated therein. The patentable scope of the invention is defined by the claims. Disclosed are manufacturing systems and methods configured to facilitate the manufacture of composite articles (e.g., ceramic composite articles), particularly composite articles having hollow constituents. The manufacturing system includes a consumable core for placement within an interior portion of a composite precursor, wherein the consumable core is configured to transform into an infiltrant during a manufacturing process and to infiltrate the composite precursor. REFERENCE NUMBER LIST 100, 300 composite object fabrication system 110 external feedblock 112,312,316 wick 120 reservoirs 122 effluent 130,330 consumable core 140,340 composite precursor 200 composite article 230 interior / hollow feature 240 composite 250 top surface 270 bottom surface 310 first external feedblock 314 second external feedblock 380, 382 Set of external blocks claims
A composite article manufacturing system (100, 300, 300) comprising: a consumable core (130, 230, 330) for placement within an interior portion of a composite precursor (140, 240, 340), the consumable core (130, 230 330) is configured to transform into an infiltrant during a manufacturing process and to infiltrate the composite precursor (140, 240, 340).
[2]
The manufacturing system (100, 200, 300) of claim 1, further comprising an external supply (110, 310, 314) connected via a wick (112, 313, 316) to the consumable core (130, 230, 303) to direct infiltration material flow to the Composite precursor (140, 240, 340) to promote.
[3]
The manufacturing system (100, 200, 300) according to claim 1 or 2, wherein the consumable core (130, 230, 303) is configured to debris free from melt infiltration into the composite precursor (140, 240, 340) during the manufacturing process to remove the interior portion of the composite precursor (140 , 240, 340) substantially free.
[4]
4. manufacturing system (100, 200, 300) according to any one of the preceding claims, wherein the consumable core (130, 230, 330) comprises a casting material or is formed from sintered powders.
[5]
The manufacturing system (100, 200, 300) of claim 1, further comprising: a composite precursor (140, 240, 340), wherein the consumable core (130, 230, 330) is disposed within an interior portion of the composite precursor (140, 240, 330). 340) is arranged; and an external feeder (110, 310, 314) connected to the consumable core (130, 230, 330) via a wick (112, 313, 316), wherein the external feeder (110, 310, 314) is arranged to supply an infiltrant flow to the composite precursor (140, 240, 340).
[6]
The manufacturing system (100, 200, 300) of claim 5, further comprising an external block (380, 382) disposed substantially proximate to the composite precursor (140, 240, 340) and configured to supply additional infiltrating material to infiltrate the composite precursor (140, 240, 340).
[7]
The manufacturing system (100, 200, 300) of claim 5 or 6, wherein the composite precursor (140, 240, 340) completely encloses the consumable core (130, 230, 330).
[8]
8. Manufacturing system (100, 200, 300) according to one of claims 5 to 7, further comprising a collecting container (120, 320) connected via a drain (122, 322) with the consumable core (130, 230, 330) wherein the sump (120, 320) is configured to receive an infiltrant flow from the consumable core (130, 230, 330).
[9]
The manufacturing system (100, 200, 300) of any of claims 5 to 7, wherein the composite precursor (140, 240, 340) is porous and carbonated.
[10]
A method of making composite articles, comprising: inserting a consumable core (130, 230, 330) into a composite precursor (140, 240, 340); Connecting an external feeder (110, 310, 314) via a wick (112, 312, 316) to the consumable core (130, 230, 330) to form a composite article manufacturing system (100, 200, 300); Setting at least one environmental condition on the composite article manufacturing system (100, 200, 300) to infiltrate the composite precursor (140, 240, 340) with an infiltrant material from the consumable core (130, 230, 330); Consuming the consumable core (130, 230, 330); and adjusting the environmental condition.
类似技术:
公开号 | 公开日 | 专利标题
CH706865B1|2017-08-31|Consumable core fabrication system for composite fabrication and related process.
DE102005047035B3|2007-04-19|A method of manufacturing a piston for an internal combustion engine and piston produced thereafter
DE3312867A1|1983-11-17|METHOD AND DEVICE FOR PRODUCING A MOLDED METAL OBJECT
DE2813892A1|1978-10-12|POWDER METALLURGICAL PROCESS FOR THE MANUFACTURE OF METAL PARTS FROM METAL POWDER BY ISOSTATIC HOT PRESSING
AT503824B1|2009-07-15|METAL SHAPING BODY AND METHOD FOR THE PRODUCTION THEREOF
DE102009017860A1|2009-12-31|Injection mold and casting method for resin molding
DE102011117317B4|2016-11-03|Forming tool arrangement for microcomponents
DE10053199B4|2008-10-30|Method for producing a metal composite compact
DE102011117316B4|2017-09-07|Forming tool arrangement for microcomponents
DE102011117318B4|2016-06-02|Forming tool arrangement for microcomponents
DE102013007735B4|2015-10-15|Method for producing a castable salt core
EP2945760A1|2015-11-25|Method and casting mold for producing castings, in particular cylinder blocks and cylinder heads, having functional connection of the feeder
DE2046721B2|1976-06-10|PROCESS FOR POWDER METALLURGICAL PRODUCTION OF A MULTI-PART MOLD
DE10243793A1|2003-04-24|Die casting machine and process
DE102011086411A1|2013-05-16|Mold for a piston
DE102015201559A1|2016-08-04|Wet pressing method and pressing tool for this
DE19820246C2|2000-10-12|Cast core
DE102010032107B4|2012-08-02|Casting tool and method for die casting
DE102014207791A1|2015-10-29|Method for investment casting of metallic components
DE2417589A1|1974-10-24|PROCESS AND ARRANGEMENT FOR MANUFACTURING COMPACTED ALLOYED OBJECTS WITH AN INTERNAL PASSAGE
AT521006B1|2021-08-15|Process for manufacturing a component with soft magnetic properties
DE102020129793A1|2021-05-27|Apparatus and method for die casting metal
DE102009024791A1|2010-12-16|Device for producing die casting component, comprises die casting tool, and lost core made of temperature-resistant and decomposition-stable fiber-reinforced thermoplastic and removable from die casting component and/or die casting tool
DE112018001220T5|2019-11-21|A method of forming a powder metal insert having a horizontal through hole
EP3616806A1|2020-03-04|Method for producing a model form core blank, a model form core and an investment casting molds and a casting method for producing a cast piece with a hollow structure
同族专利:
公开号 | 公开日
US20140048978A1|2014-02-20|
CN103588485B|2018-04-10|
CH706865A8|2014-08-15|
DE102013108739A1|2014-02-20|
CH706865A2|2014-02-28|
CN103588485A|2014-02-19|
US9751807B2|2017-09-05|
引用文献:
公开号 | 申请日 | 公开日 | 申请人 | 专利标题

NL7400271A|1973-04-24|1974-10-28|Gen Electric|A method of preparing a silicon composite article, as well as an article so prepared|
US4120731A|1976-02-23|1978-10-17|General Electric Company|Method of making molten silicon infiltration reaction products and products made thereby|
US4220455A|1978-10-24|1980-09-02|General Electric Company|Polycrystalline diamond and/or cubic boron nitride body and process for making said body|
US4238433A|1978-12-15|1980-12-09|General Electric Company|Method of making molten silicon infiltration reaction products|
US4247304A|1978-12-29|1981-01-27|General Electric Company|Process for producing a composite of polycrystalline diamond and/or cubic boron nitride body and substrate phases|
US4242106A|1979-01-02|1980-12-30|General Electric Company|Composite of polycrystalline diamond and/or cubic boron nitride body/silicon carbide substrate|
US5205970A|1992-04-03|1993-04-27|General Electric Company|Method of infiltration forming a silicon carbide body with improved surface finish|
JPH09506328A|1993-12-08|1997-06-24|マサチューセッツ・インスティテュート・オブ・テクノロジー|Casting tool|
US5758405A|1995-04-28|1998-06-02|American Superconductor Corporation|Consumable mandrel for superconducting magnetic coils|
US5795524A|1996-03-29|1998-08-18|Basso, Jr.; Robert J.|Process for producing composite tubular parts|
US6280550B1|1998-12-15|2001-08-28|General Electric Company|Fabrication of composite articles having an infiltrated matrix|
US6274078B1|1999-01-27|2001-08-14|General Electric Company|Method of removing cores from ceramic matrix composite articles|
US7658781B1|1999-07-23|2010-02-09|Marlene Rossing, legal representative|Silicon-containing composite bodies, and methods for making same|
US6749937B2|2002-03-19|2004-06-15|Honeywell International Inc.|Melt-infiltrated pitch-pan preforms|
US7404145B1|2002-03-28|2008-07-22|Emc Corporation|Generic mechanism for reporting on backups|
US20040067316A1|2002-10-04|2004-04-08|Paul Gray|Method for processing silicon-carbide materials using organic film formers|
DE10246851C1|2002-10-08|2003-12-18|Sgl Carbon Ag|Production of components made from a high temperature resistant fiber-reinforced composite ceramic comprises separating strips from neighboring strips in the region outside contact zones using a spacer made from graphite|
DE10257208B4|2002-12-06|2008-02-21|Ivoclar Vivadent Ag|Ring system|
US7628942B1|2006-04-25|2009-12-08|The United States Of America As Represented By The United States Department Of Energy|Resin infiltration transfer technique|
US7624787B2|2006-12-06|2009-12-01|General Electric Company|Disposable insert, and use thereof in a method for manufacturing an airfoil|
US8413709B2|2006-12-06|2013-04-09|General Electric Company|Composite core die, methods of manufacture thereof and articles manufactured therefrom|
DE102007006844B4|2007-02-12|2014-06-12|Bioregeneration Gmbh|Elongated hollow body for replacement of a venous blood vessel and method and mold for producing a crystalline cellulose comprising elongated hollow body|
US20090169738A1|2007-12-28|2009-07-02|General Electric Company|Method for rapid manufacture of carbon-based tooling for melt infiltration|
CN102351542B|2011-07-12|2012-12-05|中南大学|Preparation method of hollow-structure metal or ceramic part|
US8980435B2|2011-10-04|2015-03-17|General Electric Company|CMC component, power generation system and method of forming a CMC component|US9676631B2|2014-07-21|2017-06-13|Lori Bracamonte|Reaction bonded silicon carbide bodies made from high purity carbonaceous preforms|
US10207471B2|2016-05-04|2019-02-19|General Electric Company|Perforated ceramic matrix composite ply, ceramic matrix composite article, and method for forming ceramic matrix composite article|
US20180238175A1|2017-02-21|2018-08-23|General Electric Company|Method and Device for Retaining Position of a Consumable Core|
US10562210B2|2017-03-22|2020-02-18|General Electric Company|Method for forming passages in composite components|
US9931818B1|2017-04-05|2018-04-03|General Electric Company|Method for forming CMC article|
FR3071830B1|2017-10-02|2021-03-12|Safran Ceram|PROCESS FOR MAKING A HOLLOW PART IN COMPOSITE MATERIAL WITH CERAMIC MATRIX|
法律状态:
2014-08-15| PK| Correction|Free format text: ERFINDER BERICHTIGT. |
2017-03-15| NV| New agent|Representative=s name: GENERAL ELECTRIC TECHNOLOGY GMBH GLOBAL PATENT, CH |
优先权:
申请号 | 申请日 | 专利标题
US13/586,930|US9751807B2|2012-08-16|2012-08-16|Consumable core for manufacture of composite articles and related method|
[返回顶部]