CO-MOLDED METALLIC FAN CASE CONTAINMENT RING
A method of fabricating a fan case (62) for a gas turbine engine defines a metallic ring (64) including an outer surface (66) and an inner surface (68). A first composite material (70) is assembled about the outer surface (66) of the metallic ring (64). A second composite material (76) is assembled...
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| creator | KLING, Colin J LUSSIER, Darin S O'BRIEN, James F |
| description | A method of fabricating a fan case (62) for a gas turbine engine defines a metallic ring (64) including an outer surface (66) and an inner surface (68). A first composite material (70) is assembled about the outer surface (66) of the metallic ring (64). A second composite material (76) is assembled about the first composite material (70). The first composite material (70) and the second material (76) are cured about the metallic ring (64) within a tool (100) to form a first subassembly (75). The first subassembly (75) is removed from the tool (100). A fan case assembly for a gas turbine engine and a gas turbine engine are also disclosed. |
| format | Patent |
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A first composite material (70) is assembled about the outer surface (66) of the metallic ring (64). A second composite material (76) is assembled about the first composite material (70). The first composite material (70) and the second material (76) are cured about the metallic ring (64) within a tool (100) to form a first subassembly (75). The first subassembly (75) is removed from the tool (100). A fan case assembly for a gas turbine engine and a gas turbine engine are also disclosed.</description><language>eng ; fre ; ger</language><subject>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING ; BLASTING ; ENGINE PLANTS IN GENERAL ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; PERFORMING OPERATIONS ; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR ; SHAPING OR JOINING OF PLASTICS ; STEAM ENGINES ; TRANSPORTING ; WEAPONS ; WORKING OF PLASTICS ; WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</subject><creationdate>2023</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20231018&DB=EPODOC&CC=EP&NR=3106289B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76516</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20231018&DB=EPODOC&CC=EP&NR=3106289B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KLING, Colin J</creatorcontrib><creatorcontrib>LUSSIER, Darin S</creatorcontrib><creatorcontrib>O'BRIEN, James F</creatorcontrib><title>CO-MOLDED METALLIC FAN CASE CONTAINMENT RING</title><description>A method of fabricating a fan case (62) for a gas turbine engine defines a metallic ring (64) including an outer surface (66) and an inner surface (68). A first composite material (70) is assembled about the outer surface (66) of the metallic ring (64). A second composite material (76) is assembled about the first composite material (70). The first composite material (70) and the second material (76) are cured about the metallic ring (64) within a tool (100) to form a first subassembly (75). The first subassembly (75) is removed from the tool (100). A fan case assembly for a gas turbine engine and a gas turbine engine are also disclosed.</description><subject>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</subject><subject>BLASTING</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>PERFORMING OPERATIONS</subject><subject>SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR</subject><subject>SHAPING OR JOINING OF PLASTICS</subject><subject>STEAM ENGINES</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><subject>WORKING OF PLASTICS</subject><subject>WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNBx9tf19fdxcXVR8HUNcfTx8XRWcHP0U3B2DHZVcPb3C3H09PN19QtRCPL0c-dhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAcaGBmZGFpZOhsZEKAEAKZQkdw</recordid><startdate>20231018</startdate><enddate>20231018</enddate><creator>KLING, Colin J</creator><creator>LUSSIER, Darin S</creator><creator>O'BRIEN, James F</creator><scope>EVB</scope></search><sort><creationdate>20231018</creationdate><title>CO-MOLDED METALLIC FAN CASE CONTAINMENT RING</title><author>KLING, Colin J ; LUSSIER, Darin S ; O'BRIEN, James F</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3106289B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2023</creationdate><topic>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</topic><topic>BLASTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>PERFORMING OPERATIONS</topic><topic>SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR</topic><topic>SHAPING OR JOINING OF PLASTICS</topic><topic>STEAM ENGINES</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><topic>WORKING OF PLASTICS</topic><topic>WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</topic><toplevel>online_resources</toplevel><creatorcontrib>KLING, Colin J</creatorcontrib><creatorcontrib>LUSSIER, Darin S</creatorcontrib><creatorcontrib>O'BRIEN, James F</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KLING, Colin J</au><au>LUSSIER, Darin S</au><au>O'BRIEN, James F</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>CO-MOLDED METALLIC FAN CASE CONTAINMENT RING</title><date>2023-10-18</date><risdate>2023</risdate><abstract>A method of fabricating a fan case (62) for a gas turbine engine defines a metallic ring (64) including an outer surface (66) and an inner surface (68). A first composite material (70) is assembled about the outer surface (66) of the metallic ring (64). A second composite material (76) is assembled about the first composite material (70). The first composite material (70) and the second material (76) are cured about the metallic ring (64) within a tool (100) to form a first subassembly (75). The first subassembly (75) is removed from the tool (100). A fan case assembly for a gas turbine engine and a gas turbine engine are also disclosed.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS STEAM ENGINES TRANSPORTING WEAPONS WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL |
| title | CO-MOLDED METALLIC FAN CASE CONTAINMENT RING |
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