THERMOPLASTIC AEROSTRUCTURE WITH LOCALIZED PLY ISOLATION AND METHOD FOR FORMING AEROSTRUCTURE
강화 열가소성 수지로 형성된 복합 윙박스 구조물. 복합 구조물은 탄소 섬유 보강재 및 구조물 제조 공정 동안 생성된 열을 국한시키기 위한 복수의 절연 요소를 포함한다. 윙박스를 제조하는 공정은 복수의 막의 내부에 일련의 절연 요소를 개재하는 단계 및 절연 요소와 막을 통합하여 적층체를 형성하는 단계를 포함한다. 이어서, 절연 요소가 지지 구조체의 위에 놓이도록 적층체가 지지 구조체와 정렬된다. 이어서, 적층체가 유도 용접과 같은 비접촉 가열 공정을 사용하여 지지 구조체에 융착된다. A composite wingbox structur...
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| creator | ELLIS JOHN F WIMMER MARTIN A DENNISON WILLIAM DAVID STONE EARL L. III CALDER MARK A |
| description | 강화 열가소성 수지로 형성된 복합 윙박스 구조물. 복합 구조물은 탄소 섬유 보강재 및 구조물 제조 공정 동안 생성된 열을 국한시키기 위한 복수의 절연 요소를 포함한다. 윙박스를 제조하는 공정은 복수의 막의 내부에 일련의 절연 요소를 개재하는 단계 및 절연 요소와 막을 통합하여 적층체를 형성하는 단계를 포함한다. 이어서, 절연 요소가 지지 구조체의 위에 놓이도록 적층체가 지지 구조체와 정렬된다. 이어서, 적층체가 유도 용접과 같은 비접촉 가열 공정을 사용하여 지지 구조체에 융착된다.
A composite wingbox structure formed of reinforced thermoplastic. The composite includes carbon fiber reinforcement and a plurality of insulation elements to localize the heat formed during the process of manufacturing the structure. The process of manufacturing the wingbox includes the steps of interleaving a series of insulations elements within a plurality of laminae and consolidating the insulation elements and laminae to form a laminate. The laminate is then aligned with a support structure such that the insulation elements overlie the supports structure. The laminate is then fused to the support structure using a non-contact heating process, such as inductive welding. |
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A composite wingbox structure formed of reinforced thermoplastic. The composite includes carbon fiber reinforcement and a plurality of insulation elements to localize the heat formed during the process of manufacturing the structure. The process of manufacturing the wingbox includes the steps of interleaving a series of insulations elements within a plurality of laminae and consolidating the insulation elements and laminae to form a laminate. The laminate is then aligned with a support structure such that the insulation elements overlie the supports structure. The laminate is then fused to the support structure using a non-contact heating process, such as inductive welding.</description><language>eng ; kor</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT ; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR ; HELICOPTERS ; LAYERED PRODUCTS ; LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM ; PERFORMING OPERATIONS ; TRANSPORTING</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=20230228&DB=EPODOC&CC=KR&NR=20230028573A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76294</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230228&DB=EPODOC&CC=KR&NR=20230028573A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ELLIS JOHN F</creatorcontrib><creatorcontrib>WIMMER MARTIN A</creatorcontrib><creatorcontrib>DENNISON WILLIAM DAVID</creatorcontrib><creatorcontrib>STONE EARL L. III</creatorcontrib><creatorcontrib>CALDER MARK A</creatorcontrib><title>THERMOPLASTIC AEROSTRUCTURE WITH LOCALIZED PLY ISOLATION AND METHOD FOR FORMING AEROSTRUCTURE</title><description>강화 열가소성 수지로 형성된 복합 윙박스 구조물. 복합 구조물은 탄소 섬유 보강재 및 구조물 제조 공정 동안 생성된 열을 국한시키기 위한 복수의 절연 요소를 포함한다. 윙박스를 제조하는 공정은 복수의 막의 내부에 일련의 절연 요소를 개재하는 단계 및 절연 요소와 막을 통합하여 적층체를 형성하는 단계를 포함한다. 이어서, 절연 요소가 지지 구조체의 위에 놓이도록 적층체가 지지 구조체와 정렬된다. 이어서, 적층체가 유도 용접과 같은 비접촉 가열 공정을 사용하여 지지 구조체에 융착된다.
A composite wingbox structure formed of reinforced thermoplastic. The composite includes carbon fiber reinforcement and a plurality of insulation elements to localize the heat formed during the process of manufacturing the structure. The process of manufacturing the wingbox includes the steps of interleaving a series of insulations elements within a plurality of laminae and consolidating the insulation elements and laminae to form a laminate. The laminate is then aligned with a support structure such that the insulation elements overlie the supports structure. The laminate is then fused to the support structure using a non-contact heating process, such as inductive welding.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</subject><subject>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</subject><subject>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</subject><subject>HELICOPTERS</subject><subject>LAYERED PRODUCTS</subject><subject>LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZIgN8XAN8vUP8HEMDvF0VnB0DfIPDgkKdQ4JDXJVCPcM8VDw8Xd29PGMcnVRCPCJVPAM9vdxDPH091Nw9HNR8HUN8fB3UXDzDwJhX08_d1QTeBhY0xJzilN5oTQ3g7Kba4izh25qQX58anFBYnJqXmpJvHeQkYGRsYGBkYWpubGjMXGqAB-xNDY</recordid><startdate>20230228</startdate><enddate>20230228</enddate><creator>ELLIS JOHN F</creator><creator>WIMMER MARTIN A</creator><creator>DENNISON WILLIAM DAVID</creator><creator>STONE EARL L. III</creator><creator>CALDER MARK A</creator><scope>EVB</scope></search><sort><creationdate>20230228</creationdate><title>THERMOPLASTIC AEROSTRUCTURE WITH LOCALIZED PLY ISOLATION AND METHOD FOR FORMING AEROSTRUCTURE</title><author>ELLIS JOHN F ; WIMMER MARTIN A ; DENNISON WILLIAM DAVID ; STONE EARL L. III ; CALDER MARK A</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_KR20230028573A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; kor</language><creationdate>2023</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</topic><topic>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</topic><topic>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</topic><topic>HELICOPTERS</topic><topic>LAYERED PRODUCTS</topic><topic>LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>ELLIS JOHN F</creatorcontrib><creatorcontrib>WIMMER MARTIN A</creatorcontrib><creatorcontrib>DENNISON WILLIAM DAVID</creatorcontrib><creatorcontrib>STONE EARL L. III</creatorcontrib><creatorcontrib>CALDER MARK A</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ELLIS JOHN F</au><au>WIMMER MARTIN A</au><au>DENNISON WILLIAM DAVID</au><au>STONE EARL L. III</au><au>CALDER MARK A</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>THERMOPLASTIC AEROSTRUCTURE WITH LOCALIZED PLY ISOLATION AND METHOD FOR FORMING AEROSTRUCTURE</title><date>2023-02-28</date><risdate>2023</risdate><abstract>강화 열가소성 수지로 형성된 복합 윙박스 구조물. 복합 구조물은 탄소 섬유 보강재 및 구조물 제조 공정 동안 생성된 열을 국한시키기 위한 복수의 절연 요소를 포함한다. 윙박스를 제조하는 공정은 복수의 막의 내부에 일련의 절연 요소를 개재하는 단계 및 절연 요소와 막을 통합하여 적층체를 형성하는 단계를 포함한다. 이어서, 절연 요소가 지지 구조체의 위에 놓이도록 적층체가 지지 구조체와 정렬된다. 이어서, 적층체가 유도 용접과 같은 비접촉 가열 공정을 사용하여 지지 구조체에 융착된다.
A composite wingbox structure formed of reinforced thermoplastic. The composite includes carbon fiber reinforcement and a plurality of insulation elements to localize the heat formed during the process of manufacturing the structure. The process of manufacturing the wingbox includes the steps of interleaving a series of insulations elements within a plurality of laminae and consolidating the insulation elements and laminae to form a laminate. The laminate is then aligned with a support structure such that the insulation elements overlie the supports structure. The laminate is then fused to the support structure using a non-contact heating process, such as inductive welding.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HELICOPTERS LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM PERFORMING OPERATIONS TRANSPORTING |
| title | THERMOPLASTIC AEROSTRUCTURE WITH LOCALIZED PLY ISOLATION AND METHOD FOR FORMING AEROSTRUCTURE |
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