COMPRESSION MOLDING ASSEMBLY AND METHODS FOR MOLDING A THERMOPLASTIC BLOCKER DOOR
A compression molding assembly (200) for molding a honeycomb core 8137), including a plurality of cells ((170 defined by a plurality of walls (172), of a blocker door (128) is provided. The compression molding assembly includes a ram plate (206) comprising a plurality of openings (218) defined there...
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creator | GAW, Kevin O'Brien BARENE, David John LARSON, Michael H DARK, Stephen GROVE, Randy J LINGELBACH, Jeston SHAFFER, Kory NILL, Michael A FOUTCH, David W BOOKER, Garry Anthony FOURNIER, Laura |
description | A compression molding assembly (200) for molding a honeycomb core 8137), including a plurality of cells ((170 defined by a plurality of walls (172), of a blocker door (128) is provided. The compression molding assembly includes a ram plate (206) comprising a plurality of openings (218) defined therethrough and a plurality of core inserts (220) coupled to the ram plate (206) such that the plurality of core inserts are configured to form the honeycomb core of the blocker door. Each core insert is removably coupled with a respective opening of the plurality of openings such that each core insert is configured to form a respective cell of the plurality of cells. |
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The compression molding assembly includes a ram plate (206) comprising a plurality of openings (218) defined therethrough and a plurality of core inserts (220) coupled to the ram plate (206) such that the plurality of core inserts are configured to form the honeycomb core of the blocker door. Each core insert is removably coupled with a respective opening of the plurality of openings such that each core insert is configured to form a respective cell of the plurality of cells.</description><language>eng ; fre ; ger</language><subject>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULARARTICLES ; PARACHUTES ; PERFORMING OPERATIONS ; PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE ; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR ; SHAPING OR JOINING OF PLASTICS ; TRANSPORTING ; WORKING OF PLASTICS ; WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</subject><creationdate>2018</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=20180307&DB=EPODOC&CC=EP&NR=3290195A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76418</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20180307&DB=EPODOC&CC=EP&NR=3290195A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GAW, Kevin O'Brien</creatorcontrib><creatorcontrib>BARENE, David John</creatorcontrib><creatorcontrib>LARSON, Michael H</creatorcontrib><creatorcontrib>DARK, Stephen</creatorcontrib><creatorcontrib>GROVE, Randy J</creatorcontrib><creatorcontrib>LINGELBACH, Jeston</creatorcontrib><creatorcontrib>SHAFFER, Kory</creatorcontrib><creatorcontrib>NILL, Michael A</creatorcontrib><creatorcontrib>FOUTCH, David W</creatorcontrib><creatorcontrib>BOOKER, Garry Anthony</creatorcontrib><creatorcontrib>FOURNIER, Laura</creatorcontrib><title>COMPRESSION MOLDING ASSEMBLY AND METHODS FOR MOLDING A THERMOPLASTIC BLOCKER DOOR</title><description>A compression molding assembly (200) for molding a honeycomb core 8137), including a plurality of cells ((170 defined by a plurality of walls (172), of a blocker door (128) is provided. The compression molding assembly includes a ram plate (206) comprising a plurality of openings (218) defined therethrough and a plurality of core inserts (220) coupled to the ram plate (206) such that the plurality of core inserts are configured to form the honeycomb core of the blocker door. 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The compression molding assembly includes a ram plate (206) comprising a plurality of openings (218) defined therethrough and a plurality of core inserts (220) coupled to the ram plate (206) such that the plurality of core inserts are configured to form the honeycomb core of the blocker door. Each core insert is removably coupled with a respective opening of the plurality of openings such that each core insert is configured to form a respective cell of the plurality of cells.</abstract><oa>free_for_read</oa></addata></record> |
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subjects | AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULARARTICLES PARACHUTES PERFORMING OPERATIONS PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS TRANSPORTING WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL |
title | COMPRESSION MOLDING ASSEMBLY AND METHODS FOR MOLDING A THERMOPLASTIC BLOCKER DOOR |
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