COMPRESSION MOLDING ASSEMBLY AND METHODS FOR MOLDING THERMOPLASTIC BLOCKER DOOR

PROBLEM TO BE SOLVED: To provide a compression molding assembly for molding a honeycomb core, including a plurality of cells defined by a plurality of walls, of a blocker door.SOLUTION: The compression molding assembly includes a ram plate comprising a plurality of openings defined through the ram p...

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Hauptverfasser: STEPHEN DARK, RANDY J GROVE, JESTON LINGELBACH, KORY SHAFFER, GARY ANTHONY BOOKER, MICHAEL H LARSON, MICHAEL A NILL, LAURA FOURNIER, KEVIN O'BRIEN GAW, DAVID JOHN BARENE, DAVID W FOUTCH
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creator STEPHEN DARK
RANDY J GROVE
JESTON LINGELBACH
KORY SHAFFER
GARY ANTHONY BOOKER
MICHAEL H LARSON
MICHAEL A NILL
LAURA FOURNIER
KEVIN O'BRIEN GAW
DAVID JOHN BARENE
DAVID W FOUTCH
description PROBLEM TO BE SOLVED: To provide a compression molding assembly for molding a honeycomb core, including a plurality of cells defined by a plurality of walls, of a blocker door.SOLUTION: The compression molding assembly includes a ram plate comprising a plurality of openings defined through the ram plate, and a plurality of core inserts coupled to the ram plate, so 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 corresponding opening of the plurality of openings, so that each core insert is configured to form a corresponding cell of the plurality of cells.SELECTED DRAWING: Figure 1 【課題】複数の壁によって画定された複数のセルを含む、遮蔽ドアのハニカムコアを成形するための、圧縮成形組立体を提供する。【解決手段】圧縮成形組立体は、ラム板であって、当該ラム板を貫通して画定された複数の開口部を有するラム板と、ラム板に結合された複数のコアインサートとを備え、その結果、複数のコアインサートは、遮蔽ドアのハニカムコアを形成するように構成される。各コアインサートは、複数の開口部のそれぞれの開口部に取り外し可能に結合され、その結果、各コアインサートは、複数のセルのそれぞれのセルを形成するように構成される。【選択図】図1
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Each core insert is removably coupled with a corresponding opening of the plurality of openings, so that each core insert is configured to form a corresponding cell of the plurality of cells.SELECTED DRAWING: Figure 1 【課題】複数の壁によって画定された複数のセルを含む、遮蔽ドアのハニカムコアを成形するための、圧縮成形組立体を提供する。【解決手段】圧縮成形組立体は、ラム板であって、当該ラム板を貫通して画定された複数の開口部を有するラム板と、ラム板に結合された複数のコアインサートとを備え、その結果、複数のコアインサートは、遮蔽ドアのハニカムコアを形成するように構成される。各コアインサートは、複数の開口部のそれぞれの開口部に取り外し可能に結合され、その結果、各コアインサートは、複数のセルのそれぞれのセルを形成するように構成される。【選択図】図1</description><language>eng ; jpn</language><subject>AEROPLANES ; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING ; AIR INTAKES FOR JET-PROPULSION PLANTS ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; COSMONAUTICS ; ENGINE PLANTS IN GENERAL ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GAS-TURBINE PLANTS ; HEATING ; HELICOPTERS ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; JET-PROPULSION PLANTS ; LAYERED PRODUCTS ; LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; PARACHUTES ; 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>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&amp;date=20180308&amp;DB=EPODOC&amp;CC=JP&amp;NR=2018035803A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20180308&amp;DB=EPODOC&amp;CC=JP&amp;NR=2018035803A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>STEPHEN DARK</creatorcontrib><creatorcontrib>RANDY J GROVE</creatorcontrib><creatorcontrib>JESTON LINGELBACH</creatorcontrib><creatorcontrib>KORY SHAFFER</creatorcontrib><creatorcontrib>GARY ANTHONY BOOKER</creatorcontrib><creatorcontrib>MICHAEL H LARSON</creatorcontrib><creatorcontrib>MICHAEL A NILL</creatorcontrib><creatorcontrib>LAURA FOURNIER</creatorcontrib><creatorcontrib>KEVIN O'BRIEN GAW</creatorcontrib><creatorcontrib>DAVID JOHN BARENE</creatorcontrib><creatorcontrib>DAVID W FOUTCH</creatorcontrib><title>COMPRESSION MOLDING ASSEMBLY AND METHODS FOR MOLDING THERMOPLASTIC BLOCKER DOOR</title><description>PROBLEM TO BE SOLVED: To provide a compression molding assembly for molding a honeycomb core, including a plurality of cells defined by a plurality of walls, of a blocker door.SOLUTION: The compression molding assembly includes a ram plate comprising a plurality of openings defined through the ram plate, and a plurality of core inserts coupled to the ram plate, so 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 corresponding opening of the plurality of openings, so that each core insert is configured to form a corresponding cell of the plurality of cells.SELECTED DRAWING: Figure 1 【課題】複数の壁によって画定された複数のセルを含む、遮蔽ドアのハニカムコアを成形するための、圧縮成形組立体を提供する。【解決手段】圧縮成形組立体は、ラム板であって、当該ラム板を貫通して画定された複数の開口部を有するラム板と、ラム板に結合された複数のコアインサートとを備え、その結果、複数のコアインサートは、遮蔽ドアのハニカムコアを形成するように構成される。各コアインサートは、複数の開口部のそれぞれの開口部に取り外し可能に結合され、その結果、各コアインサートは、複数のセルのそれぞれのセルを形成するように構成される。【選択図】図1</description><subject>AEROPLANES</subject><subject>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</subject><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>COSMONAUTICS</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HELICOPTERS</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>JET-PROPULSION PLANTS</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>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>PARACHUTES</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>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZPB39vcNCHINDvb091Pw9fdx8fRzV3AMDnb1dfKJVHD0c1HwdQ3x8HcJVnDzD4IrCPFwDfL1D_BxDA7xdFZw8vF39nYNUnDx9w_iYWBNS8wpTuWF0twMSm6uIc4euqkF-fGpxQWJyal5qSXxXgFGBoYWBsamQOxoTJQiAMP8L28</recordid><startdate>20180308</startdate><enddate>20180308</enddate><creator>STEPHEN DARK</creator><creator>RANDY J GROVE</creator><creator>JESTON LINGELBACH</creator><creator>KORY SHAFFER</creator><creator>GARY ANTHONY BOOKER</creator><creator>MICHAEL H LARSON</creator><creator>MICHAEL A NILL</creator><creator>LAURA FOURNIER</creator><creator>KEVIN O'BRIEN GAW</creator><creator>DAVID JOHN BARENE</creator><creator>DAVID W FOUTCH</creator><scope>EVB</scope></search><sort><creationdate>20180308</creationdate><title>COMPRESSION MOLDING ASSEMBLY AND METHODS FOR MOLDING THERMOPLASTIC BLOCKER DOOR</title><author>STEPHEN DARK ; RANDY J GROVE ; JESTON LINGELBACH ; KORY SHAFFER ; GARY ANTHONY BOOKER ; MICHAEL H LARSON ; MICHAEL A NILL ; LAURA FOURNIER ; KEVIN O'BRIEN GAW ; DAVID JOHN BARENE ; DAVID W FOUTCH</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_JP2018035803A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; jpn</language><creationdate>2018</creationdate><topic>AEROPLANES</topic><topic>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</topic><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>COSMONAUTICS</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HELICOPTERS</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>JET-PROPULSION PLANTS</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>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>PARACHUTES</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>STEPHEN DARK</creatorcontrib><creatorcontrib>RANDY J GROVE</creatorcontrib><creatorcontrib>JESTON LINGELBACH</creatorcontrib><creatorcontrib>KORY SHAFFER</creatorcontrib><creatorcontrib>GARY ANTHONY BOOKER</creatorcontrib><creatorcontrib>MICHAEL H LARSON</creatorcontrib><creatorcontrib>MICHAEL A NILL</creatorcontrib><creatorcontrib>LAURA FOURNIER</creatorcontrib><creatorcontrib>KEVIN O'BRIEN GAW</creatorcontrib><creatorcontrib>DAVID JOHN BARENE</creatorcontrib><creatorcontrib>DAVID W FOUTCH</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>STEPHEN DARK</au><au>RANDY J GROVE</au><au>JESTON LINGELBACH</au><au>KORY SHAFFER</au><au>GARY ANTHONY BOOKER</au><au>MICHAEL H LARSON</au><au>MICHAEL A NILL</au><au>LAURA FOURNIER</au><au>KEVIN O'BRIEN GAW</au><au>DAVID JOHN BARENE</au><au>DAVID W FOUTCH</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>COMPRESSION MOLDING ASSEMBLY AND METHODS FOR MOLDING THERMOPLASTIC BLOCKER DOOR</title><date>2018-03-08</date><risdate>2018</risdate><abstract>PROBLEM TO BE SOLVED: To provide a compression molding assembly for molding a honeycomb core, including a plurality of cells defined by a plurality of walls, of a blocker door.SOLUTION: The compression molding assembly includes a ram plate comprising a plurality of openings defined through the ram plate, and a plurality of core inserts coupled to the ram plate, so 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 corresponding opening of the plurality of openings, so that each core insert is configured to form a corresponding cell of the plurality of cells.SELECTED DRAWING: Figure 1 【課題】複数の壁によって画定された複数のセルを含む、遮蔽ドアのハニカムコアを成形するための、圧縮成形組立体を提供する。【解決手段】圧縮成形組立体は、ラム板であって、当該ラム板を貫通して画定された複数の開口部を有するラム板と、ラム板に結合された複数のコアインサートとを備え、その結果、複数のコアインサートは、遮蔽ドアのハニカムコアを形成するように構成される。各コアインサートは、複数の開口部のそれぞれの開口部に取り外し可能に結合され、その結果、各コアインサートは、複数のセルのそれぞれのセルを形成するように構成される。【選択図】図1</abstract><oa>free_for_read</oa></addata></record>
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subjects AEROPLANES
AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
AIR INTAKES FOR JET-PROPULSION PLANTS
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
COSMONAUTICS
ENGINE PLANTS IN GENERAL
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
GAS-TURBINE PLANTS
HEATING
HELICOPTERS
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LAYERED PRODUCTS
LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
PARACHUTES
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 COMPRESSION MOLDING ASSEMBLY AND METHODS FOR MOLDING THERMOPLASTIC BLOCKER DOOR
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