SYSTEMS FOR COOLING A LEADING EDGE OF A HIGH SPEED VEHICLE
A leading edge assembly for a hypersonic vehicle is provided. The leading edge assembly includes an outer wall that tapers to a leading edge, the outer wall having a porous region at the leading edge; a coolant supply assembly in fluid communication with the porous region for selectively providing a...
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creator | Natsui, Gregory Alexander Dyson, Thomas Earl Rathay, Nicholas William |
description | A leading edge assembly for a hypersonic vehicle is provided. The leading edge assembly includes an outer wall that tapers to a leading edge, the outer wall having a porous region at the leading edge; a coolant supply assembly in fluid communication with the porous region for selectively providing a flow of coolant through the porous region of the outer wall; and an insulation layer disposed between a portion of the coolant supply assembly and the outer wall, wherein the insulation layer is configured to reduce heat transfer between the coolant supply assembly and the outer wall. |
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The leading edge assembly includes an outer wall that tapers to a leading edge, the outer wall having a porous region at the leading edge; a coolant supply assembly in fluid communication with the porous region for selectively providing a flow of coolant through the porous region of the outer wall; and an insulation layer disposed between a portion of the coolant supply assembly and the outer wall, wherein the insulation layer is configured to reduce heat transfer between the coolant supply assembly and the outer wall.</description><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; 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=20230907&DB=EPODOC&CC=US&NR=2023278695A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230907&DB=EPODOC&CC=US&NR=2023278695A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Natsui, Gregory Alexander</creatorcontrib><creatorcontrib>Dyson, Thomas Earl</creatorcontrib><creatorcontrib>Rathay, Nicholas William</creatorcontrib><title>SYSTEMS FOR COOLING A LEADING EDGE OF A HIGH SPEED VEHICLE</title><description>A leading edge assembly for a hypersonic vehicle is provided. The leading edge assembly includes an outer wall that tapers to a leading edge, the outer wall having a porous region at the leading edge; a coolant supply assembly in fluid communication with the porous region for selectively providing a flow of coolant through the porous region of the outer wall; and an insulation layer disposed between a portion of the coolant supply assembly and the outer wall, wherein the insulation layer is configured to reduce heat transfer between the coolant supply assembly and the outer wall.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLAKjgwOcfUNVnDzD1Jw9vf38fRzV3BU8HF1dAGxXF3cXRX83YAiHp7uHgrBAa6uLgphrh6ezj6uPAysaYk5xam8UJqbQdnNNcTZQze1ID8-tbggMTk1L7UkPjTYyMDI2MjcwszS1NHQmDhVAAaSKUg</recordid><startdate>20230907</startdate><enddate>20230907</enddate><creator>Natsui, Gregory Alexander</creator><creator>Dyson, Thomas Earl</creator><creator>Rathay, Nicholas William</creator><scope>EVB</scope></search><sort><creationdate>20230907</creationdate><title>SYSTEMS FOR COOLING A LEADING EDGE OF A HIGH SPEED VEHICLE</title><author>Natsui, Gregory Alexander ; Dyson, Thomas Earl ; Rathay, Nicholas William</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2023278695A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2023</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>Natsui, Gregory Alexander</creatorcontrib><creatorcontrib>Dyson, Thomas Earl</creatorcontrib><creatorcontrib>Rathay, Nicholas William</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Natsui, Gregory Alexander</au><au>Dyson, Thomas Earl</au><au>Rathay, Nicholas William</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SYSTEMS FOR COOLING A LEADING EDGE OF A HIGH SPEED VEHICLE</title><date>2023-09-07</date><risdate>2023</risdate><abstract>A leading edge assembly for a hypersonic vehicle is provided. 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subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
title | SYSTEMS FOR COOLING A LEADING EDGE OF A HIGH SPEED VEHICLE |
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