Temperature normalized structure

Temperature normalized structure

Circulation of temperature controlled fluid through cavities in structure stiffening members (30) of hypersonic aerospace vehicles allows normalizing of destructive temperature gradients in such members and preserves stress residuals for functional requirements.

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: PAXSON, PETER O, SHANKEN, MARTIN L, GUILLERMO, MAS, SHORTLAND, HARRY, JOHNSTON, DWAYNE C
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
creator PAXSON, PETER O
SHANKEN, MARTIN L
GUILLERMO, MAS
SHORTLAND, HARRY
JOHNSTON, DWAYNE C
description Circulation of temperature controlled fluid through cavities in structure stiffening members (30) of hypersonic aerospace vehicles allows normalizing of destructive temperature gradients in such members and preserves stress residuals for functional requirements.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP0677439A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP0677439A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP0677439A13</originalsourceid><addsrcrecordid>eNrjZFAISc0tSC1KLCktSlXIyy_KTczJrEpNUSguKSpNBgnyMLCmJeYUp_JCaW4GBTfXEGcP3dSC_PjU4oLE5NS81JJ41wADM3NzE2NLR0NjIpQAAFiAJas</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Temperature normalized structure</title><source>esp@cenet</source><creator>PAXSON, PETER O ; SHANKEN, MARTIN L ; GUILLERMO, MAS ; SHORTLAND, HARRY ; JOHNSTON, DWAYNE C</creator><creatorcontrib>PAXSON, PETER O ; SHANKEN, MARTIN L ; GUILLERMO, MAS ; SHORTLAND, HARRY ; JOHNSTON, DWAYNE C</creatorcontrib><description>Circulation of temperature controlled fluid through cavities in structure stiffening members (30) of hypersonic aerospace vehicles allows normalizing of destructive temperature gradients in such members and preserves stress residuals for functional requirements.</description><edition>6</edition><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING ; VEHICLES OR EQUIPMENT THEREFOR</subject><creationdate>1995</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=19951018&amp;DB=EPODOC&amp;CC=EP&amp;NR=0677439A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=19951018&amp;DB=EPODOC&amp;CC=EP&amp;NR=0677439A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>PAXSON, PETER O</creatorcontrib><creatorcontrib>SHANKEN, MARTIN L</creatorcontrib><creatorcontrib>GUILLERMO, MAS</creatorcontrib><creatorcontrib>SHORTLAND, HARRY</creatorcontrib><creatorcontrib>JOHNSTON, DWAYNE C</creatorcontrib><title>Temperature normalized structure</title><description>Circulation of temperature controlled fluid through cavities in structure stiffening members (30) of hypersonic aerospace vehicles allows normalizing of destructive temperature gradients in such members and preserves stress residuals for functional requirements.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><subject>VEHICLES OR EQUIPMENT THEREFOR</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1995</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFAISc0tSC1KLCktSlXIyy_KTczJrEpNUSguKSpNBgnyMLCmJeYUp_JCaW4GBTfXEGcP3dSC_PjU4oLE5NS81JJ41wADM3NzE2NLR0NjIpQAAFiAJas</recordid><startdate>19951018</startdate><enddate>19951018</enddate><creator>PAXSON, PETER O</creator><creator>SHANKEN, MARTIN L</creator><creator>GUILLERMO, MAS</creator><creator>SHORTLAND, HARRY</creator><creator>JOHNSTON, DWAYNE C</creator><scope>EVB</scope></search><sort><creationdate>19951018</creationdate><title>Temperature normalized structure</title><author>PAXSON, PETER O ; SHANKEN, MARTIN L ; GUILLERMO, MAS ; SHORTLAND, HARRY ; JOHNSTON, DWAYNE C</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP0677439A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>1995</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><topic>VEHICLES OR EQUIPMENT THEREFOR</topic><toplevel>online_resources</toplevel><creatorcontrib>PAXSON, PETER O</creatorcontrib><creatorcontrib>SHANKEN, MARTIN L</creatorcontrib><creatorcontrib>GUILLERMO, MAS</creatorcontrib><creatorcontrib>SHORTLAND, HARRY</creatorcontrib><creatorcontrib>JOHNSTON, DWAYNE C</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>PAXSON, PETER O</au><au>SHANKEN, MARTIN L</au><au>GUILLERMO, MAS</au><au>SHORTLAND, HARRY</au><au>JOHNSTON, DWAYNE C</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Temperature normalized structure</title><date>1995-10-18</date><risdate>1995</risdate><abstract>Circulation of temperature controlled fluid through cavities in structure stiffening members (30) of hypersonic aerospace vehicles allows normalizing of destructive temperature gradients in such members and preserves stress residuals for functional requirements.</abstract><edition>6</edition><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP0677439A1
source esp@cenet
subjects AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
title Temperature normalized structure
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-03T13%3A26%3A33IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=PAXSON,%20PETER%20O&rft.date=1995-10-18&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP0677439A1%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true