Particle collector for gas turbine engine
A material having a plurality of impurity collection spaces has an outer face facing into a cooling air flow stream for a gas turbine engine component. Impurities such as sand or dirt will collect in the plurality of spaces. In a disclosed embodiment, a honeycombed material is utilized. The material...
Gespeichert in:
Hauptverfasser: | , , , , , |
---|---|
Format: | Patent |
Sprache: | eng |
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 | Alvanos, Ioannis Andrews, Bernard A Charbonneau, Robert A Tholen, Susan M Dabbs, Thurman Carlo Bruskotter, Michael J |
description | A material having a plurality of impurity collection spaces has an outer face facing into a cooling air flow stream for a gas turbine engine component. Impurities such as sand or dirt will collect in the plurality of spaces. In a disclosed embodiment, a honeycombed material is utilized. The material may have a surface that will sit with at least a component parallel to an axial centerline of a gas turbine engine that is to receive the collection material. The material surface may also have a component which is generally perpendicular to the axial centerline. The material may be placed in a gas turbine engine upstream of the turbine section, and downstream of the combustion section. Moreover, the collection material may be placed such that there is cleaner air flow radially inwardly of the collection material, and heavier dirt-laden air passing along the collection material such that impurities can be collected. |
format | Patent |
fullrecord | <record><control><sourceid>uspatents_EFH</sourceid><recordid>TN_cdi_uspatents_grants_07770375</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>07770375</sourcerecordid><originalsourceid>FETCH-uspatents_grants_077703753</originalsourceid><addsrcrecordid>eNrjZNAMSCwqyUzOSVVIzs_JSU0uyS9SSAPi9MRihZLSoqTMvFSF1Lx0IMXDwJqWmFOcyguluRkU3FxDnD10S4sLEktS80qK49OLEkGUgbm5uYGxuakxEUoA2ggpkg</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Particle collector for gas turbine engine</title><source>USPTO Issued Patents</source><creator>Alvanos, Ioannis ; Andrews, Bernard A ; Charbonneau, Robert A ; Tholen, Susan M ; Dabbs, Thurman Carlo ; Bruskotter, Michael J</creator><creatorcontrib>Alvanos, Ioannis ; Andrews, Bernard A ; Charbonneau, Robert A ; Tholen, Susan M ; Dabbs, Thurman Carlo ; Bruskotter, Michael J ; United Technologies Corporation</creatorcontrib><description>A material having a plurality of impurity collection spaces has an outer face facing into a cooling air flow stream for a gas turbine engine component. Impurities such as sand or dirt will collect in the plurality of spaces. In a disclosed embodiment, a honeycombed material is utilized. The material may have a surface that will sit with at least a component parallel to an axial centerline of a gas turbine engine that is to receive the collection material. The material surface may also have a component which is generally perpendicular to the axial centerline. The material may be placed in a gas turbine engine upstream of the turbine section, and downstream of the combustion section. Moreover, the collection material may be placed such that there is cleaner air flow radially inwardly of the collection material, and heavier dirt-laden air passing along the collection material such that impurities can be collected.</description><language>eng</language><creationdate>2010</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7770375$$EPDF$$P50$$Guspatents$$Hfree_for_read</linktopdf><link.rule.ids>230,308,780,802,885,64039</link.rule.ids><linktorsrc>$$Uhttps://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7770375$$EView_record_in_USPTO$$FView_record_in_$$GUSPTO$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Alvanos, Ioannis</creatorcontrib><creatorcontrib>Andrews, Bernard A</creatorcontrib><creatorcontrib>Charbonneau, Robert A</creatorcontrib><creatorcontrib>Tholen, Susan M</creatorcontrib><creatorcontrib>Dabbs, Thurman Carlo</creatorcontrib><creatorcontrib>Bruskotter, Michael J</creatorcontrib><creatorcontrib>United Technologies Corporation</creatorcontrib><title>Particle collector for gas turbine engine</title><description>A material having a plurality of impurity collection spaces has an outer face facing into a cooling air flow stream for a gas turbine engine component. Impurities such as sand or dirt will collect in the plurality of spaces. In a disclosed embodiment, a honeycombed material is utilized. The material may have a surface that will sit with at least a component parallel to an axial centerline of a gas turbine engine that is to receive the collection material. The material surface may also have a component which is generally perpendicular to the axial centerline. The material may be placed in a gas turbine engine upstream of the turbine section, and downstream of the combustion section. Moreover, the collection material may be placed such that there is cleaner air flow radially inwardly of the collection material, and heavier dirt-laden air passing along the collection material such that impurities can be collected.</description><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2010</creationdate><recordtype>patent</recordtype><sourceid>EFH</sourceid><recordid>eNrjZNAMSCwqyUzOSVVIzs_JSU0uyS9SSAPi9MRihZLSoqTMvFSF1Lx0IMXDwJqWmFOcyguluRkU3FxDnD10S4sLEktS80qK49OLEkGUgbm5uYGxuakxEUoA2ggpkg</recordid><startdate>20100810</startdate><enddate>20100810</enddate><creator>Alvanos, Ioannis</creator><creator>Andrews, Bernard A</creator><creator>Charbonneau, Robert A</creator><creator>Tholen, Susan M</creator><creator>Dabbs, Thurman Carlo</creator><creator>Bruskotter, Michael J</creator><scope>EFH</scope></search><sort><creationdate>20100810</creationdate><title>Particle collector for gas turbine engine</title><author>Alvanos, Ioannis ; Andrews, Bernard A ; Charbonneau, Robert A ; Tholen, Susan M ; Dabbs, Thurman Carlo ; Bruskotter, Michael J</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-uspatents_grants_077703753</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2010</creationdate><toplevel>online_resources</toplevel><creatorcontrib>Alvanos, Ioannis</creatorcontrib><creatorcontrib>Andrews, Bernard A</creatorcontrib><creatorcontrib>Charbonneau, Robert A</creatorcontrib><creatorcontrib>Tholen, Susan M</creatorcontrib><creatorcontrib>Dabbs, Thurman Carlo</creatorcontrib><creatorcontrib>Bruskotter, Michael J</creatorcontrib><creatorcontrib>United Technologies Corporation</creatorcontrib><collection>USPTO Issued Patents</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Alvanos, Ioannis</au><au>Andrews, Bernard A</au><au>Charbonneau, Robert A</au><au>Tholen, Susan M</au><au>Dabbs, Thurman Carlo</au><au>Bruskotter, Michael J</au><aucorp>United Technologies Corporation</aucorp><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Particle collector for gas turbine engine</title><date>2010-08-10</date><risdate>2010</risdate><abstract>A material having a plurality of impurity collection spaces has an outer face facing into a cooling air flow stream for a gas turbine engine component. Impurities such as sand or dirt will collect in the plurality of spaces. In a disclosed embodiment, a honeycombed material is utilized. The material may have a surface that will sit with at least a component parallel to an axial centerline of a gas turbine engine that is to receive the collection material. The material surface may also have a component which is generally perpendicular to the axial centerline. The material may be placed in a gas turbine engine upstream of the turbine section, and downstream of the combustion section. Moreover, the collection material may be placed such that there is cleaner air flow radially inwardly of the collection material, and heavier dirt-laden air passing along the collection material such that impurities can be collected.</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | eng |
recordid | cdi_uspatents_grants_07770375 |
source | USPTO Issued Patents |
title | Particle collector for gas turbine engine |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-25T09%3A59%3A26IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-uspatents_EFH&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=Alvanos,%20Ioannis&rft.aucorp=United%20Technologies%20Corporation&rft.date=2010-08-10&rft_id=info:doi/&rft_dat=%3Cuspatents_EFH%3E07770375%3C/uspatents_EFH%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 |