ROTOR BLADE AND METHOD FOR REDUCING TIP RUB LOADING

ROTOR BLADE AND METHOD FOR REDUCING TIP RUB LOADING

An air foil (42) for use in a rotor assembly is disclosed, the airfoil having a tip- cutter (100) located on a sidewall (44) near a tip portion (60). Wherein the tip-cutter (100) ?s capable of removing a portion of an abradable material (32) during a tip rub. In another embodiment an airfoil (42) ha...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: KRAY, Nicholas, Joseph, WEAVER, Howard, P, GARDNER, Donald, Lee, JOHNSON, Marcia, Boyle, CRALL, David, W, FARSON, Max, Robert, MOLLMANN, Daniel, E
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
BLASTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
NON-POSITIVE DISPLACEMENT PUMPS
POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS
PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
STEAM ENGINES
WEAPONS
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 KRAY, Nicholas, Joseph
WEAVER, Howard, P
GARDNER, Donald, Lee
JOHNSON, Marcia, Boyle
CRALL, David, W
FARSON, Max, Robert
MOLLMANN, Daniel, E
description An air foil (42) for use in a rotor assembly is disclosed, the airfoil having a tip- cutter (100) located on a sidewall (44) near a tip portion (60). Wherein the tip-cutter (100) ?s capable of removing a portion of an abradable material (32) during a tip rub. In another embodiment an airfoil (42) has a tip-grinder (120) located on the tip portion (60) wherein the tip-grinder (120) capable of removing a portion of an abradable material (32) during a tip rub in another embodiment an airfoil (42) has a tip-rake (110) that facilitates reducing loading induced to said airfoil (42) during tip rubs. A method (300) for reducing tip rub loads in a rotor blade (15) is described comprising the steps of incorporating a tip-cutter (100) having a selected a cutter-profile (102) on a selected location on the blade (15) such that tip-cutter (100) is capable of removing a portion of a static structure (32) during a tip rub such that tip rub loads are facilitated to be reduced.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP2449216A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP2449216A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP2449216A13</originalsourceid><addsrcrecordid>eNrjZDAO8g_xD1Jw8nF0cVVw9HNR8HUN8fB3UXADCga5uoQ6e_q5K4R4BigEhTop-Pg7ugD5PAysaYk5xam8UJqbQcHNNcTZQze1ID8-tbggMTk1L7Uk3jXAyMTE0sjQzNHQmAglACUHJkg</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>ROTOR BLADE AND METHOD FOR REDUCING TIP RUB LOADING</title><source>esp@cenet</source><creator>KRAY, Nicholas, Joseph ; WEAVER, Howard, P ; GARDNER, Donald, Lee ; JOHNSON, Marcia, Boyle ; CRALL, David, W ; FARSON, Max, Robert ; MOLLMANN, Daniel, E</creator><creatorcontrib>KRAY, Nicholas, Joseph ; WEAVER, Howard, P ; GARDNER, Donald, Lee ; JOHNSON, Marcia, Boyle ; CRALL, David, W ; FARSON, Max, Robert ; MOLLMANN, Daniel, E</creatorcontrib><description>An air foil (42) for use in a rotor assembly is disclosed, the airfoil having a tip- cutter (100) located on a sidewall (44) near a tip portion (60). Wherein the tip-cutter (100) ?s capable of removing a portion of an abradable material (32) during a tip rub. In another embodiment an airfoil (42) has a tip-grinder (120) located on the tip portion (60) wherein the tip-grinder (120) capable of removing a portion of an abradable material (32) during a tip rub in another embodiment an airfoil (42) has a tip-rake (110) that facilitates reducing loading induced to said airfoil (42) during tip rubs. A method (300) for reducing tip rub loads in a rotor blade (15) is described comprising the steps of incorporating a tip-cutter (100) having a selected a cutter-profile (102) on a selected location on the blade (15) such that tip-cutter (100) is capable of removing a portion of a static structure (32) during a tip rub such that tip rub loads are facilitated to be reduced.</description><language>eng ; fre ; ger</language><subject>BLASTING ; ENGINE PLANTS IN GENERAL ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; NON-POSITIVE DISPLACEMENT PUMPS ; POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS ; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS ; STEAM ENGINES ; WEAPONS</subject><creationdate>2012</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=20120509&amp;DB=EPODOC&amp;CC=EP&amp;NR=2449216A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20120509&amp;DB=EPODOC&amp;CC=EP&amp;NR=2449216A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KRAY, Nicholas, Joseph</creatorcontrib><creatorcontrib>WEAVER, Howard, P</creatorcontrib><creatorcontrib>GARDNER, Donald, Lee</creatorcontrib><creatorcontrib>JOHNSON, Marcia, Boyle</creatorcontrib><creatorcontrib>CRALL, David, W</creatorcontrib><creatorcontrib>FARSON, Max, Robert</creatorcontrib><creatorcontrib>MOLLMANN, Daniel, E</creatorcontrib><title>ROTOR BLADE AND METHOD FOR REDUCING TIP RUB LOADING</title><description>An air foil (42) for use in a rotor assembly is disclosed, the airfoil having a tip- cutter (100) located on a sidewall (44) near a tip portion (60). Wherein the tip-cutter (100) ?s capable of removing a portion of an abradable material (32) during a tip rub. In another embodiment an airfoil (42) has a tip-grinder (120) located on the tip portion (60) wherein the tip-grinder (120) capable of removing a portion of an abradable material (32) during a tip rub in another embodiment an airfoil (42) has a tip-rake (110) that facilitates reducing loading induced to said airfoil (42) during tip rubs. A method (300) for reducing tip rub loads in a rotor blade (15) is described comprising the steps of incorporating a tip-cutter (100) having a selected a cutter-profile (102) on a selected location on the blade (15) such that tip-cutter (100) is capable of removing a portion of a static structure (32) during a tip rub such that tip rub loads are facilitated to be reduced.</description><subject>BLASTING</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>HEATING</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>NON-POSITIVE DISPLACEMENT PUMPS</subject><subject>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</subject><subject>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</subject><subject>STEAM ENGINES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2012</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDAO8g_xD1Jw8nF0cVVw9HNR8HUN8fB3UXADCga5uoQ6e_q5K4R4BigEhTop-Pg7ugD5PAysaYk5xam8UJqbQcHNNcTZQze1ID8-tbggMTk1L7Uk3jXAyMTE0sjQzNHQmAglACUHJkg</recordid><startdate>20120509</startdate><enddate>20120509</enddate><creator>KRAY, Nicholas, Joseph</creator><creator>WEAVER, Howard, P</creator><creator>GARDNER, Donald, Lee</creator><creator>JOHNSON, Marcia, Boyle</creator><creator>CRALL, David, W</creator><creator>FARSON, Max, Robert</creator><creator>MOLLMANN, Daniel, E</creator><scope>EVB</scope></search><sort><creationdate>20120509</creationdate><title>ROTOR BLADE AND METHOD FOR REDUCING TIP RUB LOADING</title><author>KRAY, Nicholas, Joseph ; WEAVER, Howard, P ; GARDNER, Donald, Lee ; JOHNSON, Marcia, Boyle ; CRALL, David, W ; FARSON, Max, Robert ; MOLLMANN, Daniel, E</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2449216A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2012</creationdate><topic>BLASTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>HEATING</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>NON-POSITIVE DISPLACEMENT PUMPS</topic><topic>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</topic><topic>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</topic><topic>STEAM ENGINES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>KRAY, Nicholas, Joseph</creatorcontrib><creatorcontrib>WEAVER, Howard, P</creatorcontrib><creatorcontrib>GARDNER, Donald, Lee</creatorcontrib><creatorcontrib>JOHNSON, Marcia, Boyle</creatorcontrib><creatorcontrib>CRALL, David, W</creatorcontrib><creatorcontrib>FARSON, Max, Robert</creatorcontrib><creatorcontrib>MOLLMANN, Daniel, E</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KRAY, Nicholas, Joseph</au><au>WEAVER, Howard, P</au><au>GARDNER, Donald, Lee</au><au>JOHNSON, Marcia, Boyle</au><au>CRALL, David, W</au><au>FARSON, Max, Robert</au><au>MOLLMANN, Daniel, E</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>ROTOR BLADE AND METHOD FOR REDUCING TIP RUB LOADING</title><date>2012-05-09</date><risdate>2012</risdate><abstract>An air foil (42) for use in a rotor assembly is disclosed, the airfoil having a tip- cutter (100) located on a sidewall (44) near a tip portion (60). Wherein the tip-cutter (100) ?s capable of removing a portion of an abradable material (32) during a tip rub. In another embodiment an airfoil (42) has a tip-grinder (120) located on the tip portion (60) wherein the tip-grinder (120) capable of removing a portion of an abradable material (32) during a tip rub in another embodiment an airfoil (42) has a tip-rake (110) that facilitates reducing loading induced to said airfoil (42) during tip rubs. A method (300) for reducing tip rub loads in a rotor blade (15) is described comprising the steps of incorporating a tip-cutter (100) having a selected a cutter-profile (102) on a selected location on the blade (15) such that tip-cutter (100) is capable of removing a portion of a static structure (32) during a tip rub such that tip rub loads are facilitated to be reduced.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP2449216A1
source esp@cenet
subjects BLASTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
NON-POSITIVE DISPLACEMENT PUMPS
POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS
PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
STEAM ENGINES
WEAPONS
title ROTOR BLADE AND METHOD FOR REDUCING TIP RUB LOADING
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-27T04%3A39%3A31IST&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=KRAY,%20Nicholas,%20Joseph&rft.date=2012-05-09&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP2449216A1%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