Retainer segment for swirler assembly
A retainer segment (50) is provided for a swirler assembly (30) having first and second members, such as a primary and secondary swirler (32, 40) or a swirler body and floating ferrule (36), disposed in sliding engagement with each other. The two members are maintained in sliding engagement by two o...
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| creator | THOMAS ANTHONY LEEN DAVID BRUCE PATTERSON |
| description | A retainer segment (50) is provided for a swirler assembly (30) having first and second members, such as a primary and secondary swirler (32, 40) or a swirler body and floating ferrule (36), disposed in sliding engagement with each other. The two members are maintained in sliding engagement by two of the retainer segments (50) which are joined to the second member (40) and engage the first member (32, 36). Each retainer segment (50) is an arcuate member defining inner and outer curved edges and first and second ends. Each end has a concave cutout (54) formed therein to reduce weld joint and bending stresses that occur from the forced vibration of the retainer segments (50). |
| format | Patent |
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The two members are maintained in sliding engagement by two of the retainer segments (50) which are joined to the second member (40) and engage the first member (32, 36). Each retainer segment (50) is an arcuate member defining inner and outer curved edges and first and second ends. Each end has a concave cutout (54) formed therein to reduce weld joint and bending stresses that occur from the forced vibration of the retainer segments (50).</description><edition>7</edition><language>eng</language><subject>AIR ; AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION APPARATUS ; COMBUSTION ENGINES ; COMBUSTION PROCESSES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; GAS-TURBINE PLANTS ; GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; METHODSOR APPARATUS FOR COMBUSTION USING FLUID FUELOR SOLID FUEL SUSPENDED IN ; WEAPONS</subject><creationdate>2005</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=20050721&DB=EPODOC&CC=AU&NR=782341B2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,778,883,25547,76298</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20050721&DB=EPODOC&CC=AU&NR=782341B2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>THOMAS ANTHONY LEEN</creatorcontrib><creatorcontrib>DAVID BRUCE PATTERSON</creatorcontrib><title>Retainer segment for swirler assembly</title><description>A retainer segment (50) is provided for a swirler assembly (30) having first and second members, such as a primary and secondary swirler (32, 40) or a swirler body and floating ferrule (36), disposed in sliding engagement with each other. The two members are maintained in sliding engagement by two of the retainer segments (50) which are joined to the second member (40) and engage the first member (32, 36). Each retainer segment (50) is an arcuate member defining inner and outer curved edges and first and second ends. Each end has a concave cutout (54) formed therein to reduce weld joint and bending stresses that occur from the forced vibration of the retainer segments (50).</description><subject>AIR</subject><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION APPARATUS</subject><subject>COMBUSTION ENGINES</subject><subject>COMBUSTION PROCESSES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>GAS-TURBINE PLANTS</subject><subject>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>METHODSOR APPARATUS FOR COMBUSTION USING FLUID FUELOR SOLID FUEL SUSPENDED IN</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2005</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFANSi1JzMxLLVIoTk3PTc0rUUjLB7LLM4tygGKJxcWpuUk5lTwMrGmJOcWpvFCam0HBzTXE2UM3tSA_PrW4IDE5NS-1JN4x1NzCyNjE0MnJyJgIJQAQlics</recordid><startdate>20050721</startdate><enddate>20050721</enddate><creator>THOMAS ANTHONY LEEN</creator><creator>DAVID BRUCE PATTERSON</creator><scope>EVB</scope></search><sort><creationdate>20050721</creationdate><title>Retainer segment for swirler assembly</title><author>THOMAS ANTHONY LEEN ; DAVID BRUCE PATTERSON</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_AU782341BB23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2005</creationdate><topic>AIR</topic><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION APPARATUS</topic><topic>COMBUSTION ENGINES</topic><topic>COMBUSTION PROCESSES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>GAS-TURBINE PLANTS</topic><topic>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>METHODSOR APPARATUS FOR COMBUSTION USING FLUID FUELOR SOLID FUEL SUSPENDED IN</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>THOMAS ANTHONY LEEN</creatorcontrib><creatorcontrib>DAVID BRUCE PATTERSON</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>THOMAS ANTHONY LEEN</au><au>DAVID BRUCE PATTERSON</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Retainer segment for swirler assembly</title><date>2005-07-21</date><risdate>2005</risdate><abstract>A retainer segment (50) is provided for a swirler assembly (30) having first and second members, such as a primary and secondary swirler (32, 40) or a swirler body and floating ferrule (36), disposed in sliding engagement with each other. The two members are maintained in sliding engagement by two of the retainer segments (50) which are joined to the second member (40) and engage the first member (32, 36). Each retainer segment (50) is an arcuate member defining inner and outer curved edges and first and second ends. Each end has a concave cutout (54) formed therein to reduce weld joint and bending stresses that occur from the forced vibration of the retainer segments (50).</abstract><edition>7</edition><oa>free_for_read</oa></addata></record> |
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| subjects | AIR AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING METHODSOR APPARATUS FOR COMBUSTION USING FLUID FUELOR SOLID FUEL SUSPENDED IN WEAPONS |
| title | Retainer segment for swirler assembly |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-16T21%3A54%3A24IST&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=THOMAS%20ANTHONY%20LEEN&rft.date=2005-07-21&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EAU782341BB2%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 |