Durable Riblets for Engine Environment
The invention relates to durable riblets for engine environment. An airfoil of a propulsion device having a first riblet laminate with a first adhesive layer on at least a first portion of the airfoil surface and a first riblet array sheet disposed on at least a portion of the first adhesive layer....
Gespeichert in:
Hauptverfasser: | , , , |
---|---|
Format: | Patent |
Sprache: | chi ; eng |
Schlagworte: | |
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 | WENDY WENLING LIN LARA LIOU CASEY LAUREN BERSCHBACK TREVOR HOWARD WOOD |
description | The invention relates to durable riblets for engine environment. An airfoil of a propulsion device having a first riblet laminate with a first adhesive layer on at least a first portion of the airfoil surface and a first riblet array sheet disposed on at least a portion of the first adhesive layer. The first riblet array sheet defines a first plurality of contiguous geometric features having rigid peaks and valleys extending in a first rib direction. The first plurality of contiguous geometric features define a total width to total height ratio W:H of about 1:1 to about 2.5:1 with a maximum total height of about 0.65 mm or less. A second riblet array laminate is also disclosed in an embodiment.
本发明涉及用于发动机环境的耐用凸肋。具体而言,种推进装置的翼型件(90)具有第凸肋叠层(136),其具有在翼型件表面(92)的至少第部分上的第粘合层(156)以及设置在第粘合层(156)的至少部分上的第凸肋阵列板(130)。第凸肋阵列板(130)限定第多个连续几何特征(110),其具有在第肋方向上延伸的刚性的峰部(146)和谷部(148)。第多个连续几何特征(110)限定带有大约0.65mm或更小的最大总高度的大约1:1到大约2.5:1的总宽度与总高度比W:H。实施例中还公开了第二凸肋阵列叠层(132)。 |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN106870452A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN106870452A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN106870452A3</originalsourceid><addsrcrecordid>eNrjZFBzKS1KTMpJVQjKBJIlxQpp-UUKrnnpmXmpQKossyg_Lzc1r4SHgTUtMac4lRdKczMourmGOHvophbkx6cWFyQmp-allsQ7-xkamFmYG5iYGjkaE6MGAFOIJ1U</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Durable Riblets for Engine Environment</title><source>esp@cenet</source><creator>WENDY WENLING LIN ; LARA LIOU ; CASEY LAUREN BERSCHBACK ; TREVOR HOWARD WOOD</creator><creatorcontrib>WENDY WENLING LIN ; LARA LIOU ; CASEY LAUREN BERSCHBACK ; TREVOR HOWARD WOOD</creatorcontrib><description>The invention relates to durable riblets for engine environment. An airfoil of a propulsion device having a first riblet laminate with a first adhesive layer on at least a first portion of the airfoil surface and a first riblet array sheet disposed on at least a portion of the first adhesive layer. The first riblet array sheet defines a first plurality of contiguous geometric features having rigid peaks and valleys extending in a first rib direction. The first plurality of contiguous geometric features define a total width to total height ratio W:H of about 1:1 to about 2.5:1 with a maximum total height of about 0.65 mm or less. A second riblet array laminate is also disclosed in an embodiment.
本发明涉及用于发动机环境的耐用凸肋。具体而言,种推进装置的翼型件(90)具有第凸肋叠层(136),其具有在翼型件表面(92)的至少第部分上的第粘合层(156)以及设置在第粘合层(156)的至少部分上的第凸肋阵列板(130)。第凸肋阵列板(130)限定第多个连续几何特征(110),其具有在第肋方向上延伸的刚性的峰部(146)和谷部(148)。第多个连续几何特征(110)限定带有大约0.65mm或更小的最大总高度的大约1:1到大约2.5:1的总宽度与总高度比W:H。实施例中还公开了第二凸肋阵列叠层(132)。</description><language>chi ; eng</language><subject>BLASTING ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT PUMPS ; POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS ; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS ; WEAPONS</subject><creationdate>2017</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=20170620&DB=EPODOC&CC=CN&NR=106870452A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76516</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20170620&DB=EPODOC&CC=CN&NR=106870452A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WENDY WENLING LIN</creatorcontrib><creatorcontrib>LARA LIOU</creatorcontrib><creatorcontrib>CASEY LAUREN BERSCHBACK</creatorcontrib><creatorcontrib>TREVOR HOWARD WOOD</creatorcontrib><title>Durable Riblets for Engine Environment</title><description>The invention relates to durable riblets for engine environment. An airfoil of a propulsion device having a first riblet laminate with a first adhesive layer on at least a first portion of the airfoil surface and a first riblet array sheet disposed on at least a portion of the first adhesive layer. The first riblet array sheet defines a first plurality of contiguous geometric features having rigid peaks and valleys extending in a first rib direction. The first plurality of contiguous geometric features define a total width to total height ratio W:H of about 1:1 to about 2.5:1 with a maximum total height of about 0.65 mm or less. A second riblet array laminate is also disclosed in an embodiment.
本发明涉及用于发动机环境的耐用凸肋。具体而言,种推进装置的翼型件(90)具有第凸肋叠层(136),其具有在翼型件表面(92)的至少第部分上的第粘合层(156)以及设置在第粘合层(156)的至少部分上的第凸肋阵列板(130)。第凸肋阵列板(130)限定第多个连续几何特征(110),其具有在第肋方向上延伸的刚性的峰部(146)和谷部(148)。第多个连续几何特征(110)限定带有大约0.65mm或更小的最大总高度的大约1:1到大约2.5:1的总宽度与总高度比W:H。实施例中还公开了第二凸肋阵列叠层(132)。</description><subject>BLASTING</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT PUMPS</subject><subject>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</subject><subject>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2017</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFBzKS1KTMpJVQjKBJIlxQpp-UUKrnnpmXmpQKossyg_Lzc1r4SHgTUtMac4lRdKczMourmGOHvophbkx6cWFyQmp-allsQ7-xkamFmYG5iYGjkaE6MGAFOIJ1U</recordid><startdate>20170620</startdate><enddate>20170620</enddate><creator>WENDY WENLING LIN</creator><creator>LARA LIOU</creator><creator>CASEY LAUREN BERSCHBACK</creator><creator>TREVOR HOWARD WOOD</creator><scope>EVB</scope></search><sort><creationdate>20170620</creationdate><title>Durable Riblets for Engine Environment</title><author>WENDY WENLING LIN ; LARA LIOU ; CASEY LAUREN BERSCHBACK ; TREVOR HOWARD WOOD</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN106870452A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2017</creationdate><topic>BLASTING</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT PUMPS</topic><topic>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</topic><topic>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>WENDY WENLING LIN</creatorcontrib><creatorcontrib>LARA LIOU</creatorcontrib><creatorcontrib>CASEY LAUREN BERSCHBACK</creatorcontrib><creatorcontrib>TREVOR HOWARD WOOD</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WENDY WENLING LIN</au><au>LARA LIOU</au><au>CASEY LAUREN BERSCHBACK</au><au>TREVOR HOWARD WOOD</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Durable Riblets for Engine Environment</title><date>2017-06-20</date><risdate>2017</risdate><abstract>The invention relates to durable riblets for engine environment. An airfoil of a propulsion device having a first riblet laminate with a first adhesive layer on at least a first portion of the airfoil surface and a first riblet array sheet disposed on at least a portion of the first adhesive layer. The first riblet array sheet defines a first plurality of contiguous geometric features having rigid peaks and valleys extending in a first rib direction. The first plurality of contiguous geometric features define a total width to total height ratio W:H of about 1:1 to about 2.5:1 with a maximum total height of about 0.65 mm or less. A second riblet array laminate is also disclosed in an embodiment.
本发明涉及用于发动机环境的耐用凸肋。具体而言,种推进装置的翼型件(90)具有第凸肋叠层(136),其具有在翼型件表面(92)的至少第部分上的第粘合层(156)以及设置在第粘合层(156)的至少部分上的第凸肋阵列板(130)。第凸肋阵列板(130)限定第多个连续几何特征(110),其具有在第肋方向上延伸的刚性的峰部(146)和谷部(148)。第多个连续几何特征(110)限定带有大约0.65mm或更小的最大总高度的大约1:1到大约2.5:1的总宽度与总高度比W:H。实施例中还公开了第二凸肋阵列叠层(132)。</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | chi ; eng |
recordid | cdi_epo_espacenet_CN106870452A |
source | esp@cenet |
subjects | BLASTING HEATING LIGHTING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS WEAPONS |
title | Durable Riblets for Engine Environment |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-20T21%3A24%3A45IST&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=WENDY%20WENLING%20LIN&rft.date=2017-06-20&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN106870452A%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 |