V-BLADE AND V-GROOVE JOINT MOLDED COMPOSITE WEAR SLEEVE
An annular molded composite wear sleeve (40) is bonded with epoxy or other bonding agent in an annular V-groove (34) in a groove ring (64). Wear sleeve (40) may include forward and aft sleeve walls (46, 48) extending at forward and aft sleeve obtuse angles (50, 52) away from a sleeve bottom (44) and...
Gespeichert in:
| Hauptverfasser: | , , , , , |
|---|---|
| Format: | Patent |
| Sprache: | eng ; fre ; ger |
| 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 | SZEHIDEWICZ, Kamil DURCHHOLZ, Anthony John BLACKBURN, Michelle Ann HERNANDEZ LANGFORD, Carla Patricia RAVENHALL, John Andrew ROBINSON, Jordan Daniel |
| description | An annular molded composite wear sleeve (40) is bonded with epoxy or other bonding agent in an annular V-groove (34) in a groove ring (64). Wear sleeve (40) may include forward and aft sleeve walls (46, 48) extending at forward and aft sleeve obtuse angles (50, 52) away from a sleeve bottom (44) and may include annular forward and aft sleeve fillets (54, 56) between sleeve bottom (44) and forward and aft sleeve walls (46, 48). Aft sleeve wall (48) may include an aft flap (60) compliant with an annular aft taper (62) on groove ring (64). An aircraft gas turbine engine cowl clamping mechanism (22) for clamping a clamshell cowl (20) to a fan casing (26) includes groove ring (64) on a fan casing (26) and molded composite wear sleeve (40) bonded with epoxy or other bonding agent in annular V-groove (34) in groove ring (64). Annular V-blade (30) is on clamshell cowl (20) rotatable to insert annular V-blade (30) in annular V-groove (34). |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3187421A2</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3187421A2</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3187421A23</originalsourceid><addsrcrecordid>eNrjZDAP03XycXRxVXD0c1EI03UP8vcPc1Xw8vf0C1Hw9fdxcXVRcPb3DfAP9gxxVQh3dQxSCPZxdQ1z5WFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BxoYW5iZGho5GxkQoAQDFkSd-</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>V-BLADE AND V-GROOVE JOINT MOLDED COMPOSITE WEAR SLEEVE</title><source>esp@cenet</source><creator>SZEHIDEWICZ, Kamil ; DURCHHOLZ, Anthony John ; BLACKBURN, Michelle Ann ; HERNANDEZ LANGFORD, Carla Patricia ; RAVENHALL, John Andrew ; ROBINSON, Jordan Daniel</creator><creatorcontrib>SZEHIDEWICZ, Kamil ; DURCHHOLZ, Anthony John ; BLACKBURN, Michelle Ann ; HERNANDEZ LANGFORD, Carla Patricia ; RAVENHALL, John Andrew ; ROBINSON, Jordan Daniel</creatorcontrib><description>An annular molded composite wear sleeve (40) is bonded with epoxy or other bonding agent in an annular V-groove (34) in a groove ring (64). Wear sleeve (40) may include forward and aft sleeve walls (46, 48) extending at forward and aft sleeve obtuse angles (50, 52) away from a sleeve bottom (44) and may include annular forward and aft sleeve fillets (54, 56) between sleeve bottom (44) and forward and aft sleeve walls (46, 48). Aft sleeve wall (48) may include an aft flap (60) compliant with an annular aft taper (62) on groove ring (64). An aircraft gas turbine engine cowl clamping mechanism (22) for clamping a clamshell cowl (20) to a fan casing (26) includes groove ring (64) on a fan casing (26) and molded composite wear sleeve (40) bonded with epoxy or other bonding agent in annular V-groove (34) in groove ring (64). Annular V-blade (30) is on clamshell cowl (20) rotatable to insert annular V-blade (30) in annular V-groove (34).</description><language>eng ; fre ; ger</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT ; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</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=20170705&DB=EPODOC&CC=EP&NR=3187421A2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20170705&DB=EPODOC&CC=EP&NR=3187421A2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SZEHIDEWICZ, Kamil</creatorcontrib><creatorcontrib>DURCHHOLZ, Anthony John</creatorcontrib><creatorcontrib>BLACKBURN, Michelle Ann</creatorcontrib><creatorcontrib>HERNANDEZ LANGFORD, Carla Patricia</creatorcontrib><creatorcontrib>RAVENHALL, John Andrew</creatorcontrib><creatorcontrib>ROBINSON, Jordan Daniel</creatorcontrib><title>V-BLADE AND V-GROOVE JOINT MOLDED COMPOSITE WEAR SLEEVE</title><description>An annular molded composite wear sleeve (40) is bonded with epoxy or other bonding agent in an annular V-groove (34) in a groove ring (64). Wear sleeve (40) may include forward and aft sleeve walls (46, 48) extending at forward and aft sleeve obtuse angles (50, 52) away from a sleeve bottom (44) and may include annular forward and aft sleeve fillets (54, 56) between sleeve bottom (44) and forward and aft sleeve walls (46, 48). Aft sleeve wall (48) may include an aft flap (60) compliant with an annular aft taper (62) on groove ring (64). An aircraft gas turbine engine cowl clamping mechanism (22) for clamping a clamshell cowl (20) to a fan casing (26) includes groove ring (64) on a fan casing (26) and molded composite wear sleeve (40) bonded with epoxy or other bonding agent in annular V-groove (34) in groove ring (64). Annular V-blade (30) is on clamshell cowl (20) rotatable to insert annular V-blade (30) in annular V-groove (34).</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</subject><subject>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2017</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDAP03XycXRxVXD0c1EI03UP8vcPc1Xw8vf0C1Hw9fdxcXVRcPb3DfAP9gxxVQh3dQxSCPZxdQ1z5WFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BxoYW5iZGho5GxkQoAQDFkSd-</recordid><startdate>20170705</startdate><enddate>20170705</enddate><creator>SZEHIDEWICZ, Kamil</creator><creator>DURCHHOLZ, Anthony John</creator><creator>BLACKBURN, Michelle Ann</creator><creator>HERNANDEZ LANGFORD, Carla Patricia</creator><creator>RAVENHALL, John Andrew</creator><creator>ROBINSON, Jordan Daniel</creator><scope>EVB</scope></search><sort><creationdate>20170705</creationdate><title>V-BLADE AND V-GROOVE JOINT MOLDED COMPOSITE WEAR SLEEVE</title><author>SZEHIDEWICZ, Kamil ; DURCHHOLZ, Anthony John ; BLACKBURN, Michelle Ann ; HERNANDEZ LANGFORD, Carla Patricia ; RAVENHALL, John Andrew ; ROBINSON, Jordan Daniel</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3187421A23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2017</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</topic><topic>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>SZEHIDEWICZ, Kamil</creatorcontrib><creatorcontrib>DURCHHOLZ, Anthony John</creatorcontrib><creatorcontrib>BLACKBURN, Michelle Ann</creatorcontrib><creatorcontrib>HERNANDEZ LANGFORD, Carla Patricia</creatorcontrib><creatorcontrib>RAVENHALL, John Andrew</creatorcontrib><creatorcontrib>ROBINSON, Jordan Daniel</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SZEHIDEWICZ, Kamil</au><au>DURCHHOLZ, Anthony John</au><au>BLACKBURN, Michelle Ann</au><au>HERNANDEZ LANGFORD, Carla Patricia</au><au>RAVENHALL, John Andrew</au><au>ROBINSON, Jordan Daniel</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>V-BLADE AND V-GROOVE JOINT MOLDED COMPOSITE WEAR SLEEVE</title><date>2017-07-05</date><risdate>2017</risdate><abstract>An annular molded composite wear sleeve (40) is bonded with epoxy or other bonding agent in an annular V-groove (34) in a groove ring (64). Wear sleeve (40) may include forward and aft sleeve walls (46, 48) extending at forward and aft sleeve obtuse angles (50, 52) away from a sleeve bottom (44) and may include annular forward and aft sleeve fillets (54, 56) between sleeve bottom (44) and forward and aft sleeve walls (46, 48). Aft sleeve wall (48) may include an aft flap (60) compliant with an annular aft taper (62) on groove ring (64). An aircraft gas turbine engine cowl clamping mechanism (22) for clamping a clamshell cowl (20) to a fan casing (26) includes groove ring (64) on a fan casing (26) and molded composite wear sleeve (40) bonded with epoxy or other bonding agent in annular V-groove (34) in groove ring (64). Annular V-blade (30) is on clamshell cowl (20) rotatable to insert annular V-blade (30) in annular V-groove (34).</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng ; fre ; ger |
| recordid | cdi_epo_espacenet_EP3187421A2 |
| source | esp@cenet |
| subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
| title | V-BLADE AND V-GROOVE JOINT MOLDED COMPOSITE WEAR SLEEVE |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-02T06%3A21%3A54IST&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=SZEHIDEWICZ,%20Kamil&rft.date=2017-07-05&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3187421A2%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 |