System for attaching a turbojet engine spinner
Disclosed is an upstream rotor of a turbomachine comprising a spinner 2 which is removably attached to the upstream end of the rotor 1 by attachment means comprising a dog clutch 3, 9, 10 and rotation-preventing means which lock the spinner 2 in place to prevent rotation of the spinner 2 relative to...
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| creator | Emmanuel Patsouris Jacques Rene Bart |
| description | Disclosed is an upstream rotor of a turbomachine comprising a spinner 2 which is removably attached to the upstream end of the rotor 1 by attachment means comprising a dog clutch 3, 9, 10 and rotation-preventing means which lock the spinner 2 in place to prevent rotation of the spinner 2 relative to the rotor 1. The rotation-preventing means comprise pegs 13 which are resiliently urged to the locked position by elastically deformable means such as spring 17. |
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| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_GB2503075A9</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>GB2503075A9</sourcerecordid><originalsourceid>FETCH-epo_espacenet_GB2503075A93</originalsourceid><addsrcrecordid>eNrjZNALriwuSc1VSMsvUkgsKUlMzsjMS1dIVCgpLUrKz0otUUjNS8_MS1UoLsjMy0st4mFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8e5ORqYGxgbmpo6WxkQoAQCrKCol</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>System for attaching a turbojet engine spinner</title><source>esp@cenet</source><creator>Emmanuel Patsouris ; Jacques Rene Bart</creator><creatorcontrib>Emmanuel Patsouris ; Jacques Rene Bart</creatorcontrib><description>Disclosed is an upstream rotor of a turbomachine comprising a spinner 2 which is removably attached to the upstream end of the rotor 1 by attachment means comprising a dog clutch 3, 9, 10 and rotation-preventing means which lock the spinner 2 in place to prevent rotation of the spinner 2 relative to the rotor 1. The rotation-preventing means comprise pegs 13 which are resiliently urged to the locked position by elastically deformable means such as spring 17.</description><language>eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; ENGINE PLANTS IN GENERAL ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; WEAPONS</subject><creationdate>2018</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=20180228&DB=EPODOC&CC=GB&NR=2503075A9$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76516</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20180228&DB=EPODOC&CC=GB&NR=2503075A9$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Emmanuel Patsouris</creatorcontrib><creatorcontrib>Jacques Rene Bart</creatorcontrib><title>System for attaching a turbojet engine spinner</title><description>Disclosed is an upstream rotor of a turbomachine comprising a spinner 2 which is removably attached to the upstream end of the rotor 1 by attachment means comprising a dog clutch 3, 9, 10 and rotation-preventing means which lock the spinner 2 in place to prevent rotation of the spinner 2 relative to the rotor 1. The rotation-preventing means comprise pegs 13 which are resiliently urged to the locked position by elastically deformable means such as spring 17.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</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>STEAM ENGINES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNALriwuSc1VSMsvUkgsKUlMzsjMS1dIVCgpLUrKz0otUUjNS8_MS1UoLsjMy0st4mFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8e5ORqYGxgbmpo6WxkQoAQCrKCol</recordid><startdate>20180228</startdate><enddate>20180228</enddate><creator>Emmanuel Patsouris</creator><creator>Jacques Rene Bart</creator><scope>EVB</scope></search><sort><creationdate>20180228</creationdate><title>System for attaching a turbojet engine spinner</title><author>Emmanuel Patsouris ; Jacques Rene Bart</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_GB2503075A93</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2018</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</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>STEAM ENGINES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>Emmanuel Patsouris</creatorcontrib><creatorcontrib>Jacques Rene Bart</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Emmanuel Patsouris</au><au>Jacques Rene Bart</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>System for attaching a turbojet engine spinner</title><date>2018-02-28</date><risdate>2018</risdate><abstract>Disclosed is an upstream rotor of a turbomachine comprising a spinner 2 which is removably attached to the upstream end of the rotor 1 by attachment means comprising a dog clutch 3, 9, 10 and rotation-preventing means which lock the spinner 2 in place to prevent rotation of the spinner 2 relative to the rotor 1. The rotation-preventing means comprise pegs 13 which are resiliently urged to the locked position by elastically deformable means such as spring 17.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS |
| title | System for attaching a turbojet engine spinner |
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