BELLCRANK FOR A VARIABLE ADJUSTMENT DEVICE FOR A TURBOMACHINE
A bellcrank (30) for a variable adjustment device for an aircraft turbomachine, this bellcrank being articulated respectively to a control housing (12), to a synchronization bar (9), to a piston stem (11) of an actuator (A) and to a turnbuckle (6a), the bellcrank comprising a part for articulation t...
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| creator | BARBIER-NEVEU, Clélia ROBERT, Yann BOSTON, Erick |
| description | A bellcrank (30) for a variable adjustment device for an aircraft turbomachine, this bellcrank being articulated respectively to a control housing (12), to a synchronization bar (9), to a piston stem (11) of an actuator (A) and to a turnbuckle (6a), the bellcrank comprising a part for articulation to the control housing which comprises, on the one hand, a tab (36) and, on the other hand, a tubular portion (38) spaced apart from the tab (36), the tab and the tubular portion (38) comprising orifices (40) that are aligned and are configured to receive a common axis of articulation of the control housing (12).
Guignol (30) pour un dispositif de calage variable d'une turbomachine d'aéronef, ce guignol articulé respectivement à un boîtier de commande (12), à une barre de synchronisation (9), à une tige de piston (11) d'un actionneur (A) et à un ridoir (6a), le guignol comportant une partie d'articulation au boîtier de commande qui comprend d'une part une patte (36) et d'autre part une portion tubulaire (38) à distance de la patte (36), la patte et la portion tubulaire (38) comportant des orifices (40) alignés configurés pour recevoir un axe commun d'articulation du boîtier de commande (12). |
| format | Patent |
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Guignol (30) pour un dispositif de calage variable d'une turbomachine d'aéronef, ce guignol articulé respectivement à un boîtier de commande (12), à une barre de synchronisation (9), à une tige de piston (11) d'un actionneur (A) et à un ridoir (6a), le guignol comportant une partie d'articulation au boîtier de commande qui comprend d'une part une patte (36) et d'autre part une portion tubulaire (38) à distance de la patte (36), la patte et la portion tubulaire (38) comportant des orifices (40) alignés configurés pour recevoir un axe commun d'articulation du boîtier de commande (12).</description><language>eng ; fre</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 ; NON-POSITIVE DISPLACEMENT PUMPS ; POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS ; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS ; STEAM ENGINES ; WEAPONS</subject><creationdate>2021</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=20210304&DB=EPODOC&CC=WO&NR=2021038161A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210304&DB=EPODOC&CC=WO&NR=2021038161A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BARBIER-NEVEU, Clélia</creatorcontrib><creatorcontrib>ROBERT, Yann</creatorcontrib><creatorcontrib>BOSTON, Erick</creatorcontrib><title>BELLCRANK FOR A VARIABLE ADJUSTMENT DEVICE FOR A TURBOMACHINE</title><description>A bellcrank (30) for a variable adjustment device for an aircraft turbomachine, this bellcrank being articulated respectively to a control housing (12), to a synchronization bar (9), to a piston stem (11) of an actuator (A) and to a turnbuckle (6a), the bellcrank comprising a part for articulation to the control housing which comprises, on the one hand, a tab (36) and, on the other hand, a tubular portion (38) spaced apart from the tab (36), the tab and the tubular portion (38) comprising orifices (40) that are aligned and are configured to receive a common axis of articulation of the control housing (12).
Guignol (30) pour un dispositif de calage variable d'une turbomachine d'aéronef, ce guignol articulé respectivement à un boîtier de commande (12), à une barre de synchronisation (9), à une tige de piston (11) d'un actionneur (A) et à un ridoir (6a), le guignol comportant une partie d'articulation au boîtier de commande qui comprend d'une part une patte (36) et d'autre part une portion tubulaire (38) à distance de la patte (36), la patte et la portion tubulaire (38) comportant des orifices (40) alignés configurés pour recevoir un axe commun d'articulation du boîtier de commande (12).</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>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>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLB1cvXxcQ5y9PNWcPMPUnBUCHMM8nR08nFVcHTxCg0O8XX1C1FwcQ3zdHaFKggJDXLy93V09vD0c-VhYE1LzClO5YXS3AzKbq4hzh66qQX58anFBYnJqXmpJfHh_kYGRoYGxhaGZoaOhsbEqQIApnAqWA</recordid><startdate>20210304</startdate><enddate>20210304</enddate><creator>BARBIER-NEVEU, Clélia</creator><creator>ROBERT, Yann</creator><creator>BOSTON, Erick</creator><scope>EVB</scope></search><sort><creationdate>20210304</creationdate><title>BELLCRANK FOR A VARIABLE ADJUSTMENT DEVICE FOR A TURBOMACHINE</title><author>BARBIER-NEVEU, Clélia ; ROBERT, Yann ; BOSTON, Erick</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO2021038161A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2021</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>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>BARBIER-NEVEU, Clélia</creatorcontrib><creatorcontrib>ROBERT, Yann</creatorcontrib><creatorcontrib>BOSTON, Erick</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>BARBIER-NEVEU, Clélia</au><au>ROBERT, Yann</au><au>BOSTON, Erick</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>BELLCRANK FOR A VARIABLE ADJUSTMENT DEVICE FOR A TURBOMACHINE</title><date>2021-03-04</date><risdate>2021</risdate><abstract>A bellcrank (30) for a variable adjustment device for an aircraft turbomachine, this bellcrank being articulated respectively to a control housing (12), to a synchronization bar (9), to a piston stem (11) of an actuator (A) and to a turnbuckle (6a), the bellcrank comprising a part for articulation to the control housing which comprises, on the one hand, a tab (36) and, on the other hand, a tubular portion (38) spaced apart from the tab (36), the tab and the tubular portion (38) comprising orifices (40) that are aligned and are configured to receive a common axis of articulation of the control housing (12).
Guignol (30) pour un dispositif de calage variable d'une turbomachine d'aéronef, ce guignol articulé respectivement à un boîtier de commande (12), à une barre de synchronisation (9), à une tige de piston (11) d'un actionneur (A) et à un ridoir (6a), le guignol comportant une partie d'articulation au boîtier de commande qui comprend d'une part une patte (36) et d'autre part une portion tubulaire (38) à distance de la patte (36), la patte et la portion tubulaire (38) comportant des orifices (40) alignés configurés pour recevoir un axe commun d'articulation du boîtier de commande (12).</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre |
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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 NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS STEAM ENGINES WEAPONS |
| title | BELLCRANK FOR A VARIABLE ADJUSTMENT DEVICE FOR A TURBOMACHINE |
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