DEVICE FOR ASSISTING A SOLID PROPELLANT PROPULSION SYSTEM OF A SINGLE-ENGINE HELICOPTER, SINGLE-ENGINE HELICOPTER COMPRISING SUCH A DEVICE
The invention relates to a device for assisting a propulsion system of a single-engine helicopter, comprising an engine connected to a power transmission gearbox (15) suitable for rotating a rotor (88) of the helicopter, characterised in that it comprises: a turbine (18) for driving in rotation an o...
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creator | Thiriet Romain Serghine Camel Marucheau De Chanaud Nicolas Marconi Patrick Besse Jean-Louis Barrat Philippe Danguy Francois Demezon Guillaume Sannino Jean-Michel Guillemet Pascal |
description | The invention relates to a device for assisting a propulsion system of a single-engine helicopter, comprising an engine connected to a power transmission gearbox (15) suitable for rotating a rotor (88) of the helicopter, characterised in that it comprises: a turbine (18) for driving in rotation an output shaft (34) that is mechanically connected to said power transmission gearbox (15); and controlled means (16) for supplying said drive turbine (18) with pressurised fluid in order to allow said turbine (18) to transform the power from said pressurised fluid into mechanical power for rotating said output shaft (34). |
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Demezon Guillaume ; Sannino Jean-Michel ; Guillemet Pascal</creator><creatorcontrib>Thiriet Romain ; Serghine Camel ; Marucheau De Chanaud Nicolas ; Marconi Patrick ; Besse Jean-Louis ; Barrat Philippe ; Danguy Francois ; Demezon Guillaume ; Sannino Jean-Michel ; Guillemet Pascal</creatorcontrib><description>The invention relates to a device for assisting a propulsion system of a single-engine helicopter, comprising an engine connected to a power transmission gearbox (15) suitable for rotating a rotor (88) of the helicopter, characterised in that it comprises: a turbine (18) for driving in rotation an output shaft (34) that is mechanically connected to said power transmission gearbox (15); and controlled means (16) for supplying said drive turbine (18) with pressurised fluid in order to allow said turbine (18) to transform the power from said pressurised fluid into mechanical power for rotating said output shaft (34).</description><language>eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; 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=20170427&DB=EPODOC&CC=US&NR=2017114723A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20170427&DB=EPODOC&CC=US&NR=2017114723A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Thiriet Romain</creatorcontrib><creatorcontrib>Serghine Camel</creatorcontrib><creatorcontrib>Marucheau De Chanaud Nicolas</creatorcontrib><creatorcontrib>Marconi Patrick</creatorcontrib><creatorcontrib>Besse Jean-Louis</creatorcontrib><creatorcontrib>Barrat Philippe</creatorcontrib><creatorcontrib>Danguy Francois</creatorcontrib><creatorcontrib>Demezon Guillaume</creatorcontrib><creatorcontrib>Sannino Jean-Michel</creatorcontrib><creatorcontrib>Guillemet Pascal</creatorcontrib><title>DEVICE FOR ASSISTING A SOLID PROPELLANT PROPULSION SYSTEM OF A SINGLE-ENGINE HELICOPTER, SINGLE-ENGINE HELICOPTER COMPRISING SUCH A DEVICE</title><description>The invention relates to a device for assisting a propulsion system of a single-engine helicopter, comprising an engine connected to a power transmission gearbox (15) suitable for rotating a rotor (88) of the helicopter, characterised in that it comprises: a turbine (18) for driving in rotation an output shaft (34) that is mechanically connected to said power transmission gearbox (15); and controlled means (16) for supplying said drive turbine (18) with pressurised fluid in order to allow said turbine (18) to transform the power from said pressurised fluid into mechanical power for rotating said output shaft (34).</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>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2017</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjsEKgkAURd20iOofHrRNaDRwPYxPfTDODL4xaCUS0ypKsK_oq9NqG7S6F87hcpfRM8cjKYTCNiCZiT2ZEiSw1ZSDa6xDraXx79pqJmuAT-yxBlvM3qRrjNGUZBAq1KSs89jsfhJQtnYNzRi4VdU08vmwjhaX_jqGzTdX0bZAr6o4DPcujEN_Drfw6FpO9iIT4pAlqRTpf9YL14g_zw</recordid><startdate>20170427</startdate><enddate>20170427</enddate><creator>Thiriet Romain</creator><creator>Serghine Camel</creator><creator>Marucheau De Chanaud Nicolas</creator><creator>Marconi Patrick</creator><creator>Besse Jean-Louis</creator><creator>Barrat Philippe</creator><creator>Danguy Francois</creator><creator>Demezon Guillaume</creator><creator>Sannino Jean-Michel</creator><creator>Guillemet Pascal</creator><scope>EVB</scope></search><sort><creationdate>20170427</creationdate><title>DEVICE FOR ASSISTING A SOLID PROPELLANT PROPULSION SYSTEM OF A SINGLE-ENGINE HELICOPTER, SINGLE-ENGINE HELICOPTER COMPRISING SUCH A DEVICE</title><author>Thiriet Romain ; Serghine Camel ; Marucheau De Chanaud Nicolas ; Marconi Patrick ; Besse Jean-Louis ; Barrat Philippe ; Danguy Francois ; Demezon Guillaume ; Sannino Jean-Michel ; Guillemet Pascal</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2017114723A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2017</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>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>Thiriet Romain</creatorcontrib><creatorcontrib>Serghine Camel</creatorcontrib><creatorcontrib>Marucheau De Chanaud Nicolas</creatorcontrib><creatorcontrib>Marconi Patrick</creatorcontrib><creatorcontrib>Besse Jean-Louis</creatorcontrib><creatorcontrib>Barrat Philippe</creatorcontrib><creatorcontrib>Danguy Francois</creatorcontrib><creatorcontrib>Demezon Guillaume</creatorcontrib><creatorcontrib>Sannino Jean-Michel</creatorcontrib><creatorcontrib>Guillemet Pascal</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Thiriet Romain</au><au>Serghine Camel</au><au>Marucheau De Chanaud Nicolas</au><au>Marconi Patrick</au><au>Besse Jean-Louis</au><au>Barrat Philippe</au><au>Danguy Francois</au><au>Demezon Guillaume</au><au>Sannino Jean-Michel</au><au>Guillemet Pascal</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>DEVICE FOR ASSISTING A SOLID PROPELLANT PROPULSION SYSTEM OF A SINGLE-ENGINE HELICOPTER, SINGLE-ENGINE HELICOPTER COMPRISING SUCH A DEVICE</title><date>2017-04-27</date><risdate>2017</risdate><abstract>The invention relates to a device for assisting a propulsion system of a single-engine helicopter, comprising an engine connected to a power transmission gearbox (15) suitable for rotating a rotor (88) of the helicopter, characterised in that it comprises: a turbine (18) for driving in rotation an output shaft (34) that is mechanically connected to said power transmission gearbox (15); and controlled means (16) for supplying said drive turbine (18) with pressurised fluid in order to allow said turbine (18) to transform the power from said pressurised fluid into mechanical power for rotating said output shaft (34).</abstract><oa>free_for_read</oa></addata></record> |
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subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS |
title | DEVICE FOR ASSISTING A SOLID PROPELLANT PROPULSION SYSTEM OF A SINGLE-ENGINE HELICOPTER, SINGLE-ENGINE HELICOPTER COMPRISING SUCH A DEVICE |
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