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...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Thiriet Romain, Serghine Camel, Marucheau De Chanaud Nicolas, Marconi Patrick, Besse Jean-Louis, Barrat Philippe, Danguy Francois, Demezon Guillaume, Sannino Jean-Michel, Guillemet Pascal
Format: Patent
Sprache: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 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).
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US2017114723A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US2017114723A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US2017114723A13</originalsourceid><addsrcrecordid>eNqNjsEKgkAURd20iOofHrRNaDRwPYxPfTDODL4xaCUS0ypKsK_oq9NqG7S6F87hcpfRM8cjKYTCNiCZiT2ZEiSw1ZSDa6xDraXx79pqJmuAT-yxBlvM3qRrjNGUZBAq1KSs89jsfhJQtnYNzRi4VdU08vmwjhaX_jqGzTdX0bZAr6o4DPcujEN_Drfw6FpO9iIT4pAlqRTpf9YL14g_zw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>DEVICE FOR ASSISTING A SOLID PROPELLANT PROPULSION SYSTEM OF A SINGLE-ENGINE HELICOPTER, SINGLE-ENGINE HELICOPTER COMPRISING SUCH A DEVICE</title><source>esp@cenet</source><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</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&amp;date=20170427&amp;DB=EPODOC&amp;CC=US&amp;NR=2017114723A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20170427&amp;DB=EPODOC&amp;CC=US&amp;NR=2017114723A1$$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>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_epo_espacenet_US2017114723A1
source esp@cenet
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
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-04T20%3A57%3A38IST&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=Thiriet%20Romain&rft.date=2017-04-27&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EUS2017114723A1%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