PROPULSION UNIT WITH PROPELLER COMPRISING A THERMAL ENGINE AND AN ELECTRIC ENGINE AS WELL AS AIRCRAFT COMPRISING SUCH A PROPULSION UNIT WITH PROPELLER
A propeller propulsion unit, comprising at least one kinematic system comprising at least: a heat engine, an electrical energy generator, an electric motor configured to generate a rotary movement as output from the electrical energy generated by the electrical energy generator, a drive and selectio...
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 | COLMAGRO, Jérôme LIEVEN, Patrick |
description | A propeller propulsion unit, comprising at least one kinematic system comprising at least: a heat engine, an electrical energy generator, an electric motor configured to generate a rotary movement as output from the electrical energy generated by the electrical energy generator, a drive and selection device configured to assume a first configuration, in which it is coupled to the output of the electric motor, and a second configuration, in which it is coupled to the main shaft of the heat engine, and a propeller rotated by the drive and selection device. Such a propeller propulsion unit with a hybrid engine allows more power to be provided and facilitates maintenance and ergonomics and is safer. |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3546366B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3546366B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3546366B13</originalsourceid><addsrcrecordid>eNqNjUEKwjAURLtxIeod_gVcSDT7GH-bD2kaflK6LEXiSrRQz-J5TUHElbgYBoaZN8vi6bnxrQ3UOGgdRegoGphDtBYZdFN7pkCuAgXRINfKArqKHIJypyxAizoy6U8coMvj2RWxZlXGb0xotcms37_rYnEZrlPavH1VQIlRm20a732axuGcbunRoxeHvRRSHnfij8oLclhB-g</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>PROPULSION UNIT WITH PROPELLER COMPRISING A THERMAL ENGINE AND AN ELECTRIC ENGINE AS WELL AS AIRCRAFT COMPRISING SUCH A PROPULSION UNIT WITH PROPELLER</title><source>esp@cenet</source><creator>COLMAGRO, Jérôme ; LIEVEN, Patrick</creator><creatorcontrib>COLMAGRO, Jérôme ; LIEVEN, Patrick</creatorcontrib><description>A propeller propulsion unit, comprising at least one kinematic system comprising at least: a heat engine, an electrical energy generator, an electric motor configured to generate a rotary movement as output from the electrical energy generated by the electrical energy generator, a drive and selection device configured to assume a first configuration, in which it is coupled to the output of the electric motor, and a second configuration, in which it is coupled to the main shaft of the heat engine, and a propeller rotated by the drive and selection device. Such a propeller propulsion unit with a hybrid engine allows more power to be provided and facilitates maintenance and ergonomics and is safer.</description><language>eng ; fre ; ger</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</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=20210922&DB=EPODOC&CC=EP&NR=3546366B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210922&DB=EPODOC&CC=EP&NR=3546366B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>COLMAGRO, Jérôme</creatorcontrib><creatorcontrib>LIEVEN, Patrick</creatorcontrib><title>PROPULSION UNIT WITH PROPELLER COMPRISING A THERMAL ENGINE AND AN ELECTRIC ENGINE AS WELL AS AIRCRAFT COMPRISING SUCH A PROPULSION UNIT WITH PROPELLER</title><description>A propeller propulsion unit, comprising at least one kinematic system comprising at least: a heat engine, an electrical energy generator, an electric motor configured to generate a rotary movement as output from the electrical energy generated by the electrical energy generator, a drive and selection device configured to assume a first configuration, in which it is coupled to the output of the electric motor, and a second configuration, in which it is coupled to the main shaft of the heat engine, and a propeller rotated by the drive and selection device. Such a propeller propulsion unit with a hybrid engine allows more power to be provided and facilitates maintenance and ergonomics and is safer.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjUEKwjAURLtxIeod_gVcSDT7GH-bD2kaflK6LEXiSrRQz-J5TUHElbgYBoaZN8vi6bnxrQ3UOGgdRegoGphDtBYZdFN7pkCuAgXRINfKArqKHIJypyxAizoy6U8coMvj2RWxZlXGb0xotcms37_rYnEZrlPavH1VQIlRm20a732axuGcbunRoxeHvRRSHnfij8oLclhB-g</recordid><startdate>20210922</startdate><enddate>20210922</enddate><creator>COLMAGRO, Jérôme</creator><creator>LIEVEN, Patrick</creator><scope>EVB</scope></search><sort><creationdate>20210922</creationdate><title>PROPULSION UNIT WITH PROPELLER COMPRISING A THERMAL ENGINE AND AN ELECTRIC ENGINE AS WELL AS AIRCRAFT COMPRISING SUCH A PROPULSION UNIT WITH PROPELLER</title><author>COLMAGRO, Jérôme ; LIEVEN, Patrick</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3546366B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2021</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>COLMAGRO, Jérôme</creatorcontrib><creatorcontrib>LIEVEN, Patrick</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>COLMAGRO, Jérôme</au><au>LIEVEN, Patrick</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>PROPULSION UNIT WITH PROPELLER COMPRISING A THERMAL ENGINE AND AN ELECTRIC ENGINE AS WELL AS AIRCRAFT COMPRISING SUCH A PROPULSION UNIT WITH PROPELLER</title><date>2021-09-22</date><risdate>2021</risdate><abstract>A propeller propulsion unit, comprising at least one kinematic system comprising at least: a heat engine, an electrical energy generator, an electric motor configured to generate a rotary movement as output from the electrical energy generated by the electrical energy generator, a drive and selection device configured to assume a first configuration, in which it is coupled to the output of the electric motor, and a second configuration, in which it is coupled to the main shaft of the heat engine, and a propeller rotated by the drive and selection device. Such a propeller propulsion unit with a hybrid engine allows more power to be provided and facilitates maintenance and ergonomics and is safer.</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | eng ; fre ; ger |
recordid | cdi_epo_espacenet_EP3546366B1 |
source | esp@cenet |
subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
title | PROPULSION UNIT WITH PROPELLER COMPRISING A THERMAL ENGINE AND AN ELECTRIC ENGINE AS WELL AS AIRCRAFT COMPRISING SUCH A PROPULSION UNIT WITH PROPELLER |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-29T02%3A54%3A16IST&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=COLMAGRO,%20J%C3%A9r%C3%B4me&rft.date=2021-09-22&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3546366B1%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 |