PROPULSION SYSTEM FOR AN AIRCRAFT

A hybrid-electric propulsion system (50) includes a propulsor (104), a turbomachine (102), and an electrical system, the electrical system including an electric machine (56) coupled to the turbomachine (102). A method for operating the propulsion system (50) includes operating at (302), by one or mo...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: GANSLER, Michael Thomas, HON, Robert Charles
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 GANSLER, Michael Thomas
HON, Robert Charles
description A hybrid-electric propulsion system (50) includes a propulsor (104), a turbomachine (102), and an electrical system, the electrical system including an electric machine (56) coupled to the turbomachine (102). A method for operating the propulsion system (50) includes operating at (302), by one or more computing devices, the turbomachine such that the turbomachine rotates the propulsor; receiving at (304), by the one or more computing devices, a command to accelerate the turbomachine while operating the turbomachine; and providing at (306), by the one or more computing devices, electrical power to the electric machine to add power to the turbomachine, the propulsor, or both in response to the received command to accelerate the turbomachine.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3421369B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3421369B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3421369B13</originalsourceid><addsrcrecordid>eNrjZFAMCPIPCPUJ9vT3UwiODA5x9VVw8w9ScPRTcPQMcg5ydAvhYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxrgHGJkaGxmaWTobGRCgBAOgWIew</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>PROPULSION SYSTEM FOR AN AIRCRAFT</title><source>esp@cenet</source><creator>GANSLER, Michael Thomas ; HON, Robert Charles</creator><creatorcontrib>GANSLER, Michael Thomas ; HON, Robert Charles</creatorcontrib><description>A hybrid-electric propulsion system (50) includes a propulsor (104), a turbomachine (102), and an electrical system, the electrical system including an electric machine (56) coupled to the turbomachine (102). A method for operating the propulsion system (50) includes operating at (302), by one or more computing devices, the turbomachine such that the turbomachine rotates the propulsor; receiving at (304), by the one or more computing devices, a command to accelerate the turbomachine while operating the turbomachine; and providing at (306), by the one or more computing devices, electrical power to the electric machine to add power to the turbomachine, the propulsor, or both in response to the received command to accelerate the turbomachine.</description><language>eng ; fre ; ger</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BLASTING ; COSMONAUTICS ; ENGINE PLANTS IN GENERAL ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; PARACHUTES ; PERFORMING OPERATIONS ; STEAM ENGINES ; TRANSPORTING ; WEAPONS</subject><creationdate>2023</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=20230913&amp;DB=EPODOC&amp;CC=EP&amp;NR=3421369B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20230913&amp;DB=EPODOC&amp;CC=EP&amp;NR=3421369B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GANSLER, Michael Thomas</creatorcontrib><creatorcontrib>HON, Robert Charles</creatorcontrib><title>PROPULSION SYSTEM FOR AN AIRCRAFT</title><description>A hybrid-electric propulsion system (50) includes a propulsor (104), a turbomachine (102), and an electrical system, the electrical system including an electric machine (56) coupled to the turbomachine (102). A method for operating the propulsion system (50) includes operating at (302), by one or more computing devices, the turbomachine such that the turbomachine rotates the propulsor; receiving at (304), by the one or more computing devices, a command to accelerate the turbomachine while operating the turbomachine; and providing at (306), by the one or more computing devices, electrical power to the electric machine to add power to the turbomachine, the propulsor, or both in response to the received command to accelerate the turbomachine.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>HEATING</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>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>STEAM ENGINES</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFAMCPIPCPUJ9vT3UwiODA5x9VVw8w9ScPRTcPQMcg5ydAvhYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxrgHGJkaGxmaWTobGRCgBAOgWIew</recordid><startdate>20230913</startdate><enddate>20230913</enddate><creator>GANSLER, Michael Thomas</creator><creator>HON, Robert Charles</creator><scope>EVB</scope></search><sort><creationdate>20230913</creationdate><title>PROPULSION SYSTEM FOR AN AIRCRAFT</title><author>GANSLER, Michael Thomas ; HON, Robert Charles</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3421369B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2023</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COSMONAUTICS</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>HEATING</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>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>STEAM ENGINES</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>GANSLER, Michael Thomas</creatorcontrib><creatorcontrib>HON, Robert Charles</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>GANSLER, Michael Thomas</au><au>HON, Robert Charles</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>PROPULSION SYSTEM FOR AN AIRCRAFT</title><date>2023-09-13</date><risdate>2023</risdate><abstract>A hybrid-electric propulsion system (50) includes a propulsor (104), a turbomachine (102), and an electrical system, the electrical system including an electric machine (56) coupled to the turbomachine (102). A method for operating the propulsion system (50) includes operating at (302), by one or more computing devices, the turbomachine such that the turbomachine rotates the propulsor; receiving at (304), by the one or more computing devices, a command to accelerate the turbomachine while operating the turbomachine; and providing at (306), by the one or more computing devices, electrical power to the electric machine to add power to the turbomachine, the propulsor, or both in response to the received command to accelerate the turbomachine.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP3421369B1
source esp@cenet
subjects AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
BLASTING
COSMONAUTICS
ENGINE PLANTS IN GENERAL
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
PARACHUTES
PERFORMING OPERATIONS
STEAM ENGINES
TRANSPORTING
WEAPONS
title PROPULSION SYSTEM FOR AN AIRCRAFT
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-12T00%3A58%3A49IST&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=GANSLER,%20Michael%20Thomas&rft.date=2023-09-13&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3421369B1%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