PROPULSION SYSTEM FOR AN AIRCRAFT
A hybrid-electric propulsion system includes a propulsor, a turbomachine, and an electrical system. The electrical system includes a first electric machine coupled to the turbomachine and an electric energy storage unit. A method for operating the propulsion system includes operating the hybrid elec...
Gespeichert in:
| Hauptverfasser: | , |
|---|---|
| Format: | Patent |
| Sprache: | eng ; fre |
| 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 includes a propulsor, a turbomachine, and an electrical system. The electrical system includes a first electric machine coupled to the turbomachine and an electric energy storage unit. A method for operating the propulsion system includes operating the hybrid electric propulsion system in a flight operation mode. The method also includes operating the hybrid electric propulsion system in a maintenance operation mode, wherein operating the hybrid electric propulsion system in the maintenance operation mode includes providing electrical power from an electrical power source to the first electric machine such that the first electric machine rotates a compressor and a turbine of the turbomachine during a borescope inspection of the turbomachine.
Un système de propulsion électrique hybride comprend un propulseur, une turbomachine et un système électrique. Le système électrique comprend une première machine électrique couplée à la turbomachine et à une unité de stockage dénergie électrique. Une mode dopération du système de propulsion consiste à opérer le système de propulsion électrique hybride dans un mode de vol. La méthode consiste également à opérer le système de propulsion électrique hybride dans un mode de maintenance, dans lequel lopération du système de propulsion électrique hybride comprend la fourniture dénergie électrique provenant dune source dalimentation à la première machine électrique de sorte cette dernière fasse tourner un compresseur et une turbine constituant la turbomachine lors de linspection endoscopique de celle-ci. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CA3008406C</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CA3008406C</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CA3008406C3</originalsourceid><addsrcrecordid>eNrjZFAMCPIPCPUJ9vT3UwiODA5x9VVw8w9ScPRTcPQMcg5ydAvhYWBNS8wpTuWF0twM8m6uIc4euqkF-fGpxQWJyal5qSXxzo7GBgYWJgZmzsaEVQAAot8hWg</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 includes a propulsor, a turbomachine, and an electrical system. The electrical system includes a first electric machine coupled to the turbomachine and an electric energy storage unit. A method for operating the propulsion system includes operating the hybrid electric propulsion system in a flight operation mode. The method also includes operating the hybrid electric propulsion system in a maintenance operation mode, wherein operating the hybrid electric propulsion system in the maintenance operation mode includes providing electrical power from an electrical power source to the first electric machine such that the first electric machine rotates a compressor and a turbine of the turbomachine during a borescope inspection of the turbomachine.
Un système de propulsion électrique hybride comprend un propulseur, une turbomachine et un système électrique. Le système électrique comprend une première machine électrique couplée à la turbomachine et à une unité de stockage dénergie électrique. Une mode dopération du système de propulsion consiste à opérer le système de propulsion électrique hybride dans un mode de vol. La méthode consiste également à opérer le système de propulsion électrique hybride dans un mode de maintenance, dans lequel lopération du système de propulsion électrique hybride comprend la fourniture dénergie électrique provenant dune source dalimentation à la première machine électrique de sorte cette dernière fasse tourner un compresseur et une turbine constituant la turbomachine lors de linspection endoscopique de celle-ci.</description><language>eng ; fre</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; COSMONAUTICS ; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GAS-TURBINE PLANTS ; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT ; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING ; WEAPONS</subject><creationdate>2022</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=20220301&DB=EPODOC&CC=CA&NR=3008406C$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220301&DB=EPODOC&CC=CA&NR=3008406C$$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 includes a propulsor, a turbomachine, and an electrical system. The electrical system includes a first electric machine coupled to the turbomachine and an electric energy storage unit. A method for operating the propulsion system includes operating the hybrid electric propulsion system in a flight operation mode. The method also includes operating the hybrid electric propulsion system in a maintenance operation mode, wherein operating the hybrid electric propulsion system in the maintenance operation mode includes providing electrical power from an electrical power source to the first electric machine such that the first electric machine rotates a compressor and a turbine of the turbomachine during a borescope inspection of the turbomachine.
Un système de propulsion électrique hybride comprend un propulseur, une turbomachine et un système électrique. Le système électrique comprend une première machine électrique couplée à la turbomachine et à une unité de stockage dénergie électrique. Une mode dopération du système de propulsion consiste à opérer le système de propulsion électrique hybride dans un mode de vol. La méthode consiste également à opérer le système de propulsion électrique hybride dans un mode de maintenance, dans lequel lopération du système de propulsion électrique hybride comprend la fourniture dénergie électrique provenant dune source dalimentation à la première machine électrique de sorte cette dernière fasse tourner un compresseur et une turbine constituant la turbomachine lors de linspection endoscopique de celle-ci.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>COSMONAUTICS</subject><subject>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>GAS-TURBINE PLANTS</subject><subject>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</subject><subject>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFAMCPIPCPUJ9vT3UwiODA5x9VVw8w9ScPRTcPQMcg5ydAvhYWBNS8wpTuWF0twM8m6uIc4euqkF-fGpxQWJyal5qSXxzo7GBgYWJgZmzsaEVQAAot8hWg</recordid><startdate>20220301</startdate><enddate>20220301</enddate><creator>GANSLER, MICHAEL THOMAS</creator><creator>HON, ROBERT CHARLES</creator><scope>EVB</scope></search><sort><creationdate>20220301</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_CA3008406C3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2022</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>COSMONAUTICS</topic><topic>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>GAS-TURBINE PLANTS</topic><topic>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</topic><topic>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</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>2022-03-01</date><risdate>2022</risdate><abstract>A hybrid-electric propulsion system includes a propulsor, a turbomachine, and an electrical system. The electrical system includes a first electric machine coupled to the turbomachine and an electric energy storage unit. A method for operating the propulsion system includes operating the hybrid electric propulsion system in a flight operation mode. The method also includes operating the hybrid electric propulsion system in a maintenance operation mode, wherein operating the hybrid electric propulsion system in the maintenance operation mode includes providing electrical power from an electrical power source to the first electric machine such that the first electric machine rotates a compressor and a turbine of the turbomachine during a borescope inspection of the turbomachine.
Un système de propulsion électrique hybride comprend un propulseur, une turbomachine et un système électrique. Le système électrique comprend une première machine électrique couplée à la turbomachine et à une unité de stockage dénergie électrique. Une mode dopération du système de propulsion consiste à opérer le système de propulsion électrique hybride dans un mode de vol. La méthode consiste également à opérer le système de propulsion électrique hybride dans un mode de maintenance, dans lequel lopération du système de propulsion électrique hybride comprend la fourniture dénergie électrique provenant dune source dalimentation à la première machine électrique de sorte cette dernière fasse tourner un compresseur et une turbine constituant la turbomachine lors de linspection endoscopique de celle-ci.</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng ; fre |
| recordid | cdi_epo_espacenet_CA3008406C |
| source | esp@cenet |
| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS 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=2025-01-17T23%3A11%3A52IST&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=2022-03-01&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECA3008406C%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 |