SYSTEMS AND METHODS FOR OVERVOLTAGE PROTECTION ON LOADS FOR USE IN AN ELECTRIC AIRCRAFT
A system for overvoltage protection on loads for use in an electric aircraft is presented. The system includes an energy storage element configured to produce an electrical output, a bus element, wherein the bus is configured to transfer the electrical output from the energy storage element, a plura...
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| creator | Richter, Timothy Gerard |
| description | A system for overvoltage protection on loads for use in an electric aircraft is presented. The system includes an energy storage element configured to produce an electrical output, a bus element, wherein the bus is configured to transfer the electrical output from the energy storage element, a plurality of inverters, wherein each inverter is configured to generate a regulated output as a function of the electrical output and detect an overvoltage output as a function of the regulated output, and a plurality of load devices connected to the plurality of inverters, wherein each load device includes a fault protection device. |
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The system includes an energy storage element configured to produce an electrical output, a bus element, wherein the bus is configured to transfer the electrical output from the energy storage element, a plurality of inverters, wherein each inverter is configured to generate a regulated output as a function of the electrical output and detect an overvoltage output as a function of the regulated output, and a plurality of load devices connected to the plurality of inverters, wherein each load device includes a fault protection device.</description><language>eng</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER ; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER ; COSMONAUTICS ; ELECTRIC EQUIPMENT OR PROPULSION OF ELECTRICALLY-PROPELLEDVEHICLES ; ELECTRICITY ; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES, IN GENERAL ; EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GENERATION ; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES ; PARACHUTES ; PERFORMING OPERATIONS ; SYSTEMS FOR STORING ELECTRIC ENERGY ; TRANSPORTING ; VEHICLES IN GENERAL</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&date=20231102&DB=EPODOC&CC=US&NR=2023352949A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25555,76308</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20231102&DB=EPODOC&CC=US&NR=2023352949A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Richter, Timothy Gerard</creatorcontrib><title>SYSTEMS AND METHODS FOR OVERVOLTAGE PROTECTION ON LOADS FOR USE IN AN ELECTRIC AIRCRAFT</title><description>A system for overvoltage protection on loads for use in an electric aircraft is presented. The system includes an energy storage element configured to produce an electrical output, a bus element, wherein the bus is configured to transfer the electrical output from the energy storage element, a plurality of inverters, wherein each inverter is configured to generate a regulated output as a function of the electrical output and detect an overvoltage output as a function of the regulated output, and a plurality of load devices connected to the plurality of inverters, wherein each load device includes a fault protection device.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER</subject><subject>CONVERSION OR DISTRIBUTION OF ELECTRIC POWER</subject><subject>COSMONAUTICS</subject><subject>ELECTRIC EQUIPMENT OR PROPULSION OF ELECTRICALLY-PROPELLEDVEHICLES</subject><subject>ELECTRICITY</subject><subject>ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES, IN GENERAL</subject><subject>EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>GENERATION</subject><subject>MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>SYSTEMS FOR STORING ELECTRIC ENERGY</subject><subject>TRANSPORTING</subject><subject>VEHICLES IN GENERAL</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZAgPjgwOcfUNVnD0c1HwdQ3x8HcJVnDzD1LwD3MNCvP3CXF0d1UICPIPcXUO8fT3UwAiH39HqJrQYFcFTz-gVgVXH6B8kKezgqNnkHOQo1sIDwNrWmJOcSovlOZmUHZzDXH20E0tyI9PLS5ITE7NSy2JDw02MjAyNjY1sjSxdDQ0Jk4VAIdxMdw</recordid><startdate>20231102</startdate><enddate>20231102</enddate><creator>Richter, Timothy Gerard</creator><scope>EVB</scope></search><sort><creationdate>20231102</creationdate><title>SYSTEMS AND METHODS FOR OVERVOLTAGE PROTECTION ON LOADS FOR USE IN AN ELECTRIC AIRCRAFT</title><author>Richter, Timothy Gerard</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2023352949A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2023</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER</topic><topic>CONVERSION OR DISTRIBUTION OF ELECTRIC POWER</topic><topic>COSMONAUTICS</topic><topic>ELECTRIC EQUIPMENT OR PROPULSION OF ELECTRICALLY-PROPELLEDVEHICLES</topic><topic>ELECTRICITY</topic><topic>ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES, IN GENERAL</topic><topic>EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>GENERATION</topic><topic>MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>SYSTEMS FOR STORING ELECTRIC ENERGY</topic><topic>TRANSPORTING</topic><topic>VEHICLES IN GENERAL</topic><toplevel>online_resources</toplevel><creatorcontrib>Richter, Timothy Gerard</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Richter, Timothy Gerard</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SYSTEMS AND METHODS FOR OVERVOLTAGE PROTECTION ON LOADS FOR USE IN AN ELECTRIC AIRCRAFT</title><date>2023-11-02</date><risdate>2023</risdate><abstract>A system for overvoltage protection on loads for use in an electric aircraft is presented. The system includes an energy storage element configured to produce an electrical output, a bus element, wherein the bus is configured to transfer the electrical output from the energy storage element, a plurality of inverters, wherein each inverter is configured to generate a regulated output as a function of the electrical output and detect an overvoltage output as a function of the regulated output, and a plurality of load devices connected to the plurality of inverters, wherein each load device includes a fault protection device.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS ELECTRIC EQUIPMENT OR PROPULSION OF ELECTRICALLY-PROPELLEDVEHICLES ELECTRICITY ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES, IN GENERAL EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERATION MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES PARACHUTES PERFORMING OPERATIONS SYSTEMS FOR STORING ELECTRIC ENERGY TRANSPORTING VEHICLES IN GENERAL |
| title | SYSTEMS AND METHODS FOR OVERVOLTAGE PROTECTION ON LOADS FOR USE IN AN ELECTRIC AIRCRAFT |
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