POWER GENERATION DEVICE AND CORRESPONDING AIRCRAFT
A power generation device, comprising: a gas turbine engine (200) including a rotor shaft (204) and a first casing (208) around the rotor shaft (204); a transmission (212) connecting the rotor shaft (204) to a gearbox (210), the transmission (212) comprising a drive shaft (216) and a second casing (...
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creator | OEHLER, Stephen D KARNOFSKI, Kent E DUCE, Jeffrey Lynn |
description | A power generation device, comprising: a gas turbine engine (200) including a rotor shaft (204) and a first casing (208) around the rotor shaft (204); a transmission (212) connecting the rotor shaft (204) to a gearbox (210), the transmission (212) comprising a drive shaft (216) and a second casing (218) around the drive shaft (216); one or more permanent magnets (202) attached to the rotor shaft (204) and/or the drive shaft (216); one or more coils (206) attached to the first casing (208) and/or the second casing (218); an electrical device connected to the coils (206), the electrical device receives electrical energy generated by the coils (206) when the engine (200) is running so as to rotate the permanent magnets (202) on the shaft, and magnetic fields generated by the permanent magnets (202) interact with the coils (206); the electrical energy reduces transient and peak electrical power demands on the engine (200). |
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fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3382157A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3382157A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3382157A13</originalsourceid><addsrcrecordid>eNrjZDAK8A93DVJwd_VzDXIM8fT3U3BxDfN0dlVw9HNRcPYPCnINDvD3c_H0c1dw9AxyDnJ0C-FhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAcbGFkaGpuaOhsZEKAEANZ4mgA</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>POWER GENERATION DEVICE AND CORRESPONDING AIRCRAFT</title><source>esp@cenet</source><creator>OEHLER, Stephen D ; KARNOFSKI, Kent E ; DUCE, Jeffrey Lynn</creator><creatorcontrib>OEHLER, Stephen D ; KARNOFSKI, Kent E ; DUCE, Jeffrey Lynn</creatorcontrib><description>A power generation device, comprising: a gas turbine engine (200) including a rotor shaft (204) and a first casing (208) around the rotor shaft (204); a transmission (212) connecting the rotor shaft (204) to a gearbox (210), the transmission (212) comprising a drive shaft (216) and a second casing (218) around the drive shaft (216); one or more permanent magnets (202) attached to the rotor shaft (204) and/or the drive shaft (216); one or more coils (206) attached to the first casing (208) and/or the second casing (218); an electrical device connected to the coils (206), the electrical device receives electrical energy generated by the coils (206) when the engine (200) is running so as to rotate the permanent magnets (202) on the shaft, and magnetic fields generated by the permanent magnets (202) interact with the coils (206); the electrical energy reduces transient and peak electrical power demands on the engine (200).</description><language>eng ; fre ; ger</language><subject>BLASTING ; ENGINE PLANTS IN GENERAL ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; 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a transmission (212) connecting the rotor shaft (204) to a gearbox (210), the transmission (212) comprising a drive shaft (216) and a second casing (218) around the drive shaft (216); one or more permanent magnets (202) attached to the rotor shaft (204) and/or the drive shaft (216); one or more coils (206) attached to the first casing (208) and/or the second casing (218); an electrical device connected to the coils (206), the electrical device receives electrical energy generated by the coils (206) when the engine (200) is running so as to rotate the permanent magnets (202) on the shaft, and magnetic fields generated by the permanent magnets (202) interact with the coils (206); the electrical energy reduces transient and peak electrical power demands on the engine (200).</description><subject>BLASTING</subject><subject>ENGINE PLANTS IN GENERAL</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>STEAM ENGINES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDAK8A93DVJwd_VzDXIM8fT3U3BxDfN0dlVw9HNRcPYPCnINDvD3c_H0c1dw9AxyDnJ0C-FhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAcbGFkaGpuaOhsZEKAEANZ4mgA</recordid><startdate>20181003</startdate><enddate>20181003</enddate><creator>OEHLER, Stephen D</creator><creator>KARNOFSKI, Kent E</creator><creator>DUCE, Jeffrey Lynn</creator><scope>EVB</scope></search><sort><creationdate>20181003</creationdate><title>POWER GENERATION DEVICE AND CORRESPONDING AIRCRAFT</title><author>OEHLER, Stephen D ; KARNOFSKI, Kent E ; DUCE, Jeffrey Lynn</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3382157A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2018</creationdate><topic>BLASTING</topic><topic>ENGINE PLANTS IN GENERAL</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>STEAM ENGINES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>OEHLER, Stephen D</creatorcontrib><creatorcontrib>KARNOFSKI, Kent E</creatorcontrib><creatorcontrib>DUCE, Jeffrey Lynn</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>OEHLER, Stephen D</au><au>KARNOFSKI, Kent E</au><au>DUCE, Jeffrey Lynn</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>POWER GENERATION DEVICE AND CORRESPONDING AIRCRAFT</title><date>2018-10-03</date><risdate>2018</risdate><abstract>A power generation device, comprising: a gas turbine engine (200) including a rotor shaft (204) and a first casing (208) around the rotor shaft (204); a transmission (212) connecting the rotor shaft (204) to a gearbox (210), the transmission (212) comprising a drive shaft (216) and a second casing (218) around the drive shaft (216); one or more permanent magnets (202) attached to the rotor shaft (204) and/or the drive shaft (216); one or more coils (206) attached to the first casing (208) and/or the second casing (218); an electrical device connected to the coils (206), the electrical device receives electrical energy generated by the coils (206) when the engine (200) is running so as to rotate the permanent magnets (202) on the shaft, and magnetic fields generated by the permanent magnets (202) interact with the coils (206); the electrical energy reduces transient and peak electrical power demands on the engine (200).</abstract><oa>free_for_read</oa></addata></record> |
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language | eng ; fre ; ger |
recordid | cdi_epo_espacenet_EP3382157A1 |
source | esp@cenet |
subjects | BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS |
title | POWER GENERATION DEVICE AND CORRESPONDING AIRCRAFT |
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