Device and system for testing high-pressure turbine rotor of aero-engine
The present disclosure relates to an apparatus and system for testing a high pressure turbine rotor of an aero-engine. The apparatus comprises an apparatus for providing signal transmission, comprising: a rotor member provided with one or more rotating conductive means thereon; a stator member compr...
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| creator | SHI WENBIN WANG YINGQI LUO JINHAN WAN FANGTENG WANG QIUYANG |
| description | The present disclosure relates to an apparatus and system for testing a high pressure turbine rotor of an aero-engine. The apparatus comprises an apparatus for providing signal transmission, comprising: a rotor member provided with one or more rotating conductive means thereon; a stator member comprising one or more conductive devices, where the one or more conductive devices on the stator member conductively contact the one or more rotating conductive devices on the rotor member; and an adapter shaft comprising a first section and a second section, where the rotor member is coupled between the second section of the adapter shaft and the stator member, and where the first section of the adapter shaft is provided with one or more holes to form a passage through the one or more holes in the first section. The equipment disclosed by the invention is connected to the rear end of the high-pressure turbine rotor, and a hole is formed in the first section of the adapter shaft, so that a high-pressure turbine rear be |
| format | Patent |
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The apparatus comprises an apparatus for providing signal transmission, comprising: a rotor member provided with one or more rotating conductive means thereon; a stator member comprising one or more conductive devices, where the one or more conductive devices on the stator member conductively contact the one or more rotating conductive devices on the rotor member; and an adapter shaft comprising a first section and a second section, where the rotor member is coupled between the second section of the adapter shaft and the stator member, and where the first section of the adapter shaft is provided with one or more holes to form a passage through the one or more holes in the first section. The equipment disclosed by the invention is connected to the rear end of the high-pressure turbine rotor, and a hole is formed in the first section of the adapter shaft, so that a high-pressure turbine rear be</description><language>chi ; eng</language><subject>ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVEREDIN A SINGLE OTHER SUBCLASS ; BASIC ELECTRIC ELEMENTS ; BLASTING ; CURRENT COLLECTORS ; ELECTRICITY ; ENGINE PLANTS IN GENERAL ; HEATING ; LIGHTING ; LINE CONNECTORS ; MACHINES OR ENGINES IN GENERAL ; MEASURING ; MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE ; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; PHYSICS ; STEAM ENGINES ; TARIFF METERING APPARATUS ; TESTING ; TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES ; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR ; 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=20221011&DB=EPODOC&CC=CN&NR=115163201A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20221011&DB=EPODOC&CC=CN&NR=115163201A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SHI WENBIN</creatorcontrib><creatorcontrib>WANG YINGQI</creatorcontrib><creatorcontrib>LUO JINHAN</creatorcontrib><creatorcontrib>WAN FANGTENG</creatorcontrib><creatorcontrib>WANG QIUYANG</creatorcontrib><title>Device and system for testing high-pressure turbine rotor of aero-engine</title><description>The present disclosure relates to an apparatus and system for testing a high pressure turbine rotor of an aero-engine. The apparatus comprises an apparatus for providing signal transmission, comprising: a rotor member provided with one or more rotating conductive means thereon; a stator member comprising one or more conductive devices, where the one or more conductive devices on the stator member conductively contact the one or more rotating conductive devices on the rotor member; and an adapter shaft comprising a first section and a second section, where the rotor member is coupled between the second section of the adapter shaft and the stator member, and where the first section of the adapter shaft is provided with one or more holes to form a passage through the one or more holes in the first section. The equipment disclosed by the invention is connected to the rear end of the high-pressure turbine rotor, and a hole is formed in the first section of the adapter shaft, so that a high-pressure turbine rear be</description><subject>ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVEREDIN A SINGLE OTHER SUBCLASS</subject><subject>BASIC ELECTRIC ELEMENTS</subject><subject>BLASTING</subject><subject>CURRENT COLLECTORS</subject><subject>ELECTRICITY</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>LINE CONNECTORS</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MEASURING</subject><subject>MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE</subject><subject>MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>PHYSICS</subject><subject>STEAM ENGINES</subject><subject>TARIFF METERING APPARATUS</subject><subject>TESTING</subject><subject>TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES</subject><subject>TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNykEKwjAQRuFsXIh6h_EAAWPRfalKV67cl1j_tAFNwsxU8PZ24QFcPXh8S9Oe8I49yKcHyUcULwqZSSEa00BjHEZbGCITg3Tie0wgzjqbHMiDs0Ua5rk2i-Cfgs2vK7O9nG9Na1FyBym-R4J2zdW5gztW-52rq3_MF6FQNDg</recordid><startdate>20221011</startdate><enddate>20221011</enddate><creator>SHI WENBIN</creator><creator>WANG YINGQI</creator><creator>LUO JINHAN</creator><creator>WAN FANGTENG</creator><creator>WANG QIUYANG</creator><scope>EVB</scope></search><sort><creationdate>20221011</creationdate><title>Device and system for testing high-pressure turbine rotor of aero-engine</title><author>SHI WENBIN ; WANG YINGQI ; LUO JINHAN ; WAN FANGTENG ; WANG QIUYANG</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN115163201A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2022</creationdate><topic>ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVEREDIN A SINGLE OTHER SUBCLASS</topic><topic>BASIC ELECTRIC ELEMENTS</topic><topic>BLASTING</topic><topic>CURRENT COLLECTORS</topic><topic>ELECTRICITY</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>LINE CONNECTORS</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MEASURING</topic><topic>MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE</topic><topic>MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>PHYSICS</topic><topic>STEAM ENGINES</topic><topic>TARIFF METERING APPARATUS</topic><topic>TESTING</topic><topic>TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES</topic><topic>TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>SHI WENBIN</creatorcontrib><creatorcontrib>WANG YINGQI</creatorcontrib><creatorcontrib>LUO JINHAN</creatorcontrib><creatorcontrib>WAN FANGTENG</creatorcontrib><creatorcontrib>WANG QIUYANG</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SHI WENBIN</au><au>WANG YINGQI</au><au>LUO JINHAN</au><au>WAN FANGTENG</au><au>WANG QIUYANG</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Device and system for testing high-pressure turbine rotor of aero-engine</title><date>2022-10-11</date><risdate>2022</risdate><abstract>The present disclosure relates to an apparatus and system for testing a high pressure turbine rotor of an aero-engine. The apparatus comprises an apparatus for providing signal transmission, comprising: a rotor member provided with one or more rotating conductive means thereon; a stator member comprising one or more conductive devices, where the one or more conductive devices on the stator member conductively contact the one or more rotating conductive devices on the rotor member; and an adapter shaft comprising a first section and a second section, where the rotor member is coupled between the second section of the adapter shaft and the stator member, and where the first section of the adapter shaft is provided with one or more holes to form a passage through the one or more holes in the first section. The equipment disclosed by the invention is connected to the rear end of the high-pressure turbine rotor, and a hole is formed in the first section of the adapter shaft, so that a high-pressure turbine rear be</abstract><oa>free_for_read</oa></addata></record> |
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| language | chi ; eng |
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| subjects | ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVEREDIN A SINGLE OTHER SUBCLASS BASIC ELECTRIC ELEMENTS BLASTING CURRENT COLLECTORS ELECTRICITY ENGINE PLANTS IN GENERAL HEATING LIGHTING LINE CONNECTORS MACHINES OR ENGINES IN GENERAL MEASURING MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PHYSICS STEAM ENGINES TARIFF METERING APPARATUS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR WEAPONS |
| title | Device and system for testing high-pressure turbine rotor of aero-engine |
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