JET TURBINE ENGINE EQUIPPED WITH BUILT-IN ELECTRIC GENERATOR
FIELD: engines and pumps. ^ SUBSTANCE: jet turbine engine includes high pressure housing; at least one rear bearing; and electric generator. High pressure housing includes high pressure compressor arranged along X-axis. High pressure compressor includes rotor and carter. The above bearing is arrange...
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| creator | BUJER FILIPP RUSSELEHN STEFAN MORR'AL' SERZH |
| description | FIELD: engines and pumps. ^ SUBSTANCE: jet turbine engine includes high pressure housing; at least one rear bearing; and electric generator. High pressure housing includes high pressure compressor arranged along X-axis. High pressure compressor includes rotor and carter. The above bearing is arranged between carter and rotor of high pressure compressor. Electric generator is located coaxially with the housing and includes inductance coil rigidly connected to rotor of high pressure compressor during rotation. Armature is rigidly connected to carter. Electric generator is located before the above rear bearing in air flow direction. Electric generator includes at least the first cooling circuit passing around the above armature and downstream lubricating jet nozzle of rear bearing after cooling. ^ EFFECT: higher efficiency. ^ 11 cl, 2 dwg
Турбореактивный двигатель содержит корпус высокого давления; по меньшей мере, один задний подшипник и генератор электрического тока. Корпус высокого давления содержит компрессор высокого давления, размещенный вдоль оси X. Компрессор высокого давления содержит ротор и картер. Указанный подшипник размещен между картером и ротором компрессора высокого давления. Генератор электрического тока расположен соосно с корпусом и содержит катушку индуктивности, жестко соединенную с ротором компрессора высокого давления в процессе вращения. Якорь жестко соединен с картером. Генератор электрического тока расположен перед указанным задним подшипником в направлении воздушного потока. Генератор электрического тока включает в себя, по меньшей мере, первый контур охлаждения, проходящий вокруг указанного якоря, и выходящий после охлаждения ниже по потоку смазочный жиклер заднего подшипника. 10 з.п. ф-лы, 2 ил. |
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Турбореактивный двигатель содержит корпус высокого давления; по меньшей мере, один задний подшипник и генератор электрического тока. Корпус высокого давления содержит компрессор высокого давления, размещенный вдоль оси X. Компрессор высокого давления содержит ротор и картер. Указанный подшипник размещен между картером и ротором компрессора высокого давления. Генератор электрического тока расположен соосно с корпусом и содержит катушку индуктивности, жестко соединенную с ротором компрессора высокого давления в процессе вращения. Якорь жестко соединен с картером. Генератор электрического тока расположен перед указанным задним подшипником в направлении воздушного потока. Генератор электрического тока включает в себя, по меньшей мере, первый контур охлаждения, проходящий вокруг указанного якоря, и выходящий после охлаждения ниже по потоку смазочный жиклер заднего подшипника. 10 з.п. ф-лы, 2 ил.</description><language>eng ; rus</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; ENGINE PLANTS IN GENERAL ; GAS-TURBINE PLANTS ; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC ; GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS ; INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 ; JET-PROPULSION PLANTS ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS ; TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE ; WEAPONS</subject><creationdate>2011</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=20110720&DB=EPODOC&CC=RU&NR=2424435C2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20110720&DB=EPODOC&CC=RU&NR=2424435C2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BUJER FILIPP</creatorcontrib><creatorcontrib>RUSSELEHN STEFAN</creatorcontrib><creatorcontrib>MORR'AL' SERZH</creatorcontrib><title>JET TURBINE ENGINE EQUIPPED WITH BUILT-IN ELECTRIC GENERATOR</title><description>FIELD: engines and pumps. ^ SUBSTANCE: jet turbine engine includes high pressure housing; at least one rear bearing; and electric generator. High pressure housing includes high pressure compressor arranged along X-axis. High pressure compressor includes rotor and carter. The above bearing is arranged between carter and rotor of high pressure compressor. Electric generator is located coaxially with the housing and includes inductance coil rigidly connected to rotor of high pressure compressor during rotation. Armature is rigidly connected to carter. Electric generator is located before the above rear bearing in air flow direction. Electric generator includes at least the first cooling circuit passing around the above armature and downstream lubricating jet nozzle of rear bearing after cooling. ^ EFFECT: higher efficiency. ^ 11 cl, 2 dwg
Турбореактивный двигатель содержит корпус высокого давления; по меньшей мере, один задний подшипник и генератор электрического тока. Корпус высокого давления содержит компрессор высокого давления, размещенный вдоль оси X. Компрессор высокого давления содержит ротор и картер. Указанный подшипник размещен между картером и ротором компрессора высокого давления. Генератор электрического тока расположен соосно с корпусом и содержит катушку индуктивности, жестко соединенную с ротором компрессора высокого давления в процессе вращения. Якорь жестко соединен с картером. Генератор электрического тока расположен перед указанным задним подшипником в направлении воздушного потока. Генератор электрического тока включает в себя, по меньшей мере, первый контур охлаждения, проходящий вокруг указанного якоря, и выходящий после охлаждения ниже по потоку смазочный жиклер заднего подшипника. 10 з.п. ф-лы, 2 ил.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>GAS-TURBINE PLANTS</subject><subject>GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC</subject><subject>GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS</subject><subject>INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04</subject><subject>JET-PROPULSION PLANTS</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>TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS</subject><subject>TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2011</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLDxcg1RCAkNcvL0c1Vw9XMHU4GhngEBri4K4Z4hHgpOoZ4-IbqefgquPq7OIUGezgrurn6uQY4h_kE8DKxpiTnFqbxQmptBwc01xNlDN7UgPz61uCAxOTUvtSQ-KNTIxMjExNjU2ciYCCUAs_UpRg</recordid><startdate>20110720</startdate><enddate>20110720</enddate><creator>BUJER FILIPP</creator><creator>RUSSELEHN STEFAN</creator><creator>MORR'AL' SERZH</creator><scope>EVB</scope></search><sort><creationdate>20110720</creationdate><title>JET TURBINE ENGINE EQUIPPED WITH BUILT-IN ELECTRIC GENERATOR</title><author>BUJER FILIPP ; RUSSELEHN STEFAN ; MORR'AL' SERZH</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_RU2424435C23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; rus</language><creationdate>2011</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>GAS-TURBINE PLANTS</topic><topic>GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC</topic><topic>GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS</topic><topic>INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04</topic><topic>JET-PROPULSION PLANTS</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>TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS</topic><topic>TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>BUJER FILIPP</creatorcontrib><creatorcontrib>RUSSELEHN STEFAN</creatorcontrib><creatorcontrib>MORR'AL' SERZH</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>BUJER FILIPP</au><au>RUSSELEHN STEFAN</au><au>MORR'AL' SERZH</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>JET TURBINE ENGINE EQUIPPED WITH BUILT-IN ELECTRIC GENERATOR</title><date>2011-07-20</date><risdate>2011</risdate><abstract>FIELD: engines and pumps. ^ SUBSTANCE: jet turbine engine includes high pressure housing; at least one rear bearing; and electric generator. High pressure housing includes high pressure compressor arranged along X-axis. High pressure compressor includes rotor and carter. The above bearing is arranged between carter and rotor of high pressure compressor. Electric generator is located coaxially with the housing and includes inductance coil rigidly connected to rotor of high pressure compressor during rotation. Armature is rigidly connected to carter. Electric generator is located before the above rear bearing in air flow direction. Electric generator includes at least the first cooling circuit passing around the above armature and downstream lubricating jet nozzle of rear bearing after cooling. ^ EFFECT: higher efficiency. ^ 11 cl, 2 dwg
Турбореактивный двигатель содержит корпус высокого давления; по меньшей мере, один задний подшипник и генератор электрического тока. Корпус высокого давления содержит компрессор высокого давления, размещенный вдоль оси X. Компрессор высокого давления содержит ротор и картер. Указанный подшипник размещен между картером и ротором компрессора высокого давления. Генератор электрического тока расположен соосно с корпусом и содержит катушку индуктивности, жестко соединенную с ротором компрессора высокого давления в процессе вращения. Якорь жестко соединен с картером. Генератор электрического тока расположен перед указанным задним подшипником в направлении воздушного потока. Генератор электрического тока включает в себя, по меньшей мере, первый контур охлаждения, проходящий вокруг указанного якоря, и выходящий после охлаждения ниже по потоку смазочный жиклер заднего подшипника. 10 з.п. ф-лы, 2 ил.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 JET-PROPULSION PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE WEAPONS |
| title | JET TURBINE ENGINE EQUIPPED WITH BUILT-IN ELECTRIC GENERATOR |
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