GAS TURBINE ENGINE
A gas turbine engine (10) for an aircraft comprises a unit (30) supplied with oil from a first oil circuit (43) and a second oil circuit (45). The first oil circuit (43) and the second oil circuit (45) each are fluidly coupled with at least one inlet (48, 49) and with at least one outlet (50, 60) of...
Gespeichert in:
| Hauptverfasser: | , , , , , , |
|---|---|
| Format: | Patent |
| Sprache: | chi ; eng |
| 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 | UHKOETTER STEPHAN EDWARDS DAVID A HAMMOND LYNN WILLIAMS DAVID MENCZYKALSKI STEFAN MASON JOHN R DAVIES NEIL |
| description | A gas turbine engine (10) for an aircraft comprises a unit (30) supplied with oil from a first oil circuit (43) and a second oil circuit (45). The first oil circuit (43) and the second oil circuit (45) each are fluidly coupled with at least one inlet (48, 49) and with at least one outlet (50, 60) of the unit (30) and with at least one inlet (51, 61) and with at least one outlet (54, 55) of an oiltank (53). The first oil circuit (43) and the second oil circuit (45) are configured to receive oil from the oil tank (53) and to direct the received oil to the unit (30). The oil tank (53) is incorporating offset outlets (25, 29) to each of the oil circuits (43, 45). The offset outlet (29) of the second oil (45) circuit is positioned higher in the oil tank (53) than the offset outlet (25) of thefirst oil circuit (43).
用于飞行器的气体涡轮机引擎（10），其包括供应有来自第一油通路（43）和第二油通路（45）的油的单元（30）。第一油通路（43）和第二油通路（45）各自与单元（30）的至少一个入口（48、49）并且与至少一个出口（50、60）以及与油箱（53）的至少一个入口（51、61）并且与至少一个出口（54、55）流体地耦合。第一油通路（43）和第二油通路（45）配置成接收来自油箱（53）的油并将接收的油引导至单 |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN110388270A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN110388270A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN110388270A3</originalsourceid><addsrcrecordid>eNrjZBBydwxWCAkNcvL0c1Vw9XMHUjwMrGmJOcWpvFCam0HRzTXE2UM3tSA_PrW4IDE5NS-1JN7Zz9DQwNjCwsjcwNGYGDUALYgd3w</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>GAS TURBINE ENGINE</title><source>esp@cenet</source><creator>UHKOETTER STEPHAN ; EDWARDS DAVID A ; HAMMOND LYNN ; WILLIAMS DAVID ; MENCZYKALSKI STEFAN ; MASON JOHN R ; DAVIES NEIL</creator><creatorcontrib>UHKOETTER STEPHAN ; EDWARDS DAVID A ; HAMMOND LYNN ; WILLIAMS DAVID ; MENCZYKALSKI STEFAN ; MASON JOHN R ; DAVIES NEIL</creatorcontrib><description>A gas turbine engine (10) for an aircraft comprises a unit (30) supplied with oil from a first oil circuit (43) and a second oil circuit (45). The first oil circuit (43) and the second oil circuit (45) each are fluidly coupled with at least one inlet (48, 49) and with at least one outlet (50, 60) of the unit (30) and with at least one inlet (51, 61) and with at least one outlet (54, 55) of an oiltank (53). The first oil circuit (43) and the second oil circuit (45) are configured to receive oil from the oil tank (53) and to direct the received oil to the unit (30). The oil tank (53) is incorporating offset outlets (25, 29) to each of the oil circuits (43, 45). The offset outlet (29) of the second oil (45) circuit is positioned higher in the oil tank (53) than the offset outlet (25) of thefirst oil circuit (43).
用于飞行器的气体涡轮机引擎（10），其包括供应有来自第一油通路（43）和第二油通路（45）的油的单元（30）。第一油通路（43）和第二油通路（45）各自与单元（30）的至少一个入口（48、49）并且与至少一个出口（50、60）以及与油箱（53）的至少一个入口（51、61）并且与至少一个出口（54、55）流体地耦合。第一油通路（43）和第二油通路（45）配置成接收来自油箱（53）的油并将接收的油引导至单</description><language>chi ; eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; ENGINEERING ELEMENTS AND UNITS ; GAS-TURBINE PLANTS ; GEARING ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; JET-PROPULSION PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; THERMAL INSULATION IN GENERAL ; WEAPONS</subject><creationdate>2019</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=20191029&DB=EPODOC&CC=CN&NR=110388270A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20191029&DB=EPODOC&CC=CN&NR=110388270A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>UHKOETTER STEPHAN</creatorcontrib><creatorcontrib>EDWARDS DAVID A</creatorcontrib><creatorcontrib>HAMMOND LYNN</creatorcontrib><creatorcontrib>WILLIAMS DAVID</creatorcontrib><creatorcontrib>MENCZYKALSKI STEFAN</creatorcontrib><creatorcontrib>MASON JOHN R</creatorcontrib><creatorcontrib>DAVIES NEIL</creatorcontrib><title>GAS TURBINE ENGINE</title><description>A gas turbine engine (10) for an aircraft comprises a unit (30) supplied with oil from a first oil circuit (43) and a second oil circuit (45). The first oil circuit (43) and the second oil circuit (45) each are fluidly coupled with at least one inlet (48, 49) and with at least one outlet (50, 60) of the unit (30) and with at least one inlet (51, 61) and with at least one outlet (54, 55) of an oiltank (53). The first oil circuit (43) and the second oil circuit (45) are configured to receive oil from the oil tank (53) and to direct the received oil to the unit (30). The oil tank (53) is incorporating offset outlets (25, 29) to each of the oil circuits (43, 45). The offset outlet (29) of the second oil (45) circuit is positioned higher in the oil tank (53) than the offset outlet (25) of thefirst oil circuit (43).
用于飞行器的气体涡轮机引擎（10），其包括供应有来自第一油通路（43）和第二油通路（45）的油的单元（30）。第一油通路（43）和第二油通路（45）各自与单元（30）的至少一个入口（48、49）并且与至少一个出口（50、60）以及与油箱（53）的至少一个入口（51、61）并且与至少一个出口（54、55）流体地耦合。第一油通路（43）和第二油通路（45）配置成接收来自油箱（53）的油并将接收的油引导至单</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>ENGINEERING ELEMENTS AND UNITS</subject><subject>GAS-TURBINE PLANTS</subject><subject>GEARING</subject><subject>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>JET-PROPULSION PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZBBydwxWCAkNcvL0c1Vw9XMHUjwMrGmJOcWpvFCam0HRzTXE2UM3tSA_PrW4IDE5NS-1JN7Zz9DQwNjCwsjcwNGYGDUALYgd3w</recordid><startdate>20191029</startdate><enddate>20191029</enddate><creator>UHKOETTER STEPHAN</creator><creator>EDWARDS DAVID A</creator><creator>HAMMOND LYNN</creator><creator>WILLIAMS DAVID</creator><creator>MENCZYKALSKI STEFAN</creator><creator>MASON JOHN R</creator><creator>DAVIES NEIL</creator><scope>EVB</scope></search><sort><creationdate>20191029</creationdate><title>GAS TURBINE ENGINE</title><author>UHKOETTER STEPHAN ; EDWARDS DAVID A ; HAMMOND LYNN ; WILLIAMS DAVID ; MENCZYKALSKI STEFAN ; MASON JOHN R ; DAVIES NEIL</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN110388270A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2019</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>ENGINEERING ELEMENTS AND UNITS</topic><topic>GAS-TURBINE PLANTS</topic><topic>GEARING</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>JET-PROPULSION PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>UHKOETTER STEPHAN</creatorcontrib><creatorcontrib>EDWARDS DAVID A</creatorcontrib><creatorcontrib>HAMMOND LYNN</creatorcontrib><creatorcontrib>WILLIAMS DAVID</creatorcontrib><creatorcontrib>MENCZYKALSKI STEFAN</creatorcontrib><creatorcontrib>MASON JOHN R</creatorcontrib><creatorcontrib>DAVIES NEIL</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>UHKOETTER STEPHAN</au><au>EDWARDS DAVID A</au><au>HAMMOND LYNN</au><au>WILLIAMS DAVID</au><au>MENCZYKALSKI STEFAN</au><au>MASON JOHN R</au><au>DAVIES NEIL</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>GAS TURBINE ENGINE</title><date>2019-10-29</date><risdate>2019</risdate><abstract>A gas turbine engine (10) for an aircraft comprises a unit (30) supplied with oil from a first oil circuit (43) and a second oil circuit (45). The first oil circuit (43) and the second oil circuit (45) each are fluidly coupled with at least one inlet (48, 49) and with at least one outlet (50, 60) of the unit (30) and with at least one inlet (51, 61) and with at least one outlet (54, 55) of an oiltank (53). The first oil circuit (43) and the second oil circuit (45) are configured to receive oil from the oil tank (53) and to direct the received oil to the unit (30). The oil tank (53) is incorporating offset outlets (25, 29) to each of the oil circuits (43, 45). The offset outlet (29) of the second oil (45) circuit is positioned higher in the oil tank (53) than the offset outlet (25) of thefirst oil circuit (43).
用于飞行器的气体涡轮机引擎（10），其包括供应有来自第一油通路（43）和第二油通路（45）的油的单元（30）。第一油通路（43）和第二油通路（45）各自与单元（30）的至少一个入口（48、49）并且与至少一个出口（50、60）以及与油箱（53）的至少一个入口（51、61）并且与至少一个出口（54、55）流体地耦合。第一油通路（43）和第二油通路（45）配置成接收来自油箱（53）的油并将接收的油引导至单</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN110388270A |
| source | esp@cenet |
| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINEERING ELEMENTS AND UNITS GAS-TURBINE PLANTS GEARING GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING THERMAL INSULATION IN GENERAL WEAPONS |
| title | GAS TURBINE ENGINE |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-06T09%3A46%3A04IST&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=UHKOETTER%20STEPHAN&rft.date=2019-10-29&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN110388270A%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 |