Civil aviation engine fuel pump support
The invention discloses a civil aviation engine fuel pump support. The civil aviation engine fuel pump support comprises a supporting frame which is used for installing a pump body, a first oil pipe and a second oil pipe, the first oil pipe and the second oil pipe communicate with the pump body, the...
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| creator | NING XUEMEI YUAN YAN |
| description | The invention discloses a civil aviation engine fuel pump support. The civil aviation engine fuel pump support comprises a supporting frame which is used for installing a pump body, a first oil pipe and a second oil pipe, the first oil pipe and the second oil pipe communicate with the pump body, the supporting frame is of a disc-shaped structure, the edge of the back face of the supporting frame is fixedly connected with a dustproof edge of a circular-ring-shaped structure, a pipe hole allowing an oil pipe to penetrate through is formed in the top end of the supporting frame, a pipe body protection mechanism is installed at the pipe hole, the pipe body protection mechanism comprises a protection block which is installed on the supporting frame and a wear-resisting ring which is arranged inthe pipe hole, and fasteners used for connecting the supporting frame with an aero-engine are distributed on the surface of the supporting frame. According to the civil aviation engine fuel pump support, the contact abrasion |
| format | Patent |
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The civil aviation engine fuel pump support comprises a supporting frame which is used for installing a pump body, a first oil pipe and a second oil pipe, the first oil pipe and the second oil pipe communicate with the pump body, the supporting frame is of a disc-shaped structure, the edge of the back face of the supporting frame is fixedly connected with a dustproof edge of a circular-ring-shaped structure, a pipe hole allowing an oil pipe to penetrate through is formed in the top end of the supporting frame, a pipe body protection mechanism is installed at the pipe hole, the pipe body protection mechanism comprises a protection block which is installed on the supporting frame and a wear-resisting ring which is arranged inthe pipe hole, and fasteners used for connecting the supporting frame with an aero-engine are distributed on the surface of the supporting frame. According to the civil aviation engine fuel pump support, the contact abrasion</description><language>chi ; eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; SUPPLYING COMBUSTION ENGINES IN GENERAL, WITH COMBUSTIBLEMIXTURES OR CONSTITUENTS THEREOF ; WEAPONS</subject><creationdate>2020</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=20201208&DB=EPODOC&CC=CN&NR=112049729A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20201208&DB=EPODOC&CC=CN&NR=112049729A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>NING XUEMEI</creatorcontrib><creatorcontrib>YUAN YAN</creatorcontrib><title>Civil aviation engine fuel pump support</title><description>The invention discloses a civil aviation engine fuel pump support. The civil aviation engine fuel pump support comprises a supporting frame which is used for installing a pump body, a first oil pipe and a second oil pipe, the first oil pipe and the second oil pipe communicate with the pump body, the supporting frame is of a disc-shaped structure, the edge of the back face of the supporting frame is fixedly connected with a dustproof edge of a circular-ring-shaped structure, a pipe hole allowing an oil pipe to penetrate through is formed in the top end of the supporting frame, a pipe body protection mechanism is installed at the pipe hole, the pipe body protection mechanism comprises a protection block which is installed on the supporting frame and a wear-resisting ring which is arranged inthe pipe hole, and fasteners used for connecting the supporting frame with an aero-engine are distributed on the surface of the supporting frame. According to the civil aviation engine fuel pump support, the contact abrasion</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>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>SUPPLYING COMBUSTION ENGINES IN GENERAL, WITH COMBUSTIBLEMIXTURES OR CONSTITUENTS THEREOF</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2020</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFB3zizLzFFILMtMLMnMz1NIzUvPzEtVSCtNzVEoKM0tUCguLSjILyrhYWBNS8wpTuWF0twMim6uIc4euqkF-fGpxQWJyal5qSXxzn6GhkYGJpbmRpaOxsSoAQClDCgH</recordid><startdate>20201208</startdate><enddate>20201208</enddate><creator>NING XUEMEI</creator><creator>YUAN YAN</creator><scope>EVB</scope></search><sort><creationdate>20201208</creationdate><title>Civil aviation engine fuel pump support</title><author>NING XUEMEI ; YUAN YAN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN112049729A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2020</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>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>SUPPLYING COMBUSTION ENGINES IN GENERAL, WITH COMBUSTIBLEMIXTURES OR CONSTITUENTS THEREOF</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>NING XUEMEI</creatorcontrib><creatorcontrib>YUAN YAN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>NING XUEMEI</au><au>YUAN YAN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Civil aviation engine fuel pump support</title><date>2020-12-08</date><risdate>2020</risdate><abstract>The invention discloses a civil aviation engine fuel pump support. The civil aviation engine fuel pump support comprises a supporting frame which is used for installing a pump body, a first oil pipe and a second oil pipe, the first oil pipe and the second oil pipe communicate with the pump body, the supporting frame is of a disc-shaped structure, the edge of the back face of the supporting frame is fixedly connected with a dustproof edge of a circular-ring-shaped structure, a pipe hole allowing an oil pipe to penetrate through is formed in the top end of the supporting frame, a pipe body protection mechanism is installed at the pipe hole, the pipe body protection mechanism comprises a protection block which is installed on the supporting frame and a wear-resisting ring which is arranged inthe pipe hole, and fasteners used for connecting the supporting frame with an aero-engine are distributed on the surface of the supporting frame. According to the civil aviation engine fuel pump support, the contact abrasion</abstract><oa>free_for_read</oa></addata></record> |
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| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN112049729A |
| source | esp@cenet |
| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING SUPPLYING COMBUSTION ENGINES IN GENERAL, WITH COMBUSTIBLEMIXTURES OR CONSTITUENTS THEREOF WEAPONS |
| title | Civil aviation engine fuel pump support |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-08T04%3A48%3A08IST&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=NING%20XUEMEI&rft.date=2020-12-08&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN112049729A%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 |