ENGINE BACKBONE BENDING REDUCTION
The present invention discloses methods, apparatus, systems and articles of manufacture. A mechanical linkage for mounting a gas turbine engine to a pylon includes: a bending restraint having a first end and a second end; a first joint at the first end of the bending restraint to connect the first e...
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 | KHANDEPARKER MAHESH COLEMAN JONATHAN EDWARD SCHELFAUT TIMOTHY LEO GARDNER DONALD L JOSEPH THOMAS PETER METZ ANTHONY MICHAEL SHINDE KUDUM |
| description | The present invention discloses methods, apparatus, systems and articles of manufacture. A mechanical linkage for mounting a gas turbine engine to a pylon includes: a bending restraint having a first end and a second end; a first joint at the first end of the bending restraint to connect the first end of the bending restraint to a fan section of the gas turbine engine; and a second joint at the second end of the bending restraint to connect the second end of the bending restraint to the pylon.
公开方法、设备、系统和制品。一种用于将燃气涡轮发动机安装到支架的机械连杆机构包含：弯曲约束件，其具有第一端和第二端；第一接头，其在弯曲约束件的第一端处，使弯曲约束件的第一端连接到燃气涡轮发动机的风扇区段；以及第二接头，其在弯曲约束件的第二端处，使弯曲约束件的第二端连接到支架。 |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN113464284A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN113464284A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN113464284A3</originalsourceid><addsrcrecordid>eNrjZFB09XP39HNVcHJ09nbyBzFc_Vw8_dwVglxdQp1DPP39eBhY0xJzilN5oTQ3g6Kba4izh25qQX58anFBYnJqXmpJvLOfoaGxiZmJkYWJozExagD_OyH5</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>ENGINE BACKBONE BENDING REDUCTION</title><source>esp@cenet</source><creator>KHANDEPARKER MAHESH ; COLEMAN JONATHAN EDWARD ; SCHELFAUT TIMOTHY LEO ; GARDNER DONALD L ; JOSEPH THOMAS PETER ; METZ ANTHONY MICHAEL ; SHINDE KUDUM</creator><creatorcontrib>KHANDEPARKER MAHESH ; COLEMAN JONATHAN EDWARD ; SCHELFAUT TIMOTHY LEO ; GARDNER DONALD L ; JOSEPH THOMAS PETER ; METZ ANTHONY MICHAEL ; SHINDE KUDUM</creatorcontrib><description>The present invention discloses methods, apparatus, systems and articles of manufacture. A mechanical linkage for mounting a gas turbine engine to a pylon includes: a bending restraint having a first end and a second end; a first joint at the first end of the bending restraint to connect the first end of the bending restraint to a fan section of the gas turbine engine; and a second joint at the second end of the bending restraint to connect the second end of the bending restraint to the pylon.
公开方法、设备、系统和制品。一种用于将燃气涡轮发动机安装到支架的机械连杆机构包含：弯曲约束件，其具有第一端和第二端；第一接头，其在弯曲约束件的第一端处，使弯曲约束件的第一端连接到燃气涡轮发动机的风扇区段；以及第二接头，其在弯曲约束件的第二端处，使弯曲约束件的第二端连接到支架。</description><language>chi ; eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING ; WEAPONS</subject><creationdate>2021</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=20211001&DB=EPODOC&CC=CN&NR=113464284A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20211001&DB=EPODOC&CC=CN&NR=113464284A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KHANDEPARKER MAHESH</creatorcontrib><creatorcontrib>COLEMAN JONATHAN EDWARD</creatorcontrib><creatorcontrib>SCHELFAUT TIMOTHY LEO</creatorcontrib><creatorcontrib>GARDNER DONALD L</creatorcontrib><creatorcontrib>JOSEPH THOMAS PETER</creatorcontrib><creatorcontrib>METZ ANTHONY MICHAEL</creatorcontrib><creatorcontrib>SHINDE KUDUM</creatorcontrib><title>ENGINE BACKBONE BENDING REDUCTION</title><description>The present invention discloses methods, apparatus, systems and articles of manufacture. A mechanical linkage for mounting a gas turbine engine to a pylon includes: a bending restraint having a first end and a second end; a first joint at the first end of the bending restraint to connect the first end of the bending restraint to a fan section of the gas turbine engine; and a second joint at the second end of the bending restraint to connect the second end of the bending restraint to the pylon.
公开方法、设备、系统和制品。一种用于将燃气涡轮发动机安装到支架的机械连杆机构包含：弯曲约束件，其具有第一端和第二端；第一接头，其在弯曲约束件的第一端处，使弯曲约束件的第一端连接到燃气涡轮发动机的风扇区段；以及第二接头，其在弯曲约束件的第二端处，使弯曲约束件的第二端连接到支架。</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</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>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFB09XP39HNVcHJ09nbyBzFc_Vw8_dwVglxdQp1DPP39eBhY0xJzilN5oTQ3g6Kba4izh25qQX58anFBYnJqXmpJvLOfoaGxiZmJkYWJozExagD_OyH5</recordid><startdate>20211001</startdate><enddate>20211001</enddate><creator>KHANDEPARKER MAHESH</creator><creator>COLEMAN JONATHAN EDWARD</creator><creator>SCHELFAUT TIMOTHY LEO</creator><creator>GARDNER DONALD L</creator><creator>JOSEPH THOMAS PETER</creator><creator>METZ ANTHONY MICHAEL</creator><creator>SHINDE KUDUM</creator><scope>EVB</scope></search><sort><creationdate>20211001</creationdate><title>ENGINE BACKBONE BENDING REDUCTION</title><author>KHANDEPARKER MAHESH ; COLEMAN JONATHAN EDWARD ; SCHELFAUT TIMOTHY LEO ; GARDNER DONALD L ; JOSEPH THOMAS PETER ; METZ ANTHONY MICHAEL ; SHINDE KUDUM</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN113464284A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2021</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</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>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>KHANDEPARKER MAHESH</creatorcontrib><creatorcontrib>COLEMAN JONATHAN EDWARD</creatorcontrib><creatorcontrib>SCHELFAUT TIMOTHY LEO</creatorcontrib><creatorcontrib>GARDNER DONALD L</creatorcontrib><creatorcontrib>JOSEPH THOMAS PETER</creatorcontrib><creatorcontrib>METZ ANTHONY MICHAEL</creatorcontrib><creatorcontrib>SHINDE KUDUM</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KHANDEPARKER MAHESH</au><au>COLEMAN JONATHAN EDWARD</au><au>SCHELFAUT TIMOTHY LEO</au><au>GARDNER DONALD L</au><au>JOSEPH THOMAS PETER</au><au>METZ ANTHONY MICHAEL</au><au>SHINDE KUDUM</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>ENGINE BACKBONE BENDING REDUCTION</title><date>2021-10-01</date><risdate>2021</risdate><abstract>The present invention discloses methods, apparatus, systems and articles of manufacture. A mechanical linkage for mounting a gas turbine engine to a pylon includes: a bending restraint having a first end and a second end; a first joint at the first end of the bending restraint to connect the first end of the bending restraint to a fan section of the gas turbine engine; and a second joint at the second end of the bending restraint to connect the second end of the bending restraint to the pylon.
公开方法、设备、系统和制品。一种用于将燃气涡轮发动机安装到支架的机械连杆机构包含：弯曲约束件，其具有第一端和第二端；第一接头，其在弯曲约束件的第一端处，使弯曲约束件的第一端连接到燃气涡轮发动机的风扇区段；以及第二接头，其在弯曲约束件的第二端处，使弯曲约束件的第二端连接到支架。</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN113464284A |
| source | esp@cenet |
| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS |
| title | ENGINE BACKBONE BENDING REDUCTION |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-24T06%3A11%3A56IST&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=KHANDEPARKER%20MAHESH&rft.date=2021-10-01&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN113464284A%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 |