Attitude adjusting bracket for empennage of large aircraft
The utility model discloses an empennage attitude adjusting bracket for a large aircraft, and aims to provide the empennage attitude adjusting bracket for the large aircraft, which is convenient for adjusting the attitude of an empennage and can stably support the empennage. The tail wing supporting...
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 | YANG XINLIANG FU JINGLI CAI JUNWEN XIE XING |
| description | The utility model discloses an empennage attitude adjusting bracket for a large aircraft, and aims to provide the empennage attitude adjusting bracket for the large aircraft, which is convenient for adjusting the attitude of an empennage and can stably support the empennage. The tail wing supporting device comprises a sliding mechanism, a main body frame is arranged on the sliding mechanism in a matched mode, a lifting mechanism is arranged on the main body frame, a supporting plate is arranged at the lifting end of the lifting mechanism in a matched mode, and two opposite tail wing supporting blocks are arranged on the supporting plate. The utility model is applied to the technical field of air transportation.
本实用新型公开了一种大型飞机尾翼调姿托架，旨在提供一种便于调整尾翼姿态及能够稳定支撑尾翼的大型飞机尾翼调姿托架。本实用新型包括滑动机构，所述滑动机构上配合设置有主体架，所述主体架上设置有升降机构，所述升降机构的升降端配合设置有支撑托板，所述支撑托板上设置有两个相对的尾翼托块。本实用新型应用于航空运输的技术领域。 |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN218519856UU</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN218519856UU</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN218519856UU3</originalsourceid><addsrcrecordid>eNrjZLByLCnJLClNSVVITMkqLS7JzEtXSCpKTM5OLVFIyy9SSM0tSM3LS0xPVchPU8hJLAIyEjOLkosS00p4GFjTEnOKU3mhNDeDkptriLOHbmpBfnxqcUFicmpeakm8s5-RoYWpoaWFqVloqDFRigDl_S_7</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Attitude adjusting bracket for empennage of large aircraft</title><source>esp@cenet</source><creator>YANG XINLIANG ; FU JINGLI ; CAI JUNWEN ; XIE XING</creator><creatorcontrib>YANG XINLIANG ; FU JINGLI ; CAI JUNWEN ; XIE XING</creatorcontrib><description>The utility model discloses an empennage attitude adjusting bracket for a large aircraft, and aims to provide the empennage attitude adjusting bracket for the large aircraft, which is convenient for adjusting the attitude of an empennage and can stably support the empennage. The tail wing supporting device comprises a sliding mechanism, a main body frame is arranged on the sliding mechanism in a matched mode, a lifting mechanism is arranged on the main body frame, a supporting plate is arranged at the lifting end of the lifting mechanism in a matched mode, and two opposite tail wing supporting blocks are arranged on the supporting plate. The utility model is applied to the technical field of air transportation.
本实用新型公开了一种大型飞机尾翼调姿托架，旨在提供一种便于调整尾翼姿态及能够稳定支撑尾翼的大型飞机尾翼调姿托架。本实用新型包括滑动机构，所述滑动机构上配合设置有主体架，所述主体架上设置有升降机构，所述升降机构的升降端配合设置有支撑托板，所述支撑托板上设置有两个相对的尾翼托块。本实用新型应用于航空运输的技术领域。</description><language>chi ; eng</language><subject>AIRCRAFT ; AVIATION ; COSMONAUTICS ; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT ; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2023</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=20230224&DB=EPODOC&CC=CN&NR=218519856U$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76516</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230224&DB=EPODOC&CC=CN&NR=218519856U$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>YANG XINLIANG</creatorcontrib><creatorcontrib>FU JINGLI</creatorcontrib><creatorcontrib>CAI JUNWEN</creatorcontrib><creatorcontrib>XIE XING</creatorcontrib><title>Attitude adjusting bracket for empennage of large aircraft</title><description>The utility model discloses an empennage attitude adjusting bracket for a large aircraft, and aims to provide the empennage attitude adjusting bracket for the large aircraft, which is convenient for adjusting the attitude of an empennage and can stably support the empennage. The tail wing supporting device comprises a sliding mechanism, a main body frame is arranged on the sliding mechanism in a matched mode, a lifting mechanism is arranged on the main body frame, a supporting plate is arranged at the lifting end of the lifting mechanism in a matched mode, and two opposite tail wing supporting blocks are arranged on the supporting plate. The utility model is applied to the technical field of air transportation.
本实用新型公开了一种大型飞机尾翼调姿托架，旨在提供一种便于调整尾翼姿态及能够稳定支撑尾翼的大型飞机尾翼调姿托架。本实用新型包括滑动机构，所述滑动机构上配合设置有主体架，所述主体架上设置有升降机构，所述升降机构的升降端配合设置有支撑托板，所述支撑托板上设置有两个相对的尾翼托块。本实用新型应用于航空运输的技术领域。</description><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</subject><subject>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</subject><subject>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLByLCnJLClNSVVITMkqLS7JzEtXSCpKTM5OLVFIyy9SSM0tSM3LS0xPVchPU8hJLAIyEjOLkosS00p4GFjTEnOKU3mhNDeDkptriLOHbmpBfnxqcUFicmpeakm8s5-RoYWpoaWFqVloqDFRigDl_S_7</recordid><startdate>20230224</startdate><enddate>20230224</enddate><creator>YANG XINLIANG</creator><creator>FU JINGLI</creator><creator>CAI JUNWEN</creator><creator>XIE XING</creator><scope>EVB</scope></search><sort><creationdate>20230224</creationdate><title>Attitude adjusting bracket for empennage of large aircraft</title><author>YANG XINLIANG ; FU JINGLI ; CAI JUNWEN ; XIE XING</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN218519856UU3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2023</creationdate><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</topic><topic>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</topic><topic>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>YANG XINLIANG</creatorcontrib><creatorcontrib>FU JINGLI</creatorcontrib><creatorcontrib>CAI JUNWEN</creatorcontrib><creatorcontrib>XIE XING</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>YANG XINLIANG</au><au>FU JINGLI</au><au>CAI JUNWEN</au><au>XIE XING</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Attitude adjusting bracket for empennage of large aircraft</title><date>2023-02-24</date><risdate>2023</risdate><abstract>The utility model discloses an empennage attitude adjusting bracket for a large aircraft, and aims to provide the empennage attitude adjusting bracket for the large aircraft, which is convenient for adjusting the attitude of an empennage and can stably support the empennage. The tail wing supporting device comprises a sliding mechanism, a main body frame is arranged on the sliding mechanism in a matched mode, a lifting mechanism is arranged on the main body frame, a supporting plate is arranged at the lifting end of the lifting mechanism in a matched mode, and two opposite tail wing supporting blocks are arranged on the supporting plate. The utility model is applied to the technical field of air transportation.
本实用新型公开了一种大型飞机尾翼调姿托架，旨在提供一种便于调整尾翼姿态及能够稳定支撑尾翼的大型飞机尾翼调姿托架。本实用新型包括滑动机构，所述滑动机构上配合设置有主体架，所述主体架上设置有升降机构，所述升降机构的升降端配合设置有支撑托板，所述支撑托板上设置有两个相对的尾翼托块。本实用新型应用于航空运输的技术领域。</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN218519856UU |
| source | esp@cenet |
| subjects | AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR PERFORMING OPERATIONS TRANSPORTING |
| title | Attitude adjusting bracket for empennage of large aircraft |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-18T22%3A00%3A20IST&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=YANG%20XINLIANG&rft.date=2023-02-24&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN218519856UU%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 |