Wing component testing device
The embodiment of the invention discloses a wing component testing device which comprises a rack, a fixed seat and a torsion mechanism, the fixed seat and the torsion mechanism are arranged on the rack, the fixed seat is arranged to be capable of fixing and positioning a wing component, the torsion...
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 | YU XINGZHE XIANG ZHIHAI JIN MINJING XU MANQIONG |
| description | The embodiment of the invention discloses a wing component testing device which comprises a rack, a fixed seat and a torsion mechanism, the fixed seat and the torsion mechanism are arranged on the rack, the fixed seat is arranged to be capable of fixing and positioning a wing component, the torsion mechanism is arranged to be capable of clamping the wing component and applying torque to the wing component, and the wing component testing device further comprises a bag body, the bag body is arranged to be capable of being inflated with gas or liquid and acting on the wing type component.
本发明实施例公开一种机翼类构件测试装置，包括机架、设于机架上的固定座和扭转机构，固定座设置成能够固定并定位机翼类构件，扭转机构设置成能够夹持机翼类构件并对机翼类构件施加扭矩，机翼类构件测试装置还包括囊体，囊体设置成能够充入气体或者液体并作用于机翼类构件。 |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN112498739A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN112498739A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN112498739A3</originalsourceid><addsrcrecordid>eNrjZJANz8xLV0jOzy3Iz0vNK1EoSS0uAYmkpJZlJqfyMLCmJeYUp_JCaW4GRTfXEGcP3dSC_PjU4oLE5NS81JJ4Zz9DQyMTSwtzY0tHY2LUAADZKCRS</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Wing component testing device</title><source>esp@cenet</source><creator>YU XINGZHE ; XIANG ZHIHAI ; JIN MINJING ; XU MANQIONG</creator><creatorcontrib>YU XINGZHE ; XIANG ZHIHAI ; JIN MINJING ; XU MANQIONG</creatorcontrib><description>The embodiment of the invention discloses a wing component testing device which comprises a rack, a fixed seat and a torsion mechanism, the fixed seat and the torsion mechanism are arranged on the rack, the fixed seat is arranged to be capable of fixing and positioning a wing component, the torsion mechanism is arranged to be capable of clamping the wing component and applying torque to the wing component, and the wing component testing device further comprises a bag body, the bag body is arranged to be capable of being inflated with gas or liquid and acting on the wing type component.
本发明实施例公开一种机翼类构件测试装置，包括机架、设于机架上的固定座和扭转机构，固定座设置成能够固定并定位机翼类构件，扭转机构设置成能够夹持机翼类构件并对机翼类构件施加扭矩，机翼类构件测试装置还包括囊体，囊体设置成能够充入气体或者液体并作用于机翼类构件。</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>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=20210316&DB=EPODOC&CC=CN&NR=112498739A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76318</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210316&DB=EPODOC&CC=CN&NR=112498739A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>YU XINGZHE</creatorcontrib><creatorcontrib>XIANG ZHIHAI</creatorcontrib><creatorcontrib>JIN MINJING</creatorcontrib><creatorcontrib>XU MANQIONG</creatorcontrib><title>Wing component testing device</title><description>The embodiment of the invention discloses a wing component testing device which comprises a rack, a fixed seat and a torsion mechanism, the fixed seat and the torsion mechanism are arranged on the rack, the fixed seat is arranged to be capable of fixing and positioning a wing component, the torsion mechanism is arranged to be capable of clamping the wing component and applying torque to the wing component, and the wing component testing device further comprises a bag body, the bag body is arranged to be capable of being inflated with gas or liquid and acting on the wing type component.
本发明实施例公开一种机翼类构件测试装置，包括机架、设于机架上的固定座和扭转机构，固定座设置成能够固定并定位机翼类构件，扭转机构设置成能够夹持机翼类构件并对机翼类构件施加扭矩，机翼类构件测试装置还包括囊体，囊体设置成能够充入气体或者液体并作用于机翼类构件。</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>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJANz8xLV0jOzy3Iz0vNK1EoSS0uAYmkpJZlJqfyMLCmJeYUp_JCaW4GRTfXEGcP3dSC_PjU4oLE5NS81JJ4Zz9DQyMTSwtzY0tHY2LUAADZKCRS</recordid><startdate>20210316</startdate><enddate>20210316</enddate><creator>YU XINGZHE</creator><creator>XIANG ZHIHAI</creator><creator>JIN MINJING</creator><creator>XU MANQIONG</creator><scope>EVB</scope></search><sort><creationdate>20210316</creationdate><title>Wing component testing device</title><author>YU XINGZHE ; XIANG ZHIHAI ; JIN MINJING ; XU MANQIONG</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN112498739A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2021</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>YU XINGZHE</creatorcontrib><creatorcontrib>XIANG ZHIHAI</creatorcontrib><creatorcontrib>JIN MINJING</creatorcontrib><creatorcontrib>XU MANQIONG</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>YU XINGZHE</au><au>XIANG ZHIHAI</au><au>JIN MINJING</au><au>XU MANQIONG</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Wing component testing device</title><date>2021-03-16</date><risdate>2021</risdate><abstract>The embodiment of the invention discloses a wing component testing device which comprises a rack, a fixed seat and a torsion mechanism, the fixed seat and the torsion mechanism are arranged on the rack, the fixed seat is arranged to be capable of fixing and positioning a wing component, the torsion mechanism is arranged to be capable of clamping the wing component and applying torque to the wing component, and the wing component testing device further comprises a bag body, the bag body is arranged to be capable of being inflated with gas or liquid and acting on the wing type component.
本发明实施例公开一种机翼类构件测试装置，包括机架、设于机架上的固定座和扭转机构，固定座设置成能够固定并定位机翼类构件，扭转机构设置成能够夹持机翼类构件并对机翼类构件施加扭矩，机翼类构件测试装置还包括囊体，囊体设置成能够充入气体或者液体并作用于机翼类构件。</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN112498739A |
| 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 | Wing component testing device |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-10T11%3A25%3A39IST&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=YU%20XINGZHE&rft.date=2021-03-16&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN112498739A%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 |