Unmanned helicopter main rotor lift test board
The invention discloses an unmanned helicopter main rotor lift force test board, belongs to the technical field of test devices, and solves the problem that the flight lift force of a main rotor cannot be tested on the ground at present. The test board comprises a main rotor system, a belt wheel sys...
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 | HONG PING NI HUI SUN ZHONGHUI QIU SHUYA NIU ANYI WU SHUANG ZHANG GUORAN |
| description | The invention discloses an unmanned helicopter main rotor lift force test board, belongs to the technical field of test devices, and solves the problem that the flight lift force of a main rotor cannot be tested on the ground at present. The test board comprises a main rotor system, a belt wheel system, a motor, a first fixing frame, a second fixing frame, a pull pressure sensor, a counterweight device, a test bed and a third fixing frame; the fixed frame I is placed on the test bed; the second fixing frame is located above the first fixing frame, and one end of the second fixing frame is connected with the first fixing frame through a bearing A; the middle of the second fixing frame is connected with the first fixing frame through a pull pressure sensor. The third fixing frame is placed at the other end of the first fixing frame, and the balance weight device is placed on the third fixing frame. The motor, the belt wheel system and the main rotor system are all installed on the second fixing frame, and the m |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN114715427A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN114715427A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN114715427A3</originalsourceid><addsrcrecordid>eNrjZNALzctNzMtLTVHISM3JTM4vKEktUshNzMxTKMovyS9SyMlMK1EoSS0uUUjKTyxK4WFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFicmpeakl8c5-hoYm5oamJkbmjsbEqAEA_sUqjA</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Unmanned helicopter main rotor lift test board</title><source>esp@cenet</source><creator>HONG PING ; NI HUI ; SUN ZHONGHUI ; QIU SHUYA ; NIU ANYI ; WU SHUANG ; ZHANG GUORAN</creator><creatorcontrib>HONG PING ; NI HUI ; SUN ZHONGHUI ; QIU SHUYA ; NIU ANYI ; WU SHUANG ; ZHANG GUORAN</creatorcontrib><description>The invention discloses an unmanned helicopter main rotor lift force test board, belongs to the technical field of test devices, and solves the problem that the flight lift force of a main rotor cannot be tested on the ground at present. The test board comprises a main rotor system, a belt wheel system, a motor, a first fixing frame, a second fixing frame, a pull pressure sensor, a counterweight device, a test bed and a third fixing frame; the fixed frame I is placed on the test bed; the second fixing frame is located above the first fixing frame, and one end of the second fixing frame is connected with the first fixing frame through a bearing A; the middle of the second fixing frame is connected with the first fixing frame through a pull pressure sensor. The third fixing frame is placed at the other end of the first fixing frame, and the balance weight device is placed on the third fixing frame. The motor, the belt wheel system and the main rotor system are all installed on the second fixing frame, and the m</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>2022</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=20220708&DB=EPODOC&CC=CN&NR=114715427A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220708&DB=EPODOC&CC=CN&NR=114715427A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HONG PING</creatorcontrib><creatorcontrib>NI HUI</creatorcontrib><creatorcontrib>SUN ZHONGHUI</creatorcontrib><creatorcontrib>QIU SHUYA</creatorcontrib><creatorcontrib>NIU ANYI</creatorcontrib><creatorcontrib>WU SHUANG</creatorcontrib><creatorcontrib>ZHANG GUORAN</creatorcontrib><title>Unmanned helicopter main rotor lift test board</title><description>The invention discloses an unmanned helicopter main rotor lift force test board, belongs to the technical field of test devices, and solves the problem that the flight lift force of a main rotor cannot be tested on the ground at present. The test board comprises a main rotor system, a belt wheel system, a motor, a first fixing frame, a second fixing frame, a pull pressure sensor, a counterweight device, a test bed and a third fixing frame; the fixed frame I is placed on the test bed; the second fixing frame is located above the first fixing frame, and one end of the second fixing frame is connected with the first fixing frame through a bearing A; the middle of the second fixing frame is connected with the first fixing frame through a pull pressure sensor. The third fixing frame is placed at the other end of the first fixing frame, and the balance weight device is placed on the third fixing frame. The motor, the belt wheel system and the main rotor system are all installed on the second fixing frame, and the m</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>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNALzctNzMtLTVHISM3JTM4vKEktUshNzMxTKMovyS9SyMlMK1EoSS0uUUjKTyxK4WFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFicmpeakl8c5-hoYm5oamJkbmjsbEqAEA_sUqjA</recordid><startdate>20220708</startdate><enddate>20220708</enddate><creator>HONG PING</creator><creator>NI HUI</creator><creator>SUN ZHONGHUI</creator><creator>QIU SHUYA</creator><creator>NIU ANYI</creator><creator>WU SHUANG</creator><creator>ZHANG GUORAN</creator><scope>EVB</scope></search><sort><creationdate>20220708</creationdate><title>Unmanned helicopter main rotor lift test board</title><author>HONG PING ; NI HUI ; SUN ZHONGHUI ; QIU SHUYA ; NIU ANYI ; WU SHUANG ; ZHANG GUORAN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN114715427A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2022</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>HONG PING</creatorcontrib><creatorcontrib>NI HUI</creatorcontrib><creatorcontrib>SUN ZHONGHUI</creatorcontrib><creatorcontrib>QIU SHUYA</creatorcontrib><creatorcontrib>NIU ANYI</creatorcontrib><creatorcontrib>WU SHUANG</creatorcontrib><creatorcontrib>ZHANG GUORAN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HONG PING</au><au>NI HUI</au><au>SUN ZHONGHUI</au><au>QIU SHUYA</au><au>NIU ANYI</au><au>WU SHUANG</au><au>ZHANG GUORAN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Unmanned helicopter main rotor lift test board</title><date>2022-07-08</date><risdate>2022</risdate><abstract>The invention discloses an unmanned helicopter main rotor lift force test board, belongs to the technical field of test devices, and solves the problem that the flight lift force of a main rotor cannot be tested on the ground at present. The test board comprises a main rotor system, a belt wheel system, a motor, a first fixing frame, a second fixing frame, a pull pressure sensor, a counterweight device, a test bed and a third fixing frame; the fixed frame I is placed on the test bed; the second fixing frame is located above the first fixing frame, and one end of the second fixing frame is connected with the first fixing frame through a bearing A; the middle of the second fixing frame is connected with the first fixing frame through a pull pressure sensor. The third fixing frame is placed at the other end of the first fixing frame, and the balance weight device is placed on the third fixing frame. The motor, the belt wheel system and the main rotor system are all installed on the second fixing frame, and the m</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN114715427A |
| 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 | Unmanned helicopter main rotor lift test board |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-05T14%3A26%3A26IST&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=HONG%20PING&rft.date=2022-07-08&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN114715427A%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 |