Aircraft control device force displacement measuring device and method
The invention belongs to the field of flight control system design and test in the field of aircraft design, and particularly relates to an aircraft control device force displacement measuring device and method. The device comprises a clamping piece (1), an assembly frame (2), a grip (3), a force me...
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| creator | YANG LINYA DU XIAODONG JIANG FEIHONG WANG HUI |
| description | The invention belongs to the field of flight control system design and test in the field of aircraft design, and particularly relates to an aircraft control device force displacement measuring device and method. The device comprises a clamping piece (1), an assembly frame (2), a grip (3), a force measurement unit and an inertia measurement unit, the clamping piece (1) is clamped on an aircraft control device, the grip (3) is fixedly connected with the clamping piece (1) through the assembly frame (2), and the force measurement unit and the inertia measurement unit are laid in the assembly frame (2). The inertia measurement unit and the force measurement unit are arranged to realize combined measurement of the force displacement of the aircraft control device, and the use is simple and convenient; the inertia measurement unit and the force measurement strain gauge are integrated by arranging the assembly frame, miniaturization and integration of the device are achieved, and the device is convenient to use in a |
| format | Patent |
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The device comprises a clamping piece (1), an assembly frame (2), a grip (3), a force measurement unit and an inertia measurement unit, the clamping piece (1) is clamped on an aircraft control device, the grip (3) is fixedly connected with the clamping piece (1) through the assembly frame (2), and the force measurement unit and the inertia measurement unit are laid in the assembly frame (2). The inertia measurement unit and the force measurement unit are arranged to realize combined measurement of the force displacement of the aircraft control device, and the use is simple and convenient; the inertia measurement unit and the force measurement strain gauge are integrated by arranging the assembly frame, miniaturization and integration of the device are achieved, and the device is convenient to use in a</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=20210409&DB=EPODOC&CC=CN&NR=112623257A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210409&DB=EPODOC&CC=CN&NR=112623257A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>YANG LINYA</creatorcontrib><creatorcontrib>DU XIAODONG</creatorcontrib><creatorcontrib>JIANG FEIHONG</creatorcontrib><creatorcontrib>WANG HUI</creatorcontrib><title>Aircraft control device force displacement measuring device and method</title><description>The invention belongs to the field of flight control system design and test in the field of aircraft design, and particularly relates to an aircraft control device force displacement measuring device and method. 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| 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 | Aircraft control device force displacement measuring device and method |
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