Loading test system for simulating torsional static force of propeller
The invention provides a loading test system for simulating torsional static force of a propeller. The loading test system comprises a base body, a traction connecting piece and a suspension arm piece, the base body comprises a first side and a second side which are oppositely arranged in the first...
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| creator | GUO BINGBIN ZHONG MEIFA LIN ZHUANGLONG ZHU PAN YANG ZHOU CHENG QIANG |
| description | The invention provides a loading test system for simulating torsional static force of a propeller. The loading test system comprises a base body, a traction connecting piece and a suspension arm piece, the base body comprises a first side and a second side which are oppositely arranged in the first direction, the traction connecting piece is arranged on the first side, and a traction connecting structure is arranged on the traction connecting piece; the second side is provided with a fixed connection structure, the fixed connection structure is used for being fixedly connected with a mounting frame of an aircraft propeller engine and enabling the base body to be located at the position corresponding to the aircraft propeller engine, and the first direction is the axial direction of the aircraft propeller engine; in the second direction perpendicular to the first direction, the base body is provided with an inserting hole, the first extending end of the suspension arm piece is detachably installed in the inser |
| format | Patent |
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The loading test system comprises a base body, a traction connecting piece and a suspension arm piece, the base body comprises a first side and a second side which are oppositely arranged in the first direction, the traction connecting piece is arranged on the first side, and a traction connecting structure is arranged on the traction connecting piece; the second side is provided with a fixed connection structure, the fixed connection structure is used for being fixedly connected with a mounting frame of an aircraft propeller engine and enabling the base body to be located at the position corresponding to the aircraft propeller engine, and the first direction is the axial direction of the aircraft propeller engine; in the second direction perpendicular to the first direction, the base body is provided with an inserting hole, the first extending end of the suspension arm piece is detachably installed in the inser</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 ; INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES ; MEASURING ; PERFORMING OPERATIONS ; PHYSICS ; TESTING ; TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES ; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR ; TRANSPORTING</subject><creationdate>2024</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=20240614&DB=EPODOC&CC=CN&NR=118190662A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76516</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240614&DB=EPODOC&CC=CN&NR=118190662A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GUO BINGBIN</creatorcontrib><creatorcontrib>ZHONG MEIFA</creatorcontrib><creatorcontrib>LIN ZHUANGLONG</creatorcontrib><creatorcontrib>ZHU PAN</creatorcontrib><creatorcontrib>YANG ZHOU</creatorcontrib><creatorcontrib>CHENG QIANG</creatorcontrib><title>Loading test system for simulating torsional static force of propeller</title><description>The invention provides a loading test system for simulating torsional static force of a propeller. 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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 INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES MEASURING PERFORMING OPERATIONS PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR TRANSPORTING |
| title | Loading test system for simulating torsional static force of propeller |
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