Wind tunnel test model parallel mechanism support device for aircraft formation flight
The invention relates to the technical field of wind tunnel tests, in particular to a wind tunnel test model parallel mechanism support device for aircraft formation flight. The parallel mechanism support device includes a frame, aircraft models for formation flight, a plurality of first rope tracti...
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| creator | LIU TING LIN QI WU HUISONG PENG MIAOJIAO JI YANGFENG |
| description | The invention relates to the technical field of wind tunnel tests, in particular to a wind tunnel test model parallel mechanism support device for aircraft formation flight. The parallel mechanism support device includes a frame, aircraft models for formation flight, a plurality of first rope traction assemblies, a plurality of second rope traction assemblies, two guide rail assemblies, and a machine vision camera. The aircraft models are all pulled by ropes and achieve six-degree-of-freedom motion through a parallel mechanism. The parallel mechanism support device not only has high rigidity,good stability, large working space, and can conveniently realize various formation flight of the aircraft models, but also can effectively avoid interference between the traction ropes, interferencebetween the traction ropes and the aircraft models, and interference between the aircraft models and surrounding obstacles. The parallel mechanism support mechanism has little interference on the flowfield around the models, i |
| format | Patent |
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| subjects | MEASURING PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR |
| title | Wind tunnel test model parallel mechanism support device for aircraft formation flight |
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