Wing tip support device for wind tunnel test
A technology of wind tunnel test and support device, which is applied in the direction of measuring device, aerodynamic test, machine/structural component test, etc. It can solve the interference of air flow, affect the reliability of test results, and cannot realize the model angle of attack and sideslip Angle changes and other issues, to improve reliability and facilitate research
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[0027] This embodiment is an aircraft model wingtip support device. It can not only be used to measure the aerodynamic force of the aircraft model in the wind tunnel, but also use the delivery mechanism to drop the airdrop model from the hollow aircraft model, and use the camera to record the trajectory of the airdrop model.
[0028] This embodiment includes a force-measuring balance 1 , a single-component resistance balance 10 , a force platform 11 , a support beam 2 , a support column 3 , a mechanism for changing the angle of attack 4 , a mechanism for changing the angle of sideslip 6 and a model connector 7 . Variable angle of attack mechanism 4 consists of motor 12, reducer 13, gear pair 14, worm screw 15, turbine 16, internal spline shaft 19, turbine bearing 20, turbine bearing seat 21, flange spline shaft 5, worm bearing 18, worm bearing Seat 17 and some screws are formed; Variable side slip angle mechanism 6 is made up of slide plate 22, sliding flange 23, bearing pin 2...
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