A circuit board locking structure for high-speed rotation test in low-speed wind tunnel
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- LOW SPEED AERODYNAMIC INST OF CHINESE AERODYNAMIC RES & DEV CENT
- Publication Date
- 2020-11-06
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Abstract
Description
technical field
[0001] The invention relates to the field of low-speed wind tunnel measurement, in particular to a circuit board locking structure used in low-speed wind tunnel high-speed rotation tests. Background technique
[0002] The rotor is the key moving part of the helicopter. The performance of the rotor is the key to the performance of the helicopter. The aerodynamic characteristics of the helicopter rotor have an important impact on the performance, flight quality, noise characteristics, vibration characteristics, etc. of the helicopter. During the development of helicopters, many experimental studies are carried out, among which the model wind tunnel test is one of the basic test items. Through wind tunnel tests, important parameters such as rotor performance, blade surface pressure, and aeroelastic torsion can be obtained. At present, the acquisition of blade surface pressure and aeroelastic torsion parameters mainly adopts the electrical measurement method, wh...