FIELD: measurement technology; electronics.
SUBSTANCE: invention is used for multi-channel pressure measurements on the surface of aircraft models using a drainless method. The proposed multichannel pressure transducer contains strain gauge sensitive pressure elements, built on the basis of strain gauge measuring bridges, manufactured using surface micromechanics technology and mounted inside a thin flexible polyimide tape with holes in the tape located opposite each pressure sensitive element in one line in the centre of the tape, a pneumatic channel, combining the return cavities of the pressure sensitive elements, electrical power lines and lines of measuring diagonals of strain gauge measuring bridges laid inside the tape, a tape temperature sensor, a multi-channel analogue-to-digital converter, a microcontroller, a power supply voltage driver for the converter elements, a pneumatic channel fitting that combines the return cavities of the pressure sensitive elements installed on the mounting part of the tape.
EFFECT: ability to measure pressure distribution on the surface of models and full-scale aircraft samples using a drainless method; expansion of the frequency range of measured pressures; simplification of the circuit, design and reduction of dimensions of the pressure transducer.
3 cl, 1 dwg
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Authors
Dates
2024-01-25—Published
2023-08-15—Filed