A wireless passive pressure sensor based on aperture coupled microstrip patch antenna

• Published in: Sensor review Vol. 38; no. 2; pp. 156 - 162
• Main Authors: Guo, YanJie, Tan, QiuLin, Lu, Fei, Wu, GuoZhu, Zhang, Lei
• Format: Journal Article
• Language: English
• Published: Bradford Emerald Publishing Limited 06.03.2018; Emerald Group Publishing Limited
• Subjects: Aircraft engines; Antennas; Apertures; Electric fields; High temperature environments; Microstrip antennas; Passive pressure; Patch antennas; Permittivity; Pressure measurement; Pressure sensors; Questioning; Resonant frequencies; Sensors; Simulation; Substrates; Embedded air cavity; Wireless sensing; Pressure sensor; Microstrip antenna; Resonant frequency
• ISSN: 0260-2288; 1758-6828
• DOI: 10.1108/SR-05-2017-0076

Purpose This paper aims to present a novel wireless passive pressure sensor based on an aperture coupled microstrip patch antenna embedded with an air cavity for pressure measurement. Design/methodology/approach In this paper, the sensitive membrane deformed when pressure was applied on the surface of the sensor and the relative permittivity of the mixed substrate changed, resulting in a change in the center frequency of the microstrip antenna. The size of the pressure sensor is determined by theoretical calculation and software simulation. Then, the sensor is fabricated separately as three layers using printed circuit board technology and glued together at last. The pressure test of the sensor is carried out in a sealed metal tank. Findings The extracted resonant frequency was found to monotonically shift from 2.219 to 1.974 GHz when the pressure varied from 0 to 300 kPa, leading to an average absolute sensitivity of 0.817 MHz/kPa. Research limitations/implications This pressure sensor proposed here is mainly to verify the feasibility of this wireless passive maneuvering structure, and when the base material of this structure is replaced with some high-temperature-resistant material, the sensor can be used to measure the pressure inside the aircraft engine. Originality/value The sensor structure proposed here can be used to test the pressure in a high-temperature environment when the base material is replaced with some high-temperature-resistant material.