Kaijo Sonic Corporation has developed in collaboration with the Japan Aerospace Exploration Agency (JAXA) an UltaSonic Velocimeter (USV) for aviation (Matayoshi et al 2005). The USV is based on a conventional ultrasonic anemometer that consists of two main components: (1) A probe, which senses the three-dimensional aircraft-relative airflow vector and ambient temperature by measuring ultrasonic pulse transit time between three mounts (see figure at right); And (2) a control box and a junction box, which control ultrasonic pulse emissions, and output the measured data via RS-232C. The main advantage of the USV as compared to a pitot-static system is that it can provide accurate measurements at low speed. This is obviously important for helicopters. Unlike conventional ultrasonic anemometers, the USV uses high-frequency (200 kHz) ultrasonic pulses to reduce acoustic noise, and its probe shape minimizes airflow disturbance at high airspeeds. These modifications allow a broad range of airflow measurements, from 0 to 70 m/s, which covers the entire flight envelope of most commercial helicopters.
As part of a collaboration agreement that we developed with JAXA, we mounted a prototype version of the USV on the nose of the HOP, next to the AIMMS-20. We are exploring the performance of the USV (as compared to the AIMMS-20) in flights at different altitudes and under different meteorological conditions.