Ultrasonic angular measurement system

Aeronautics and astronautics – Aircraft structure – Passenger or cargo loading or discharging

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14 711, 73628, 367 96, 367 99, 410 69, 414537, 4145751, B64D 112, G01S 1502

Patent

active

060708328

ABSTRACT:
An ultrasonic angular measurement system is disclosed. The system is comprised of three parts, a control box used to collect and process data, an ultrasonic transducer, and a reflector block. The reflector block is configured so that it intercepts transmitted pulses received over a wide range of angles back to the transducer. All the components are self contained within a transportable housing which is attached to the aircraft deck during measurement of tip-off angle. The range of angle measurement is permitted because of the use of the unique reflector block which comprises a plurality of reflector segments for reflecting ultrasonic pulses transmitted at various ranges of angles.

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Marioli, Daniele et al, "Ultrasonic Distance Measurement for Linear and Angular Position Control", IEEE Transactions on Instrumentation and Measurement, vol. 37, No. 4, Dec. 1988 pp. 578-581.
Published Technical paper, Jun. 22-24 1993, Seventeenth Transducer Workshop, San Diego, CA, entitled "An Ultrasonic Angular Measurement System" by inventor Justin D. Redd, pp. 252-259.
Published Technical paper, Oct. 25-28 1993, International Telemetering Conference, Las Vegas, Nevada, entitled "An Ultrasonic Angular Measreuemtn System" by Inventor Justin D. Redd, pp. 747-754.

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