SkyView System Installation Guide - Dynon Avionics

15. Accessory Installation and ConfigurationThis chapter contains information regarding installation and configuration of various Dynonsuppliedaccessories for the SkyView system.Angle of Attack Pitot Probe Installation and ConfigurationThis section walks you through the general steps to install and calibrate both the heated andunheated versions of the AOA/Pitot Probe. The heated probe consists of a heater controllermodule and a probe while the standard version is a probe only.While the probe senses standard pitot pressure, allowing it to work with any standard airspeedindicator, its AOA functionality is designed specifically to work with Dynon’s EFIS series ofproducts. Do not expect it to work properly with another AOA system.To ensure accuracy, it is very important that you install the probe correctly andperform the specified calibration steps. We recommend that you read andunderstand this entire section before proceeding with the installation.Dynon’s Heated AOA/Pitot Probe is nickel-plated. Do not polish the probe as thiswill cause the finish to come off.AOA Calculation: Principles of OperationDynon Avionics’ AOA/Pitot probe performs two functions: airspeed sensing and angle of attacksensing. These functions require two pressure ports on the tip of the probe. The normal pitotpressure port is on the front face of the probe and is designed to be insensitive to angle ofattack. The second pressure port is located on an angled surface just under the pitot port and isdesigned to be very sensitive to AOA. The SkyView system then uses the difference betweenthese two pressures to calculate the current angle of attack.Heating: Principles of OperationThe heated version of Dynon’s AOA/Pitot Probe utilizes a nichrome heating element whosetemperature is accurately measured and regulated by the heater controller. This controller–located in an enclosure which can be mounted in a wing or elsewhere–regulates the heat at thetip of the probe to a constant temperature. There are several advantages to this: lower powerconsumption, increased heating element lifespan, and a much cooler pitot on the ground whende-icing is not necessary. This unique technique ensures that the pitot can be rapidly de-icedwhen required, but does not needlessly waste electricity when not in icing conditions.The probe operates at a fairly hot temperature. During normal operation, itregulates its internal temperature to about 70°C to 80°C. You can verify nominaloperation by touching the end of the pitot farthest from the snout after oneminute of operation. It should be warm.SkyView System Installation Guide - Revision O 15-1