Integrated Airborne Data System for Aircraft

摘要

An embodiment of the present invention relates to an integrated atmospheric data system of an aircraft, and the technical problem to be solved is formed by integrating a voltage port, a static port, and an angle of attack port. The purpose is to provide an integrated atmospheric data system for aircraft capable of accurately measuring the voltage, static pressure, and gradient pressure of aircraft by preventing the pressure applied to each of the voltage ports, static pressure ports, and gradient pressure ports from affecting other ports. To this end, the present invention is a probe assembly into which air pressure is introduced; A pressure sensor unit connected to the probe assembly to measure air pressure; A main processing unit that receives and processes the pneumatic signal from the pressure sensor unit, converts it into an electrical signal, and outputs it to the flight control computer; And a housing coupled to the probe assembly and the aircraft, accommodating the pressure sensor unit and the main processing unit, wherein the probe assembly has a voltage port formed at the front, a positive pressure port formed at the side, and inclined on an inclined surface between the front and the side. A probe cover having a pressure port formed thereon, a voltage connector connecting the voltage port to the voltage sensor of the pressure sensor unit, a static pressure connector connecting the static pressure port to the static pressure sensor of the pressure sensor unit, and the inclined pressure port of the pressure sensor unit. Disclosed is an aircraft's integrated atmospheric data system, including a tilt pressure connector that connects to the tilt pressure sensor.