Gregory's ServerAn aircraft has a pressure port to measure the static air pressure and a pitot tube to measure the total pressure due to speed. These were connected by tubes to the front of the CADC. 2/13
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 As the pressure changed, metal bellows inside the dome expanded, rotating a shaft. But these rotations were too weak to turn all the gears of the CADC, so a motorized servo loop amplified the rotations. 4/13 This diagram shows the servo loop. A sensitive inductive pickup detected the rotation and generated an error signal that went to an amplifier. The motor rotated to counteract the bellows motion. When the error signal was 0, the output shaft rotation matched the pressure. 5/13 The amplifier took three boards: transistors in conjunction with magnetic amplifiers (yellow units). Transistors weren't good enough at the time to drive the motors directly, so transistors controlled the magnetic amplifiers, which drove the motors. 6/13  @kenshirriff I don't think I've ever seen (or otherwise would ever see) such a label as "CAUTION: DO NOT BLOW IN TUBES" on any piece of equipment. I wonder what the danger is - are the pressure sensors really that sensitive to damage? |
Inside the CADC, two sealed black domes hold the pressure sensors. Each sensor has a stack of associated electronics boards. The boards are amplifiers that drive the motors that turn the gears. 3/13