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Ken Shirriff

Here's a closeup of the gears and differentials that perform the computations. 4/12

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Ken Shirriff

The outputs from the CADC are transmitted electrically to other parts of the aircraft.
Cylindrical devices called synchros convert shaft rotations to 3-wire electrical signals. This diagram shows the synchros and other components inside the CADC. 5/12

Ken Shirriff

The CADC receives pressures from the aircraft's pitot tube. One problem is that the airflow over the aircraft distorts the static pressure reading. The fix is to apply a Pressure Error Correction factor. This factor is determined by the Compensator, an external unit. 6/12

Ken Shirriff

The Compensator uses a 3-D cam to generate the correction factor, sent to the CADC as a synchro signal. The CADC uses a servo loop to generate a rotation corresponding to this factor, then multiplies it with a differential. 7/12

Ken Shirriff

An amplifier board uses transistors and magnetic amplifiers to drive the motor that turns the shaft. They didn't use a printed circuit board, but components soldered to metal pegs. Here's the schematic I reverse-engineered. 8/12

Ken Shirriff

The CADC is a boring cylinder from the outside. You wouldn't expect that amazing mechanical complexity would be found inside. 9/12

Mars 1024 πŸŽ„πŸŽ

@kenshirriff : Wow! You are a legend! 😲😲😲

Thank you, kind Sir, for this knowledge!

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