
A synchronizer for coupling a corrective servo mechanism to a pneumatic altitude sensor in an aircraft to provide a display with a positive pressure altitude indication. The synchronizer has a first rotor retained on a shaft with gear teeth that are positively engaged with the servomotor. The synchronizer has a second rotor concentric to said first rotor with gear teeth that positively engage the altitude sensor. A coil in the synchronizer is energized and lines of magnetic flux developed which ...









