Servo Accelerometer
AssigneeJapan Aviation Electronics Industry, Limited
InventorsKenji Kuramoto, Yoshiyuki Ando, Hiroyuki Motoki, Shuichi Yamamoto, Takazumi Yamada
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AssigneeJapan Aviation Electronics Industry, Limited
InventorsKenji Kuramoto, Yoshiyuki Ando, Hiroyuki Motoki, Shuichi Yamamoto, Takazumi Yamada
Estimating the term…
Canister-shaped magnetic reinforcing elements 31, 32 made of a ferromagnetic material having a Curie temperature higher than magnetic yokes 11, 12 are provided inside the magnetic yokes 11, 12. The inner periphery 31a, 32a of an opening in each of the magnetic reinforcing elements 31, 32 is opposed to the outer periphery 51a, 52a of each of pole piece tops 51, 52. A torquer coil 61, 62 is located between the inner periphery 31a, 32a of the opening in each of the magnetic reinforcing elements 31, 32 and the outer periphery 51a, 52a of each pole piece top 51, 52. The magnetic reinforcing elements 31, 32 provided inside the magnetic yokes 11, 12 form independent magnetic circuits. Since the magnetic reinforcing elements 31, 32 have a Curie temperature higher than the magnetic yokes 11, 12, a high accuracy of acceleration measurement in a high-temperature range can be achieved.
A servo accelerometer in which a position to which a pendulum swings from a neutral position is detected, the pendulum is returned to the neutral position by an electromagnetic action based on the swing of the pendulum, and acceleration is detected based on the amount of current required for the electromagnetic action, the servo accelerometer comprising:
Dependencies are inferred from the claim text.