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Title:
サーボ型加速度計
Document Type and Number:
Japanese Patent JP5530219
Kind Code:
B2
Abstract:
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.

Inventors:
Kenji Kuramoto
Yoshiyuki Ando
Hiroyuki Motoki
Shuichi Yamamoto
Takazumi Yamada
Application Number:
JP2010041199A
Publication Date:
June 25, 2014
Filing Date:
February 26, 2010
Export Citation:
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Assignee:
Japan Aviation Electronics Industry Co., Ltd.
International Classes:
G01P15/13
Domestic Patent References:
JP8292208A
JP62007101A
JP2001167935A
JP2002168878A
JP64012273A
JP2005206944A
JP2004031274A
JP2003290031A
JP2001284219A
JP6081084A
JP61017959A
Attorney, Agent or Firm:
Naoki Nakao
Yukio Nakamura
Taku Kusano



 
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