DocumentCode
3360322
Title
Torquer and hinge design for dry tuned-rotor gyroscopes
Author
Mansour, William M. ; Lacchini, Corrado
Author_Institution
Dept. of Mech. Eng., Inst. Technologico de Aeronaut., Sao Jose dos Campos, Brazil
fYear
1992
fDate
4-9 Oct. 1992
Firstpage
1659
Abstract
The authors report in some detail on the design of the torquer and hinge for the dry tuned rotor gyroscope. They describe a strategy for the thermal design of the torquers that takes into account the temperature dependence of the magnetic field, the resistivity of the wire, and the coefficient of heat transmission. A method is presented for the design of the hinge for tuning and for minimizing anisoelastic drifts. The pickoffs and the torquer coils are fixed to the gyro case. The hinge is designed in such a way as to offer no elastic restraint torques if the rotor is driven at the tuning speed. The gaps between the rotor and the gyro case are sensed by the pickoffs. The operational aspects of the gyro are discussed.<>
Keywords
design engineering; gyroscopes; hysteresis motors; machine theory; magnetic circuits; rotors; torque; anisoelastic drifts; design; dry tuned rotor gyroscope; heat transmission; hinge; hysteresis motors; magnetic circuits; magnetic field; pickoffs; resistivity; thermal analysis; torquer; tuning; Angular velocity; Coils; Conductivity; Fasteners; Gyroscopes; Mechanical engineering; Permanent magnets; Space vehicles; Thermal resistance; Wire;
fLanguage
English
Publisher
ieee
Conference_Titel
Industry Applications Society Annual Meeting, 1992., Conference Record of the 1992 IEEE
Conference_Location
Houston, TX, USA
Print_ISBN
0-7803-0635-X
Type
conf
DOI
10.1109/IAS.1992.244237
Filename
244237
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