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US3679960A Expired / Lapsed US ⏱️ 0.0 years remaining

Electric power source system for gyroscopic instrument

Assignee: Tokyo Keiki Inc
•
Filing: 1971-01-19
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Granted: 1972-07-25
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Expires: 1991-01-19
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Abstract

Abstract An electric power source system for a gyroscopic instrument in which the kinetic energy of the gyro rotor revolving at high speed is used as an induction generator during times when the normal electrical power source for the gyroscopic instrument fails and to maintain the gyroscopic instrument in its normal operative condition during the time the electrical power source is disconnected.

Inventors

  • 👤 Yoichi Hirokawa
  • 👤 Masatoshi Sato

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-23 19:02
CPC Classifications
G; G01; G01C; G01C19/00; G01C19/02; G01C19/04; G01C19/06; G01C19/08; G01C19/10; G01C19/34; G01C19/38

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 260 words
An electrical power source system for a gyroscopic instrument driven by polyphase A.C. motor comprising: a gyro rotor mounted in said gyroscopic instrument; a polyphase A.C. motor connected to drive said gyro rotor at high speed and having a plurality of windings; a single-phase electrical power source; a converter circuit means connected between said single-phase electrical power source and said polyphase motor for converting power from said single-phase source to polyphase power, a first capacitor in said converter circuit having a capacitance such that said capacitor resonates with the inductances of the windings of said polyphase A.C. motor in the region of the frequency of said single-phase power source, and whereby said single-phase electrical power source is interrupted when said polyphase A.C. motor operates as an induction generator being driven by said gyro rotor to supply electrical power; an electrical utilization circuit associated with said gyroscopic instrument electrically connected to said polyphase A.C. motor and energized thereby when said single-phase power source is interrupted, a second capacitor is inserted between two of said windings of said polyphase motor which are not connected to said first capacitor, a relay connected to said single-phase source for controlling a pair of movable contacts with one disconnecting said single-phase electrical power source and said utilization electrical circuit of said gyroscopic instrument and another movable contact connects said second capacitor in circuit, whereby when said single-phase electrical power source is interrupted, the first movable contact is opened and the second movable contact is closed to disconnect said single-phase electrical power source from said induction generator.
Claim 2
Dependent Claim 260 words
An electrical power source system for a gyroscopic instrument driven by polyphase A.C. motor comprising: a gyro rotor mounted in said gyroscopic instrument; a polyphase A.C. motor connected to drive said gyro rotor at high speed and having a plurality of windings; a single-phase electrical power source; a converter circuit means connected between said single-phase electrical power source and said polyphase motor for converting power from said single-phase source to polyphase power, a first capacitor in said converter circuit having a capacitance such that said capacitor resonates with the inductances of the windings of said polyphase A.C. motor in the region of the frequency of said single-phase power source, and whereby said single-phase electrical power source is interrupted when said polyphase A.C. motor operates as an induction generator being driven by said gyro rotor to supply electrical power; an electrical utilization circuit associated with said gyroscopic instrument electrically connected to said polyphase A.C. motor and energized thereby when said single-phase power source is interrupted, a second capacitor is inserted between two of said windings of said polyphase motor which are not connected to said first capacitor, a relay connected to said single-phase source for controlling a pair of movable contacts with one disconnecting said single-phase electrical power source and said utilization electrical circuit of said gyroscopic instrument and another movable contact connects said second capacitor in circuit, whereby when said single-phase electrical power source is interrupted, the first movable contact is opened and the second movable contact is closed to disconnect said single-phase electrical power source from said induction generator.

References Cited (Backward Citations)

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USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1975-07-25 1976-01-24 1976-07-25 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1979-07-25 1980-01-24 1980-07-25 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1983-07-25 1984-01-24 1984-07-25 $7700.00 Window Closed / Lapsed

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