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Patent US4314307A successfully refreshed from Google Patents.
US4314307A
Expired / Lapsed
US
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Electro-mechanical sensor power up circuit
Assignee: United States Department of the Navy
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Filing: 1980-05-05
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Granted: 1982-02-02
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Expires: 2000-05-05
Abstract
Abstract An electrical circuit for allowing electrical power to be applied to the ctro-mechanical sensors of an automatic flight control system of an aircraft only when either the Engine Start switch or AFCS Engage switch is closed separately or simultaneously. Upon the closing of either one or both of the switches, a pair of latching relays are energized which in turn provide electric power to the electro-mechanical sensors.
Inventors
- 👤 Albert Sivahop
- 👤 Don L. Adams, Sr.
- 👤 William C. Fischer
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-07 21:34
CPC Classifications
H; H01; H01H; H01H47/00; H01H47/001; H02; H02H; H02H11/00
Claims Analysis
Total Claims: 2
Claim 1
Independent Claim
147 words
An electrical circuit for improving the useful life of a plurality of electromechanical sensors including rate gyros of an automatic flight control system of an aircraft comprising: means for energizing a plurality of latching circuits upon command including at least one pair of push button switches closable separately or simultaneously; a plurality of relays which are activated upon energizing separately or simultaneously of said plurality of latching circuits, said relays having means for providing electric power to said plurality of electro-mechanical sensors; and means for energizing said plurality of electro-mechanical sensors only when the aircraft power and at least one of said pair of push button switches are on including a plurality of transistors which are short circuited upon closing of at least one of said pair of push button switches and thus energizing and keeping energized said plurality of relays during power-on interval of the aircraft.
Claim 2
Dependent Claim
147 words
An electrical circuit for improving the useful life of a plurality of electromechanical sensors including rate gyros of an automatic flight control system of an aircraft comprising: means for energizing a plurality of latching circuits upon command including at least one pair of push button switches closable separately or simultaneously; a plurality of relays which are activated upon energizing separately or simultaneously of said plurality of latching circuits, said relays having means for providing electric power to said plurality of electro-mechanical sensors; and means for energizing said plurality of electro-mechanical sensors only when the aircraft power and at least one of said pair of push button switches are on including a plurality of transistors which are short circuited upon closing of at least one of said pair of push button switches and thus energizing and keeping energized said plurality of relays during power-on interval of the aircraft.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1985-02-01 | 1985-08-03 | 1986-02-02 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1989-02-01 | 1989-08-03 | 1990-02-02 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1993-02-01 | 1993-08-03 | 1994-02-02 | $7700.00 | Window Closed / Lapsed |