Patent US4313081A successfully refreshed from Google Patents.
US4313081A
Expired / Lapsed
US
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Line drop compensation device for an electrical distribution system
Assignee: CACI Inc Federal
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Filing: 1980-04-01
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Granted: 1982-01-26
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Expires: 2000-04-01
Abstract
Abstract A line drop compensator device for an aircraft flight line electrical distribution system has a plurality of service points connected at spaced locations along a three-phase power line and the current flow at each service point is sensed. In response to the sensed current flow, capacitance is added between the conductor lines and neutral of the power line so as to correct the voltage in proportion to the demand. Compensation is thus added proportional to the current drawn from the line.
Inventors
- 👤 David W. Smith
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-29 19:41
CPC Classifications
H; H02; H02J; H02J3/00; H02J3/12; H02J3/16; Y; Y02; Y02E; Y02E40/00; Y02E40/30
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
139 words
A line drop compensator device for a service point of an aircraft flight line electrical distribution system comprising a plurality of service points for aircraft connected at spaced locations to a three-phase power line including a neutral line, said power line connected to a single power source, means at each of said service points for sensing the current flow at that service point and generating a proportional signal, means at that service point for comparing said proportional signal with a reference signal and generating a control signal, and means at that service point responsive to said control signal for adding capacitance between a line and neutral to compensate for line inductance and any lagging power factor caused by the aircraft load at that service point so as to correct the voltage supplied to the aircraft proportional to the demand.
Claim 2
Dependent Claim
139 words
A line drop compensator device for a service point of an aircraft flight line electrical distribution system comprising a plurality of service points for aircraft connected at spaced locations to a three-phase power line including a neutral line, said power line connected to a single power source, means at each of said service points for sensing the current flow at that service point and generating a proportional signal, means at that service point for comparing said proportional signal with a reference signal and generating a control signal, and means at that service point responsive to said control signal for adding capacitance between a line and neutral to compensate for line inductance and any lagging power factor caused by the aircraft load at that service point so as to correct the voltage supplied to the aircraft proportional to the demand.
Claim 3
Dependent Claim
34 words
A line drop compensator device as claimed in claim 1 and further comprising means for connecting additional capacitance across the phase conductor and neutral in response to predetermined increases in the sensed current flow.
Claim 4
Dependent Claim
25 words
A line drop compensator device as claimed in claim 1 wherein said current flow sensing means is in one phase conductor in the power line.
Claim 5
Dependent Claim
36 words
A line drop compensator device as claimed in claim 3 wherein said capacitance adding means comprises a control circuit connected to said comparing means to receive said control signal and a compensation circuit including a capacitance.
Claim 6
Dependent Claim
32 words
A line drop compensator device as claimed in claim 4 wherein said control circuit and said compensation circuit are connected across the neutral line and the phase conductors of said power line.
Claim 7
Dependent Claim
36 words
A line drop compensator device as claimed in claim 4 and further comprising a plurality of said control circuits and said compensation circuits connectable across said neutral line and the phase conductors of said power line.
Claim 8
Dependent Claim
42 words
A line drop compensator device as claimed in claim 6 and means for connecting additional control circuits and capacitance circuits across said neutral line and phase conductors of said power line at predetermined increments of current flow sensed by said sensing means.
References Cited (Backward Citations)
US3002147A
Cited
US4101100A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1985-01-25 | 1985-07-27 | 1986-01-26 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1989-01-25 | 1989-07-27 | 1990-01-26 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1993-01-25 | 1993-07-27 | 1994-01-26 | $7700.00 | Window Closed / Lapsed |