Patent US1366131A successfully refreshed from Google Patents.
Patent US5272387A successfully refreshed from Google Patents.
← Back to Patent Explorer
US5272387A Expired / Lapsed US ⏱️ 0.0 years remaining

Connecting device of an external electrical power supply source to an aircraft on the ground

Assignee: Merlin Gerin SA
•
Filing: 1991-11-07
•
Granted: 1993-12-21
•
Expires: 2011-11-07
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract A device connects an external electrical power supply source to an aircraft on the ground to temporarily replace its auxiliary power units. During the overlap period of the two switches used in the aircraft to achieve this transfer, an impedance, preferably a resistance much greater than the internal impedance of the external source is connected in series on the external line. As soon as switching to the external source has been completed, measurement of a sudden drop in the external voltage brings about closing of a static switch which short-circuits the resistance.

Inventors

  • 👤 Jean-Noel Fiorina
  • 👤 Jean-Jacques Pillet

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-06 16:28
CPC Classifications
H; H02; H02J; H02J3/00; H02J3/38; H02J3/40; H02J3/007; H01; H01H; H01H9/00; H01H9/54; H01H9/548

Claims Analysis

Total Claims: 12
Claim 1
Independent Claim 90 words
A device for connecting an external A.C. electrical power supply source to an aircraft on the ground, comprising a two-way static switch connected between the external source and a power supply input socket of the aircraft, an impedance connected in parallel to the static switch, means for measuring the voltage at terminals of the socket and a processing unit connected to the means for measuring the voltage and to control terminals of the switch so as to close the switch when the voltage measured drops below a first preset threshold.
Claim 2
Independent Claim 90 words
A device for connecting an external A.C. electrical power supply source to an aircraft on the ground, comprising a two-way static switch connected between the external source and a power supply input socket of the aircraft, an impedance connected in parallel to the static switch, means for measuring the voltage at terminals of the socket and a processing unit connected to the means for measuring the voltage and to control terminals of the switch so as to close the switch when the voltage measured drops below a first preset threshold.
Claim 3
Dependent Claim 48 words
The device according to claim 1, comprising means for measuring the current flowing through said device, the processing unit being connected to the means for measuring the current so as to bring about opening of the switch when the current measured is greater than a second preset threshold.
Claim 4
Dependent Claim 41 words
The device according to claim 2, wherein the processing unit comprises means for computing the active power supplied by the device, according to the voltage and current measured, and brings about opening of the switch when said active power is negative.
Claim 5
Dependent Claim 28 words
The device according to claim 3, wherein the processing unit comprises blocking means keeping the switch open for means a preset time delay period after making it open.
Claim 6
Dependent Claim 16 words
The device according to claim 4, wherein the time delay period is lower than 60 ms.
Claim 7
Dependent Claim 14 words
The device according to claim 4, wherein the time delay period is 30 ms.
Claim 8
Dependent Claim 19 words
The device according to claim 1, wherein the switch comprises two head-to-tail thyristors controlled simultaneously by the processing unit.
Claim 9
Dependent Claim 13 words
The device according to claim 1, wherein the impedance about a hundred ohms.
Claim 10
Dependent Claim 52 words
The device according to claim 1, wherein the power supply source is a multiphase power supply, said device comprising a switch and associated impedance per phase, the means for measuring the voltage and current measuring the voltage and current of each of the phases, the processing unit controlling all the switches simultaneously.
Claim 11
Dependent Claim 33 words
The device according to claim 8, wherein the processing unit comprises means for rectifying the voltages measured and means for comparing the output signal of the rectifying means with the first preset threshold.
Claim 12
Dependent Claim 57 words
The device according to claim 8, wherein the processing unit comprises summing means for performing vector summing of the voltages measured on the different phases, and means for comparing the output signal of said summing means with a third preset threshold so as to close the switches when said output signal is lower than said third threshold.

References Cited (Backward Citations)

GB1108964A Cited
GB1108963A Cited
US3390275A Cited
US3601659A Cited
US3761733A Cited
US4937462A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1996-12-20 1997-06-21 1997-12-21 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 2000-12-20 2001-06-21 2001-12-21 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2004-12-20 2005-06-21 2005-12-21 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag