IP Library Granted Patent US 7,796,413
Granted Patent B2
US 7,796,413 · App. 12/018,104 · Granted Sep 14, 2010

AC to DC Power converter for aerospace applications

Assignee: ELDEC Corporation
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Quick Facts
Patent No.
US 7,796,413
App. No.
12/018,104
Granted
Sep 14, 2010
Kind
B2
Abstract

Three coils, each having several serial windings, have selected windings connected in a delta. Input AC power is applied through outrigger windings at the delta apices. At least two strategically located, direct tap, natural output points are provided at each side of the delta. For 6-phase output, only the six natural output points are required. For 9-phase output, an additional central output terminal connects to each side of the delta through a stub winding. The 6-phase or 9-phase output is passed to a rectifier circuit.

Claims (19)

1. An autotransformer for converting three-phase AC power to at least six phase AC power comprising:

three coils, each of said coils having at least four serial windings including an outrigger winding and three serial side windings, said coils having their serial windings arranged in a delta with one of said outrigger windings extending from an apex of the delta, whereby each side of the delta has at least three serial windings and each apex of the delta has one of the outrigger windings extending therefrom;

each of the outrigger coils having an end terminal remote from the adjacent apex from which such outrigger coil connects for connection of said terminals to a three-phase AC input; and

at least two direct outputs along each side of the delta, each direct output being a direct tap at a natural point between adjacent side windings with no additional phase correction or stub windings for said direct outputs, whereby at least six equiangularly spaced phases are presented at said direct outputs.

2. An AC to DC power converter for converting 3-phase 230 volt AC input power to 6-phase 270 volt DC output power comprising:

three coils, each of said coils having four serial windings (A 1 , A 2 , A 3 , A 4 ; B 1 , B 2 , B 3 , B 4 ; C 1 , C 2 , C 3 , C 4 ) including an outrigger winding (A 1 ; B 1 ; C 1 ) and three serial side windings (A 2 , A 3 , A 4 ; B 2 , B 3 , B 4 ; C 2 , C 3 , C 4 ), said coils having their serial windings arranged in a delta with one of said outrigger windings extending from an apex of the delta, whereby each side of the delta has three serial windings (A 2 , A 3 , A 4 ; B 2 , B 3 , B 4 ; C 2 , C 3 , C 4 ) and each apex of the delta has one of the outrigger windings (A 1 ; B 1 ; C 1 ) extending therefrom;

each of the outrigger coils having an end terminal (PA; PB; PC) remote from the adjacent apex from which such outrigger coil connects for connection of said terminals to a 3-phase 230 volt input;

two direct outputs ( 02 , 03 ; 04 , 05 ; 06 , 01 ) along each side of the delta, each direct output being a direct tap at a natural point between adjacent side windings with no additional phase correction or stub windings for said direct outputs, whereby six equiangularly spaced phases are presented at said direct outputs; and

a rectifier circuit (R) receiving said six phases for conversion to a 270 volt DC output.

3. The converter of claim 2 , in which the three serial windings of each side of the delta have turns ratios of approximately 0.417:0.370:0.213, as compared to the total number of turns forming a side of the delta.

4. The converter of claim 3 , in which each outrigger winding has a turns ratio of approximately 0.315, as compared to the number of turns of the three serial windings forming a side of the delta.

5. An AC to DC power converter for converting 3-phase 230volt AC input power to 9-phase 270 volt DC output power comprising:

three coils, each of said coils having five serial windings (A 1 , A 2 , A 3 , A 4 , A 5 ; B 1 , B 2 , B 3 , B 4 , B 5 ; C 1 , C 2 , C 3 , C 4 , C 5 ) including an outrigger winding (A 1 ; B 1 ; C 1 ) and four serial side windings (A 2 , A 3 , A 4 , A 5 ; B 2 , B 3 , B 4 , B 5 ; C 2 , C 3 , C 4 , C 5 ), said coils having their serial windings arranged in a delta with one of said outrigger windings extending from an apex of the delta, whereby each side of the delta has four serial windings (A 2 , A 3 , A 4 , A 5 ; B 2 , B 3 , B 4 , B 5 ; C 2 , C 3 , C 4 , C 5 ) and each apex of the delta has one of the outrigger windings (A 1 ; B 1 ; C 1 ) extending therefrom;

each of the outrigger coils having an end terminal (PA; PB; PC) remote from the adjacent apex from which such outrigger coil connects for connection of said terminals to a 3-phase 230 volt input;

two direct outputs ( 02 , 04 ; 05 , 07 ; 08 , 01 ) along each side of the delta, each direct output being a direct tap at a natural point between adjacent side windings, and one additional output ( 03 , 06 , 09 ) connected to the central portion of each side of the delta through a stub winding (A 6 , B 6 , C 6 ), whereby nine equiangularly spaced phases are presented at said outputs; and

a rectifier circuit (R) receiving said nine phases for conversion to a 270 volt DC output.

6. The converter of claim 5 , in which the four serial windings of each side of the delta have turns ratios of approximately 0.257:0.193:0.293:0.257, as compared to the total number of turns forming a side of the delta.

7. The converter of claim 6 , in which each outrigger winding has a turns ratio of approximately 0.313, as compared to the number of turns of the four serial windings forming a side of the delta.

8. The converter of claim 7 , in which each stub winding has a ratio of approximately 0.107, as compared to the total number of turns forming a side of the delta.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 9, 2022
From: ELDEC CORPORATION
To: ELDEC AEROSPACE CORP.
Reel/Frame 058942/0854 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 17, 2008
From: FURMANCZYK, KAZ
To: ELDEC CORPORATION
Reel/Frame 021105/0949 →
Continuity (2)
Provisional Application 6088189700 · Jan 22, 2007
Related Publication 20080278967A1 · Nov 13, 2008