IP Library Granted Patent US 8,847,560
Granted Patent B2
US 8,847,560 · App. 13/884,795 · Granted Sep 30, 2014

Aircraft power supply circuit including an asynchronous machine

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Quick Facts
Patent No.
US 8,847,560
App. No.
13/884,795
Granted
Sep 30, 2014
Kind
B2
Abstract

A power supply circuit for supplying electrical energy in an aircraft, the circuit including a power supply generator configured to be driven in rotation by the engine of the aircraft to power electrical equipment of the aircraft engine. The power supply generator includes an asynchronous machine connected to an excitation device. The asynchronous machine includes a rotor configured to be driven in rotation by the engine and a stator connected to the electrical equipment. The excitation device is configured to cause a reactive current of flow in the stator.

Claims (32)

1. A power supply circuit for supplying electrical energy in an aircraft, the circuit comprising:

a power supply generator configured to be driven in rotation by an engine of the aircraft to power electrical equipment of the aircraft engine, the power supply generator comprising an asynchronous machine connected to an excitation device;

the asynchronous machine including a rotor configured to be driven in rotation by the engine and a stator connected to the electrical equipment; and

the excitation device is configured to cause a reactive current of flow in the stator;

wherein the excitation device includes one or more capacitors; and

the asynchronous machine presents magnetization inductance Lm expressed by relationship:

L

m

=

L

0

I

μ

2

α

I

μ

2

α

+

I

m

α

in which L 0 is magnetization induction at zero current, I μ2 is magnetization current that decreases the magnetization inductance L m by a factor of 2, I m is magnetization current, and α is a coefficient that depends on characteristics of the asynchronous machine, wherein α is less than 2.5.

2. A power supply circuit according to claim 1 , further comprising a second excitation device connected to the asynchronous machine.

3. An aeroengine comprising a power supply circuit according to claim 1 .

4. An aeroengine comprising a power supply circuit according to claim 2 .

Assignments (3)
CHANGE OF NAME Recorded Apr 22, 2018
From: LABINAL POWER SYSTEMS
To: SAFRAN ELECTRICAL & POWER
Reel/Frame 046678/0487 →
TRANSFER OF PATENT RIGHTS Recorded May 12, 2015
From: HISPANO SUIZA
To: LABINAL POWER SYSTEMS
Reel/Frame 035654/0789 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 30, 2014
From: DE WERGIFOSSE, ERIC
To: HISPANO-SUIZA
Reel/Frame 032086/0677 →