IP Library Granted Patent US 10,483,848
Granted Patent B2
US 10,483,848 · App. 15/662,128 · Granted Nov 19, 2019

Assembly for controlling solid-state switching elements in an aircraft

Inventor: Loïc Aoustin (Montreuil, FR)
Assignee: ZODIAC AERO ELECTRIC
H02M3/156H02J4/00
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Quick Facts
Patent No.
US 10,483,848
App. No.
15/662,128
Granted
Nov 19, 2019
Kind
B2
Abstract

Disclosed herein is an assembly for controlling solid-state switching elements in an aircraft having at least one power pathway comprising at least one power line supplying power to at least one item of equipment on board an aircraft from at least one electrical power source via a power switch, and at least one control member controlling at least one power switch according to control signals arising from a control means. The control assembly comprises a single power supply supplying power to the control members.

Claims (14)

1. An assembly for controlling solid-state switching elements in an aircraft having at least one power pathway comprising at least one power line supplying power to at least one item of equipment on board an aircraft from at least one electrical power source via a power switch,

at least one control member controlling at least one power switch according to control signals arising from a control means,

wherein the control assembly comprises a single power supply supplying power to all of the control members, the single power supply being electrically isolated with respect to the control means,

wherein the assembly comprises at least one analogue level offset means positioned between the control means and a control member, and

the analogue level offset means being capable of maintaining the amplitude of the control signal transmitted by the control means while changing the reference potential of the control signal from the reference potential of the control means to the reference potential of the control member and of the isolated power supply.

2. The assembly of claim 1 , in which the control member comprises a Darlington transistor capable of switching the power switch to an off position when no command is received from the control means.

3. The assembly of claim 1 , in which the control member comprises a first transistor, the base of which is connected to a first input, the collector of the first transistor being connected to the power switch, a first resistor and a second resistor being connected in parallel by one of their terminals to the emitter of the first transistor, the first resistor being connected by its other terminal to the collector of a second transistor, the emitter of the second transistor being connected to ground and to the other terminal of the second resistor, the base of the second transistor being connected to the second input,

the control member being capable of controlling the power switch in analogue or digital according to the control signals received at input.

4. The assembly of claim 1 , in which at least one means, which is electrically isolated, for measuring the current flowing through the power pathway is connected both to the control means and to at least one power line.

5. The assembly of claim 1 , in which at least one means, which is not electrically isolated, for measuring the current flowing through the power pathway is connected both to the control means and to at least one power line.

6. The assembly of claim 1 , in which the offset means comprises a first transistor and a second transistor,

the first transistor being connected by its emitter to the reference potential of a control means, its collector being connected to the isolated power supply, its base being connected to the control terminal of the control means,

the second transistor being connected by its base to the drain of the first transistor, by its emitter to the isolated power supply and by its collector to the power switch.

7. A circuit board comprising at least one assembly of claim 1 .

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 29, 2021
From: SAFRAN ELECTRONICS & DEFENSE COCKPIT SOLUTIONS
To: SAFRAN ELECTRICAL & POWER
Reel/Frame 055074/0024 →
CHANGE OF NAME Recorded Jan 29, 2021
From: ZODIAC AERO ELECTRIC
To: SAFRAN ELECTRONICS & DEFENSE COCKPIT SOLUTIONS
Reel/Frame 055177/0037 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 4, 2017
From: AOUSTIN, LOÏC
To: ZODIAC AERO ELECTRIC
Reel/Frame 044134/0751 →
Priority Claims (1)
FR 16 57239 · Jul 27, 2016 · national
Continuity (1)
Related Publication 20180034366A1 · Feb 1, 2018