Dc voltage filter for an input of an inverter of an electric machine for propelling an aircraft

Patent metadata

Field	Value
Publication number	US-2025033489-A1
Application number	US-202218686073-A
Country	US
Kind code	A1
Filing date	Aug 21, 2022
Priority date	Aug 31, 2021
Publication date	Jan 30, 2025
Grant date	—

Abstract

A filter includes a positive busbar and a negative busbar that have a positive terminal and a negative terminal, respectively; at least one positive output terminal and at least one negative output terminal, respectively; and two portions, respectively, each portion having parallel folds to define planes which succeed one another. Each plane is inclined relative to the next plane. One of the portions is an internal portion that is fitted inside the other portion, which is an external portion. Each plane of one portion extends in parallel with and facing an associated plane of the other portion. Differential mode capacitors connected between the two portions.

First claim

1 . A filter of DC voltage (U) for an inverter input of an electric machine for propelling an aircraft, comprising:
a positive busbar and a negative busbar; and differential mode capacitors (Cdm) connected between two respective portions of the positive busbar and the negative busbar; wherein each of the two portions each have parallel folds so as to define at least three planes following one another and inclined with respect to one another, one of the two portions referred being an internal portion and the other of the two portions being an external portion, the internal portion being nested in the external portion so that each plane of one of the two portions extends parallel opposite an associated plane of the other of the two portions.

2 . The filter of claim 1 , wherein more differential mode capacitors (Cdm) are connected between central pair or pairs of planes than between two peripheral pairs of planes.

3 . The filter according to claim 1 , wherein the differential mode capacitors (Cdm) are arranged on an external face of the external portion and/or on an internal face of the internal portion.

4 . A voltage converter comprising:
at least one power module performing an inverter function; and the filter according to claim 1 , each power module being connected to a respective pair of positive and negative output terminals.

5 . An electric drive comprising:
the voltage converter according to claim 4 ; an electric motor; an output shaft secured to a rotor of the electric motor, the filter being an input filter arranged around the output shaft so that the portions of the busbars surround the output shaft.

6 . The electric drive according to claim 5 , further comprising a plurality of voltage converters distributed around the output shaft.

7 . The electric drive according to claim 6 , further comprising a casing surrounding the output shaft and having a plurality of internal or external planar faces in succession around the output shaft, the input filter being pressed against the planar faces of the casing so that each plane of a lower portion of the casing extends parallel opposite an associated planar face of the casing.

8 . An aircraft comprising the electric drive according to claim 5 .

Assignees

• Safran Electrical & Power

Inventors

• Nehme Samir
• Dhokkar Sonia
• Goncalves Rémi
• M'Fumu Ambil Raïs
• Souahlia Rachid
• Dievart Jean-Laurent
• Thiam Abdoulahad

Classifications

• H02M1/14 Primary

  Arrangements for reducing ripples from DC input or output · CPC title

• B60L2210/42

  Voltage source inverters · CPC title

• B60L2200/10

  Air crafts · CPC title

• H05K7/14329

  specially adapted for the configuration of power bus bars · CPC title

• H02M7/003

  Constructional details, e.g. physical layout, assembly, wiring or busbar connections · CPC title