Granted Patent B2

US 12,567,523 · App. 18/341,222 · Granted Mar 3, 2026

Inventors: Gerhard Steiner (Taufkirchen, DE); Florian Kapaun (Taufkirchen, DE); Ludovic Ybanez (Blagnac, FR); Ravi Kiran Surapaneni (Blagnac, FR); Gowtham Galla (Blagnac, FR)

Assignee: Airbus SAS

H01F6/06H01F5/06H01F41/048

Abstract

Claims (12)

1 . An inductive component comprising:

an inductive element comprising a stack of an outer plurality of first strips of magnetic material, a central plurality of second strips of superconducting material, and an outer plurality of third strips of magnetic material, the inductive element being flexible and configured to form at least one loop of said stack of first strips, second strips, and third strips, wound on itself.

2 . The inductive component according to claim 1 , wherein each first and third strip of magnetic material is surrounded by an electrically insulating and thermally conductive layer.

3 . The inductive component according to claim 1 , comprising a magnetic element, the inductive element being wound on said magnetic element.

4 . An inductive device comprising:

the inductive component according to claim 1 arranged in a cryogenic fluid volume.

5 . The inductive device according to claim 4 , wherein the inductive device is configured to operate a connection between a power converter device and a powertrain.

6 . An inductive device comprising:

the inductive component according to claim 1 held in contact with a cold source comprising a cryogenic fluid.

7 . The inductive device according to claim 6 , wherein the inductive device is configured to operate a connection between a power converter device and a powertrain.

8 . An aircraft comprising the inductive component according to claim 1 .

9 . An aircraft comprising the inductive device according to claim 4 .

Assignments (1)

Priority Claims (1)

Continuity (1)

References Cited (11)