IP Library › Granted Patent US 12,592,350
Granted Patent B2
US 12,592,350 · App. 18/470,019 · Granted Mar 31, 2026

Power fuse and aircraft comprising such a power fuse

Inventors: Ludovic Ybanez (Blagnac, FR); Ravi Kiran Surapaneni (Blagnac, FR); Gowtham Galla (Blagnac, FR)
Assignee: Airbus SAS
H01H33/666H01F6/04H01H85/055
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Quick Facts
Patent No.
US 12,592,350
App. No.
18/470,019
Granted
Mar 31, 2026
Kind
B2
Abstract

A cryogenic fuse comprising a superconducting element arranged in a first chamber, the first chamber containing a cryogenic fluid, the cryogenic fuse being such that the superconducting element comprises a breaker initiation zone configured to determine a melting current and the first chamber is surrounded by a second chamber, placed under vacuum. The melting current or a melting time of the breakdown initiation zone may be adjusted.

Claims (18)

1 . An aircraft comprising:

a cryogenic fuse comprising:

a superconducting element arranged in a first chamber, the first chamber containing a cryogenic fluid,

wherein said superconducting element includes a breakdown initiation zone configured to determine a melting current,

wherein said first chamber is surrounded by a second chamber, placed under vacuum, and,

wherein said cryogenic fuse further comprises an additional module for adjusting said melting current or for adjusting a melting time of said breakdown initiation zone.

2 . The aircraft according to claim 1 , wherein said breakdown initiation zone comprises impurities inserted in said superconducting element.

3 . The aircraft according to claim 2 , wherein said impurities comprise aluminum or copper fragments.

4 . The aircraft according to claim 1 , wherein said breakdown initiation zone has a local reduction in a cross-sectional area of the superconducting element.

5 . The aircraft according to claim 1 , wherein said breakdown initiation zone has at least one bend in said superconducting element.

6 . The aircraft according to claim 1 , wherein the superconducting element is in a form of a strip or a tape.

7 . The aircraft according claim 1 ,

wherein the first chamber comprises at least one inlet opening for said cryogenic fluid.

8 . The aircraft according to claim 1 , wherein said additional module for controlling said melting current is configured to control a temperature of said cryogenic fluid.

9 . The aircraft according to claim 1 , wherein said additional module for controlling said melting current is a controlled electromagnetic field source.

10 . The aircraft according to claim 1 , further comprising:

a power transmission cable comprising:

the cryogenic fuse.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 30, 2024
From: YBANEZ, LUDOVIC; SURAPANENI, RAVI KIRAN; GALLA, GOWTHAM
To: AIRBUS SAS
Reel/Frame 067270/0827 →
Priority Claims (1)
EP 22306380 · Sep 21, 2022 · regional
Continuity (1)
Related Publication 20240096574A1 · Mar 21, 2024
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