IP Library Granted Patent US 11,887,766
Granted Patent B2
US 11,887,766 · App. 17/001,171 · Granted Jan 30, 2024

Magnetic component and method of forming

Inventors: Ramanujam Ramabhadran (Jericho, NY); Ruxi Wang (Cohoes, NY); Juan Manuel Rivas Davila (Palo Alto, CA); Jiale Xu (Sunnyvale, CA)
Assignee: GE Aviation Systems LLC
H01F27/08B23K1/0016B33Y80/00H01F27/245H01F41/0233H05K1/181H05K3/341B23K2101/42B23K2103/02B33Y10/00H05K2201/1003
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 11,887,766
App. No.
17/001,171
Granted
Jan 30, 2024
Kind
B2
Abstract

A component includes a magnetic core having a body formed of a first material, defining a first opening and a second opening thereon. A duct formed of a second material extends at least partially through the body between the first opening and the second opening. The first opening and the second opening are in fluid communication by way of the duct.

Claims (16)

1. A method of forming a component having a body, comprising:

printing the body via a layer-by-layer process, except for the final layer of the body, including heating each printed layer;

for the final layer of the body, depositing the final layer of the body without applying heat to the deposited final layer;

coupling the body to a PCB;

applying a solder material to the PCB; and

coupling the component to the PCB via a reflow soldering process.

2. The method of claim 1 , wherein the heating comprises sintering each printed layer of the body except the last printed layer of the body.

3. The method of claim 1 , wherein the printing the body includes printing a magnetic core having a first opening and a second opening defined thereon; and

printing a duct extending at least partially through the magnetic core between the first opening and the second opening, the first opening and the second opening being in fluid communication by way of the duct.

4. The method of claim 3 , wherein the printing the body includes printing the magnetic core with a first material, and printing the duct with a second material.

5. The method of claim 4 , wherein the first material is a ferritic material.

6. The method of claim 4 , wherein the second material is a thermally conductive and electrically insulative material.

7. The method of claim 1 , additionally comprising printing a set of windings arranged around a portion of the body.

8. The method of claim 7 , wherein printing the set of windings includes printing the windings with a conductive third material.

9. The method of claim 1 , wherein, for the final layer of the body, the depositing the final layer of the body without applying heat further comprises omitting a sintering step to sinter the deposited final layer of the body.

10. The method of claim 1 , wherein, for the final layer of the body, the depositing the final layer of the body without applying heat further comprises leaving the deposited layer as an unbound powder layer.

Assignments (2)
CONFIRMATORY LICENSE Recorded Mar 15, 2021
From: GENERAL ELECTRIC GLOBAL RESEARCH
To: UNITED STATES DEPARTMENT OF ENERGY
Reel/Frame 055587/0729 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 24, 2020
From: RAMABHADRAN, RAMANUJAM; WANG, RUXI; RIVAS DAVILA, JUAN MANUEL; XU, JIALE
To: GE AVIATION SYSTEMS LLC
Reel/Frame 053578/0271 →
Continuity (1)
Related Publication 20220059272A1 · Feb 24, 2022