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For the Inventor, By the Inventor

Niskayuna, NY, United States of America

Andrew Joseph Wickersham

This inventor holds 17 USPTO granted patents and 7 published patent applications and 2 EPO patents, primarily in Turbine Engine Technology. Top assignee: General Electric Company. Active years: 2020-2026.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Andrew Joseph Wickersham. Retrieved from https://idiyas.com/inventor/andrew-joseph-wickersham

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

Calculating rank
USPTO Granted Patents = 17 

% Patents Active = 94.1

 

Average Co-Inventor Count = 5.1

ph-index = 3

Forward Citations = 29(Granted Patents)


Location History:

  • Niskayuna, NY (US) (2020 - 2022)
  • Liberty Township, OH (US) (2022 - 2024)

Company Filing History:

goldMedal17 out of 52,404 
 
General Electric Company
 patents

Years Active: 2020-2026

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Areas of Expertise:
Dual Fuel Combustor
Turbine Engine
Combustion Section
Fuel Nozzle
Gas Turbine
Integrated Fuel Cell
Flame Speed Control
Diffuser
Swirl-Cup Combustors
Fuel Staging
Damper
Aircraft Engines
17 patents (USPTO):Explore Patents
1. 12747863 - Dual fuel combustor for a turbine engine (2026-09-29),
2. 12716586 - Turbine engine having a combustion section with a fuel nozzle having a gaseous fuel supply channel (2026-08-25),
3. 12613036 - Turbine engine having a combustion section with a fuel nozzle (2026-04-28),
4. 12571539 - Turbine engine having a combustion section with a fuel nozzle (2026-03-10),
5. 12448918 - Diffuser with passlets (2025-10-21),
6. 12410746 - Gas turbine and fuel nozzle assembly for mixing hydrogen fuel and steam to control flame speed (2025-09-09),
7. 12374696 - Integrated fuel cell and combustion system (2025-07-29),
8. 12339006 - Turbine engine having a combustion section with a fuel nozzle assembly (2025-06-24),
9. 11923586 - Gas turbine combustion section having an integrated fuel cell assembly (2024-03-05),
10. 11859820 - Gas turbine combustion section having an integrated fuel cell assembly (2024-01-02),
11. 11753179 - Aircraft engines with a fuel cell (2023-09-12),
12. 11686474 - Damper for swirl-cup combustors (2023-06-27),
13. 11486262 - Diffuser bleed assembly (2022-11-01),
14. 11239470 - Integrated fuel cell and combustion system (2022-02-01),
15. 11236908 - Fuel staging for rotating detonation combustor (2022-02-01),

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Profile summary based on public USPTO records.
Data Sources: USPTO Patent Grant XML, Patent Center, EPO & CIPO • Normalized by IDiyas Innovation Graph. Methodology & provenance architecturePlease report any incorrect information to [email protected]
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