Log in
Sign up
Golden has been acquired by ComplyAdvantage.Read about it here ⟶
‌

US Patent 11913353 Airfoil tip arrangement for gas turbine engine

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
0
Date Filed
August 5, 2022
0
Date of Patent
February 27, 2024
0
Patent Applicant
Raytheon Technologies
Raytheon Technologies
0
Patent Application Number
17881803
0
Patent Citations
‌
US Patent 7413403 Turbine blade tip cooling
0
‌
US Patent 7597539 Turbine blade with vortex cooled end tip rail
0
‌
US Patent 7625178 High effectiveness cooled turbine blade
0
‌
US Patent 7857587 Turbine blades and turbine blade cooling systems and methods
0
‌
US Patent 7972115 Moving blade for a turbomachine
0
‌
US Patent 8011889 Turbine blade with trailing edge tip corner cooling
0
‌
US Patent 8092179 Blade tip cooling groove
0
‌
US Patent 9470096 Turbine bucket with notched squealer tip
0
‌
US Patent 9605545 Gas turbine blade with tip sections offset towards the pressure side and with cooling channels
0
‌
US Patent 9890644 Foundry core assembly for manufacturing a turbomachine blade, associated method of manufacturing a blade and associated blade
0
•••
Patent Inventor Names
Jeremy B. Fredette
0
Emma J. Place
0
Dominic J. Mongillo
0
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
0
Patent Number
11913353
0
Patent Primary Examiner
‌
Eldon T Brockman
0
CPC Code
‌
F01D 5/20
0
‌
F05D 2260/202
0
‌
F01D 5/186
0
‌
F01D 5/141
0
‌
F05D 2240/30
0

Find more entities like US Patent 11913353 Airfoil tip arrangement for gas turbine engine

Use the Golden Query Tool to find similar entities by any field in the Knowledge Graph, including industry, location, and more.
Open Query Tool
Access by API
Golden Query Tool
Golden logo
By using this site, you agree to our Terms of Service.