Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Method of manufacturing seamless self-supporting aerodynamically contoured sheet metal aircraft engine parts using nickel vapor deposition

Method of manufacturing seamless self-supporting aerodynamically contoured sheet metal aircraft engine parts using nickel vapor deposition

US Patent 6463992 · Granted Oct 15, 2002

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Gas turbine auxiliary power unit2021
Gas turbine engine recuperator with floating connection2020
Steel soft wall fan case2019
Method of applying a nanocrystalline coating to a gas turbine engine component2019
Integrally bladed fan rotor2019
Airfoil blade2019
Method and assembly for providing an anti-icing airflow2019
Structural case for aircraft gas turbine engine2019
Gas turbine fuel control system2018
Vane assemblies for gas turbine engines2018
Steel soft wall fan case2018
Cooling system and method for supplying a cooling gas flow2018