Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Rotor tip clearance control apparatus for a gas turbine engine

Rotor tip clearance control apparatus for a gas turbine engine

US Patent 4330234 · Granted May 18, 1982

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Fluid propulsion engine with flow exit control device1988
Combustion equipment for a gas turbine engine including a fuel burner capable of1984
Constant speed drive1982