Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Liner of a gas turbine engine combustor including dilution holes with airflow features

Liner of a gas turbine engine combustor including dilution holes with airflow features

US Patent 10890327 · Granted Jan 12, 2021

Estimated economic value: $71,417,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Granular tracking of locking queries to reduce locking2025
Cowl damper for combustor2025
Cowl damper for combustor2025
Gas turbine engine fuel nozzle having a secondary fuel passage through a swirler2025
Gas turbine engine fuel nozzle having a secondary fuel passage through a swirler2025
Gas turbine engine fuel nozzle having a secondary fuel passage through a swirler2025
Combustor for a gas turbine engine2025
Combustor having a main chamber and one or more trapped vortex cavities2025
Combustor having a main chamber and one or more trapped vortex cavities2025
Combustor having a main chamber and one or more trapped vortex cavities2025
Diffuser with passlets2025
Gas turbine engine combustor with a set of dilution passages2025