{"@context": "https://schema.org", "@type": "BreadcrumbList", "itemListElement": [{"@type": "ListItem", "position": 1, "name": "Home", "item": "https://www.patentleaderboard.com/"}, {"@type": "ListItem", "position": 2, "name": "Combustor liner for a gas turbine engine and an associated method thereof", "item": "https://www.patentleaderboard.com/patent/10816202"}]}
Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Combustor liner for a gas turbine engine and an associated method thereof

Combustor liner for a gas turbine engine and an associated method thereof

US Patent 10816202 · Granted Oct 27, 2020

Estimated economic value: $9,227,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

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
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
Components for combustor2025
Combustion section with a primary combustor and a set of secondary combustors2025
Combustion section with a primary combustor and a set of secondary combustors2025
Combustion section with a primary combustor and a set of secondary combustors2025
Combustor deflector assembly2025