About 13 results
https://drivepatents.com/patents/1392388 · 11 Mar 2026
A combustion section (114) defines an axial direction, a radial direction, and a circumferential direction. The combustion section (114) includes a casing (400) that defines a diffusion chamber (406). A combustion liner (402) is disposed within the diffusi...
https://drivepatents.com/patents/1398701 · 11 Mar 2026
A method for operating a gas turbine assembly for a power plant comprises the steps of:- providing a gas turbine assembly (1) comprising a compressor (2), a combustor assembly (4), a turbine (5) and an generator; the compressor (2), the turbine (5) and the...
https://drivepatents.com/patents/1391537 · 18 Feb 2026
A gas turbine engine includes an annular combustion chamber (7) and a plurality of combustors (6) communicating with the annular combustion chamber (7). Each combustor (6) defines a respective gas flow path (20) along a respective combustor axis (C) and ha...
https://drivepatents.com/patents/1398702 · 18 Feb 2026
A gas turbine engine includes a combustor assembly (5) having a plurality of can combustor units (8) and a control unit (20). Each combustor unit (8) has a first-stage combustor (12), a second-stage combustor (13) and a mixer (15), arranged between the fir...
https://drivepatents.com/patents/1392364 · 26 Nov 2025
A combustion section (114) defines an axial direction, a radial direction, and a circumferential direction. The combustion section (114) includes a casing (400) that defines a diffusion chamber (406). A combustion liner (402) is disposed within the diffusi...
https://drivepatents.com/patents/1398374 · 8 Oct 2025
An aircraft propulsion system includes a fan shaft (410) connected to a fan (406) and defining a centerline axis (404) of the aircraft propulsion system (400), one or more offset cores (402) arranged at an angle to the centerline axis (404), the one or mor...
https://drivepatents.com/patents/1400159 · 26 Jun 2024
A combustor arrangement (100) includes a fuel injector (114), and a seal (200, 1300) arranged around the fuel injector (114) and having an upstream end (202, 1302) and a downstream end (204, 1304). The seal (200, 1300) includes an annular body (206, 1306) ...
https://drivepatents.com/patents/967514 · 12 Nov 2014
This burner comprises a burner outer cylinder, a cylindrical burner inner cylinder provided inside the burner outer cylinder, a compressed air flow channel demarcated between the burner outer cylinder and the burner inner cylinder, and a plurality of fuel ...
https://drivepatents.com/patents/979655 · 15 Jan 2014
The invention concerns a gas turbine system, comprising a compressor, at least one combustion chamber (10), and eventually a secondary combustion chamber, for generating working gas. An intermediate turbine may be placed between two combustion chambers. Th...
https://drivepatents.com/patents/985548 · 20 Mar 2013
A system for conditioning a working fluid in a combustor includes a primary combustion chamber (20), a liner (18) circumferentially surrounding the primary combustion chamber (20), and a primary nozzle (12) in fluid communication with the primary combustio...