About 26 results
https://drivepatents.com/patents/1388833 · 29 Apr 2026
A gas turbine engine (10) including a compressor section (12) and a combustion section (14) in serial flow arrangement along an engine centerline (21), the combustion section having an annular dome wall circumscribing the engine centerline; an annular comb...
https://drivepatents.com/patents/1394558 · 29 Apr 2026
A method of operating an aircraft power plant (112) includes: driving a load (16) onboard an aircraft with a combustion engine (14); heating a solid metal hydride (34) onboard the aircraft to cause hydrogen gas (26) to be released from the solid metal hydr...
https://drivepatents.com/patents/1399301 · 1 Apr 2026
A method and a system for synthesizing output power provided by an engine (10) are provided. The engine (10) comprising a compressor section (14), a combustor (16), and a turbine section (18) in serial fluid flow communication. The engine is operated and, ...
https://drivepatents.com/patents/1399482 · 25 Mar 2026
The gas turbine engine (1) comprises a compressor (2), a combustion system (3) and a turbine (4). The combustion system (3) comprises a heat exchanger (6) for heating compressed air from the compressor (2) to a predefined temperature, a burner (7) for mixi...
https://drivepatents.com/patents/1388202 · 25 Feb 2026
A propulsion system (20) for an aircraft includes a fan (22), a core engine (24) configured for generating a gas flow (36) utilized to generate shaft power for driving the fan (22), a nacelle (48) that surrounds the core engine (24) and the fan (22), a con...
https://drivepatents.com/patents/1388383 · 28 Jan 2026
An anti-icing system (38) for a gas turbine system (10) includes multiple nozzles (40), wherein each nozzle (40) of the multiple nozzles (40) includes one or more outlets (102) that are configured to inject a heated fluid into an airflow (34) within an air...
https://drivepatents.com/patents/1391899 · 19 Nov 2025
A combustor (10) including a liner (11) provided with a combustion chamber at an inner side of which a mixture of fuel and compressed air is combusted, a transition piece (12) connected to an end of the liner, a fluid-flowing sleeve (13) disposed at an out...
https://drivepatents.com/patents/1394017 · 1 Oct 2025
An assembly for an aircraft propulsion system (20) includes an engine core (26), a bypass duct (58) and a bleed circuit (102). The engine core (26) includes a compressor section (48), a combustor section (49), a turbine section (50) and a core flowpath (90...
https://drivepatents.com/patents/1394365 · 27 Aug 2025
A gas turbine engine (20) includes a compressor section (92), a turbine section (28) and an intermediate combustor (56). The compressor section (92) has a plurality of rotating compressor blades (101, 103) rotating about an axis of rotation, and static sta...
https://drivepatents.com/patents/1398323 · 23 Apr 2025
The present disclosure is directed to an annular combustion system. The annular combustion system includes an inner liner and an outer liner that define therebetween an annulus that circumscribes a centerline of the combustion system. The annulus includes ...