About 108 results
https://drivepatents.com/patents/1395566 · 11 Mar 2026
A propulsion system for an aircraft including a gas generating core engine (70) that generates an exhaust gas flow (52) that is expanded through a turbine section (32). A power turbine (38) engine is forward of the core engine (70). A propulsor (22) is cou...
https://drivepatents.com/patents/1395943 · 11 Mar 2026
A face sheet (110A) of an acoustic liner (110) for a gas turbine engine (20), having: a first surface (120), a second surface (140), and a sheet body (130) extending from the first surface (120) to the second surface (140); a forward end (150), an aft end ...
https://drivepatents.com/patents/1397488 · 11 Mar 2026
An assembly (60; 160; 560; 660) for a gas turbine engine (20) according to an aspect of the present disclosure includes, among other things, a gas turbine engine component (66; 166; 566) that has a first interface portion (74; 174), and a support (68; 168)...
https://drivepatents.com/patents/1393620 · 4 Mar 2026
An assembly (20) for an aerial vehicle includes a vehicle body (24), a gas turbine engine (22) and a support structure (26). The vehicle body (24) includes a body section (111). The gas turbine engine (22) includes a stationary structure (66). The gas turb...
https://drivepatents.com/patents/1394664 · 4 Mar 2026
An aircraft engine system includes a core assembly having at least a burner section and a fuel cell (344) configured to generate electrical power. A cryogenic fuel source (324) is configured to supply a fuel through a fuel supply line (326) to each of the ...
https://drivepatents.com/patents/1396307 · 4 Mar 2026
An assembly (200) of a gas turbine engine (20) includes a low pressure compressor (44), a high pressure compressor (52), an intermediate case (45) between the low pressure compressor (44) and the high pressure compressor (52), and a cleaning apparatus (70)...
https://drivepatents.com/patents/1392213 · 25 Feb 2026
A gas turbine engine (100) includes a fan shaft (110) rotatable about an axis (A), a fan (112) connected to the fan shaft (110), and an outer housing (114) surrounding the fan (112) to define a bypass passage (B). A compressor section (24) has both a low p...
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/1393417 · 18 Feb 2026
A gas turbine engine assembly includes a core engine (20) that includes a core flow path where a core airflow (25) is compressed in a compressor section (24), communicated to a combustor section (56), mixed with fuel and ignited to generate an exhaust gas ...
https://drivepatents.com/patents/1400442 · 18 Feb 2026
A gas turbine engine (20) including a core having a compressor section (24) fluidly connected to a combustor (56) via a primary flowpath and a turbine section (28) connected to the combustor (56) via the core flow path (C). An assembly is disposed within t...