AIRCRAFT AND DIRECT DRIVE ENGINE UNDER WING INSTALLATION
AIRCRAFT AND DIRECT DRIVE ENGINE UNDER WING INSTALLATION
- New search for: MONIZ THOMAS ORY
- New search for: VONDRELL RANDY M
- New search for: CLEMENTS JEFFREY DONALD
- New search for: MILLER BRANDON WAYNE
- New search for: MONIZ THOMAS ORY
- New search for: VONDRELL RANDY M
- New search for: CLEMENTS JEFFREY DONALD
- New search for: MILLER BRANDON WAYNE
The present disclosure is directed to a gas turbine engine defining a radial direction, a longitudinal direction, and a circumferential direction, an upstream end and a downstream end along the longitudinal direction, and an axial centerline extended along the longitudinal direction. The gas turbine engine includes a fan assembly including a plurality of fan blades rotatably coupled to a fan rotor in which the fan blades define a maximum fan diameter and a fan pressure ratio. The gas turbine engine further includes a low pressure (LP) turbine defining a core flowpath therethrough generally along the longitudinal direction. The core flowpath defines a maximum outer flowpath diameter relative to the axial centerline. The gas turbine engine defines a fan to turbine diameter ratio of the maximum fan diameter to the maximum outer flowpath diameter. The fan to turbine diameter ratio over the fan pressure ratio is approximately 0.90 or greater.
Document information
AIRCRAFT AND DIRECT DRIVE ENGINE UNDER WING INSTALLATION
2022-12-22
Patent
Electronic Resource
English
| IPC: | F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS |
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