A nosecone assembly (40) having an axially extending centerline (58) is provided. The assembly (40) includes a nosecone body (42) and at least one access panel (44). The nosecone body (42) has at least one wall (52) that defines an interior cavity (50). The wall (52) has an interior surface (60) contiguous with the interior cavity (50), and at least one window aperture (66) extending through the wall (52). The access panel (44) has first and second face surfaces. The access panel (44) is attached to the wall interior surface (60) within an attachment region that includes first and second attachment region portions partially contiguous with one another. The first and second attachment region portions define an interior unattached region, and the interior unattached region is aligned with the window aperture (66).
GAS TURBINE ENGINE NOSE CONE ASSEMBLY
BUGKONUSANORDNUNG EINES GASTURBINENMOTORS
ENSEMBLE DE POINTE AVANT DE MOTEUR À TURBINE À GAZ
2021-05-19
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge / 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 |