About 43 results
https://drivepatents.com/patents/1395153 · 29 Apr 2026
A method is provided during which a preform is provided that includes an electric heater (44) and thermoplastic material. The preform is consolidated to provide an aircraft component (22). The consolidating includes heating the thermoplastic material using...
https://drivepatents.com/patents/1395151 · 22 Apr 2026
A method is provided during which a composite preform is provided that includes an electric heater (44), fiber-reinforcement and thermoset material. The composite preform is consolidated to provide a composite aircraft component (22). The consolidating inc...
https://drivepatents.com/patents/1387810 · 22 Apr 2026
An assembly (54) for an aircraft propulsion system (20) includes a nacelle inlet structure (34) extending axially along and circumferentially about an axis. The nacelle inlet structure (34) includes an inlet lip skin (58), an inner barrel (60), an outer ba...
https://drivepatents.com/patents/1394152 · 15 Apr 2026
An apparatus (20) is provided for an aircraft propulsion system (22). This apparatus (20) includes a thrust reverser cascade (64) extending longitudinally between a cascade forward end (68) and a cascade aft end (70). The thrust reverser cascade (64) exten...
https://drivepatents.com/patents/1399971 · 15 Apr 2026
A hook body (330) for a latch mechanism includes a plurality of longitudinal members (331, 333), each of the plurality of longitudinal members extending in a longitudinal direction with respect to the hook body (330); and a load slot (340) at a proximal en...
https://drivepatents.com/patents/1399821 · 11 Mar 2026
An articulating exhaust nozzle thrust reverser includes an outer articulating panel (210) comprising an outer skin (212) and an outer thrust reverser door (214) and an inner articulating panel (220) comprising a forward inner skin (222), an aft inner skin ...
https://drivepatents.com/patents/1391152 · 25 Feb 2026
An air inlet section (40) for an aircraft propulsion system nacelle (24) includes an outer skin (48), an inner skin (50), and a lip skin (54). The lip skin (54) extends between and to an outer end (70) and an inner end (72). The outer end (70) is disposed ...
https://drivepatents.com/patents/1391153 · 25 Feb 2026
An air inlet (40) for an aircraft propulsion system nacelle (24) includes an outer skin (44), an inner skin (46), a lip skin (48), and a forward bulkhead (50). The lip skin (48) extends between and to an outer end (62) and an inner end (64). The outer end ...
https://drivepatents.com/patents/1398689 · 17 Dec 2025
A variable area nozzle assembly (36) includes a fixed structure (38) surrounding an exhaust duct (40) extending along a nozzle (44) axis. The fixed structure (38) defines an exhaust duct outlet (46) of the exhaust duct (40). The fixed structure (38) includ...
https://drivepatents.com/patents/1391173 · 3 Dec 2025
An assembly for an aircraft includes a variable area inlet (62, 78) for an aircraft propulsion system (22). The variable area inlet (62, 78) extends along a longitudinal centerline (34, 90). The variable area inlet (62, 78) includes an inlet structure (80)...