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EP4667709 Art A1 24. Dezember 2025

Anmelder: PRATT & WHITNEY CANADA CORP. 🇨🇦

Details

Veröffentlichungs-Nr.
EP4667709
Aktenzeichen
EP25184002
Anmeldetag
19. Juni 2025
Veröffentlichung
24. Dezember 2025
Rechtsraum
EP
IPC
F01D21/04F01D25/16
Offizieller Volltext

Abstract

A bearing arrangement (60) of a gas turbine engine includes a first bearing (26) supportive of a shaft, and a second bearing (28) axially offset from the first bearing (26). A first bearing support (62) extends from a bearing housing (64) to the first bearing (26), and a second bearing support (66) extends from a bearing housing (64) to the second bearing (28). One or more radial bearing supports (72) including a plurality of radial spokes (76) extend between the bearing housing (64) and the second bearing (28). The spokes (76) are configured to buckle under compression when radial loads at the second bearing (28) exceed a predetermined force threshold. An axially-extending spoke foot (80) extends from at least one radial spoke (76). The axially-extending spoke foot (80) is configured to contact the second bearing (28) in the event of a tilt of the second bearing (28) beyond a predetermined angle threshold, reducing the buckling force of the plurality of radial spokes (76) below a second predetermined force threshold.

Anmelder

Firma
PRATT & WHITNEY CANADA CORP.
Land
🇨🇦 Kanada
🇨🇦 Pratt & Whitney Canada

Kanadische Tochtergesellschaft von Pratt & Whitney mit Sitz in Longueuil, Québec. Entwickelt und fertigt Flugzeugtriebwerke für kleinere Verkehrsflugzeuge, Geschäftsflugzeuge und Hubschrauber.

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