Rotor mit Sicherung
Anmelder: Hamilton Sundstrand Corporation 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP4311911
- Aktenzeichen
- EP23186147
- Anmeldetag
- 18. Juli 2023
- Veröffentlichung
- 31. Januar 2024
- Rechtsraum
- EP
- IPC
- F01D5/04
Abstract
A rotor includes a base member (64) including a first side (66), a second side (68) opposite the first side, and a central opening (70) passing through the first side and the second side. The second side includes an outer circumferential edge (74) having a first dimension and the central opening having an inner circumferential edge (72) having a second dimension. A plurality of blades (80) extend outwardly from the first side. The plurality of blades extend about the central opening. A fuse element (86, 102, 112, 154, 170) is formed in the second side and extends along one of a radial direction and a circumferential direction. The fuse element has a length that is less than the first dimension.
Anmelder
- Firma
- Hamilton Sundstrand Corporation
- Land
- 🇺🇸 USA
US-amerikanisches Unternehmen der Luft- und Raumfahrtindustrie, das Flugzeugsysteme wie Umweltkontroll-, Energie- und Antriebssysteme entwickelt; heute Teil von Collins Aerospace innerhalb von RTX.
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