Generator mit Torsionsdämpfer
Anmelder: Hamilton Sundstrand Corporation 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP4027499
- Aktenzeichen
- EP21215183
- Anmeldetag
- 16. Dezember 2021
- Veröffentlichung
- 14. September 2022
- Rechtsraum
- EP
- IPC
- H02K7/10F16F15/16
Abstract
A rotor assembly (12) of an electric machine (10) includes a rotor body (16) and a shaft assembly (18) positioned at a central axis of the rotor assembly, and operably connected thereto. The shaft assembly includes a main rotor shaft (32) operably connected to the rotor body, a center drive shaft (34) located inside of the main rotor shaft, and a hydraulic damper sleeve (46) located radially between the main rotor shaft and the center drive shaft. The hydraulic damper sleeve defines a plurality of cavities (52) between the hydraulic damper sleeve and the center drive shaft. The hydraulic damper sleeve is configured to urge a fluid into and out of the plurality of cavities thereby damping relative circumferential motion between the main rotor shaft and the center drive shaft. A plurality of flow restrictors are configured to easily allow fluid into the plurality of cavities, while restricting flow of fluid out of the plurality of cavities.
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.
4.459 Patente in unserer Datenbank