Generator mit Torsionsdämpfer

EP4027499 Art A3 14. September 2022

Anmelder: Hamilton Sundstrand Corporation 🇺🇸

Details

Veröffentlichungs-Nr.
EP4027499
Aktenzeichen
EP21215183
Anmeldetag
16. Dezember 2021
Veröffentlichung
14. September 2022
Rechtsraum
EP
IPC
H02K7/10F16F15/16
Offizieller Volltext

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
🇺🇸 Hamilton Sundstrand

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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