Klammeranordnung

EP2559907 Art B1 14. Januar 2015

Anmelder: Rolls-Royce plc 🇬🇧

Details

Veröffentlichungs-Nr.
EP2559907
Aktenzeichen
EP12179197
Anmeldetag
3. August 2012
Veröffentlichung
14. Januar 2015
Erteilung
14. Januar 2015
Rechtsraum
EP
IPC
F16C35/063
Offizieller Volltext

Abstract

A clamping assembly 1 for clamping a first component in the form of a bearing race 50 to a second component in the form of a shaft 34, which in use is clamped coaxially with the bearing race 50. The clamping assembly 1 comprises a first member in the form of a first ring 42 having a retaining formation in the form of a thread 44 for retaining the first ring to the shaft 34, a second member in the form of a segmented second ring 46, a third member in the form of a third segmented ring 48, a spacer ring 52 and a locking ring. Each of the segments of the second ring and third ring are pivotable or rollable relative to one another. The clamping assembly 1 is arranged such that when in a first, relative position, the overall length of the clamping assembly 1 is such that the third segmented ring 48 is forced against the bearing race 50 to thereby clamp the bearing race and shaft together.

Anmelder

Firma
Rolls-Royce plc
Land
🇬🇧 Großbritannien
🇬🇧 Rolls-Royce

Britisches Unternehmen mit Sitz in Derby, das Flugzeugtriebwerke sowie Antriebssysteme für Luftfahrt, Marine und Energieerzeugung entwickelt und herstellt.

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