The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Dec. 22, 1981

Filed:

Mar. 31, 1980
Applicant:
Inventor:

Derek A Roberts, Bristol, GB;

Assignee:

Rolls-Royce Limited, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16C / ; F16C / ; F16C / ;
U.S. Cl.
CPC ...
3081 / ; 308188 ; 308191 ; 3082 / ;
Abstract

A rotor assembly, particularly for a gas turbine engine, comprising a torsionally stiff drive shaft 16 mounted at two spaced locations in first and second bearings 22,23 which are substantially immovable bodily in radial directions. The drive shaft 16 has a flexible end portion 15 constituted by a shaft 25, projecting beyond the first bearing 23 which is more flexible in bending than the span of the drive shaft 16 between the first and second bearings 22,23. A support means 27 is mounted for rotation in a third bearing 28. The rotor 11 is mounted on the flexible end portion 15 of the drive shaft 16 to be driven thereby and is also mounted on the support means 27 for rotation in the third bearing 28. The third bearing 28 is capable of accommodating radial deflections of the support means 27 when the rotor becomes unbalanced.


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