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:
Mar. 04, 2008

Filed:

Oct. 01, 2004
Applicants:

Ian G Martindale, Derby, GB;

Sivasubramaniam K Sathianathan, Burton on Trent, GB;

Inventors:

Ian G Martindale, Derby, GB;

Sivasubramaniam K Sathianathan, Burton on Trent, GB;

Assignee:

Rolls-Royce plc, London, GB;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01B 25/16 (2006.01);
U.S. Cl.
CPC ...
Abstract

A gas turbine engine rotor blade containment assembly () comprises a containment casing () and the containment casing () has a plurality of axially spaced ribs (). The ribs () extend circumferentially and radially inwardly from the containment casing () to define a plurality of circumferentially extending grooves () and a perforate sheet () is secured to the radially inner ends () of the ribs (). In the arrangement of the present invention the blade containment function and the acoustic treatment function are combined.


Find Patent Forward Citations

Martindale, Ian. (2008). Gas turbine engine blade containment assembly (U.S. Patent No. 7338250). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/7338250

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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