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:
Jan. 14, 2003

Filed:

Jul. 10, 2001
Applicant:
Inventor:

Geoffrey M Dailey, Derby, GB;

Assignee:

Rolls-Royce plc, London, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/18 ;
U.S. Cl.
CPC ...
F01D 5/18 ;
Abstract

A turbine assembly for a gas turbine engine includes a plurality of turbine blades ( ) mounted on a rotatable support means in the form of a turbine disc so as to extend radially therefrom. The turbine blades include circumferentially extending blade platforms ( ) spaced from the turbine disc and means are provided for allowing the passage of air between an internal region of the blades ( ) and a space located between the blade platforms ( ) and the turbine disc. The air may flow out of and back into the same turbine blade, or may flow into an adjacent blade. This flow of air results in the cooling of the blade platforms ( ).


Find Patent Forward Citations

Dailey, Geoffrey. (2003). Blade platform cooling (U.S. Patent No. 6506020). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/6506020

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

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