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.

Patent No.:

US 7507070 B1

PDF
Full Text
Expired
Date of Patent:
Mar. 24, 2009

Filed:

Jul. 25, 2005
Applicant:

Alan R Jones, Derby, GB;

Inventor:

Alan R Jones, Derby, GB;

Assignee:

Rolls-Royce plc, London, GB;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/08 (2006.01);
U.S. Cl.
CPC ...
Abstract

A rotor () for a gas turbine engine () has a low emissivity surface finish, or high emissivity surface finish (), on at least a portion of its surface () to reduce temperature differentials between an upper portion and a lower portion of the rotor (). This reduces bowing of the rotor () to allow the gas turbine engine () to be started without harmful vibrations of the rotor ().


Find Patent Forward Citations

Jones, Alan. (2009). Gas turbine engine and a rotor for a gas turbine engine (U.S. Patent No. 7507070). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/7507070

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

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