or
Bookmark and Share
Hollow turbine blade stiffening
   
Document Number
US Patent 7001150
Issued Date
February 21, 2006
Link
Inventors
Map
Abstract
An apparatus and method for at least one of stiffening a rotor blade of a gas turbine engine and raising a natural vibration frequency of the blade. The blade has a recess extending radially and inwardly into the blade. A reinforcing element is provided in the recess at a selected position to thereby allow a large blade chord at the tip end of the blade.
Tags:
Description:
Amusing 0%
Clever 0%
Complex 0%
Efficient 0%
Historic 0%
Important 0%
Innovative 0%
Interesting 0%
Practical 0%
Simple 0%
Number of Claims:
11
Comments:
no comments yet
Owner
Published
February 21, 2006
Application Number
10/685,707
Filed
October 16, 2003
US Classification
416/1   416/231R 416/500
Int'l Classification
F01D   5/14   (20060101)  
Examiner
Attorney/Law Firm
USPTO Field of Search
416/232   416/233   416/1   416/231R   416/500  
Related Patents
Claims
Description
About| FAQs| Terms & Disclaimer| Link to Us| Contact Us