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:
Aug. 14, 2018

Filed:

Dec. 14, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Todd Alan Anderson, Niskayuna, NY (US);

Nicholas Joseph Kray, Mason, OH (US);

Bryant Edward Walker, Cincinnati, OH (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/32 (2006.01); F04D 29/64 (2006.01); F01D 5/30 (2006.01);
U.S. Cl.
CPC ...
F04D 29/322 (2013.01); F01D 5/3023 (2013.01); F04D 29/324 (2013.01); F04D 29/644 (2013.01); F05B 2220/302 (2013.01); F05B 2230/60 (2013.01); F05B 2260/30 (2013.01); F05D 2220/36 (2013.01); F05D 2260/31 (2013.01);
Abstract

A rotor assembly for use in a turbofan engine is provided. The rotor assembly includes an annular spool including a first blade opening defined therein, a first rotor blade configured to be radially inserted through the first blade opening, and a fairing positioned on a radially outer side of the annular spool. The first rotor blade includes a blade portion and a flange portion that extends substantially perpendicularly relative to the blade portion such that the flange portion is positioned on a radially inner side of the annular spool. The fairing is configured to receive a fastener radially inserted through the flange portion and the annular spool such that the first rotor blade is secured to the annular spool.


Find Patent Forward Citations

Loading…