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:
Sep. 15, 2020

Filed:

Sep. 20, 2017
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Richard Alan Wesling, Cincinnati, OH (US);

Darek Tomasz Zatorski, Fort Wright, KY (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 11/12 (2006.01); F02C 3/067 (2006.01); F01D 5/03 (2006.01); F01D 5/22 (2006.01); F01D 11/14 (2006.01); F01D 11/16 (2006.01); F01D 11/08 (2006.01); F01D 11/02 (2006.01); F01D 11/00 (2006.01); F02K 3/072 (2006.01);
U.S. Cl.
CPC ...
F01D 11/122 (2013.01); F01D 5/03 (2013.01); F01D 5/225 (2013.01); F01D 11/001 (2013.01); F01D 11/02 (2013.01); F01D 11/08 (2013.01); F01D 11/12 (2013.01); F01D 11/14 (2013.01); F01D 11/16 (2013.01); F02C 3/067 (2013.01); F02K 3/072 (2013.01); F05D 2240/56 (2013.01); F05D 2240/59 (2013.01);
Abstract

The present disclosure is directed to a gas turbine engine including a turbine rotor assembly that includes a first turbine rotor and a second turbine rotor. The first turbine rotor includes an outer rotor and a plurality of outer rotors extended inwardly along a radial direction from the outer rotor. The second turbine rotor includes an inner rotor and a plurality of inner rotor airfoils extended outwardly along the radial direction from the inner rotor. The plurality of outer rotor airfoils and inner rotor airfoils are disposed in alternating arrangement along a longitudinal direction. One or more rotating seal interfaces are defined between the first turbine rotor and the second turbine rotor.


Find Patent Forward Citations

Loading…