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:
Dec. 17, 2019

Filed:

Sep. 20, 2017
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Peeyush Pankaj, Bangalore, IN;

Shashank Suresh Puranik, Bangalore, IN;

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

Christopher Charles Glynn, Clearwater Beach, FL (US);

Richard Schmidt, Loveland, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/03 (2006.01); F01D 5/14 (2006.01); F01D 1/26 (2006.01); F01D 9/04 (2006.01); F02C 7/06 (2006.01); F02C 7/32 (2006.01); F02C 7/36 (2006.01); F02C 3/067 (2006.01); F01D 25/16 (2006.01);
U.S. Cl.
CPC ...
F01D 5/03 (2013.01); F01D 1/26 (2013.01); F01D 5/142 (2013.01); F01D 9/041 (2013.01); F01D 25/164 (2013.01); F02C 3/067 (2013.01); F02C 7/06 (2013.01); F02C 7/32 (2013.01); F02C 7/36 (2013.01); F05D 2240/12 (2013.01); F05D 2240/24 (2013.01); F05D 2260/4031 (2013.01); F05D 2260/40311 (2013.01);
Abstract

A turbomachine includes a turbine section including a turbine, the turbine having a plurality of turbine rotor blades spaced along the axial direction, each turbine rotor blade extending generally along the radial direction between a radial inner end and a radial outer end. The plurality of turbine rotor blades includes a first turbine rotor blade; and a second turbine rotor blade spaced from the first turbine rotor blade along the axial direction, the radial outer end of the first turbine rotor blade coupled to the radial outer end of the second turbine rotor blade. The plurality of turbine rotor blades additionally includes a third turbine rotor blade spaced from the second turbine rotor blade along the axial direction, the radial inner end of the second turbine rotor blade coupled to the radial inner end of the third turbine rotor blade.


Find Patent Forward Citations

Pankaj, Peeyush. (2019). Turbomachine with alternatingly spaced turbine rotor blades (U.S. Patent No. 10508546). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10508546

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

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