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:
Oct. 06, 2020

Filed:

Jul. 30, 2018
Applicant:

Florida Turbine Technologies, Inc., Jupiter, FL (US);

Inventors:

Robert L Memmen, Stuart, FL (US);

William L Plank, Tequesta, FL (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/08 (2006.01); F01D 5/18 (2006.01); F01D 5/34 (2006.01); B22C 9/10 (2006.01);
U.S. Cl.
CPC ...
F01D 5/087 (2013.01); B22C 9/10 (2013.01); F01D 5/186 (2013.01); F01D 5/34 (2013.01); F05D 2220/323 (2013.01); F05D 2230/21 (2013.01); F05D 2240/24 (2013.01); F05D 2250/14 (2013.01); F05D 2250/232 (2013.01); F05D 2250/33 (2013.01); F05D 2250/51 (2013.01); F05D 2250/71 (2013.01); F05D 2250/72 (2013.01); F05D 2260/202 (2013.01);
Abstract

An air cooled integrally bladed rotor with bore entry cooling holes for a small gas turbine engine cast using a ceramic core having an axial bore forming piece with a plurality of radial extending spokes that end in an annular ring to form cooling air supply passages for air cooled turbine blades. Bulbous chambers are formed in a circumferential cooling air supply channel formed below each blade, where cooling air holes are drilled from a tip of each blade and into the bulbous chambers. The radial spokes have an elliptical cross sectional shape with a major axis perpendicular to a rotational axis of the central bore of the IBR. A spacing of the inlet openings in the bore are minimized to reduce stress.


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