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:
Jun. 08, 2021

Filed:

Jun. 20, 2019
Applicant:

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

Inventors:

Russell B Jones, North Palm Beach, FL (US);

Edwin L Kite, Stuart, FL (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/02 (2006.01); F01D 5/04 (2006.01); F04D 29/26 (2006.01); F04D 29/28 (2006.01); F01D 5/28 (2006.01);
U.S. Cl.
CPC ...
F01D 5/025 (2013.01); F01D 5/046 (2013.01); F01D 5/048 (2013.01); F01D 5/284 (2013.01); F04D 29/266 (2013.01); F04D 29/284 (2013.01); F05D 2220/32 (2013.01); F05D 2240/24 (2013.01); F05D 2260/20 (2013.01); F05D 2260/31 (2013.01); F05D 2300/20 (2013.01);
Abstract

A small gas turbine engine with a ceramic turbine to allow for higher turbine inlet temperatures, where a metallic compressor is secured to a ceramic shaft extending from a ceramic turbine to form a single piece ceramic shaft and turbine, where a threaded nut secures a split ring retainer on the compressor end of the ceramic shaft. A hollow thrust runner is compressed between the compressor disk and the turbine disk by the threaded nut to secure rotor together. A centering spring forms a tight fit between the metallic thrust runner and the ceramic shaft on the turbine side.


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