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. 25, 2020

Filed:

Jun. 30, 2017
Applicant:

Honeywell International Inc., Morris Plains, NJ (US);

Inventors:

Michael Kahrs, Phoenix, AZ (US);

Daniel C. Crites, Mesa, AZ (US);

Jude Miller, Phoenix, AZ (US);

Steve Halfmann, Chandler, AZ (US);

Jason Smoke, Phoenix, AZ (US);

Ardeshir Riahi, Scottsdale, AZ (US);

David K. Jan, Fountain Hills, AZ (US);

Assignee:

HONEYWELL INTERNATIONAL INC., Morris Plains, NJ (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B23P 15/00 (2006.01); F01D 5/02 (2006.01); F01D 5/30 (2006.01); F01D 5/08 (2006.01);
U.S. Cl.
CPC ...
B23P 15/006 (2013.01); F01D 5/02 (2013.01); F01D 5/025 (2013.01); F01D 5/085 (2013.01); F01D 5/3015 (2013.01); F01D 5/3061 (2013.01); F01D 5/08 (2013.01); F05D 2220/32 (2013.01); F05D 2230/232 (2013.01); F05D 2240/24 (2013.01); F05D 2240/81 (2013.01);
Abstract

Turbine wheels, turbine engines, and methods of fabricating the turbine wheels are provided. An exemplary method includes fabricating a turbine wheel that includes a rotor disk and a plurality of turbine blades operatively connected to the rotor disk through a blade mount. The method includes locating a cooling passage within a blade mount preliminary configuration and a cooling inlet on a surface of the blade mount preliminary configuration. A rotor disk bonding surface geometry and a blade mount bonding surface geometry are designed based upon a stress analysis of the turbine wheel and locations of the cooling passage and cooling inlet. A rotor disk production configuration and a blade mount production configuration are generated based upon the preliminary configurations. A blade mount and a rotor disk are formed based upon the production configurations. A blade ring including a plurality of blade mounts is formed and bonded to the rotor disk.


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