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:
May. 21, 2019

Filed:

Aug. 11, 2015
Applicants:

Jason Smoke, Phoenix, AZ (US);

Eric Blumer, Scottsdale, AZ (US);

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

Robbie Joseph Adams, Phoenix, AZ (US);

Harry Lester Kington, Scottsdale, AZ (US);

Inventors:

Jason Smoke, Phoenix, AZ (US);

Eric Blumer, Scottsdale, AZ (US);

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

Robbie Joseph Adams, Phoenix, AZ (US);

Harry Lester Kington, Scottsdale, AZ (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/30 (2006.01); B23K 1/00 (2006.01); F01D 5/02 (2006.01); F01D 5/14 (2006.01); F01D 5/22 (2006.01); F01D 5/06 (2006.01); F01D 25/12 (2006.01); F02C 9/18 (2006.01);
U.S. Cl.
CPC ...
F01D 5/3061 (2013.01); B23K 1/0018 (2013.01); F01D 5/02 (2013.01); F01D 5/06 (2013.01); F01D 5/066 (2013.01); F01D 5/147 (2013.01); F01D 5/22 (2013.01); F01D 25/12 (2013.01); F02C 9/18 (2013.01); F05D 2220/32 (2013.01); F05D 2230/233 (2013.01); F05D 2230/234 (2013.01); F05D 2230/236 (2013.01); F05D 2230/30 (2013.01); F05D 2300/17 (2013.01); F05D 2300/5023 (2013.01); F05D 2300/518 (2013.01); Y02T 50/671 (2013.01); Y02T 50/675 (2013.01);
Abstract

Dual alloy Gas Turbine Engine (GTE) rotors and method for producing GTE rotors are provided. In one embodiment, the method include includes arranging bladed pieces in an annular grouping or ring formation such that shank-to-shank junctions are formed between circumferentially-adjacent bladed pieces. A first or bonding alloy is deposited along the shank-to-shank junctions utilizing a localized fusion deposition process to produce a plurality of alloy-filled joints, which join the bladed pieces in a bonded blade ring. The bonding alloy is preferably selected to have a ductility higher than and a melt point lower than the alloy from which the bladed pieces are produced. After deposition of the first alloy and formation of the alloy-filled joints, a hub disk is inserted into the central opening of the bonded blade ring. The hub disk and blade ring are then bonded utilizing, for example, a Hot Isostatic Pressing process.


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