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:
Apr. 10, 2018

Filed:

Apr. 30, 2015
Applicant:

Honeywell International Inc., Morristown, NJ (US);

Inventors:

Eric Blumer, Scottsdale, AZ (US);

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

Jason Smoke, Phoenix, 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:
Int. Cl.
CPC ...
F01D 5/06 (2006.01); B22F 3/105 (2006.01); B22F 3/15 (2006.01); B23P 15/00 (2006.01); F01D 5/30 (2006.01); F01D 5/34 (2006.01); F01D 5/04 (2006.01); F04D 29/28 (2006.01); F04D 29/32 (2006.01); F04D 29/60 (2006.01); F04D 29/64 (2006.01);
U.S. Cl.
CPC ...
F01D 5/066 (2013.01); B22F 3/1055 (2013.01); B22F 3/15 (2013.01); B23P 15/006 (2013.01); F01D 5/04 (2013.01); F01D 5/3061 (2013.01); F01D 5/34 (2013.01); F04D 29/284 (2013.01); F04D 29/321 (2013.01); F04D 29/322 (2013.01); F04D 29/329 (2013.01); F04D 29/601 (2013.01); F04D 29/644 (2013.01); F05D 2220/32 (2013.01); F05D 2230/10 (2013.01); F05D 2230/23 (2013.01); F05D 2230/31 (2013.01); Y02P 10/295 (2015.11); Y02T 50/671 (2013.01);
Abstract

Bladed Gas Turbine Engine (GTE) rotors including deposited transition rings are provided, as are embodiments of methods for manufacturing bladed GTE rotors. In one embodiment, the method includes providing an outer blade ring having an inner circumferential surface defining a central opening, and depositing a deposited transition ring on the inner circumferential surface of the outer blade ring. The outer blade ring can be a full bladed ring or an annular grouping of individually-fabricated bladed pieces. After deposition of the transition ring, a hub disk is inserted into the central opening such that the transition ring extends around an outer circumferential surface of the hub disk. The transition ring is then bonded to the outer circumferential surface of the hub disk utilizing, for example, a hot isostatic pressing technique to join the transition ring and the outer blade ring thereto.


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