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. 20, 2020

Filed:

Jan. 11, 2019
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Daniel A. Bales, Avon, CT (US);

Thomas DeMichael, Stafford Springs, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B23K 101/00 (2006.01); F01D 5/14 (2006.01); B23K 35/38 (2006.01); B23K 37/00 (2006.01); B23K 37/04 (2006.01);
U.S. Cl.
CPC ...
F01D 5/147 (2013.01); B23K 35/383 (2013.01); B23K 37/003 (2013.01); B23K 37/04 (2013.01); B23K 2101/001 (2018.08); F05D 2230/232 (2013.01); F05D 2230/40 (2013.01); F05D 2230/64 (2013.01); F05D 2240/30 (2013.01);
Abstract

A method of forming a gas turbine engine component according to an example of the present disclosure includes, among other things, attaching a cover skin to an airfoil body, the airfoil body and the cover skin cooperating to define pressure and suction sides of an airfoil, and moving the airfoil in a forming line including a plurality of stations. The plurality of stations include a set of heating stations, a deforming station and a set of cool down stations. The moving step includes positioning the airfoil in the set of heating stations to progressively increase a temperature of the airfoil, then positioning the airfoil in the deforming station including causing the airfoil to deform between first and second dies, and then positioning the airfoil in the set of cool down stations to progressively decrease the temperature of the airfoil.


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