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:
Jan. 14, 2020

Filed:

Feb. 06, 2018
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Gabrielle Murphy, West Hartford, CT (US);

Gregory E. Reinhardt, South Glastonbury, CT (US);

Robert M. Lewis, Berlin, CT (US);

Scott L. Peterson, Longmeadow, MA (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/20 (2006.01); B66C 11/12 (2006.01); B66C 11/04 (2006.01); F01D 25/28 (2006.01);
U.S. Cl.
CPC ...
F02C 7/20 (2013.01); B66C 11/04 (2013.01); B66C 11/12 (2013.01); F01D 25/285 (2013.01); F05D 2230/68 (2013.01); Y10T 29/49236 (2015.01);
Abstract

An assembly system for assembling a gas turbine engine including a support beam defining a horizontal plane for assembly of engine components along a horizontal axis substantially parallel with the support beam. A forward arm is supported on the support beam for supporting a forward portion of an engine component. An aft arm is supported on the support beam for supporting an aft portion of the engine component. An aft mounting ring is attachable to an aft end of an engine assembly. A forward mounting ring is attachable to a forward end of the engine assembly. A drive is mounted to the aft arm engageable to the aft mounting ring for rotating the engine assembly about the horizontal axis. A roller is supported on the forward arm and engageable to the forward mounting ring to support the first end of the engine assembly during rotation about the horizontal axis. A method is also disclosed.


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