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:

Jul. 27, 2018
Applicant:

United Technologies Corporation, Famington, CT (US);

Inventors:

Gabriel L. Suciu, Glastonbury, CT (US);

Ioannis Alvanos, West Springfield, MA (US);

Brian Merry, Andover, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/00 (2006.01); F02C 7/20 (2006.01); B64D 27/26 (2006.01); B64D 27/10 (2006.01);
U.S. Cl.
CPC ...
F02C 7/20 (2013.01); B64D 27/10 (2013.01); B64D 27/26 (2013.01); B64D 2027/262 (2013.01); B64D 2027/266 (2013.01); F05D 2220/323 (2013.01); F05D 2230/60 (2013.01); F05D 2240/90 (2013.01); Y02T 50/44 (2013.01); Y10T 29/49947 (2015.01);
Abstract

A method for mounting a gas turbine engine having a compressor section, a combustor section, a turbine section, a pylon and a rear mount bracket, includes positioning the mounting bracket between the gas turbine engine and the pylon. The mounting bracket is connected to the turbine case reacting a least a vertical load, a side load, a thrust load, and a torque load from the gas turbine engine through the mounting bracket. The mounting bracket is attached to the pylon reacting the same loads from the gas turbine engine.


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