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. 08, 2019

Filed:

Aug. 17, 2012
Applicants:

Shawn M. Mcmahon, Agawam, MA (US);

Kirk A. Shute, New Britain, CT (US);

Jeffrey R. Lavin, Bloomfield, CT (US);

Russell P. Parrish, Glastonbury, CT (US);

Inventors:

Shawn M. McMahon, Agawam, MA (US);

Kirk A. Shute, New Britain, CT (US);

Jeffrey R. Lavin, Bloomfield, CT (US);

Russell P. Parrish, Glastonbury, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/20 (2006.01); F01D 25/16 (2006.01); F02K 1/80 (2006.01); B64D 27/26 (2006.01);
U.S. Cl.
CPC ...
F01D 25/16 (2013.01); B64D 27/26 (2013.01); F02C 7/20 (2013.01); F02K 1/80 (2013.01); B64D 2027/268 (2013.01);
Abstract

An assembly is provided for mounting a turbine engine to an airframe. The turbine engine extends along an axial centerline and includes an engine core mount and an engine exhaust mount. The assembly includes a thrust pin linkage connecting and extending axially between a core thrust pin and an exhaust thrust pin. The core thrust pin is adapted to connect to the engine core mount, and the exhaust thrust pin is adapted to connect to the engine exhaust mount. One of the core thrust pin, the exhaust thrust pin and the thrust pin linkage is also adapted to connect to the airframe.


Find Patent Forward Citations

Loading…