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:
Jun. 13, 2023

Filed:

Aug. 04, 2021
Applicants:

GE Avio S.r.l., Rivalta di Turin, IT;

Avio Polska Sp. Z O.o., Biata-Bielsko, PL;

Inventors:

Matteo Renato Usseglio, Turin, IT;

Enrico Ganzitti, Avigliana, IT;

Gianfranco Brandino, Chieri, IT;

Rafal Robak, Pszczyna, PL;

Tomasz Mucha, Meszna, PL;

Assignees:

GE AVIO S.R.L., Rivalta di Torino, IT;

AVIO POLSKA SP. Z O.O, Biata-Bielsko, PL;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01); F01D 9/02 (2006.01); F01D 25/24 (2006.01); F01D 11/00 (2006.01);
U.S. Cl.
CPC ...
F01D 9/02 (2013.01); F01D 9/041 (2013.01); F01D 11/005 (2013.01); F01D 25/243 (2013.01); F01D 25/246 (2013.01); F05D 2220/32 (2013.01); F05D 2240/128 (2013.01);
Abstract

A gas turbine engine including a frame assembly; a turbine assembly; and a nozzle disposed in the turbine assembly, wherein the nozzle defines an inner end along a radial direction and an outer end along the radial direction, wherein the outer end of the nozzle is supported by the frame assembly, wherein the inner end of the nozzle is supported by the frame assembly, and wherein the inner end of the nozzle is displaceable relative to the frame assembly in at least the radial direction.


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