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:
Nov. 03, 2026

Filed:

Apr. 18, 2024
Applicant:

Rtx Corporation, Farmington, CT (US);

Inventors:

Thomas E. Clark, Wells, ME (US);

Andrew E. Breault, Bolton, CT (US);

William K. Ackermann, East Hartford, CT (US);

Assignee:

RTX Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/60 (2006.01); F01D 5/08 (2006.01); F23R 3/00 (2006.01); F23R 3/50 (2006.01);
U.S. Cl.
CPC ...
F23R 3/60 (2013.01); F01D 5/082 (2013.01); F23R 3/002 (2013.01); F23R 3/50 (2013.01); F23R 2900/00017 (2013.01);
Abstract

A gas turbine engine is provided having an axial centerline, a compressor section, a turbine section, and a combustor section. The turbine section has a turbine first vane assembly that includes an annular first vane inner radial support. The combustor section has an outer casing, an annular combustor, and a unitary inner diffuser structure. The annular combustor has an inner radial flange. The unitary inner diffuser structure includes a compressor discharge, an inner diffuser case, and a tangential onboard injector (TOBI) inseparably attached to one another. The unitary inner diffuser structure further includes an outer radial flange and a TOBI connection flange. The annular FV inner radial support, the combustor inner radial flange, and the TOBI connection flange are secured to one another.


Find Patent Forward Citations

Quick Actions:

Clark, Thomas. (2026). Gas turbine engine configured for decreased diffuser windage and method of assembling the same (U.S. Patent No. 12781966). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12781966

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