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.
Patent No.:
Date of Patent:
Sep. 23, 2025
Filed:
Jan. 18, 2024
Honeywell International Inc., Charlotte, NC (US);
Eric Bridges, Phoenix, AZ (US);
Mark Morris, Phoenix, AZ (US);
Jason Smoke, Phoenix, AZ (US);
Joseph Yanof, Phoenix, AZ (US);
John Mcclintic, Phoenix, AZ (US);
Steven Whitaker, Phoenix, AZ (US);
Partha Das, Phoenix, AZ (US);
HONEYWELL INTERNATIONAL INC., Charlotte, NC (US);
Abstract
Gas turbine engines and methods for reducing spool thrust in a combustor section thereof are provided. The engines include an impeller, a shaft coupled to the impeller, an inner cavity downstream of the impeller, a thrust bearing assembly mechanically coupled to the shaft, a seal assembly having a seal land, and a controller. The controller is configured to detect a loss of oil event to the thrust bearing assembly and, in response, actuate the seal assembly to move the seal land toward a downstream face of the impeller to form a continuous axial seal about the inner cavity, vent gases from the inner cavity to decrease pressure therein to an extent less than an operating gas pressure thereof, and maintain the axial seal and the pressure within the inner cavity and thereby reduce the axial loads on the shaft.