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:
Aug. 05, 2025

Filed:

Feb. 20, 2023
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Christopher A. Murray, Nottingham, GB;

Mark J E Bellis, Derby, GB;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 13/02 (2006.01); F02C 6/06 (2006.01); F02C 7/32 (2006.01); B64D 13/06 (2006.01);
U.S. Cl.
CPC ...
B64D 13/02 (2013.01); F02C 6/06 (2013.01); F02C 7/32 (2013.01); B64D 2013/0603 (2013.01);
Abstract

A blower system for a gas turbine engine comprising: a rotor assembly, an airframe port and a routing-control valve. The rotor assembly is configured to be mechanically coupled to a spool of the gas turbine engine. The airframe port is configured to receive and discharge air to an airframe system. The routing-control valve comprises: a primary channel for bidirectional flow between the rotor assembly and the airframe port; a primary valve member configured to open and close the primary channel; and an auxiliary channel branched from the primary channel. The auxiliary channel is configured to bypass the primary valve member for: a first auxiliary flow from the airframe port to the rotor assembly; or a second auxiliary flow for purging air from the rotor assembly to a discharge port. The blower system is configured to operate in an engine drive mode and in a blower mode.


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