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:
Jan. 02, 2024

Filed:

Dec. 20, 2021
Applicant:

Rolls-royce North American Technologies, Inc., Indianapolis, IN (US);

Inventors:

Richard K Keller, Indianapolis, IN (US);

Paul Johnson, Indianapolis, IN (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 6/04 (2006.01); F02C 9/18 (2006.01); F02K 3/02 (2006.01);
U.S. Cl.
CPC ...
F02C 6/04 (2013.01); F02C 9/18 (2013.01); F02K 3/025 (2013.01); F05D 2220/90 (2013.01); F05D 2240/128 (2013.01); F05D 2260/606 (2013.01); F05D 2270/053 (2013.01); F05D 2270/335 (2013.01);
Abstract

A system including a turbine engine configured to generate rotor power and produce an engine air flow. The system is configured to provide rotor power to one of more shaft-driven lift fans to generate a first thrust on an aircraft body and provide a gas flow to one or more gas-driven lift fans to generate a second thrust on the aircraft body. The gas flow may be at least a portion of the engine air flow produced by the turbine engine. The turbine engine may be configured to exhaust another portion of the engine air flow through a jet nozzle to generate an engine thrust. In examples, the system includes at least a second turbine engine. The one of more shaft-driven lift fans and/or one of more gas-driven lift fans be powered by the turbine engine, the second turbine engine, or both the turbine engine and the second turbine engine.


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