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:
Sep. 13, 2022

Filed:

Oct. 21, 2019
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Michael O Hales, Derby, GB;

Stephen J Bradbrook, Derby, GB;

Assignee:

ROLLS-ROYCE PLC, London, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 30/00 (2006.01); B64D 27/20 (2006.01); F02K 7/02 (2006.01); B64D 27/18 (2006.01); B64D 31/06 (2006.01); B64D 33/02 (2006.01);
U.S. Cl.
CPC ...
F02K 7/02 (2013.01); B64C 30/00 (2013.01); B64D 27/18 (2013.01); B64D 27/20 (2013.01); B64D 31/06 (2013.01); B64D 33/02 (2013.01); B64D 2033/026 (2013.01); B64D 2033/0273 (2013.01);
Abstract

A supersonic jet aircraft and a method of operating the same. The supersonic jet aircraft having at least three turbofan engines and an engine management computer. A first engine of the at least three turbofan engines is configured to be de-activatable during flight to move from an operational state in which it provides thrust to an operational state in which it stops providing thrust. Other engines of the at least three turbofan engines are configured to provide sufficient thrust to the supersonic jet aircraft when the first engine is de-activated such that the aircraft can perform a supersonic climb operation and/or a supersonic cruise operation.


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