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:
Jul. 05, 2022

Filed:

Jun. 21, 2019
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Rory D Stieger, Derby, GB;

Conor Hickey, Bristol, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/20 (2006.01); B64D 31/06 (2006.01); B64D 33/02 (2006.01); B64D 33/04 (2006.01); F02C 9/54 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F02C 9/20 (2013.01); B64D 31/06 (2013.01); B64D 33/02 (2013.01); B64D 33/04 (2013.01); F02C 9/54 (2013.01); F02K 3/06 (2013.01); B64D 2033/0286 (2013.01); F05D 2220/323 (2013.01); F05D 2220/80 (2013.01); F05D 2260/96 (2013.01); F05D 2270/051 (2013.01); F05D 2270/095 (2013.01); F05D 2270/71 (2013.01);
Abstract

A turbofan engine has an engine core including in flow series a compressor, a combustor and a turbine. The engine further has a fan located upstream of the engine core, has a supersonic intake for slowing down incoming air to subsonic velocities at an inlet to the fan formed by the intake, has a bypass duct surrounding the engine core, wherein the fan generates a core airflow to the engine core and a bypass airflow through the bypass duct, and has a mixer for mixing an exhaust gas flow exiting the engine core and bypass airflow exiting bypass duct. The engine further has a thrust nozzle rearwards of the mixer for discharging mixed flows, the thrust nozzle having a variable area throat. The engine further has a controller controlling the thrust produced by the engine over a range of flight operations including on-the-ground subsonic take-off and subsequent off-the-ground subsonic climb.


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