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:
Dec. 01, 2020

Filed:

Oct. 10, 2019
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Emile Raya, Derby, GB;

Lucian Ingley, Derby, GB;

Zahid M. Hussain, Derby, GB;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/14 (2006.01); F02C 7/12 (2006.01); F02K 3/06 (2006.01); F02C 7/32 (2006.01);
U.S. Cl.
CPC ...
F01D 25/14 (2013.01); F02C 7/12 (2013.01); F02C 7/32 (2013.01); F02K 3/06 (2013.01); F05D 2240/14 (2013.01); F05D 2260/201 (2013.01);
Abstract

A gas turbine engine for an aircraft is provided. The engine includes an engine core comprising a turbine, a compressor, and a core shaft connecting the turbine to the compressor. The engine further includes core casings surrounding the engine core. The engine further includes an aerodynamic cowl which surrounds the core casings. The engine further includes a propulsive fan located upstream of the engine core, the fan generating a core airflow which enters the core engine and a bypass airflow which enters a bypass duct surrounding the aerodynamic cowl. The engine further includes one or more engine accessories mounted in a space between the core casings and the aerodynamic cowl.


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