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:
Oct. 26, 2021

Filed:

Mar. 13, 2019
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Richard G. Stretton, Ashby-de-la-Zouch, GB;

Tim O'Hanrahan, Bristol, GB;

Assignee:

ROLLS-ROYCE PLC, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/36 (2006.01); F02C 3/06 (2006.01); F02C 3/107 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F02C 7/36 (2013.01); F02C 3/06 (2013.01); F02C 3/107 (2013.01); F02K 3/06 (2013.01); F05D 2240/14 (2013.01); F05D 2260/40311 (2013.01);
Abstract

A gas turbine engine comprising a planetary gear train, and a core engine casing. The gear train has a ratio of greater than approximately 3.0, with an input to the gear train being operatively connected to the compressor section, and an output from the gear train being operatively connected to the fan. The core engine casing encloses the compressor section and the turbine section. The fan has a diameter F, and the core engine casing has a diameter C. The core engine casing diameter C varies along an axial length of the core engine casing, and a ratio (C/F) of the core engine casing diameter C to the fan diameter F is within the range 0.2<(C/F)<0.4, along an axial length of the core engine casing.


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