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:
Jun. 30, 2020

Filed:

Dec. 18, 2019
Applicant:

Rolls-royce Plc, London, GB;

Inventor:

Ian J Bousfield, Nottingham, GB;

Assignee:

ROLLS-ROYCE PLC, London, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/36 (2006.01); F02C 7/057 (2006.01); F02C 3/06 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F02C 7/36 (2013.01); F02C 3/06 (2013.01); F02C 7/057 (2013.01); F02K 3/06 (2013.01); F05D 2220/327 (2013.01); F05D 2260/40311 (2013.01); F05D 2270/021 (2013.01);
Abstract

A gas turbine engine includes an inlet duct to guide a core engine flow to a compressor and an engine section stator arranged in the inlet duct upstream of the compressor including vanes with leading edges defining a first annulus area in the inlet duct, a mid-span leading edge point of the engine section stator vanes being arranged at a first radius. The compressor includes a first rotor with a row of first blades with leading edges defining a second annulus area; a mid-span leading edge point of the compressor first blades being arranged at a second radius and an axial distance from the engine section stator vane mid-span leading edge point. The ratio of the second to the first annulus area is equal or greater than 0.75, and the ratio of a difference between the first and second radius to the axial distance is equal or greater than 0.23.


Find Patent Forward Citations

Bousfield, Ian. (2020). Highly loaded inlet duct in a geared turbofan (U.S. Patent No. 10697374). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10697374

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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