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:
Aug. 10, 2021

Filed:

Jul. 22, 2019
Applicant:

Mtu Aero Engines Ag, Munich, DE;

Inventors:

Harsimar Sahota, Unterschleissheim, DE;

Alexander Halcoussis, Haimhausen, DE;

Sergio Elorza Gomez, Munich, DE;

Assignee:

MTU Aero Engines AG, Munich, DE;

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 19/02 (2006.01); F01D 1/10 (2006.01); F04D 29/54 (2006.01); F04D 29/18 (2006.01); F02C 3/06 (2006.01);
U.S. Cl.
CPC ...
F04D 19/02 (2013.01); F01D 1/10 (2013.01); F02C 3/06 (2013.01); F04D 29/181 (2013.01); F04D 29/541 (2013.01);
Abstract

An engine, having a first, second, third and fourth quasi-stage, each with a stator and a downstream rotor, wherein a particular blade/vane solidity in the center section is in the first quasi-stage, at least 1.04 and at most 1.16 for the stator and at least 1.46 and at most 1.67 for the rotor; in the second quasi-stage, at least 1.13 and at most 1.32 for the stator and at least 1.32 and at most 1.61 for the rotor; in the third quasi-stage, at least 1.20 and at most 1.39 for the stator and at least 1.16 and at most 1.41 for the rotor; in the fourth quasi-stage, at least 1.37 and at most 1.63 for the stator and at least 1.15 and at most 1.41 for the rotor.


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