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:
Jan. 21, 2020

Filed:

Nov. 08, 2011
Applicants:

Sylvain Yves Jean Duval, Tournan en Brie, FR;

Clement Roussille, Bordeaux, FR;

Alain Schweitzer, Leognan, FR;

Patrick Joseph Marie Girard, Saint Fargeau Ponthierry, FR;

Inventors:

Sylvain Yves Jean Duval, Tournan en Brie, FR;

Clement Roussille, Bordeaux, FR;

Alain Schweitzer, Leognan, FR;

Patrick Joseph Marie Girard, Saint Fargeau Ponthierry, FR;

Assignees:

SNECMA, Paris, FR;

HERAKLES, Le Haillan, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/28 (2006.01); F04D 29/38 (2006.01); G06F 17/50 (2006.01);
U.S. Cl.
CPC ...
F01D 5/282 (2013.01); G06F 17/50 (2013.01);
Abstract

A method optimizing a composite material blade profile for a rotor wheel of a turbine engine, and a blade including a tang compensated by the method. The method includes: compensating a blade airfoil by subdividing the airfoil into slices, and for each airfoil slice and a predetermined rotation speed of a disk of the wheel, calculating centrifugal force applied to the slice, calculating an aerodynamic force moment acting on a bottom section of the slice, and calculating shift values to be applied to a center of gravity of the slice to cancel the aerodynamic force moment; and compensating the blade tang by calculating centrifugal force applied to a blade portion situated beyond the airfoil neck, calculating an aerodynamic force moment acting on a bottom section of the blade tang, and calculating shift values to be applied to a center of gravity of the blade tang to cancel the aerodynamic force moment.


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