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. 16, 2012

Filed:

Feb. 22, 2008
Applicants:

Jerome Alain Dupeux, Vaux le Penil, FR;

Jean-pierre Francois Lombard, Pamfou, FR;

Virendra Sharma, Paris, FR;

Samy Mitha, Ste Genevieve des Bois, FR;

Inventors:

Jerome Alain Dupeux, Vaux le Penil, FR;

Jean-Pierre Francois Lombard, Pamfou, FR;

Virendra Sharma, Paris, FR;

Samy Mitha, Ste Genevieve des Bois, FR;

Assignee:

SNECMA, Paris, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B21K 25/00 (2006.01); B23P 15/04 (2006.01);
U.S. Cl.
CPC ...
Abstract

A method for reducing vibration levels in a turbomachine including at least a first and a second bladed wheel, due to aerodynamic perturbations that are produced by the second bladed wheel or an obstacle on the first bladed wheel is disclosed. The method includes: defining an initial configuration of the blades; calculating the synchronous forced response on the first bladed wheel as a function of the harmonic excitation force produced by the second bladed wheel expressed in the form of a linear function of the generalized aerodynamic force for the mode considered; determining a geometric tangential shift value θ for the stacked cross sections of one of the two wheels to reduce the corresponding term to the generalized aerodynamic force. The set of cross sections with the tangential shifts thus defines a new configuration of the blades of one of the two wheels.


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