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:
Nov. 28, 2023

Filed:

Nov. 01, 2018
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Thomas Merzhaeuser, Munich, DE;

Andrew Mitchell Rodwell, Greenville, SC (US);

Mohammad Salah Attia, Niskayuna, NY (US);

Matthew Brian Dudon, Mauldin, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F03D 1/06 (2006.01); F03D 80/00 (2016.01);
U.S. Cl.
CPC ...
F03D 1/0675 (2013.01); F03D 80/00 (2016.05); F05B 2210/12 (2013.01); F05B 2220/30 (2013.01); F05B 2230/60 (2013.01); F05B 2240/221 (2013.01); F05B 2240/30 (2013.01);
Abstract

A rotor blade includes a first blade segment and a second blade segment extending in opposite directions from a chord-wise joint. Each of the first and second blade segments has at least one shell member defining an airfoil surface. The first blade segment includes a beam structure having a receiving end with at least one span-wise extending pin extending therefrom. The second blade segment includes a receiving section that receives the beam structure. The receiving section includes a chord-wise member having a pin joint slot defined therethrough. The pin joint slot receives the span-wise extending pin at the receiving end of the beam structure so as to secure the first and second blade segments together. Moreover, the chord-wise member, the pin joint slot, and/or the span-wise extending pin includes at least one compliant structure formed of a compliant material that allows a deformation thereof to follow a shear deformation of the rotor blade.


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