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. 28, 2022

Filed:

Mar. 27, 2018
Applicant:

Siemens Energy Global Gmbh & Co. KG, Munich, DE;

Inventors:

Viraj Wadatkar, Charlotte, NC (US);

Adam J. Weaver, Oviedo, FL (US);

Robert H. Bartley, Oviedo, FL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 11/00 (2006.01); F01D 9/02 (2006.01); F01D 25/24 (2006.01); F01D 25/30 (2006.01); F02C 7/28 (2006.01);
U.S. Cl.
CPC ...
F01D 9/02 (2013.01); F01D 11/00 (2013.01); F01D 25/24 (2013.01); F01D 25/30 (2013.01); F02C 7/28 (2013.01); F05D 2220/32 (2013.01); F05D 2240/128 (2013.01); F05D 2240/55 (2013.01);
Abstract

A sealing arrangement in a gas turbine engine to seal a gap between first and second turbine components is provided. The sealing arrangement includes a first arcuate feather seal connected to an anchoring assembly of the sealing arrangement affixed to the first turbine component. A second arcuate feather seal is affixed to the second turbine component. The first arcuate feather seal and the second arcuate feather seal are responsive to a pressure differential that develops across the gap to form a pressure-loaded sealing joint between respective sealing surfaces of the first arcuate feather seal and the second arcuate feather seal. The sealing arrangement provides substantial design flexibility since it can reliably provide appropriate sealing functionality while enabling multiple degrees of freedom, such as to accommodate radial and/or axial displacements that can develop between the first turbine component and the second turbine component.


Find Patent Forward Citations

Loading…