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:
Feb. 16, 2021

Filed:

Oct. 06, 2017
Applicant:

Ansaldo Energia Switzerland Ag, Baden, CH;

Inventors:

Marcos Escudero Olano, Zurich, CH;

Stephan Strueken, Zurich, CH;

Thomas Zierer, Ennetbaden, CH;

Frank Graf, Nussbaumen, CH;

Adnan Eroglu, Untersiggenthal, CH;

Joshua R. McNally, Jupiter, FL (US);

Stephen W. Jorgensen, Palm City, FL (US);

Afzal Pasha Mohammed, Jupiter, FL (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/28 (2006.01); F01D 11/00 (2006.01); F01D 9/02 (2006.01); F16J 15/46 (2006.01); F01D 9/04 (2006.01); F16J 15/06 (2006.01); F02C 3/04 (2006.01);
U.S. Cl.
CPC ...
F02C 7/28 (2013.01); F01D 9/023 (2013.01); F01D 9/041 (2013.01); F01D 11/003 (2013.01); F16J 15/06 (2013.01); F16J 15/46 (2013.01); F02C 3/04 (2013.01); F05D 2220/32 (2013.01); F05D 2240/35 (2013.01); F05D 2240/55 (2013.01); F05D 2250/283 (2013.01); F16J 15/065 (2013.01);
Abstract

A sealing arrangement at an interface between a combustor and a turbine of a gas turbine. The turbine can include deflecting vanes at its inlet, which deflecting vanes are each mounted within the turbine so as to define an inner or outer diameter platform and are in sealing engagement via an inner or outer diameter vane tooth with a seal arranged at the corresponding inner or outer diameter part of the outlet of the combustor. The seal is movable and is pressed on the inner or outer diameter vane tooth by a differential pressure such that the pressure of the mainstream hot gas flow is a lower pressure.


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