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Title: Airfoil seal system for gas turbine engine

Abstract

A turbine airfoil seal system of a turbine engine having a seal base with a plurality of seal strips extending therefrom for sealing gaps between rotational airfoils and adjacent stationary components. The seal strips may overlap each other and may be generally aligned with each other. The seal strips may flex during operation to further reduce the gap between the rotational airfoils and adjacent stationary components.

Publication Date:
Research Org.:
Siemens Energy, Inc. (Orlando, FL)
Sponsoring Org.:
USDOE
OSTI Identifier:
1087365
Patent Number(s):
8,469,656
Application Number:
12/014,298
Assignee:
Siemens Energy, Inc. (Orlando, FL)
DOE Contract Number:  
FC26-05NT42644
Resource Type:
Patent
Country of Publication:
United States
Language:
English
Subject:
33 ADVANCED PROPULSION SYSTEMS

Citation Formats

None, None. Airfoil seal system for gas turbine engine. United States: N. p., 2013. Web.
None, None. Airfoil seal system for gas turbine engine. United States.
None, None. Tue . "Airfoil seal system for gas turbine engine". United States. https://www.osti.gov/servlets/purl/1087365.
@article{osti_1087365,
title = {Airfoil seal system for gas turbine engine},
author = {None, None},
abstractNote = {A turbine airfoil seal system of a turbine engine having a seal base with a plurality of seal strips extending therefrom for sealing gaps between rotational airfoils and adjacent stationary components. The seal strips may overlap each other and may be generally aligned with each other. The seal strips may flex during operation to further reduce the gap between the rotational airfoils and adjacent stationary components.},
doi = {},
url = {https://www.osti.gov/biblio/1087365}, journal = {},
number = ,
volume = ,
place = {United States},
year = {2013},
month = {6}
}

Patent:

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