Multiple piece turbine engine airfoil with a structural spar
Abstract
A multiple piece turbine airfoil having an outer shell with an airfoil tip that is attached to a root with an internal structural spar is disclosed. The root may be formed from first and second sections that include an internal cavity configured to receive and secure the one or more components forming the generally elongated airfoil. The internal structural spar may be attached to an airfoil tip and place the generally elongated airfoil in compression. The configuration enables each component to be formed from different materials to reduce the cost of the materials and to optimize the choice of material for each component.
- Inventors:
-
- Orlando, FL
- Publication Date:
- Research Org.:
- National Energy Technology Laboratory (NETL), Pittsburgh, PA, Morgantown, WV (United States); Siemens Energy, Inc. (Orlando, FL)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1029264
- Patent Number(s):
- 8,033,790
- Application Number:
- 12/239,016
- Assignee:
- Siemens Energy, Inc. (Orlando, FL)
- DOE Contract Number:
- FC26-05NT42646
- Resource Type:
- Patent
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 33 ADVANCED PROPULSION SYSTEMS
Citation Formats
Vance, Steven J. Multiple piece turbine engine airfoil with a structural spar. United States: N. p., 2011.
Web.
Vance, Steven J. Multiple piece turbine engine airfoil with a structural spar. United States.
Vance, Steven J. 2011.
"Multiple piece turbine engine airfoil with a structural spar". United States. https://www.osti.gov/servlets/purl/1029264.
@article{osti_1029264,
title = {Multiple piece turbine engine airfoil with a structural spar},
author = {Vance, Steven J},
abstractNote = {A multiple piece turbine airfoil having an outer shell with an airfoil tip that is attached to a root with an internal structural spar is disclosed. The root may be formed from first and second sections that include an internal cavity configured to receive and secure the one or more components forming the generally elongated airfoil. The internal structural spar may be attached to an airfoil tip and place the generally elongated airfoil in compression. The configuration enables each component to be formed from different materials to reduce the cost of the materials and to optimize the choice of material for each component.},
doi = {},
url = {https://www.osti.gov/biblio/1029264},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Oct 11 00:00:00 EDT 2011},
month = {Tue Oct 11 00:00:00 EDT 2011}
}
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