Turbine engine compressor blade
An airfoil for a compressor blade of a gas turbine engine has a chord between a leading edge and a trailing edge and a span between a root and a tip. The airfoil can further include a reduction in local chord from about 75% span to the tip for about a 5% reduction in local solidity. The airfoil can...
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Format | Patent |
Language | English |
Published |
05.03.2019
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Subjects | |
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Abstract | An airfoil for a compressor blade of a gas turbine engine has a chord between a leading edge and a trailing edge and a span between a root and a tip. The airfoil can further include a reduction in local chord from about 75% span to the tip for about a 5% reduction in local solidity. The airfoil can have decreasing sweep angles for the leading edge and the trailing edge from 50% span to the tip and can have decreasing leading and trailing edge dihedral angles from 50% span to the tip. |
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AbstractList | An airfoil for a compressor blade of a gas turbine engine has a chord between a leading edge and a trailing edge and a span between a root and a tip. The airfoil can further include a reduction in local chord from about 75% span to the tip for about a 5% reduction in local solidity. The airfoil can have decreasing sweep angles for the leading edge and the trailing edge from 50% span to the tip and can have decreasing leading and trailing edge dihedral angles from 50% span to the tip. |
Author | Adam, Matthew Ford Moeckel, Curtis William Stecher, Mark Joseph Falk, Eric Andrew Wood, Peter John |
Author_xml | – fullname: Adam, Matthew Ford – fullname: Wood, Peter John – fullname: Falk, Eric Andrew – fullname: Moeckel, Curtis William – fullname: Stecher, Mark Joseph |
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Notes | Application Number: US201615018126 |
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RelatedCompanies | General Electric Company |
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Snippet | An airfoil for a compressor blade of a gas turbine engine has a chord between a leading edge and a trailing edge and a span between a root and a tip. The... |
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SubjectTerms | BLASTING HEATING LIGHTING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS WEAPONS |
Title | Turbine engine compressor blade |
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