Kompressor- und Turbinenmantel
The compressor section of a gas turbine engine contains a insert (24) installed around the compressor blades that includes cells (28) in a honeycomb configuration. Each cell is at a compound angle to the blade tip to energize the tip air flow as the tip passes over the cell as the blade rotates, imp...
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Main Author | |
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Format | Patent |
Language | German |
Published |
12.10.2000
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Edition | 7 |
Subjects | |
Online Access | Get full text |
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