Machined aerodynamic intercompressor bleed ports
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United States of America Patent
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May 2, 2017
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app pub date -
Jun 20, 2012
filing date -
Jun 20, 2012
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Abstract
An air bleed system for a jet engine is provided. The air bleed system is located in the low pressure compressor chamber and comprises a movable bleed valve and a stationary, annular bleed case having a forward section and an aft section and ligaments connecting the two sections and providing structural support to the bleed case. The ligaments are machined from the bleed case into an aerodynamic shape that maximizes the flow of air through the bleed ports.
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