Figure 4.28. Interstage Bleed System, Cutaway View.

Figure 4.27. Interstage Bleed System, External Components.

Figure 4.29. Antiicing System Diagram.

Army Aircraft Gas Turbine Engines
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and to an adapter located on top of the impeller housing. The tube

and elbow pass air through the impeller housing to the hot air

solenoid valve.

Figure 4.28. Interstage Bleed System, Cutaway View.

128

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