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H6 - Federal Item Name Directory
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61683
COMPRESSOR ROTOR,AXIAL-CENTRIFUGAL,TURBINE ENGINE
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FIIG: A23900
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Entry Date: Oct-27-1989
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Concept:
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Status: C
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Applicability: A
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Type: 2
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Definition: INC 61683 CANCELLED/REPLACED BY, INC 50588, FIIG A10700, APP-KEY J, INC 50587, FIIG A10700, APP-KEY J, ON 021513~(All Except USA). A multistage item consisting of a series of axial disk and blade assemblies and a centrifugal compressor rotor assembled together on a central shaft or axis. Air is impelled rearward by the blades of the axial stages of the rotor, by reason of blade angle and air foil contour, and is accelerated outward by the blades of the centrifugal section of the compressor, for the purpose of increasing the pressure of ambient air before impelling the air into the combustion chamber.
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Basic INC: 70299
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Basic Name: COMPRESSOR
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Description: 1. A machine in which the pressure of a gas increased from an initial intake pressure to a final discharge pressure of 10 or more pounds (4.536 kg) per square inch (6.452 sq cms) gage.
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Corresponding NIINs: 5
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