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H6 - Federal Item Name Directory
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60244
COMPRESSOR ROTOR,AXIAL,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: (All Except USA) A single or multistage item consisting of a disk or series of disks fastened together on a drum or central shaft or a series of curved blades mounted on an integral part of the disk(s), set at an angle and extending radially from the disk, or extending from the axis of rotation to the rim of the disk. It is designed to impart energy of motion to the air between the blade surfaces in an axial direction in the compressor section of a turbine engine.
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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: 66
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