Product Details | TURBINE ENGINE AXIAL-CENTRIFUGAL COMPRESSOR ROTOR

2840-00-032-2784 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.20228350096Gas Turbines and Jet Engines; Non-Aircraft Prime Mover, Aircraft Non-Prime Mover, and Components28400068Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components

Part Alternates: 6020T69G03, 2840-00-032-2784, 00-032-2784, 2840000322784, 000322784

Engines, Turbines, and Components | Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components

Supply Group (FSG) NSN Assign. NIIN
28 00-032-2784

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Restrictions/Controls & Freight Information | NSN 2840-00-032-2784

Category Code Description
Hazardous Material Indicator CodeNThere is no data in the HMIS and the NSN is in an FSC not generally suspected of containing hazardous materials
Category Code Description
No Freight Information