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A component of a rotor, compressor, nonaircraft gas turbine engine. it is designed to attach to the front and/or rear of the rotor providing support, alignment, and a means of attachment for a shaft, turbine, nonaircraft gas turbine engine. it may have provisions for installing bearings, and/or oil and air seals. see also disk and hub, compressor, nonaircraft gas turbine engine.
Solicitation | Description | Qty | UOM | Close Date |
---|---|---|---|---|
SPE4A117T0971 | Hub, Compressor, Nona | 56 | EA | 06/09/2017 |
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