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National Stock Number:
2840-01-467-8591
Federal Supply Class:
2840
National Item Identification Number:
014678591
Description:
HUB,COMPRESSOR,AIRCRAFT GAS TURB
Detail:
A COMPONENT OF A ROTOR, COMPRESSOR, AIRCRAFT 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, AIRCRAFT GAS TURBINE ENGINE. IT MAY HAVE PROVISIONS FOR INSTALLING BEARINGS, AND/OR OIL AND AIR SEALS. SEE ALSO DISK AND HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE.
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Manufacturer Information:
| 710410 | 77445 | RTX CORPORATION | | 822630 | 77445 | RTX CORPORATION |
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Techincal Specification:
| ENGINE SECTION LOCATION | COMPRESSOR | | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5660 ASSN STD SINGLE MATERIAL RESPONSE OVERALL | | III MATERIAL | NICKEL ALLOY HUB | | PART NAME ASSIGNED BY CONTROLLING AGENCY | HUB-REAR, COMPRESSOR | | DESIGN TYPE | COMPRESSOR | | DIAMETER | 18.740 INCHES MINIMUM AND 18.760 INCHES MAXIMUM | | CRITICALITY CODE JUSTIFICATION | AGAV | | PROPRIETARY CHARACTERISTICS | PACS | | OVERALL LENGTH | 16.550 INCHES MINIMUM AND 16.570 INCHES MAXIMUM | | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4, FIG. 19, IND 15 | | SPECIAL FEATURES | 16 HOLES EQUALLY SPACED 0127-.132DIA; SPLINE AT END OF SHAFT, NO. OF TEETH 51, DP 10/20, 30 DEG.; SPLINE AT FWD OF SHAFT, NO. OF TEETH 87, DP 16/32, 30 DEG. ANGLE |
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