|
|
|
National Stock Number:
2840-01-438-8400
Federal Supply Class:
2840
National Item Identification Number:
014388400
Description:
ROTOR,COMPRESSOR,AIRCRAFT GAS TU
Detail:
A SINGLE OR MULTISTAGE ASSEMBLY DESIGNED TO DELIVER AIR AT THE PROPER PRESSURE, DIRECTION AND VELOCITY. IT CONSISTS OF DISKS, BLADES, HUBS, AND THE LIKE. IT IS THE MOVING PART OF COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. IT HAS FACILITIES FOR ATTACHING TO A SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
|
Manufacturer Information:
| 1559M63G02-110 | 07482 | GENERAL ELECTRIC COMPANY |
|
Techincal Specification:
| CRITICALITY CODE JUSTIFICATION | FEAT AND ABHP AND ABMZ AND CZBJ | | DESIGN TYPE | AXIAL COMPRESSOR | | DIAMETER | 17.300 INCHES NOMINAL | | ENGINE SECTION LOCATION | HIGH PRESSURE COMPRESSOR | | OVERALL LENGTH | 6.143 INCHES MINIMUM AND 6.163 INCHES MAXIMUM | | MATERIAL DOCUMENT AND CLASSIFICATION | TI-17 MFR REF SINGLE MATERIAL RESPONSE OVERALL | | MATERIAL | TITANIUM ALLOY OVERALL | | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SPOOL,COMPRESSOR ROTOR | | SPECIAL FEATURES | T.O. 2J-F110-14, FIG 67, IND 5 UNDER P/N 1559M63G02; INCLUDES STAGE 2; ALSO CONSISTS NO. 1 DISK AND NO. 2 DISK AND FORWARD SHAFT THAT MAKES A 1 PIECE CONSTRUCTION THAT HOLDS BOTH STGS; WEIGHS 40.3 LBS; BASIC P/N CAN BE USED ON ALL ENGINE TYPES, BUT ONCE USED ON THE F110, IT CAN ONLY BE USED ON AN F110 ENGINE; REIDENTIFICATION WILL CONSIST OF ADDING THE ENGINE TYPE AS A DASH NUMBER FOLLOWING THE P/N | | STAGE NUMBER | 1 |
|
|