|
|
|
National Stock Number:
2840-01-444-7012
Federal Supply Class:
2840
National Item Identification Number:
014447012
Description:
BLADE,TURBINE ROTOR,AIRCRAFT GAS
Detail:
AN ITEM MOUNTED ON A DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE. IT IS DESIGNED TO CREATE THE FLOW OF AIR IN THE TURBINE SECTION OF AN ENGINE, GAS TURBINE, AIRCRAFT.
|
Manufacturer Information:
| 1807M26 | 07482 | GENERAL ELECTRIC COMPANY | | 1807M26G01 | 07482 | GENERAL ELECTRIC COMPANY |
|
Techincal Specification:
| MATERIAL | ALUMINUM BLADE | | DESIGN TYPE | AXIAL COMPRESSOR | | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE | | STAGE NUMBER | 2 | | BLADE ATTACHMENT METHOD | FIR TREE | | OVERALL LENGTH | 4.891 INCHES NOMINAL | | OVERALL WIDTH | 1.347 INCHES MINIMUM AND | | 1.352 INCHES MAXIMUM | | SPECIAL FEATURES | MATERIAL EXTERNAL PLATINUM ALUMINIDE COATING, THIS IS PART OF THE HT90 MOD FOR THE TF39, ORIGINAL DRAWING NAME BLADE,HIGH PRESSURE TURBINE ROTOR STAGE 2, TRAIL | | CRITICALITY CODE JUSTIFICATION | AGAV |
|
|