|
|
|
National Stock Number:
2840-01-394-5231
Federal Supply Class:
2840
National Item Identification Number:
013945231
Description:
NOZZLE,TURBINE,AIRCRAFT GAS TURB
Detail:
A single stationary item designed for the purpose of directing air at the proper angle and velocity to a ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud.
|
Manufacturer Information:
| 804351 | 77445 | RTX CORPORATION | | 804351CL18 | 77445 | RTX CORPORATION | | 804351CL18 | 96965 | TURBINE AIRFOIL DESIGNS INC. | | 804351CL18 | 99160 | THERM, INCORPORATED |
|
Techincal Specification:
| BLADE ATTACHMENT METHOD | SLOT | | CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND CZCJ AND BGLW AND FEAT | | DESIGN TYPE | AXIAL COMPRESSOR | | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE | | OVERALL HEIGHT | 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM | | OVERALL LENGTH | 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM | | OVERALL WIDTH | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM | | MATERIAL DOCUMENT AND CLASSIFICATION | PWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL | | MATERIAL | COBALT ALLOY OVERALL | | PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE,HPT,1 STG | | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG31 IND50 | | SPECIAL FEATURES | FLOW AREA 1.427-1.436; PITCH 34 DEG. 2 MIN. 28 SEC.; 2ND END WIDTH 0.760-0.780 | | STAGE NUMBER | 1 |
|
|