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National Stock Number:
2840-01-394-5230
Federal Supply Class:
2840
National Item Identification Number:
013945230
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.
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Manufacturer Information:
| 804351 | 77445 | RTX CORPORATION | | 804351CL17 | 77445 | RTX CORPORATION | | 804351CL17 | 96965 | TURBINE AIRFOIL DESIGNS INC. | | 804351CL17 | 99160 | THERM, INCORPORATED |
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Techincal Specification:
| MATERIAL | COBALT ALLOY OVERALL | | MATERIAL DOCUMENT AND CLASSIFICATION | APWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL | | DESIGN TYPE | AXIAL COMPRESSOR | | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE | | STAGE NUMBER | 1 | | BLADE ATTACHMENT METHOD | SLOT | | OVERALL LENGTH | 2.035 INCHES MINIMUM AND | | 2.045 INCHES MAXIMUM | | OVERALL WIDTH | 1.110 INCHES MINIMUM AND | | 1.130 INCHES MAXIMUM | | OVERALL HEIGHT | 4.270 INCHES MINIMUM AND | | 4.300 INCHES MAXIMUM | | SPECIAL FEATURES | FLOW AREA 1.418-1.427; PITCH 33 DEG. 53 MIN. 28 SEC. | | CRITICALITY CODE JUSTIFICATION | APGF AND | | CZBJ AND | | CZCJ AND | | BGLW AND | | FEAT | | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG 31 IND 50 | | PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE,HPT,1 STG |
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