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National Stock Number: 2840-01-200-6464
Federal Supply Class: 2840
National Item Identification Number: 012006464
Description: SHROUD SEGMENT,TURBINE,AIRCRAFT
Detail: A STATIONARY ARCHED METAL SEGMENT USED TO ESTABLISH CLEARANCE AND A SEAL FOR THE TIP OF A BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE. THE INNER DIMENSION MAY HAVE OPEN HONEYCOMB OR COMPOSITION FILLED SURFACE OR MAY BE FORMED BY THE KNIFE EDGE METAL PROTRUSIONS OF A SEAL RING, LABYRINTH, AIRCRAFT GAS TURBINE ENGINE.
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Manufacturer Information:
1284M82G01 | 07482 | GENERAL ELECTRIC COMPANY | 1284M82G05 | 07482 | GENERAL ELECTRIC COMPANY | 1284M82G05 | 08244 | MOELLER MFG. COMPANY, LLC | 1284M82G05 | 28884 | TSS TECHNOLOGIES, INC. | 1284M82G05 | 33617 | ELECTRO METHODS INC | 1284M82G05 | 51992 | UNION MACHINE CO OF LYNN, INC | 1284M82G05 | 57613 | SUN COUNTRY INDUSTRIES, LLC | 1284M82G05 | 59665 | TECOMET-ALBUQUERQUE | 1284M82G05 | 60819 | MODERN INDUSTRIES INC | 1284M82G05 | 82T87 | WARFIGHTER FOCUSED LOGISTICS INC | 1284M82G05 | 91913 | MECO, INC. | 1284M82G05 | 96454 | GENERAL TOOL COMPANY | 1284M82G05 | 8U485 | COLUMBIA MANUFACTURING, INC |
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Techincal Specification:
CRITICALITY CODE JUSTIFICATION | AGAV | ENGINE SECTION LOCATION | COMPRESSOR | OVERALL LENGTH | 12.233 INCHES NOMINAL | OVERALL WIDTH | 1.890 INCHES NOMINAL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS4132 ASSN STD SINGLE MATERIAL RESPONSE OVERALL | MATERIAL | ALUMINUM ALLOY 2618 OVERALL | SPECIAL FEATURES | OUTER RADIUS 2ND END 11.908 IN.; INNER RADIUS 1ST END 11.393 IN.; INNER RADIUS 2ND END 11.14 IN.; FORMED SHAPE 45 DEG. 57 MIN. 27 SEC.; 11 HOLES 0.3535 IN. DIA. COUNTERBORE 0.520 IN. DIA. W/2 CUTTER RUN OUTS PER EA HOLE | STAGE NUMBER | 2 | SURFACE TREATMENT | ANODIZE OVERALL |
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