2840-01-200-6463 VANE,FAN,AIRCRAFT GAS TURBINE EN Index 2840-01-200-6465 SHROUD SEGMENT,TURBINE,AIRCRAFT

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.


Manufacturer Information:
1284M82G0107482GENERAL ELECTRIC COMPANY
1284M82G0507482GENERAL ELECTRIC COMPANY
1284M82G0508244MOELLER MFG. COMPANY, LLC
1284M82G0528884TSS TECHNOLOGIES, INC.
1284M82G0533617ELECTRO METHODS INC
1284M82G0551992UNION MACHINE CO OF LYNN, INC
1284M82G0557613SUN COUNTRY INDUSTRIES, LLC
1284M82G0559665TECOMET-ALBUQUERQUE
1284M82G0560819MODERN INDUSTRIES INC
1284M82G0582T87WARFIGHTER FOCUSED LOGISTICS INC
1284M82G0591913MECO, INC.
1284M82G0596454GENERAL TOOL COMPANY
1284M82G058U485COLUMBIA MANUFACTURING, INC


Techincal Specification:
CRITICALITY CODE JUSTIFICATIONAGAV
ENGINE SECTION LOCATIONCOMPRESSOR
OVERALL LENGTH12.233 INCHES NOMINAL
OVERALL WIDTH1.890 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONAMS4132 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
MATERIALALUMINUM ALLOY 2618 OVERALL
SPECIAL FEATURESOUTER 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 NUMBER2
SURFACE TREATMENTANODIZE OVERALL


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