1660-01-175-3021 SHAFT AND ROTOR ASSEMBLY Index 6625-01-175-3024 TEST FIXTURE,FILTER AND RELAY

National Stock Number:
2840-01-175-3023

Federal Supply Class:
2840

National Item Identification Number:
011753023

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:
9523M21P0102GZ1ADOM ENGINEERING, INC.
9523M21P0103550VANGUARD ELECTRONICS, LLC
9523M21P0107482GENERAL ELECTRIC COMPANY
9523M21P0113779LPI INDUSTRIES CORPORATION
9523M21P0116190UNISON ENGINE COMPONENTS INC
9523M21P0151992UNION MACHINE CO OF LYNN, INC
9532M21P0113779LPI INDUSTRIES CORPORATION
9532M21P0124115PALMER MANUFACTURING CO., LLC
9532M21P0128884TSS TECHNOLOGIES, INC.
9532M21P0133617ELECTRO-METHODS, L.P.
9532M21P0134336TECT HYPERVELOCITY, INC.
9532M21P0147940HI-TEK MANUFACTURING, INC.
9523M21P0157488LKM INDUSTRIES, INC
9523M21P0158828CFM INTERNATIONAL INC
9532M21P014J952GENERAL AVIATION
9532M21P0158199W M Z MFG CO INC
9532M21P018U485COLUMBIA MANUFACTURING, INC
9532M21P019Y765NUMET ACQUISITION INC


Techincal Specification:
DESIGN TYPECOMPRESSOR
ENGINE SECTION LOCATIONHIGH PRESSURE TURBINE
OVERALL LENGTH0.254 INCHES MINIMUM AND 0.375 INCHES MAXIMUM
MATERIAL THICKNESS0.077 INCHES MINIMUM AND 0.085 INCHES MAXIMUM
MATERIALNICKEL ALLOY OUTER CASE
STAGE NUMBER1
SPECIAL FEATUREST.O. 2J-F108-4; HIGH PRESSURE TURBINE SHROUD AND 1ST STAGE L.P. TURBINE NOZZLE; U-SHAPED CLIPS


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