![]() | PCC AIRFOILS LLC |
3860 UNION AVE SE MINERVA OH 44657-8901 UNITED STATES Telephone: 3308687311 |
PCC AIRFOILS LLC is an Active Manufacturer with the Cage Code 01996 and is tracked by Dun & Bradstreet under DUNS Number 004179339.
B: PURCHASE ORDER
IGF::OT::IGFFABRICATION OF SINGLE CRYSTAL BARS
9515: PLATE, SHEET, STRIP, FOIL, AND LEAF
B: PURCHASE ORDER
MOD 1 TO CHANGE CONTRACTING OFFICER. SINGLE CRYSTAL SEAL PRELOAD DEVICES
9340: GLASS FABRICATED MATERIALS
B: PURCHASE ORDER
SINGLE CRYSTAL SEAL PRELOAD DEVICES
9340: GLASS FABRICATED MATERIALS
B: PURCHASE ORDER
CMSX-4 SINGLE CRYSTAL (SX) AND POLYCRYSTALINE (EQ) SLABS
9515: PLATE, SHEET, STRIP, FOIL, AND LEAF
PO Purchase Order
MOD #1 TO ADD FUNDS FOR THE CRYSTAL CAST INGOT SINGLE CRYSTAL CAST INGOT ALLOY MANUFACTURE - MOLD
9535: PLATE, SHEET, STRIP, AND FOIL; NONFERROUS BASE METAL
PO Purchase Order
NPN RENE N5 SUPERALLOY BARS
9510: BARS AND RODS
PO Purchase Order
MOLD FOR PROTOTYPE PRELOAD DEVICES.
9535: PLATE, SHEET, STRIP, AND FOIL; NONFERROUS BASE METAL
PO Purchase Order
MOD #1 TO ADD FUNDS FOR THE CRYSTAL CAST INGOT SINGLE CRYSTAL CAST INGOT ALLOY MANUFACTURE - MOLD
9535: PLATE, SHEET, STRIP, AND FOIL; NONFERROUS BASE METAL
PO Purchase Order
MOLD FOR PROTOTYPE PRELOAD DEVICES.
9535: PLATE, SHEET, STRIP, AND FOIL; NONFERROUS BASE METAL
PO Purchase Order
SINGLE CRYSTAL CAST INGOT ALLOY MANUFACTURE - MOLD
9535: PLATE, SHEET, STRIP, AND FOIL; NONFERROUS BASE METAL
PO Purchase Order
MOD 1 TO ADD QUOTE # AND GE AUTHORIZATION LETTER SUPPERALLOY SLABS NPN 5.5" X 2.25" X .67"
9515: PLATE, SHEET, STRIP, FOIL, AND LEAF
PO Purchase Order
SUPPERALLOY SLABS NPN 5.5" X 2.25" X .67"
9515: PLATE, SHEET, STRIP, FOIL, AND LEAF
PO Purchase Order
ALLOY SLABS
9530: BARS AND RODS, NONFERROUS BASE METAL
PO Purchase Order
SINGLE CRYSTAL LDS - 1501 MOLD
6850: MISCELLANEOUS CHEMICAL SPECIALTIES
PO Purchase Order
SINGLE CRYSTAL LDS - 1501 MOLD
6850: MISCELLANEOUS CHEMICAL SPECIALTIES
PO Purchase Order
SAP PURCHASE REQUISITION: 4200259057
6640: LABORATORY EQUIPMENT AND SUPPLIES
PO Purchase Order
SAP PURCHASE REQUISITION: 4200259057. THIS PROCUREMENT IS FOR SINGLE CRYSTAL SUPERALLOY SLAB CASTINGS MADE OF SIX NEW SUPERALLOY COMPOSITIONS. AFTER DIRECTIONAL SOLIDIFICATION, THE SINGLE CRYSTAL CASTINGS SHALL ALL BE HEAT TREATED TOGETHER IN A SINGLE BATCH HEAT TREAT LOAD ACCORDING TO THE PARAMETERS PROVIDED IN THE STATEMENT OF WORK. THE RESULTS GENERATED ON PRIOR ALLOYS HELPED DESIGN IMPROVED, OPTIMAL ALLOYS FOR TURBINE BLADE APPLICATIONS. THE QUALITY AND MECHANICAL PROPERTIES OF ADVANCED SUPERALLOYS ARE HIGHLY SENSITIVE TO THE PROCESS AND HANDLING TECHNIQUES EMPLOYED DURING CASTING BY A VENDOR. THIS IS ESPECIALLY TRUE FOR SINGLE CRYSTAL SUPERALLOY AIRFOIL MATERIALS, WHERE SINGLE CRYSTALS ARE GROWN USING A DIRECTIONAL SOLIDIFICATION PROCESS. THE HEAT TRANSFER CHARACTERISTICS OF THE PROPRIETARY CASTING EQUIPMENT AND ITS ENVIRONMENT DURING THE DIRECTIONAL SOLIDIFICATION PROCESS INVARIABLY INDUCE LOCALIZED, DENDRITIC SEGREGATION IN COMPOSITION AND MICROSTRUCTURE OF A SINGLE CRYSTAL CASTING. THIS SEGREGATION HAS SIGNIFICANT EFFECTS ON IMPORTANT MECHANICAL PROPERTIES SUCH AS CREEP RESISTANCE, AS WELL AS MICROSTRUCTURAL PHASE STABILITY. AFTER SOLIDIFICATION, HEAT TREATMENTS ARE PERFORMED TO REDUCE SOME OF THE SEGREGATION IN CHEMISTRY AND TO REFINE THE PRECIPITATE MICROSTRUCTURE. THE HEAT TREATMENT EFFECTS ON THE CASTING MATERIAL ARE AGAIN SENSITIVE TO THE PROPRIETARY DESIGN AND CHARACTERISTICS OF THE FURNACES AND COOLING SYSTEMS USED IN THESE HEAT TREATMENTS. . THE UEET ($1M) AND SUBSONICS FIXED WING AIRFOIL PROJECTS HAVE BEEN CONDUCTING COMPREHENSIVE INVESTIGATIONS OF THE EFFECTS OF EXPERIMENTAL COMPOSITIONS ON CREEP AND OXIDATION RESISTANCE, AS WELL AS PHASE STABILITY. IN THIS WORK, THE UNIQUE PROPRIETARY EQUIPMENT AND PROCEDURES TO CONSISTENTLY CAST AND HEAT TREAT SINGLE CRYSTAL AIRFOIL MATERIALS TO OUR SPECIFIC COMPOSITIONS AND SPECIFICATIONS. GRC HAS SPENT OVER THE LAST SIX YEARS OVER $1M MEASURING THE EFFECTS OF COMPOSITION ON AIRFOIL PROPERTIES USING CREEP TESTING, ANALYTICAL SCIENCE, METALLOGRAPHIC, AND FRACTOGRAPHIC EVALUATIONS ON APPROXIMATELY 15 DIFFERENT ALLOY COMPOSITIONS. THE RESULTS REPRESENT A COMPREHENSIVE DATABASE ON SINGLE CRYSTAL AIRFOIL ALLOYS, ALL BASELINED ON THE CASTING AND HEAT TREATING OPERATIONS PERFORMED. GRC WOULD NEED TO REPEAT A SUBSTANTIAL PORTION OF THE $1M ALREADY INVESTED IN ORDER TO ENSURE COMPATIBILITY WITH ANY NEW VENDOR. GRC CAN NOT FORCE THE COMPANY TO RELEASE ALL INFORMATION ON THESE PROPRIETARY OPERATIONS. THE TESTING AND EVALUATION OF MATERIAL FROM AN ALTERNATE VENDOR WOULD EVEN THEN STILL BE VERY DISADVANTAGEOUS AND RISKY TO THE SUCCESS OF THIS PROGRAM, BECAUSE THE SEPARATION OF DIFFERENCES IN TEST RESULTS DUE TO THE VENDOR FROM THOSE DUE TO THE MATERIAL COMPOSITION AND PROCESSING PROPERTIES WOULD BE VERY DIFFICULT, IF NOT IMPOSSIBLE. THE PROGRAM CANNOT INCUR THE RESULTING CONSUMPTION OF ADDITIONAL FUNDS AND SCHEDULE FOR THIS CONTINGENCY.
6640: LABORATORY EQUIPMENT AND SUPPLIES
PO Purchase Order
SAP PURCHASE REQUISITION: 4200259057. THIS PROCUREMENT IS FOR SINGLE CRYSTAL SUPERALLOY SLAB CASTINGS MADE OF SIX NEW SUPERALLOY COMPOSITIONS. AFTER DIRECTIONAL SOLIDIFICATION, THE SINGLE CRYSTAL CASTINGS SHALL ALL BE HEAT TREATED TOGETHER IN A SINGLE BATCH HEAT TREAT LOAD ACCORDING TO THE PARAMETERS PROVIDED IN THE STATEMENT OF WORK. THE RESULTS GENERATED ON PRIOR ALLOYS HELPED DESIGN IMPROVED, OPTIMAL ALLOYS FOR TURBINE BLADE APPLICATIONS. THE QUALITY AND MECHANICAL PROPERTIES OF ADVANCED SUPERALLOYS ARE HIGHLY SENSITIVE TO THE PROCESS AND HANDLING TECHNIQUES EMPLOYED DURING CASTING BY A VENDOR. THIS IS ESPECIALLY TRUE FOR SINGLE CRYSTAL SUPERALLOY AIRFOIL MATERIALS, WHERE SINGLE CRYSTALS ARE GROWN USING A DIRECTIONAL SOLIDIFICATION PROCESS. THE HEAT TRANSFER CHARACTERISTICS OF THE PROPRIETARY CASTING EQUIPMENT AND ITS ENVIRONMENT DURING THE DIRECTIONAL SOLIDIFICATION PROCESS INVARIABLY INDUCE LOCALIZED, DENDRITIC SEGREGATION IN COMPOSITION AND MICROSTRUCTURE OF A SINGLE CRYSTAL CASTING. THIS SEGREGATION HAS SIGNIFICANT EFFECTS ON IMPORTANT MECHANICAL PROPERTIES SUCH AS CREEP RESISTANCE, AS WELL AS MICROSTRUCTURAL PHASE STABILITY. AFTER SOLIDIFICATION, HEAT TREATMENTS ARE PERFORMED TO REDUCE SOME OF THE SEGREGATION IN CHEMISTRY AND TO REFINE THE PRECIPITATE MICROSTRUCTURE. THE HEAT TREATMENT EFFECTS ON THE CASTING MATERIAL ARE AGAIN SENSITIVE TO THE PROPRIETARY DESIGN AND CHARACTERISTICS OF THE FURNACES AND COOLING SYSTEMS USED IN THESE HEAT TREATMENTS. . THE UEET ($1M) AND SUBSONICS FIXED WING AIRFOIL PROJECTS HAVE BEEN CONDUCTING COMPREHENSIVE INVESTIGATIONS OF THE EFFECTS OF EXPERIMENTAL COMPOSITIONS ON CREEP AND OXIDATION RESISTANCE, AS WELL AS PHASE STABILITY. IN THIS WORK, THE UNIQUE PROPRIETARY EQUIPMENT AND PROCEDURES TO CONSISTENTLY CAST AND HEAT TREAT SINGLE CRYSTAL AIRFOIL MATERIALS TO OUR SPECIFIC COMPOSITIONS AND SPECIFICATIONS. GRC HAS SPENT OVER THE LAST SIX YEARS OVER $1M MEASURING THE EFFECTS OF COMPOSITION ON AIRFOIL PROPERTIES USING CREEP TESTING, ANALYTICAL SCIENCE, METALLOGRAPHIC, AND FRACTOGRAPHIC EVALUATIONS ON APPROXIMATELY 15 DIFFERENT ALLOY COMPOSITIONS. THE RESULTS REPRESENT A COMPREHENSIVE DATABASE ON SINGLE CRYSTAL AIRFOIL ALLOYS, ALL BASELINED ON THE CASTING AND HEAT TREATING OPERATIONS PERFORMED. GRC WOULD NEED TO REPEAT A SUBSTANTIAL PORTION OF THE $1M ALREADY INVESTED IN ORDER TO ENSURE COMPATIBILITY WITH ANY NEW VENDOR. GRC CAN NOT FORCE THE COMPANY TO RELEASE ALL INFORMATION ON THESE PROPRIETARY OPERATIONS. THE TESTING AND EVALUATION OF MATERIAL FROM AN ALTERNATE VENDOR WOULD EVEN THEN STILL BE VERY DISADVANTAGEOUS AND RISKY TO THE SUCCESS OF THIS PROGRAM, BECAUSE THE SEPARATION OF DIFFERENCES IN TEST RESULTS DUE TO THE VENDOR FROM THOSE DUE TO THE MATERIAL COMPOSITION AND PROCESSING PROPERTIES WOULD BE VERY DIFFICULT, IF NOT IMPOSSIBLE. THE PROGRAM CANNOT INCUR THE RESULTING CONSUMPTION OF ADDITIONAL FUNDS AND SCHEDULE FOR THIS CONTINGENCY.
6640: LABORATORY EQUIPMENT AND SUPPLIES
PO Purchase Order
MOLDS OF PLATES AND BARS
1680: MISCL AIRCRAFT ACCESSORIES COMPS
PO Purchase Order
NPN N5 ALLOY BARS 1.02"X5"
6850: MISCELLANEOUS CHEMICAL SPECIALTIES
PO Purchase Order
ALLOY METAL BARS
2995: MISC ENGINE ACCESSORIES - AIRCRAFT
PO Purchase Order
SINGLE CRYSTAL CASTINGS OF NICKEL-BASE SUPERALLOY MATERIAL. SAP PURCHASE REQUISITION: 4200198339
9530: BARS & RODS NONFERROUS BASE METAL
PO Purchase Order
CMSX-4 + Y SUPER ALLOY SAP PURCHASE REQUISITION: 4200196243
9530: BARS & RODS NONFERROUS BASE METAL
PO Purchase Order
PLATES, BARS OF CMSX-486 ALLOY
9530: BARS & RODS NONFERROUS BASE METAL
PO Purchase Order
MASTER MELTS, SLAB MOLDS AND HEAT TREATMENT
9650: NONFERROUS BASE METAL REFINERY
PO Purchase Order
SLABS, BARS OF CMSX-486+ ALLOY
9530: BARS & RODS NONFERROUS BASE METAL
PO Purchase Order
ALLOY LONG BARS - N5 & IN738LC
2995: MISC ENGINE ACCESSORIES - AIRCRAFT
PO Purchase Order
SINGLE CRYSTAL CASTINGS OF NICKEL-BASE SUPERALLOY MATERIAL. SAP PURCHASE REQUISITION: 4200198339
9530: BARS & RODS NONFERROUS BASE METAL
PO Purchase Order
CMSX-4 + Y SUPER ALLOY SAP PURCHASE REQUISITION: 4200196243
9530: BARS & RODS NONFERROUS BASE METAL
PO Purchase Order
MASTER MELTS, SLAB MOLDS AND HEAT TREATMENT
9650: NONFERROUS BASE METAL REFINERY
PO Purchase Order
SUPERALLOY BARS
9510: BARS AND RODS
PO Purchase Order
N5 SLABS GE SPEC C50TF87 CLASS C
PO Purchase Order
6080: FIBER OPTIC KITS AND SETS
PO Purchase Order
9999: MISCELLANEOUS ITEMS
FSG | FSC | NSN | Part Number | Name | |
| 59 | 5961 | 5961-00-031-3645 | 2N3773 | TRANSISTOR Alternate References: , 000313645 |
| 28 | 2835 | 2835-01-208-7063 | 3-110-005-43 | NOZZLE,TURBINE,NONAIRCRAFT GAS TURBINE ENGINE CANCELLED Alternate References: , 012087063 |