Cold Spray Materials Manufacturing Technology Research

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Cold Spray Materials Manufacturing Technology Research Blake Barnett Materials Engineer, Advanced Materials & Processes Team Blake.d.Barnett.civ@mail.mil

Outline The Case for Cold Spray: Nonthermal Additive Manufacturing ARL Center for Cold Spray Research & Technology Background 1 st Generation Cold Spray Repairs Beyond Nonstructural Repair Holistic Modeling Approach and Results Modeling-Enabled Performance and Applications Future AM Efforts and Capabilities

Nonthermal Additive Consolidation Traditional Process Casting, Welding Sintering Extrusion Forging Additive Process SLM, EBM, Wire-Arc Additive Manufacturing (WAAM) Powder Binder Jet, Single-Pass Jetting Fused Deposition Modeling Strain-Mediated Additive Manufacturing Architected Feedstocks Solid-State Deformation Processing Retained & Refined Microstructures for Enhanced Net & Near-Net Shape Materials

Cold Spray Overview ARL is Recognized as International Leader in Cold Spray Technology Modeling & Simulation Powder Development Cold Spray Materials Characterization Advanced Processing Applications Development Equipment (VRC Gen III-JOA) Specifications, Stds. & Training Transition & Implementation

TRL 7 TRL 6 TRL 5 TRL 4 TRL 3 TRL 2 Cold Spray Technology Evolution VISION: Non-structural Repair Structural Repair Near-net Parts Industry PRODUCTION SCALE-UP F & Army RIFTRL 9 UH-60 Sump Repair MEO B1671 RDECOM TMR TRL 8 OSD & Army Mantech NAVAIR AFRL Navy-TIPS ESTCP DLA SBIR SERDP Flexible Robot Environment Near Net Shape Spray Form Components CHARACTERIZATION & TESTING POWDER SYNTHESIS First Approved Army-Navy & Air Force Applications Powder UTS = to wrought 60 40 20 0 TD-63 Actuator B-1 FEB Panels & Hydro PROCESS DEVELOPMENT UTS, ksi YS, ksi %EL annealed T4-T451 T6-T651 cold sprayed MODELING & SIMULATION ARL,ONR TRL 1

Cold Spray Background Main Gas Stagnation Pressure 0.5-5 MPa Gas Temperature 0-1000ºC Main Gas Flow Rate 30-200 m 3 /hr Powder Feed Rate 1 to 15 kg/hr Particle Velocity 300-1500 m/sec. Particle Size 1-50um diameter

Cold Spray Demonstration

UH-60 Sump - Magnesium Housing Corrosion Sites UH-60 Sump UH-60 Sump Before After ROI for the UH-60 Sump Unit Cost: $11K Annual Demand Rate: 85 Repair Cost: $880 Investment: $60K Annual Savings $860K Official Approval Documents and Commitment 1. Maintenance Engineering Order (MEO) T7631 UH-60 Sump Repair Army Aviation & Missile Research, Development & Engineering Center (AMRDEC) Program Office UH-60 Blackhawk Corpus Christi Army Depot-SAFR Program Office 2. Overhaul Repair Instruction (ORI) SS8491 UH-60 Sump Repair Sikorsky Aircraft Company-Technology Integration

Process Model for Materials Development Holistic Approach to Cold Spray AM Integrated Computational Materials Engineering (ICME) Powder Production Powder Processing Powder Microchemistry Degassing Powder Microstructure Heat treating Process Production Processing Milling Output parameters from Powder Production & Powder Blending Pre-Processing models Particle are & grain used as input to the Particle Impact Model size Predictive models to complement experimental approach Process Parameters Gas temperature Process Cold Spray Process Gas pressure Gas Parameters composition Particle feeder temp. User-input Laser assistance Parameters Particle Impact Particle Deformation Heat generation Impact Recrystallization Post- Processing Machining Heat treating Forming Surface treating Bulk Material Prediction of Properties 9

Technical Results-CS Al Alloys Alloy Parameters Specimen ID HRB %IACS Press. Temp UTS MPa (ksi) 6061 20 bar 400 C CS-12-275 31.0 44.03 239 (34.6) 7 6061 25 bar 450 C CS-13-096 40.4 41.5 310 (45.0) 5 %El 2024 25 bar 400 C CS-14-150 64.6 30.18 392 (56.8) 5.8 2024 30 bar 500 C CS-14-152 57.3 31.96 346 (50.2) 10.9 7075 25 bar 400 C CS-14-128 65.2 31.08 387 (56.2) 6.9 7075 25 bar 400 C CS-14-120 50.1 35.92 326 (47.3) 11.8 7075 30 bar 500 C CS-14-125 62.7 31.11 394 (57.2) 11.5 5056 20 bar 500 C CS-14-101 63 26.25 406 (58.9) 15.4

Fielded Applications of Cold Spray Fielded SH-60 Seahawk with Cold Spray Mg Repair Operating Since August, 2009-Australian Navy ARL/JSF/DSTO Collaboration Three Fielded Blackhawk Medvac Units with Cold Spray Al Repair Operating Since August, 2009 ARL/AMCOM/Ft. Hood Collaboration Fielded B-1 Bomber with Cold Spray Ti Repair Operating Since September 2009- Tinker AFB ARL/Tinker AFB/HF Webster Collaboration Two Expeditionary Fighting Vehicles with Cold Spray Mg Repair Fielded and Operating Since September, 2008 Power Transfer Module - PTM - 10 Magnesium Castings Transmission - 13 Magnesium Castings

Fielded Applications (Cont d)

Approved Cold Spray Repair Processes ARMY AH-64 Intermediate Gear Support ( EYAB: 12-153 top & outer land repair) UH-60 Sump (MEO T7631B MEO B1671 packing seal surface repair) MEO-B1718 T-700 Turbine Engine Front Frame FY15 UH-60 Intermediate Gearbox (MEO B1089 center, input, output housings) UH-60 Tail Rotor Gearbox (MEO B1090 center, input, output housings) UH-60 Accessory Gearbox (MEO B1091 cover and housing) UH-60 Input Module (MEO B1092 center, input, output housings) NAVY F/A-18E/F AMAD Main Housing (hydraulic pad restoration) F/A-18E/F AMAD Main Housing (gear failure repair) F/A-18E/F AMAD Hydraulic Gear Shaft seal surface repair) H-1 Mixer Gearbox (external chafing repair) AIR FORCE B-1 Forward Equipment Bay (FEB) Panels (ETAR) E12-00248 B-1 Hydraulic Tube Repair (ETAR) E09-00065 MOOG has been approved by Boeing, Sikorsky and Bell Helicopters as a Qualified Cold Spray Vendor

Cold Spray Additive Manufacturing Axisymmetric Near-Net Shape Components

Questions? ARL Installation Spring 2018