Capabilities & Equipment Research Projects Partnerships
Automated Manufacturing
- Automated Fiber Placement (AFP) and Automated Tape Laying (ATL) for thermoset, thermoplastic,
CMC, and dry fiber material systems.
- Electroimpact System 1 (翹 and 翻 AFP with Laser| 6, 9, and 12 ATL) 36 X-Axis and 15,000 lb Rotator
- Electroimpact System 2 (翹 and 翻 AFP with Variable Spot Size Laser) 72 X-Axis, 30,000 lb Rotator, and Dual-Axis Rotator
- Coriolis System (翹 AFP) 26 X-Axis
- Mikrosam Dual Robot System (翹 AFP & 2 ATL) for Tool-less Manufacturing 30 X-Axis and Filament Winding
- Laser and Humm3 heating options for thermoplastic materials
- Integrated 6 x 20-feet Vacuum Table and Rotators for AFP
- Mikrosam Slitter-Rewinder Machine with In-Process Laser Inspection System
- Fiber Patch Placement (FPP) Additive 3D Fiber Layup Technology for Complex Composite Parts
- KraussMaffei 450 Ton Spin-Form with Dual 1400 Injection Units and Rotary Turn Table
- Integrated Polyurethane ColorForm and High-Pressure Metering Systems
- Integrated FiberForm IR Oven
- ENGEL V-DUO 1900 Ton Industrial Press with Thermoplastic Capabilities
- Integrated Robot, (IR) Oven, Injection Molding Unit, and HP-RTM System
- Electroimpact Scalable Robotic Additive Manufacturing (SCRAM)
- Additive (Polymer and Metals), Subtractive, and Thermoplastic AFP
- 5 Dia. Vertical Rotator & 5,000 lb Horizontal Rotator (7 Dia. & 16 Build Volume)
- 5 x 13 Heated Build Table and 27 X-Axis
- Automated Thermoplastic Welding with Closed-Loop Controls and In-Process Inspections
- Induction, Resistance, and Ultrasonic Welding
- Autoclaves
- 13 x 26-feet with 800 deg-F / 200 psi Capability
- Integrated Wireless Temperature Sensors and Rheometer for Material State Monitoring
High-Fidelity Inspections
- Dual Tube Dual Detector NSI X7000 X-Ray CT System
- Micro-focus (up to 5繕m resolution) & Mini-focus X-ray Tubes; X-ray Energies from 10kV- 450Kv; Flat Panel Detector & Linear Diode Array Detection Technology
- In-Situ XCT Scanning with Load Fixture, Extensometer, and DIC
- Capable of scanning large components up to 60 in diameter x 60 in tall nominal scan envelope
- ZEISS Xradia 520 Versa Submicron 3D X-ray CT System
- 160kV high-energy microfocus X-ray source & staging
- Ultrasonic (MAUS): Pulse Echo testing, MIA Testing, Resonance Testing, Pitch Catch, Phased Array
- Pulse Thermography
- Shearography
- Acoustic Emission (16 Channel System)
- GOM and Vic 3D Digital Image Correlation Systems (Microscopic 5MP to 29 MP)
Structural Test & Evaluations
- Electrodynamic Test Systems (670 lbf Max Capability at 200Hz)
- Permanent Magnet Shakers for Modal & Structural Analysis
- Planar Biaxial Testing (Axial: 55-kip / Torsion: 簣10,000 in-lbf)
- Large-Scale Test Rig (6 x 38 x 16 test envelope)
- Over 40 MTS Structural Actuators (Range: 10 110-kip)
- MTS AeroPro Software and MTS FlexDAC 20 Data Acquisition System (40 Control Channels and 400+ Strain Channels)
- DMG MORI 5-Axis High-Precision Machining
- Ultrasonic 85 - Ultrasonic Superimposition of the Tool Rotation
- DMU 340 Gantry
Computer-Aided Simulations & Analysis
- High-Performance Computing
- Manufacturing Simulations and Process Modeling
- Residual Stress and Failure Analysis
Training
- Composite Hands-on Training (Manufacturing, Inspections, Repair, and Testing)
- Metals Hands-on Training
- Ultrasonic 5-Axis CNC (DMG Mori Ultrasonic 85)
- AFRL Advanced Material Characterization and Structural Certification (AMCSC)
- AFRL Modeling for Affordable Sustainable Composites (MASC)
- AFRL/Boeing Composite Airframe Life Extension (CALE)
- AFRL/Lockheed Quantification of Aging from Long-term Exposure (QALE)
- AFRL/Northrop Fail-Safe Technologies for Bonded Unitized Composite Structures (FASTBUCS)
- Army Combat Capabilities Development Command Aviation & Missile Center (CCDC) Rotorcraft Inspection and Repair, Composites Training, and Adhesive Characterization
- FAA Joint Advanced Materials & Structures (JAMS)
- Certification Efficiency and Safety, Damage Tolerance of Composites, Inspection and Teardown of Aged In-Service Bonded Repairs, Structural joints (Adhesive and Thermoplastic Welds), and Sandwich Damage Growth
- NASA Advanced Composite Consortium (ACC)
- NASA High Rate Composite Manufacturing (HiCAM)
- Navy Process Simulation Models and Noninvasive In-Situ Material State Monitoring for Detection of Process-Induced Damages in Polymer Composites
- Navy Fatigue Damage Initiation and Progression of Composites and Bonded Joints under Variable Amplitude Cyclic Loading
- Navy Electrodeposition of Nanocrystalline Coating on Additive Manufactured Parts for Enhanced Structural Performance
- NTSB Composite Aircraft Crash Investigations
CONSORTIUM MEMBERSHIPS AND RESEARCH PARTNERSHIPS
- Composite Materials Handbook (CMH-17)
- FAA Joint Advanced Materials & Structures (JAMS)
- Kansas Aviation Research & Technology (KART)
- NASA Advanced Composite Consortium (ACC)
- NASA High-Rate Composite Manufacturing (HiCAM)
- Navy Composites Manufacturing Technology Consortium (CMTC) - The Composite Consortium