GE Aircraft Engines Numerical Models...
Analysis Type: Finite Element Analysis
Applications: Numerical Analysis of Gas Turbines...
Engines Model:
Projects at TES:
- Complete Building of Thermal Models
- Update of Legacy Thermal Model to Current Standards
- Validation of Thermal Models to Test Engine Data
- Thermal Analysis of Engines under “Flight” Conditions
- Development of Custom GUI’s and Tools to Aid in Modeling
Model Details:
- Flow Modeling Including Primary and Secondary Flows
- Multi-mode Heat Transfer Including Convection, Radiation and Conduction
- Application of Deflection Modeling for Calculation of Critical Tolerances
- Standardized Techniques for Modeling of Structural Interfaces
Engine Components:
- High-Pressure Turbines
- Low Pressure Turbines
- High Pressure Compressors
- Internal Nozzles and Support Structures
Modeling Environment:
- State-of-the-Art CAE Thermal Software
- Custom Toolkits and GUI’s Developed at TES
- GE Developed Enhancements to Standard CAE Modeling Software
- Flexible/Customizable Operating Environment
Note: Due to proprietary restrictions illustrative examples are not available.
Flex Board
Hydrocarbon Sensor
GaAs Flip Chip
Engine Controller
Relay Box
Intake Manifold
Wall Mounted TO220
Populated PCB Modal
PWB Enclosure Modal
Plug-in Modules
Aircraft Engines