Aero Structures

The Company provides custom engineering solutions for Aircraft Structures for OEM and Tier 1 Suppliers. The structures analysis and 3D modeling work is quoted for a fixed fee and delivery date. The company will provide the best engineering solutions at a very competitive price in North America. These are stand alone applications developed by the company and are available for sale :(Hiring Applications Engineers for Sales / 10% commission!) 1. Section Analysis 2. Beam Analysis 3. Buckling Analyis 4. Crippling Analysis 5. Composite Analysis 6. Composite Plate Buckling Analysis 7. Composite Skin / Stringer Anaysis with Buckling and Crippling The software can be used for sizing of aircraft composite laminate panels, wing skins, composite stringers and fuselage panels. The software is very user friendly and only requires material data, loads and ply orientation as input. It will calculate the critical ply failure, the margins and the mode of failure.It can also be used for residual strength estimation for damage tolerance analysis. What the company does Finite Element Modeling in PATRAN PATRAN COMMAND LANGUAGE PCL Aircraft Stress Analysis Structural Loads input in Patran Material Properties Database (Metallic & Composite ) Nastran Solutions SOL 101, 103, 105, 106 SOL 200 ( Design Study Optimization ) Verification of Nastran solutions with hand calculations for FAA certification Preparation of Stress Reports for FAA certification Custom PCL Applications for increasing productivity in Patran (Patran Command Language Applications) Excel / Visual Basic Applications for structural analysis Fatigue and Damage Tolerance for Commercial Aircraft Structures MRB Stress Support for manufacturing Aircraft Structural Analysis Landing Gear Analysis Specialties: The Company provides custom PCL code for client applications, which appear as pull down menus (Graphic User Interface) in client's Patran window.