Stress Analysis and Weight Optimization
Initial Sizing, Detailed Hand Calculations, Aircraft Finite Element Models, Fetailed FE Models, Stress Reports. We do it all from preliminary analysis to certification reports. Light and safe. We will keep an eye on manufacturability and complexity and deliver the best least weight, least cost, balanced solution.
We provide a basic loads engineering solution. Certification level loads for traditional part 23 aircraft configurations and preliminary loads work for advanced aircraft prototypes. Our knowledge of loads engineering plays an important part in our holistic approach to aircraft design and development.
Composite and metallic subassemblies, CNC machinings, weldments or sheet metal fabrications. CAD major sub-assembly work or drawing production to strict manufacturing deadlines. We know what is important to you to make sure you meet your scheduled milestones.
Mechanical Systems Design
We design and analyse moving structures – we develop all aspects of landing gear, flight controls and door mechanisms. From loads development to preliminary kinematic models, stress analysis, fatigue assessments, weight optimization, CAD models and detail drawings.
Composite M&P, Design and Analysis
Abbott Aerospace has had significant involvement in many composite aircraft development and modification programs.Glas fiber, carbon fiber, prepreg, wet laminate, infusion. We have taken multiple composite aircraft designs from initial layout to first flight.
We distribute our in-house authored engineering text book and spreadsheet methods globally and create company stress amnuals for international clients. We have specialist knowledge of NACA, NASA, ARC and other public domain resources. Abbott Aerospace has developed analysis methods for a global leader in the provision of online analysis solutions.