Tra i programmi più importanti a cui la LDP ha preso parte e che rappresentano oggi il nostro Know How si annotano:
Wing pylon drawings: outboard, inboard, and stub-pylon Internal Systems & Engine Cowling drawings Wing pylons structural verification in all flight conditions
Nacelle Structural analisys and flight certification of the Pratt & Withney PW6000 engine Nacelle for the Airbus A318
Structural Design (Metallic and Carbon Fibre Composite) of the complete fuselage including Kinematics of the canopy,Flight Control systems, Flight Deck instrumentation installation, Radome and Nose Landing Gear Doors Structural analysis and stress reports for the aforementioned
Studies and development for the following System installations:
Primary and secondary structure dimensioning and checks through hand-made calculations and Lockheed Martin tools (IDAT – beams, panels, bolts, fittings).
PAX FLOOR MAIN DECK
design, Stress and Fatigue Analysis, manufacturing drawings of the Pax Floor Main Deck structure of the A380 Aircraft from frame C38 to frame C45: floor beams, rails, crash links, trolley lift attachment;
Design of the secondary structure: supports for all aircraft equipments;
CARGO FLOOR MAIN DECK
Design, Stress and Fatigue Analysis manufacturing drawings of the Cargo Floor Deck structure of the A380 Aircraft from frame C38 to frame C45: cargo beam, main structures.
Design of the floor handling and transportation devices;
Flight Readiness and Certification analysis and reports of the Rolls-Royce Trent 900 engine nacelle and General Electric GP7200 for the Airbus A380; Structural verifications, static and fatigue, optimizations.
Initial Design of door structural main features: Frames, Beams, Skins, etc. Door FEM model;
Development of a specific post-processing software with Nastran interface, aimed at performing the detail stress analysis;
Detail analysis of the interface between door and fuselage;
Analysis preliminary reports using Airbus Methodology;
3D and 2D models and drawings of the MDCD integrated in VPM
Production support
Main Deck Cargo Door FEM (65000 elements) model;detail models
Detail analysis of the interfaces between door and fuselage;
Static, Fatigue and Damage Tolerance reports using Airbus Methodology;
Design and Production support: