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ITU LCH Structural Design Criteria and Structure Analysis. March 19, 2003. Outline. General Strength Requirements Load Determination Structure Analysis. General Strength Requirements. Loads Factor of Safety Strength and Deformation Proof of Structure Design limitations
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ITU LCH Structural Design Criteria andStructure Analysis March 19, 2003
Outline • General Strength Requirements • Load Determination • Structure Analysis
General Strength Requirements • Loads • Factor of Safety • Strength and Deformation • Proof of Structure • Design limitations • Miscellaneous Structure Strength Requirements • FAR 27
Load Determination • External Loads • Flight Loads • Ground Loads • Inertia Loads • Component Loads
Load Determination • Flight Loads • Limit Maneuvering Load Factor • Maximum 3.5 • Minimum -1.0 • load factor envelope
Load Determination • Flight Loads • Symmetrical Pull-ups and Rolling Pull-outs • Gust Loads • Yawing Conditions
Load Determination • Flight Loads • Load Calculation • Flight Lab • Input Parameters • Results Analysis
Load Determination • Ground Loads • Landing Load factor • Energy absorption requirements • Limit drop height: 13 inches • Reserve energy drop height: 19.5 inches • With rotor lift • Determine the load factor • Software
Load Determination • Ground Loads • Landing load conditions: (landing gear with skids) • Level landing with Verticalreactions only • Level landing with Drag load • Level landing with side Load • One skid landing • Special conditions
Load Determination • Ground Loads • Ground Handing • Hoisting • Mooring • Jacking • Towing • Emergency Landing conditions
Load Determination • Inertia Loads • Weights and its distribution • Equilibrium equations • Translational and rotational load factor • Distributed inertia loads
Load Determination • Component Loads • Main rotor loads • Load conditions • Flight load conditions • Ground flapping, ground gust • Torque • Load calculation
Load Determination • Component Loads • Fuselage, landing gear, and rotor pylon structures • Load conditions • Flight load conditions • Landing Conditions • Ground Handing • Emergency Landing conditions • Load calculation
Load Determination • Component Loads • Control System Loads • Limit pilot forces and torques • Tail rotor loads • Flight loads • Ground gust • Empennage loads • Transmission system
Structure Analysis • Rotors • Fuselage (including rotor pylon Landing gear, Empennage) • Control system • Transmission system