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Published byJemima Baker Modified over 9 years ago
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ITU LCH Structural Design Criteria and Structure Analysis March 19, 2003
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Outline General Strength Requirements Load Determination Structure Analysis
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General Strength Requirements Loads Factor of Safety Strength and Deformation Proof of Structure Design limitations Miscellaneous Structure Strength Requirements FAR 27
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Load Determination External Loads –Flight Loads –Ground Loads Inertia Loads Component Loads
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Load Determination Flight Loads –Limit Maneuvering Load Factor Maximum 3.5 Minimum -1.0 load factor envelope
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Load Determination Flight Loads –Symmetrical Pull-ups and Rolling Pull-outs –Gust Loads –Yawing Conditions
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Load Determination Flight Loads –Load Calculation Flight Lab Input Parameters Results Analysis
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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
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Load Determination Ground Loads –Landing load conditions: (landing gear with skids) Level landing with Vertical reactions only Level landing with Drag load Level landing with side Load One skid landing Special conditions
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Load Determination Ground Loads –Ground Handing Hoisting Mooring Jacking Towing –Emergency Landing conditions
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Load Determination Inertia Loads –Weights and its distribution –Equilibrium equations –Translational and rotational load factor –Distributed inertia loads
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Load Determination Component Loads –Main rotor loads Load conditions –Flight load conditions –Ground flapping, ground gust –Torque Load calculation
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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
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Load Determination Component Loads –Control System Loads Limit pilot forces and torques –Tail rotor loads Flight loads Ground gust –Empennage loads –Transmission system
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Structure Analysis Rotors Fuselage (including rotor pylon Landing gear, Empennage) Control system Transmission system
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