H-Airframe Benefits for Constructing Quad- Rotor Unmanned Helicopters
Petar Getsov, Svetoslav Zabunov, Garo Mardirossian
Abstract
Petar Getsov, Svetoslav Zabunov, Garo Mardirossian
Abstract
The H-airframe also called fuselage-airframe is a quad-rotor airframe structure that exhibits a number of benefits over the classical four-rotor helicopter airframes, but it is still underestimated and not widespread among designers. The current paper aims at disclosing these benefits and comparing the H-airframe against most well-known airframes used in the modern quad-rotor unmanned helicopters. Special attention is drawn to the dynamical characteristics of the H-airframe and how unmanned helicopters based on this airframe structure excel the standard quad-rotor airframes in mechanical rigidity, efficiency and maneuverability.
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The H-airframe also called fuselage-airframe is a quad-rotor airframe structure that exhibits a number of benefits over the classical four-rotor helicopter airframes, but it is still underestimated and not widespread among designers. The current paper aims at disclosing these benefits and comparing the H-airframe against most well-known airframes used in the modern quad-rotor unmanned helicopters. Special attention is drawn to the dynamical characteristics of the H-airframe and how unmanned helicopters based on this airframe structure excel the standard quad-rotor airframes in mechanical rigidity, efficiency and maneuverability.
Key concepts: Airframe, Fuselage, Aerospace engineering, Engineering, Rotor (electric), Aeronautics, Helicopter rotor, Mechanical engineering