Ground effect removal device for attitude stabilization at the time of take-off and landing of small scale unmanned helicopters

The present invention relates to a ground effect removal device for stabilizing the posture of an unmanned aerial vehicle having a small rotor at the time of taking off and landing and, more specifically, to a ground effect removal device for stabilizing the posture of an unmanned aerial vehicle hav...

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Bibliographische Detailangaben
Hauptverfasser:	PARK, WON IK, CHANG, HYE MIN, YOU, JI SANG, CHU, JEUNG HO
Format:	Patent
Sprache:	eng ; kor
Schlagworte:	AIRCRAFT AVIATION BLASTING COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOWOF GASES OR LIQUIDS FLUID-PRESSURE ACTUATORS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HEATING HYDRAULICS OR PNEUMATICS IN GENERAL LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	The present invention relates to a ground effect removal device for stabilizing the posture of an unmanned aerial vehicle having a small rotor at the time of taking off and landing and, more specifically, to a ground effect removal device for stabilizing the posture of an unmanned aerial vehicle having a small rotor at the time of taking off and landing, which provides flying conditions, such as being located at a high altitude without a ground effect, to an unmanned aerial vehicle even if the unmanned aerial vehicle is close to the ground in order to allow the unmanned aerial vehicle to stably take off and land even under a space restriction. The ground effect removal device for stabilizing the posture of an unmanned aerial vehicle having a small rotor at the time of taking off and landing comprises an air flow inducing device which has an air flow inducing part for inducing air, an installation part where the air flow inducing part is installed, and a support part installed in the end of the installation part. 제안기술은 소형 회전익 무인 비행체의 이착륙 시 자세 안정화를 위한 지면효과 제거 장치에 관한 발명으로, 더욱 상세하게는 비행체가 공간상의 제약 하에서도 보다 안정적으로 이착륙이 가능하도록 비행체가 지면에 가까이 있으면서도 지면효과가 없는 높은 고도에 있는 것과 같은 비행조건을 만들어주는 소형 회전익 무인 비행체의 이착륙 시 자세 안정화를 위한 지면효과 제거 장치에 관한 발명이다.