Aircraft with emergency floatation system

• Main Author: JOHANN RAPPL
• Format: Patent
• Language: Chinese; English
• Published: 09.03.2018
• Subjects: AEROPLANES; AIRCRAFT; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT; AVIATION; COSMONAUTICS; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; HELICOPTERS; PARACHUTES; PERFORMING OPERATIONS; TRANSPORTING

The invention is related to an aircraft 1 with an emergency floatation system 7, the emergency floatation system 7 being activated upon an emergency landing of the aircraft 1 on water, for preventingat least sinking of the aircraft 1, characterized in that a capsizing avoidance buoyancy system 8 is provided, the capsizing avoidance buoyancy system 8 being activated if predetermined activation criteria are satisfied and only after activation of the emergency floatation system 7 upon an emergency landing of the aircraft 1 on water, for preventing at least capsizing of the aircraft. 本发明涉及种具有紧急漂浮系统7的飞行器1，所述紧急漂浮系统7在所述飞行器1紧急降落在水上之际被激活，以用于防止至少所述飞行器1的沉没，其特征在于，提供了倾覆避免浮力系统8，所述倾覆避免浮力系统8在预定激活准则被满足且只有在所述飞行器1紧急降落在水上之际所述紧急漂浮系统7激活之后才被激活，以用于防止至少所述飞行器的倾覆。