Aircraft

The invention relates to an aircraft, in particular an aircraft capable of vertical takeoff and landing, comprising a fuselage and a variable lift body defining an airfoil and movably attached to the fuselage wherein the variable lift body is pivotable about a first axis extending in a spanwise dire...

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Bibliographic Details
Main Authors MOBIUS ANDREAS, WYDER, MATT, BLATT KILIAN, SINES DE LA MAZZA JAVIER
Format Patent
LanguageChinese
English
Published 30.08.2022
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:The invention relates to an aircraft, in particular an aircraft capable of vertical takeoff and landing, comprising a fuselage and a variable lift body defining an airfoil and movably attached to the fuselage wherein the variable lift body is pivotable about a first axis extending in a spanwise direction; wherein the aircraft has a rotary actuator adapted to pivot the variable lift body relative to the fuselage and to be disposed within the airfoil portion. 本发明涉及一种飞行器，特别是能够垂直起飞和着陆的飞行器，该飞行器包括机身和可变升降本体，该可变升降本体限定翼型部并且可移动地附接到机身，其中，可变升降本体可围绕在翼展方向上延伸的第一轴线枢转；其中，该飞行器具有旋转作用器，该旋转作用器适于使可变升降本体相对于机身枢转并且布置在翼型部内。
Bibliography:Application Number: CN202210158453