Aircraft

The invention provides an aircraft. The aircraft comprises a helium cabin, a load cabin, two direction steering engines, a landing support, at least two rotor boosters and a buoyancy adjusting device,the buoyancy adjusting device comprises a compressed air tank, a compressed helium tank, a gas compr...

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Bibliographic Details
Main Authors REN TIANYOU, TONG TIAN
Format Patent
LanguageChinese
English
Published 02.06.2020
Subjects
AIRCRAFT
AVIATION
COSMONAUTICS
LIGHTER-THAN AIR AIRCRAFT
PERFORMING OPERATIONS
TRANSPORTING
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Summary:The invention provides an aircraft. The aircraft comprises a helium cabin, a load cabin, two direction steering engines, a landing support, at least two rotor boosters and a buoyancy adjusting device,the buoyancy adjusting device comprises a compressed air tank, a compressed helium tank, a gas compression/turbine system and a controller. By applying the aircraft, the buoyancy of the aircraft canbe effectively adjusted in a large range at any stage (taking off, cruising and landing) of the flight of the aircraft. 本发明提供了一种飞行器。该飞行器包括：氦气舱、载荷舱、两个方向舵机、降落支撑、至少两个旋翼助推器和浮力调节装置；所述浮力调节装置包括：压缩空气罐、压缩氦气罐、气体压缩/透平系统和控制器。应用本发明可以在该飞行器飞行的任何阶段(起飞、巡航以及降落)有效地、大范围地调节该飞行器的浮力大小。
Bibliography:Application Number: CN201811423134