High-altitude flight device with vertical take-off and landing functions

A high-altitude flight device with vertical take-off and landing functions is characterized in that undercarriages are symmetrically and fixedly connected to the bottom of a case, engines are symmetrically arranged on the outer side of the middle of the case, propellers are connected onto the engine...

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Bibliographic Details
Main Author CHEN YUNGEN
Format Patent
LanguageChinese
English
Published 25.06.2014
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:A high-altitude flight device with vertical take-off and landing functions is characterized in that undercarriages are symmetrically and fixedly connected to the bottom of a case, engines are symmetrically arranged on the outer side of the middle of the case, propellers are connected onto the engines, the engines are connected onto the case through spindles, and two ends of each supporting rod are connected with the middle of each spindle and the case; two built-in engines are symmetrically arranged at the lower part of the case and connected with bevel gears II meshed with a bevel gear I, the bevel gear I is connected with a sun gear, four planet gears meshed with the sun gear are evenly arranged on the periphery of the sun gear and connected in the case through bearings, the four planet gears are meshed with annular teeth on the inner side of a wheel disc, the periphery of the wheel disc located outside the case is evenly connected with rotor wings, the upper surface of the wheel disc is closely attached to
Bibliography:Application Number: CN2014222712U