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Hollowed-out lander for electric vertical take-off and landing aircraft
The hollowed-out lander for the electric vertical take-off and landing aircraft comprises a transport vehicle and a net weaving platform, the lower end of the net weaving platform is in bolted connection with a force bearing support, a lifting joint is installed at the rear end of the force bearing support, and a lifting supporting column is installed in the middle of the lifting joint; the lifting supporting column is composed of a plurality of standard knot components, a supporting column base is welded to the lower top end of the lifting supporting column, the force bearing support, the lifting joints, the standard knots and the lifting supporting column are all of hollowed-out steel beam structures, the net weaving platform and the force bearing support form a landing platform, and the landing platform can be separated from the lifting joints. According to the device, the height of the whole aircraft is increased or the time spent in the landing and hovering stage is shortened, so that the operation time of the aircraft in the stage with the fastest energy consumption rate is greatly shortened, the purpose of saving energy is successfully achieved, and the endurance mileage of the aircraft is also increased through the saved energy.
本发明公开了一种用于电动垂直起降飞行器的镂空着陆器,包括运输车和网织平台,所述网织平台下端螺栓连接有承力支架,所述承力支架后端安装设置有升降节,所述升降节中部安装设置有升降支柱,所述升降支柱由若干个标准节构件组成,所述升降支柱下顶端焊接有支柱底座,所述承力支架、升降节、标准节和升降支柱均为采用镂空钢梁结构,所述网织平台与承力支架构成着陆平台,所述陆平台可与升降节脱离。本发明通过该装置来抬升整个飞行器高度或者降低降落悬停阶段所花费的时间,从而使飞行器在能量消耗速率最快阶段的运行时间大大减少,成功实现了节省能量的目的,所节省的能量也提升了飞行器的续航里程。
Hollowed-out lander for electric vertical take-off and landing aircraft
The hollowed-out lander for the electric vertical take-off and landing aircraft comprises a transport vehicle and a net weaving platform, the lower end of the net weaving platform is in bolted connection with a force bearing support, a lifting joint is installed at the rear end of the force bearing support, and a lifting supporting column is installed in the middle of the lifting joint; the lifting supporting column is composed of a plurality of standard knot components, a supporting column base is welded to the lower top end of the lifting supporting column, the force bearing support, the lifting joints, the standard knots and the lifting supporting column are all of hollowed-out steel beam structures, the net weaving platform and the force bearing support form a landing platform, and the landing platform can be separated from the lifting joints. According to the device, the height of the whole aircraft is increased or the time spent in the landing and hovering stage is shortened, so that the operation time of the aircraft in the stage with the fastest energy consumption rate is greatly shortened, the purpose of saving energy is successfully achieved, and the endurance mileage of the aircraft is also increased through the saved energy.
本发明公开了一种用于电动垂直起降飞行器的镂空着陆器,包括运输车和网织平台,所述网织平台下端螺栓连接有承力支架,所述承力支架后端安装设置有升降节,所述升降节中部安装设置有升降支柱,所述升降支柱由若干个标准节构件组成,所述升降支柱下顶端焊接有支柱底座,所述承力支架、升降节、标准节和升降支柱均为采用镂空钢梁结构,所述网织平台与承力支架构成着陆平台,所述陆平台可与升降节脱离。本发明通过该装置来抬升整个飞行器高度或者降低降落悬停阶段所花费的时间,从而使飞行器在能量消耗速率最快阶段的运行时间大大减少,成功实现了节省能量的目的,所节省的能量也提升了飞行器的续航里程。
Hollowed-out lander for electric vertical take-off and landing aircraft
一种用于电动垂直起降飞行器的镂空着陆器
SUN SHUANG (Autor:in) / DING SHUO (Autor:in) / LIAO YU (Autor:in) / ZHAO ZIQING (Autor:in) / DAN MIN (Autor:in) / HU XIZHUO (Autor:in) / CHEN JIAXIN (Autor:in)
29.08.2023
Patent
Elektronische Ressource
Chinesisch
IPC:
E01F
ADDITIONAL WORK, SUCH AS EQUIPPING ROADS OR THE CONSTRUCTION OF PLATFORMS, HELICOPTER LANDING STAGES, SIGNS, SNOW FENCES, OR THE LIKE
,
Zusätzliche Baumaßnahmen, wie die Ausstattung von Straßen oder die bauliche Ausbildung von Bahnsteigen, Landeplätzen für Hubschrauber, Wegweisern, Schneezäunen oder dgl.
/
B64F
GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT
,
Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen
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