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    • 1. 发明申请
    • MODULARIZED AIRPLANE STRUCTURES AND METHODS
    • 模块化飞机结构和方法
    • WO2009148670A3
    • 2010-03-18
    • PCT/US2009036405
    • 2009-03-06
    • ZHAO JIE
    • ZHAO JIE
    • B64C1/00A63H27/18B64C13/20B64C13/24
    • A63H27/02A63H29/22
    • A controllable flying airplane includes two separably interconnected modules: a plane module, incorporating substantial airplane style characteristics, comprising a fuselage and a fin mounted thereon with a movable control surface, a component module having a support structure and a set of components mounted thereon including a servo controlled by a control device facilitating controlled flight. At least one pair of mutually magnetically attractive connectors oppositely affixed on said two module members provide means for inter-modular structural connection. A linkage means includes two mutually magnetically attractive linkage portions separably connectable to form a linkage assembly linking said servo and said control surface. The structural connection and the control linkage means disclosed facilitate substantially effortless inter-modular connection to form a controllable airplane as well as nondestructive inter-modular disconnection. Multiple plane modules of differing styles and aerodynamic specifications can be made interconnectable with one component module to form differing airplanes, sharing essential components, for differing applications.
    • 一种可控飞行飞机包括两个可分离地相互连接的模块:具有大量飞机样式特征的平面模块,包括机身和安装在其上的具有可移动控制表面的鳍片,具有支撑结构和安装在其上的一组部件的部件模块, 通过控制装置进行伺服控制,以便控制飞行。 相对地固定在所述两个模块构件上的至少一对相互吸引磁性的连接器提供用于模块间结构连接的装置。 连杆装置包括两个彼此磁性吸引的连杆部分,所述连杆部分可分离地连接以形成连接所述伺服器和所述控制表面的连杆组件。 所公开的结构连接和控制连接装置有利于基本上毫不费力的模块间连接以形成可控飞机以及非破坏性的模块间断开。 具有不同风格和空气动力学规格的多平面模块可与一个组件模块互连以形成不同的飞机,共享不同的应用所需的基本组件。
    • 2. 发明申请
    • MODULARIZED AIRPLANE STRUCTURES AND METHODS
    • 模块化飞机结构与方法
    • WO2009148670A9
    • 2010-01-28
    • PCT/US2009036405
    • 2009-03-06
    • ZHAO JIE
    • ZHAO JIE
    • B64C1/00A63H27/18B64C13/20B64C13/24
    • A63H27/02A63H29/22
    • A controllable flying airplane includes two separably interconnected modules: a plane module, incorporating substantial airplane style characteristics, comprising a fuselage and a fin mounted thereon with a movable control surface, a component module having a support structure and a set of components mounted thereon including a servo controlled by a control device facilitating controlled flight. At least one pair of mutually magnetically attractive connectors oppositely affixed on said two module members provide means for inter-modular structural connection. A linkage means includes two mutually magnetically attractive linkage portions separably connectable to form a linkage assembly linking said servo and said control surface. The structural connection and the control linkage means disclosed facilitate substantially effortless inter-modular connection to form a controllable airplane as well as nondestructive inter-modular disconnection. Multiple plane modules of differing styles and aerodynamic specifications can be made interconnectable with one component module to form differing airplanes, sharing essential components, for differing applications.
    • 可控制的飞行飞机包括两个可分离地互连的模块:平面模块,其包含实质的飞机风格特征,包括机身和安装在其上的翅片,具有可移动控制表面,具有支撑结构的部件模块和安装在其上的一组部件, 伺服由控制装置控制,便于控制飞行。 至少一对相互吸引力的连接器相对地固定在所述两个模块构件上,提供用于模块间结构连接的装置。 连接装置包括两个可互相分离地连接的相互吸引力的连杆部分,以形成连接所述伺服机构和所述控制表面的联动组件。 所公开的结构连接和控制联动装置促进了基本上毫不费力的模块间连接以形成可控的飞机以及非破坏性的模块间断开。 具有不同风格和空气动力学规格的多个平面模块可以与一个组件模块相互连接,以形成不同的飞机,为不同的应用共享基本组件。