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WO2017107977A1 - Multi-rotor air vehicle capable of being assembled - Google Patents

Multi-rotor air vehicle capable of being assembled Download PDF

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Publication number
WO2017107977A1
WO2017107977A1 PCT/CN2016/111727 CN2016111727W WO2017107977A1 WO 2017107977 A1 WO2017107977 A1 WO 2017107977A1 CN 2016111727 W CN2016111727 W CN 2016111727W WO 2017107977 A1 WO2017107977 A1 WO 2017107977A1
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Prior art keywords
main control
fitting
control module
floating point
battery module
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PCT/CN2016/111727
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French (fr)
Chinese (zh)
Inventor
彭斌
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Hangzhou Zero Zero Technology Co Ltd
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Hangzhou Zero Zero Technology Co Ltd
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Publication of WO2017107977A1 publication Critical patent/WO2017107977A1/en
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/13—Flying platforms
    • B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/30—Supply or distribution of electrical power

Definitions

  • This application belongs to an aircraft and is specifically a multi-axis rotorcraft.
  • the multi-axis rotorcraft is a four-axis rotorcraft based on a double number of axles.
  • the multi-rotor aircraft relies on the precise control of the input current of each motor by the main control board to control the flight of the aircraft, such as forward, backward, ascending and descending, left and right side shifting, and rolling.
  • Some unmanned opportunities integrate gyroscopes and accelerometers to detect changes in the attitude of the aircraft, and then use the master's precise control of the motor's current to achieve "dynamic stability" in the air.
  • the aircraft provides a structural interface that can be tiled with your own kit or combined with the LEGO kit to add additional features and appearance.
  • a multi-axis rotorcraft that can be assembled, comprising a fuselage, an arm, and a power component, wherein: the body comprises a main control module and a battery module, and the main control module and the battery module are connected by a fitting structure;
  • the structure comprises a detachable fitting portion A and a fitting portion B;
  • the top of the main control module 1 is provided with a fitting portion A, and the bottom of the battery module is provided with correspondingly capable of being embedded with the top of the main control module 1 a fitting portion B;
  • one end of the arm is provided with a connecting portion, one side of the connecting portion is provided with a fitting portion B fitted to the top of the main control module 1, and the other surface is provided with a fitting of the bottom of the battery module a joint A;
  • the arm is detachably disposed between the main control module and the battery module through the connecting portion;
  • the other end of the arm is detachably mounted with the motor group through the connecting structure; a corner of the motor group passes
  • the fitting structure includes the detachable fitting portion A and the fitting portion B which are fitted to each other, and the fitting portion A is a ring a floating point, the fitting portion B is a structure that is fitted to the annular floating point, such as a curved structure or an annular floating point that is offset from the annular floating point, and the two-phase fitting annular floating point may be a LEGO annular floating point. .
  • fitting portion B is a curved structure or an annular floating point that is offset from the above-mentioned annular floating point.
  • the arm comprises an elongated porous connecting member, a long locking buckle, a short locking buckle and a connecting portion, and one end of the elongated porous connecting member is connected to the connecting portion by a long and short locking buckle, and the long locking buckle is a cylinder with a ring cap at one end.
  • the cylinder sequentially passes through one side hole of the elongated porous connecting member, the through hole of the connecting portion, and the other side hole of the elongated porous joint, the short lock is a cylinder with a ring cap at one end, and the cylinder of the short lock is inserted into the long lock Inside the cylindrical hole of the buckle.
  • a differently shaped assembling block may be added between the main control module and the battery module, and the assembling block may be one or more, and the assembling block is connected to the main control module and the battery module through the fitting structure.
  • assembling blocks with bumps may be added to the elongated porous connecting member, and the assembling blocks may be one or more, and the assembling blocks and the elongated porous connecting members are fitted through the holes and the bumps.
  • Figure 1 Overall assembly effect of a multi-axis rotorcraft at rest
  • Figure 2 Schematic diagram of the disassembly and assembly of the fuselage, arm and power components
  • Figure 3 Schematic diagram of the disassembly and assembly of the fuselage parts
  • Figure 4 Schematic diagram of the disassembly and assembly of the components of the arm
  • Figure 5 Schematic diagram of the disassembly and assembly of the components of the power unit
  • a multi-axis rotorcraft that can be assembled, including a fuselage, an arm, and a power assembly.
  • the fuselage includes a main control module 1 and a battery module 2; the arm may be, for example, a long porous connector; the power assembly includes a motor block, a bracket, and a fan blade.
  • the fitting structure includes a detachable fitting portion A and a fitting portion B which are fitted to each other, the fitting portion A is an annular floating point, and the fitting portion B is a structure that is fitted to the annular floating point, such as a curve.
  • the structure or the annular floating point which is offset from the above-mentioned annular floating point, the two-phase fitting annular floating point may be a LEGO annular floating point.
  • the top of the main control module 1 is provided with a fitting portion A
  • the bottom of the battery module is provided with a fitting portion B corresponding to the top of the main control module 1.
  • One end of the arm is provided with a connecting portion for connecting One side of the portion is provided with a fitting portion B that is fitted to the top of the main control module 1, and the other surface is provided with a fitting portion A to which the bottom of the battery module is fitted.
  • the arm is detachably fitted between the main control module and the battery module through the connecting portion.
  • the other end of the arm is detachably mounted with a motor unit through a connecting structure, and the connecting structure may be a matching annular ring and a bump, and the annular ring is disposed on the arm, and the bump is disposed on the motor casing.
  • a support frame is further connected to a corner of the motor unit through the connection structure, and an annular ring is arranged on the support frame.
  • the top of the motor unit is provided with a fan blade, and the motor group drives the blade to rotate through the speed reduction mechanism.
  • the main control module is electrically connected to the battery component, the main control module and the motor component.
  • the arm comprises an elongated porous connecting member, a long locking buckle, a short locking buckle and a connecting portion.
  • One end of the elongated porous connecting member is connected to the connecting portion by a long and short locking buckle, and the long locking buckle is a cylinder with a ring cap at one end, and the cylindrical thread is sequentially worn.
  • One side hole of the over-shaped porous connecting piece, the through hole of the connecting portion, the other side hole of the long porous connection, the short lock is a cylinder with a ring cap at one end, and the cylinder of the short lock is inserted into the cylinder of the long lock Inside the hole.
  • the assembly block can be one or more, the assembly block and the main control module, and the battery module also pass The chimeric structure is connected.
  • the long porous connecting member of the arm can be provided with different shaped assembling blocks with bumps on the elongated porous connecting member, and the assembling blocks can be one or more, and the assembling blocks and the elongated porous connecting members pass through the holes and the bumps. Chimerism.
  • the main control module comprises a PCB board, 8 Micro USB interfaces and a Mini T power interface; wherein the battery module comprises a Mini T power plug.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Toys (AREA)

Abstract

Disclosed is a multi-rotor air vehicle which is simple in structure and can be assembled and disassembled. A four-axis multi-rotor air vehicle or a six-axis multi-rotor air vehicle can be assembled by reusing components of an unmanned air vehicle. With structural connectors provided, the air vehicle can be assembled with its own components, and can also be assembled with Lego components to achieve other additional different functions and appearance characteristics.

Description

可拼装多旋翼飞行器Multi-rotor aircraft can be assembled 技术领域Technical field

本申请属于飞行器，具体属于多轴旋翼飞行器。This application belongs to an aircraft and is specifically a multi-axis rotorcraft.

背景技术Background technique

多轴旋翼飞行器，是一种以双数轴数为基础的，最少为4轴的旋翼飞行器。多旋翼飞行器依靠主控板对各个电机输入电流的精确控制来达到控制飞行器飞行，比如前进，后退，上升下降，左右侧移，翻滚等动作。部分无人机会集成陀螺仪和加速度传感器，来检测飞行器姿态的变化，然后利用主控对电机的电流的精确控制来达到空中“动态稳定”。民用市场所存在的四轴和多轴旋翼飞行器，通常为固定型或者可折叠型多轴飞行器，其飞行器不可以拆卸，重新拼装以及拼装为其他类型的多轴飞行器，并且市场所存在的多轴旋翼飞行器也不能随意添加结构部件使飞行器拥有其他功能或者不同外观特点。The multi-axis rotorcraft is a four-axis rotorcraft based on a double number of axles. The multi-rotor aircraft relies on the precise control of the input current of each motor by the main control board to control the flight of the aircraft, such as forward, backward, ascending and descending, left and right side shifting, and rolling. Some unmanned opportunities integrate gyroscopes and accelerometers to detect changes in the attitude of the aircraft, and then use the master's precise control of the motor's current to achieve "dynamic stability" in the air. Four-axis and multi-axis rotorcraft in the civilian market, usually fixed or collapsible multi-axis aircraft, the aircraft can not be disassembled, reassembled and assembled into other types of multi-axis aircraft, and the market has multiple axes Rotorcraft cannot also add structural components at will to give the aircraft other functions or different appearance characteristics.

发明内容Summary of the invention

本申请所采用的技术方案为：The technical solution adopted in this application is:

本发明的目的是提供一种结构简单的可以拼装和拆卸的多旋翼飞行器，并且可以重复利用这种无人机飞行器的套件组装成4轴，6轴多旋翼飞行器。本飞行器提供了结构接口，可以与自己套件互相拼合，也可与乐高套件拼合以附加其他不同功能和外观特点。SUMMARY OF THE INVENTION It is an object of the present invention to provide a multi-rotor aircraft that can be assembled and disassembled in a simple structure and that can be assembled into a four-axis, six-axis multi-rotor aircraft using the kit of such an unmanned aerial vehicle. The aircraft provides a structural interface that can be tiled with your own kit or combined with the LEGO kit to add additional features and appearance.

1.一种可拼装多轴旋翼飞行器，包括机身、支臂、动力组件，其特征在于：机身包括主控模块和电池模块，主控模块与电池模块之间通过嵌合结构相连；嵌合结构，包括可拆装的相互嵌合的嵌合部A和嵌合部B；主控模块1的顶部设置有嵌合部A、电池模块的底部设置有相应能与主控模块1顶部嵌合的嵌合部B；支臂的一端设置有连接部，连接部的一面设置有与主控模块1的顶部相嵌合的嵌合部B，另一面设置有电池模块底部相嵌合的嵌合部A；支臂通过连接部嵌合地可拆装地设置在主控模块与电池模块之间；支臂的另一端通过连接结构可拆装地安装有电机组；电机组的一角处通过该连接结构还连接有支撑架；电机组的顶部设置有扇叶，电机组通过减速机构驱动扇叶旋转；主控模块与电池组件、主控模块与电机组件之间电连接；或者主控模块1的顶部设置有嵌合部B，连接部与主控模块配合之处、连接部与电池模块底部的配合之处、电池模块底部作相应调整。1. A multi-axis rotorcraft that can be assembled, comprising a fuselage, an arm, and a power component, wherein: the body comprises a main control module and a battery module, and the main control module and the battery module are connected by a fitting structure; The structure comprises a detachable fitting portion A and a fitting portion B; the top of the main control module 1 is provided with a fitting portion A, and the bottom of the battery module is provided with correspondingly capable of being embedded with the top of the main control module 1 a fitting portion B; one end of the arm is provided with a connecting portion, one side of the connecting portion is provided with a fitting portion B fitted to the top of the main control module 1, and the other surface is provided with a fitting of the bottom of the battery module a joint A; the arm is detachably disposed between the main control module and the battery module through the connecting portion; the other end of the arm is detachably mounted with the motor group through the connecting structure; a corner of the motor group passes The connecting structure is further connected with a support frame; the top of the motor group is provided with a fan blade, the motor group drives the fan blade to rotate through the speed reduction mechanism; the main control module is electrically connected with the battery component, the main control module and the motor component; or the main control module The top of 1 is fitted with a fitting B, the fitting of the module is connected with the main control portion connected to the bottom portion of the battery module mating, the bottom of the battery module to be adjusted accordingly.

进一步地，嵌合结构，包括可拆装的相互嵌合的嵌合部A和嵌合部B，嵌合部A为环 形浮点，嵌合部B为与该环形浮点相嵌合的结构，例如曲线结构或者与上述环形浮点相错开的环形浮点，两相嵌合的环形浮点可以为乐高环形浮点。Further, the fitting structure includes the detachable fitting portion A and the fitting portion B which are fitted to each other, and the fitting portion A is a ring a floating point, the fitting portion B is a structure that is fitted to the annular floating point, such as a curved structure or an annular floating point that is offset from the annular floating point, and the two-phase fitting annular floating point may be a LEGO annular floating point. .

进一步地，嵌合部B为曲线结构或者与上述环形浮点相错开的环形浮点。Further, the fitting portion B is a curved structure or an annular floating point that is offset from the above-mentioned annular floating point.

进一步地，支臂有四条，分别安装在机身的四边上。Further, there are four arms, which are respectively mounted on the four sides of the fuselage.

进一步地，支臂包括长形多孔连接件、长锁扣、短锁扣、连接部，长形多孔连接件的一端通过长短锁扣与连接部相连，长锁扣为一端带环帽的圆柱，圆柱依次穿过长形多孔连接件的一侧孔、连接部的通孔、长形多孔连接的另一侧孔，短锁扣为一端带环环帽的圆柱，短锁扣的圆柱插入长锁扣的圆柱孔内。Further, the arm comprises an elongated porous connecting member, a long locking buckle, a short locking buckle and a connecting portion, and one end of the elongated porous connecting member is connected to the connecting portion by a long and short locking buckle, and the long locking buckle is a cylinder with a ring cap at one end. The cylinder sequentially passes through one side hole of the elongated porous connecting member, the through hole of the connecting portion, and the other side hole of the elongated porous joint, the short lock is a cylinder with a ring cap at one end, and the cylinder of the short lock is inserted into the long lock Inside the cylindrical hole of the buckle.

进一步地，还可在主控模块与电池模块之间增加不同形状的拼装块，拼装块可为一个或者多个，拼装块与主控模块、电池模块也通过嵌合结构连接。Further, a differently shaped assembling block may be added between the main control module and the battery module, and the assembling block may be one or more, and the assembling block is connected to the main control module and the battery module through the fitting structure.

进一步地，可在长形多孔连接件上增设带凸点的不同形状的拼装块，拼装块可为一个或者多个，拼装块与长形多孔连接件通过孔与凸点嵌合。Further, different shaped assembling blocks with bumps may be added to the elongated porous connecting member, and the assembling blocks may be one or more, and the assembling blocks and the elongated porous connecting members are fitted through the holes and the bumps.

附图说明DRAWINGS

图1：多轴旋翼飞行器静止状态整体拼装效果Figure 1: Overall assembly effect of a multi-axis rotorcraft at rest

图2：机身，支臂，动力组件分拆安装示意图Figure 2: Schematic diagram of the disassembly and assembly of the fuselage, arm and power components

图3：机身各部件分拆安装示意图Figure 3: Schematic diagram of the disassembly and assembly of the fuselage parts

图4：支臂各部件分拆安装示意图Figure 4: Schematic diagram of the disassembly and assembly of the components of the arm

图5：动力组件各部件分拆安装示意图Figure 5: Schematic diagram of the disassembly and assembly of the components of the power unit

图6：环形浮点与曲线结构的配合方式Figure 6: How the ring float interacts with the curve structure

附图标记说明：1主控模块 2电池模块 3扇叶 4电机组 5支撑架 6拼装块 7长形多孔连接件 8长锁扣 9连接部 10短锁扣DESCRIPTION OF REFERENCE NUMERALS: 1 main control module 2 battery module 3 fan blade 4 motor group 5 support frame 6 assembly block 7 long porous connector 8 long lock buckle 9 connection portion 10 short lock buckle

具体实施方式detailed description

一种可拼装多轴旋翼飞行器，包括机身、支臂、动力组件。机身包括主控模块1和电池模块2；支臂，例如可以为长型多孔连接件；动力组件包括电机组、支架和扇叶。嵌合结构，包括可拆装的相互嵌合的嵌合部A和嵌合部B，嵌合部A为环形浮点，嵌合部B为与该环形浮点相嵌合的结构，例如曲线结构或者与上述环形浮点相错开的环形浮点，两相嵌合的环形浮点可以为乐高环形浮点。主控模块1的顶部设置有嵌合部A、电池模块的底部设置有相应能与主控模块1顶部嵌合的嵌合部B。支臂的一端设置有连接部，连接 部的一面设置有与主控模块1的顶部相嵌合的嵌合部B，另一面设置有电池模块底部相嵌合的嵌合部A。支臂通过连接部嵌合地可拆装地设置在主控模块与电池模块之间。支臂有四条，分别安装在机身的四边上。支臂的另一端通过连接结构可拆装地安装有电机组，连接结构可以为相嵌合的环形圈与凸点，环形圈设置在支臂上，凸点设置在电机组外壳上。电机组的一角处通过该连接结构还连接有支撑架，支撑架上设置有环形圈。电机组的顶部设置有扇叶，电机组通过减速机构驱动扇叶旋转。主控模块与电池组件、主控模块与电机组件之间电连接。支臂包括长形多孔连接件、长锁扣、短锁扣、连接部，长形多孔连接件的一端通过长短锁扣与连接部相连，长锁扣为一端带环帽的圆柱，圆柱依次穿过长形多孔连接件的一侧孔、连接部的通孔、长形多孔连接的另一侧孔，短锁扣为一端带环环帽的圆柱，短锁扣的圆柱插入长锁扣的圆柱孔内。A multi-axis rotorcraft that can be assembled, including a fuselage, an arm, and a power assembly. The fuselage includes a main control module 1 and a battery module 2; the arm may be, for example, a long porous connector; the power assembly includes a motor block, a bracket, and a fan blade. The fitting structure includes a detachable fitting portion A and a fitting portion B which are fitted to each other, the fitting portion A is an annular floating point, and the fitting portion B is a structure that is fitted to the annular floating point, such as a curve. The structure or the annular floating point which is offset from the above-mentioned annular floating point, the two-phase fitting annular floating point may be a LEGO annular floating point. The top of the main control module 1 is provided with a fitting portion A, and the bottom of the battery module is provided with a fitting portion B corresponding to the top of the main control module 1. One end of the arm is provided with a connecting portion for connecting One side of the portion is provided with a fitting portion B that is fitted to the top of the main control module 1, and the other surface is provided with a fitting portion A to which the bottom of the battery module is fitted. The arm is detachably fitted between the main control module and the battery module through the connecting portion. There are four arms, which are mounted on the four sides of the fuselage. The other end of the arm is detachably mounted with a motor unit through a connecting structure, and the connecting structure may be a matching annular ring and a bump, and the annular ring is disposed on the arm, and the bump is disposed on the motor casing. A support frame is further connected to a corner of the motor unit through the connection structure, and an annular ring is arranged on the support frame. The top of the motor unit is provided with a fan blade, and the motor group drives the blade to rotate through the speed reduction mechanism. The main control module is electrically connected to the battery component, the main control module and the motor component. The arm comprises an elongated porous connecting member, a long locking buckle, a short locking buckle and a connecting portion. One end of the elongated porous connecting member is connected to the connecting portion by a long and short locking buckle, and the long locking buckle is a cylinder with a ring cap at one end, and the cylindrical thread is sequentially worn. One side hole of the over-shaped porous connecting piece, the through hole of the connecting portion, the other side hole of the long porous connection, the short lock is a cylinder with a ring cap at one end, and the cylinder of the short lock is inserted into the cylinder of the long lock Inside the hole.

还可在主控模块与电池模块之间增加不同形状的拼装块，例如方形拼装块、长条形拼装块等，拼装块可为一个或者多个，拼装块与主控模块、电池模块也通过嵌合结构连接。支臂的长型多孔连接件，可在长形多孔连接件上增设带凸点的不同形状的拼装块，拼装块可为一个或者多个，拼装块与长形多孔连接件通过孔与凸点嵌合。其中所述主控模块包括PCB板，8个Micro USB接口和一个Mini T电源接口；其中所述电池模块包括一个Mini T电源插头。 It is also possible to add different shapes of the assembly block between the main control module and the battery module, such as a square assembly block, a long strip assembly block, etc., the assembly block can be one or more, the assembly block and the main control module, and the battery module also pass The chimeric structure is connected. The long porous connecting member of the arm can be provided with different shaped assembling blocks with bumps on the elongated porous connecting member, and the assembling blocks can be one or more, and the assembling blocks and the elongated porous connecting members pass through the holes and the bumps. Chimerism. The main control module comprises a PCB board, 8 Micro USB interfaces and a Mini T power interface; wherein the battery module comprises a Mini T power plug.

Claims (7)

一种可拼装多轴旋翼飞行器，包括机身、支臂、动力组件，其特征在于：机身包括主控模块和电池模块，主控模块与电池模块之间通过嵌合结构相连；嵌合结构，包括可拆装的相互嵌合的嵌合部A和嵌合部B；主控模块1的顶部设置有嵌合部A、电池模块的底部设置有相应能与主控模块1顶部嵌合的嵌合部B；支臂的一端设置有连接部，连接部的一面设置有与主控模块1的顶部相嵌合的嵌合部B，另一面设置有电池模块底部相嵌合的嵌合部A；支臂通过连接部嵌合地可拆装地设置在主控模块与电池模块之间；支臂的另一端通过连接结构可拆装地安装有电机组；电机组的一角处通过该连接结构还连接有支撑架；电机组的顶部设置有扇叶，电机组通过减速机构驱动扇叶旋转；主控模块与电池组件、主控模块与电机组件之间电连接；或者主控模块1的顶部设置有嵌合部B，连接部与主控模块配合之处、连接部与电池模块底部的配合之处、电池模块底部作相应调整。A multi-rotor aircraft capable of assembling, comprising a fuselage, an arm, and a power component, wherein: the body comprises a main control module and a battery module, and the main control module and the battery module are connected by a fitting structure; the fitting structure The utility model comprises a detachable fitting portion A and a fitting portion B; the top of the main control module 1 is provided with a fitting portion A, and the bottom of the battery module is provided with correspondingly fitting with the top of the main control module 1 The fitting portion B; one end of the arm is provided with a connecting portion, one side of the connecting portion is provided with a fitting portion B fitted to the top of the main control module 1, and the other surface is provided with a fitting portion at the bottom of the battery module A; the arm is detachably disposed between the main control module and the battery module through the connecting portion; the other end of the arm is detachably mounted with the motor group through the connecting structure; the corner of the motor group passes through the connection The structure is also connected with a support frame; the top of the motor group is provided with a fan blade, and the motor group drives the fan blade to rotate through the speed reduction mechanism; the main control module is electrically connected with the battery component, the main control module and the motor component; or the main control module 1 The top is provided with a fitting part B. Where the connection part cooperates with the main control module, the connection part and the bottom of the battery module, and the bottom of the battery module are adjusted accordingly. 一种如权利要求1所述的可拼装多轴旋翼飞行器，其特征进一步包括：嵌合结构，包括可拆装的相互嵌合的嵌合部A和嵌合部B，嵌合部A为环形浮点，嵌合部B为与该环形浮点相嵌合的结构，例如曲线结构或者与上述环形浮点相错开的环形浮点，两相嵌合的环形浮点可以为乐高环形浮点。A assemblable multi-axis rotorcraft according to claim 1, further comprising: a fitting structure comprising detachably fitting fitting portions A and fitting portions B, the fitting portion A being annular The floating point, the fitting portion B is a structure that is fitted to the annular floating point, such as a curved structure or an annular floating point that is offset from the annular floating point, and the two-phase fitting annular floating point may be a LEGO annular floating point. 一种如权利要求2所述的可拼装多轴旋翼飞行器，其特征进一步包括：嵌合部B为曲线结构或者与上述环形浮点相错开的环形浮点。A assemblable multi-axis rotorcraft according to claim 2, further characterized in that the fitting portion B is a curved structure or an annular floating point that is offset from the annular floating point. 一种如权利要求1所述的可拼装多轴旋翼飞行器，其特征进一步包括：支臂有四条，分别安装在机身的四边上。A assemblable multi-axis rotorcraft according to claim 1, further comprising four arms extending from each other on four sides of the fuselage. 一种如权利要求1所述的可拼装多轴旋翼飞行器，其特征进一步包括：支臂包括长形多孔连接件、长锁扣、短锁扣、连接部，长形多孔连接件的一端通过长短锁扣与连接部相连，长锁扣为一端带环帽的圆柱，圆柱依次穿过长形多孔连接件的一侧孔、连接部的通孔、长形多孔连接的另一侧孔，短锁扣为一端带环环帽的圆柱，短锁扣的圆柱插入长锁扣的圆柱孔内。A assemblable multi-axis rotorcraft according to claim 1, further comprising: the arm comprises an elongated porous connector, a long lock, a short lock, a connecting portion, and one end of the elongated porous connecting member passes through the length The buckle is connected to the connecting portion, and the long locking buckle is a cylinder with a ring cap at one end, the cylinder sequentially passes through one side hole of the elongated porous connecting member, the through hole of the connecting portion, the other side hole of the long porous connection, the short lock The buckle is a cylinder with a ring cap at one end, and the cylinder of the short lock is inserted into the cylindrical hole of the long lock. 一种如权利要求1所述的可拼装多轴旋翼飞行器，其特征进一步包括：还可在主控模块与电池模块之间增加不同形状的拼装块，拼装块可为一个或者多个，拼装块与主控模块、电池模块也通过嵌合结构连接。A assemblable multi-axis rotorcraft according to claim 1, further comprising: adding a differently shaped assembling block between the main control module and the battery module, the assembling block may be one or more, assembling the block The main control module and the battery module are also connected by a fitting structure. 一种如权利要求5所述的可拼装多轴旋翼飞行器，其特征进一步包括：可在长形多孔 连接件上增设带凸点的不同形状的拼装块，拼装块可为一个或者多个，拼装块与长形多孔连接件通过孔与凸点嵌合。 A assemblable multi-axis rotorcraft according to claim 5, further characterized by: A differently shaped assembling block with bumps may be added to the connecting member, and the assembling block may be one or more, and the assembling block and the elongated porous connecting member are fitted through the holes and the bumps.
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