WO2021169022A1 - 一种快速拆解的飞艇吊舱 - Google Patents

一种快速拆解的飞艇吊舱 Download PDF

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Publication number
WO2021169022A1
WO2021169022A1 PCT/CN2020/087064 CN2020087064W WO2021169022A1 WO 2021169022 A1 WO2021169022 A1 WO 2021169022A1 CN 2020087064 W CN2020087064 W CN 2020087064W WO 2021169022 A1 WO2021169022 A1 WO 2021169022A1
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WIPO (PCT)
Prior art keywords
pod
airship
connecting rod
engine
sides
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PCT/CN2020/087064
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English (en)
French (fr)
Inventor
杨思强
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南京祖航航空科技有限公司
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Publication of WO2021169022A1 publication Critical patent/WO2021169022A1/zh

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/06—Rigid airships; Semi-rigid airships
    • B64B1/12—Movable control surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/06—Rigid airships; Semi-rigid airships
    • B64B1/22—Arrangement of cabins or gondolas
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/06—Rigid airships; Semi-rigid airships
    • B64B1/24—Arrangement of propulsion plant

Definitions

  • the utility model belongs to the airship transportation field, in particular to a quickly disassembled airship pod.
  • An airship refers to an aircraft whose pod is driven by an airbag to stay in the air. It has good stability in the air.
  • the structure of the airship mainly includes an airbag, a pod and a rudder.
  • One of the existing airships is to use unmanned technology to drive the airship. Environmental monitoring in the air.
  • the purpose of the utility model is to provide a fast disassembled airship pod to solve the above-mentioned problems in the prior art.
  • a quickly disassembled airship pod includes a pod body, an airbag installed above the nacelle body to provide lift for the airship, and a rudder installed on both sides of the nacelle body to provide power and steering force for the airship.
  • the airbag and the pod body are detachably connected through a connecting component.
  • the rudder includes a connecting rod detachably connected with one end of the pod body, and a power assembly detachably connected with the other end of the connecting rod.
  • the power assembly includes an engine that is detachably connected to the connecting rod, and a blade and a duct that are detachably connected to the engine, the engine includes a base and an output shaft, and the blade is connected to the engine.
  • the output shaft is detachably connected
  • the duct is detachably connected to the base of the engine
  • the duct is sleeved on the outside of the engine and the blade
  • the width of the duct is greater than the distance from the blade to the connecting rod .
  • the duct avoids the collision of the blades with external debris when rotating, improves the service life of the blades, and facilitates the disassembly and assembly of the engine, the blades and the duct during maintenance through the detachable connection.
  • it further includes two landing gears that are detachably installed on both sides of the bottom of the pod body, and the landing gear includes a crossbar and at least two vertical rods fixedly mounted on the crossbar, The vertical rod is fixed on the bottom of the pod body by screws, the wear of the bottom of the pod body is reduced by the landing gear, the service life of the pod body is improved, and the detachable connection facilitates the disassembly, replacement and maintenance of the landing gear when the landing gear is damaged.
  • the pod body, connecting rod, duct, and landing gear are all made of carbon fiber balsa composite material
  • the carbon fiber balsa composite material is made of balsa wood and carbon fiber cloth bonded by epoxy resin.
  • the connecting assembly includes a flange extending outward from the top edge of the pod body, and a groove block fixedly installed at the bottom end of the airbag to cooperate with the flange, and the flange has an oval shape. shape.
  • the groove block is a U-shaped block with one end closed and the other end communicating with the outside.
  • the U-shaped block has a groove matching with a flange on the inner side, and at least one For a symmetrical threaded hole, the flange is provided with a through hole matching the threaded hole, wherein the flange is inserted into the groove of the groove block, and the pod is realized by a combination of inserting and screwing.
  • a pair of hinge rods are symmetrically installed at one end of the connecting rod connected with the pod body, and the hinge rods are symmetrically installed on both sides of the connecting rod and rotate on both sides of the connecting rod.
  • the two sides of the pod body are provided with rectangular holes, the inner two sides of the pod body are also provided with slideways that cooperate with the hinge rods, and at least one pair of slideways are opened on both sides of the rectangular holes.
  • a threaded hole matching the through hole is opened on the hinge rod, wherein the hinge rod passes through the rectangular hole and is inserted into the slideway, and the pod is realized by a combination of insertion and screw connection.
  • one end of the connecting rod connected with the engine is provided with a connector, one side of the connector is opened with a T-shaped groove from top to bottom, the bottom end of the T-shaped groove is closed, and the top end is connected with Connect with the outside world.
  • the base of the engine is provided with a T-shaped block at one end away from the output shaft, at least a pair of symmetrical threaded holes are opened on both sides of the top of the T-shaped groove, and both sides of the T-shaped block are opened with a T-shaped groove.
  • the threaded holes are matched with the through holes, wherein the T-shaped block is inserted into the T-shaped groove, and the detachable connection between the pod body and the engine can be achieved by the combination of insertion and screw connection, which can reduce the number of screws and pins , It is convenient for disassembly and assembly during maintenance.
  • the utility model realizes the connection of the airbag, the rudder and the pod body through the detachable connection mode of the plug connection and the screw connection.
  • the use of screw connection leads to an excessive number of screws and positioning pins, which is not conducive to the problem of assembly and disassembly during maintenance.
  • the airbag, rudder and pod body are positioned by plugging to ensure the quality of the connection.
  • Figure 1 is a schematic diagram of the assembly of the utility model.
  • Figure 2 is a schematic diagram of the pod body of the present invention.
  • Figure 3 is a schematic diagram of the bottom isometric view of the airbag of the present invention.
  • Figure 4 is a partial cross-sectional view of the connecting rod of the present invention.
  • Fig. 5 is a schematic partial cross-sectional view of the rudder of the present invention.
  • FIG. 1 to 5 The reference signs shown in Figures 1 to 5 are: pod body 1, airbag 2, rudder 3, landing gear 4, flange 11, slot block 21, connecting rod 31, power assembly 32, vertical rod 42, cross rod 41 , Hinge rod 311, slide 312, connector 313, engine 321, groove 211, blade 322, duct 323, base 3211, output shaft 3212, T-shaped block 3213.
  • An airship refers to an aircraft whose pod is driven by an airbag to stay in the air. It has good stability in the air.
  • the structure of the airship mainly includes an airbag, a pod and a rudder.
  • One of the existing airships is to use unmanned technology to drive the airship.
  • a quick-dismantling airship pod including: pod body 1, air bag 2, rudder 3, landing gear 4, flange 11, groove block 21, connecting rod 31, and power assembly 32 , Vertical rod 42, cross rod 41, hinge rod 311, slide 312, connector 313, engine 321, groove 211, blade 322, duct 323, base 3211, output shaft 3212, T-shaped block 3213.
  • the airbag 2 is installed above the pod body 1 to provide lift for the airship.
  • Two rudders 3 symmetrically installed on both sides of the pod body 1 provide power and steering force for the airship.
  • the airbag 2 and the pod body 1 are detachably connected by a connecting component.
  • the rudder 3 includes a connecting rod 31 detachably connected to the pod body 1 at one end, and a power assembly 32 detachably connected to the other end of the connecting rod 31 .
  • pod body 1 and rudder 3 When one of the components of the airship's airbag 2, pod body 1 and rudder 3 is damaged, the damaged part is quickly removed and replaced with a new component through a detachable connection, so that the airship can quickly return to work.
  • the power assembly 32 includes an engine 321 that is detachably connected to the connecting rod 31, and a blade 322 that is detachably connected to the engine 321.
  • the blade 322 is easily exposed to external debris when it rotates. In the event of a collision, it is necessary to maintain the blades 322 frequently. Therefore, the utility model also has a duct 323 detachably connected with the engine 321.
  • the engine 321 includes a base 3211 and an output shaft 3212, and the blades 322 and the output shaft of the engine 321 3212 is detachably connected.
  • the duct 323 is detachably connected to the base of the engine 321.
  • the duct 323 is sleeved on the outside of the engine 321 and the blades 322.
  • the end of the output shaft 3212 away from the base 3211 is threaded.
  • a keyway is also opened on the side between and the base 3211.
  • the blade 322 is rotatably connected with the output shaft 3212 through a key connection. Two nuts are screwed on the end of the output shaft 3212 away from the base 3211 to realize the blade 322 and the engine 321.
  • the detachable connection of the output shaft 3212 in which the width of the duct 323 is greater than the distance between the blade 322 and the connecting rod 31, the duct 323 avoids the collision of the blade 322 with external debris when the blade 322 rotates, and improves the use of the blade 322
  • the service life is convenient for the disassembly and assembly of the engine 321, the blades 322 and the duct 323 through the detachable connection method.
  • two symmetrical landing gears 4 can be detachably installed on both sides of the bottom of the pod body 1
  • the landing gear 4 includes a crossbar 41 and at least two vertical rods 42 fixedly mounted on the crossbar 41.
  • the vertical rods 42 are fixed to the bottom of the nacelle body 1 by screws, and the landing gear 4 lowers the lower part of the nacelle body 1.
  • the wear of the bottom improves the service life of the nacelle body 1, and the detachable connection of the landing gear 4 and the nacelle body 1 is realized by screws, which facilitates the disassembly, replacement and maintenance of the landing gear 4 when it is damaged.
  • the pod body 1, the connecting rod 31, the duct 323 and the landing gear 4 are all made of carbon fiber light.
  • the carbon fiber balsa composite material is made of balsa wood and carbon fiber cloth through epoxy resin bonding.
  • the balsa wood is combined with the The carbon fiber cloth is glued with epoxy resin to form a skeleton, and the joints are glued with epoxy resin. After being fixed by the extrusion of the shape tooling, the epoxy resin can be solidified.
  • the landing gear 4 needs The airship supported by the ground is under greater pressure, which may exceed the strength of the balsa wood chips. Therefore, the landing gear 4 can also be made of lightweight and high-strength aluminum alloy tubes.
  • the vertical rod 42 is also From the center line of the pod body 1, it curves and extends to both sides. By using the balsa wood composite material made of balsa wood and carbon fiber cloth, it can ensure the strength of the pod body 1, the connecting rod 31, the duct 323 and the landing gear 4 while reducing its own weight, which solves the problem of increasing the detachable connection structure.
  • the increased weight of the airship makes it possible to use the airship normally.
  • connection assembly includes A flange 11 extending outward from the top edge of the pod body 1 and a groove block 21 fixedly mounted on the bottom end of the airbag 2 to cooperate with the flange 11, and the flange 11 has an oval shape.
  • the groove block 21 is a U-shaped block with one end closed and the other end communicating with the outside.
  • the inside of the U-shaped block is opened with a groove 211 that matches with the flange 11, and at least a pair of symmetrical ends are opened on both sides of the groove block 21.
  • the flange 11 is provided with a through hole that matches the threaded hole.
  • the flange 11 is inserted into the groove 211 of the groove block 21, and the pod body 1 is realized by a combination of inserting and screwing.
  • the detachable connection with the airbag 2 solves the problem of the excessive number of screws and pins. After the flange 11 is positioned through the groove 211, only two screws need to be installed at the end to complete the airbag 2 and the pod body 1.
  • the fixed space greatly reduces the number of screws and pins, which is convenient for disassembly and assembly during maintenance.
  • a pair of hinge rods 311 are symmetrically installed at one end of the connecting rod 31 connected with the pod body 1.
  • the hinge rods 311 are symmetrically installed on both sides of the connecting rod 31 and rotate on both sides of the connecting rod 31.
  • Rectangular holes are opened on both sides of the pod body 1, and slideways 312 matched with hinge rods 311 are opened on both sides of the interior of the pod body 1, and at least one pair of slideways 312 are opened on both sides of the rectangular holes.
  • the hinge rod 311 is also provided with a threaded hole that matches the through hole. The hinge rod 311 passes through the rectangular hole and is inserted into the slideway 312, and the hinge rod 311 is restricted by the slideway 312.
  • the detachable connection of the pod body 1 and the connecting rod 31 through the combination of plug connection and screw connection can reduce the number of screws and pins, and facilitate the disassembly and assembly during maintenance.
  • one end of the connecting rod 31 connected with the engine 321 is provided with a connector 313, one side of the connector 313 is opened with a T-shaped groove from top to bottom, the bottom end of the T-shaped groove is closed, and the top end is connected with Connect with the outside world.
  • the base of the engine 321 is provided with a T-shaped block 3213 at one end away from the output shaft 3212, at least a pair of symmetrical threaded holes are opened on both sides of the top of the T-shaped groove, and both sides of the T-shaped block 3213 are provided with threads with the T-shaped groove A through hole with matching holes, wherein the T-shaped block 3213 is inserted in the T-shaped groove, and the detachable connection between the pod body 1 and the engine 321 can be achieved by the combination of insertion and screw connection, which can reduce the number of screws and pins. It is convenient for disassembly and assembly during maintenance.

Abstract

一种快速拆解的飞艇吊舱，快速拆解的飞艇吊舱包括吊舱本体（1）、气囊（2）和方向舵（3），气囊（2）安装在吊舱本体（1）上方为飞艇提供升力，方向舵（3）安装在吊舱本体（1）两侧为飞艇提供动力和转向力，其中，气囊（2）与吊舱本体（1）之间通过连接组件可拆卸连接，方向舵（3）包括一端与吊舱本体（1）可拆卸连接的连接杆（31），以及与连接杆（31）的另一端可拆卸连接的动力组件（32）。

Description

一种快速拆解的飞艇吊舱 技术领域
本实用新型属于飞艇运输领域，尤其是一种快速拆解的飞艇吊舱。
 背景技术
飞艇是指由气囊带动吊舱滞留空中的飞行器，其在空中具有良好的稳定性，飞艇的结构主要包括气囊、吊舱和方向舵，现有飞艇的广泛用途之一就是使用无人驾驶技术驾驶飞艇在空中进行环境监测。
在上述飞艇的结构中，除吊舱外其余组件均为易损耗组件，然而现有飞艇组件的连接结构是使用焊接的形式进行固定连接，不利于维护时的装配和拆卸，为此需要提供一种能够快速拆解的飞艇吊舱，方便飞艇的维护。
 技术问题
实用新型目的：提供一种快速拆解的飞艇吊舱，以解决现有技术存在的上述问题。
 技术解决方案
一种快速拆解的飞艇吊舱包括：吊舱本体，安装在吊舱本体上方为飞艇提供升力的气囊，以及安装在吊舱本体两侧为飞艇提供动力和转向力的方向舵。
所述气囊与吊舱本体之间通过连接组件可拆卸连接。
所述方向舵包括一端与吊舱本体可拆卸连接的连接杆，以及与连接杆的另一端可拆卸连接的动力组件。
在进一步的实施例中，所述动力组件包括与连接杆可拆卸连接的发动机，以及与发动机可拆卸连接的桨叶和涵道，所述发动机包括机座和输出轴，所述桨叶与发动机的输出轴可拆卸连接，所述涵道与发动机的基座可拆卸连接，所述涵道套接在发动机和桨叶的外侧，其中，所述涵道的宽度大于桨叶至连接杆的距离。通过涵道避免桨叶旋转时与外界杂物发生碰撞，提高桨叶的使用寿命，通过可拆卸连接的方式方便发动机、桨叶和涵道维护时的拆卸与装配。
在进一步的实施例中，还包括可拆卸安装在吊舱本体底部两侧相互对称的两个起落架，所述起落架包括一个横杆，以及固定安装在横杆上的至少两个竖杆，所述竖杆通过螺钉固定在吊舱本体的底部，通过起落架降低吊舱本体的底部的磨损，提高吊舱本体的使用寿命，通过可拆卸连接方便起落架损坏时的拆卸、更换与维护。
在进一步的实施例中，所述吊舱本体、连接杆、涵道和起落架均由碳纤维轻木复合材料制成，所述碳纤维轻木复合材料由轻木板和碳纤维布通过环氧树脂粘合而成，通过使用由轻木板和碳纤维布制成的轻木复合材料能够在保证吊舱本体、连接杆、涵道和起落架自身强度的同时降低自重，解决了增加可拆连接结构带来的重量增加问题，使飞艇能够正常使用。
在进一步的实施例中，所述连接组件包括吊舱本体的顶端边缘向外侧延伸的凸缘，以及固定安装在气囊的底端与凸缘相配合的槽块，所述凸缘的外形呈椭圆形。
所述槽块为一端封闭，另一端与外界相通的U形块，所述U形块的内侧开有与凸缘相配合的凹槽，所述槽块的两侧端部还开有至少一对对称的螺纹孔，所述凸缘上开有与螺纹孔相配合的通孔，其中，所述凸缘插接在槽块的凹槽内，通过插接和螺接结合的方式实现吊舱本体和气囊的可拆卸连接能够降低螺钉和销钉的数量，方便维护时的拆卸和装配。
在进一步的实施例中，所述连接杆与吊舱本体连接的一端对称安装有一对铰接杆，所述铰接杆对称安装在连接杆的两侧，并在连接杆的两侧转动。
所述吊舱本体的两侧开有矩形孔，所述吊舱本体的内部两侧还开有与铰接杆相配合的滑道，所述矩形孔的两侧还开有至少一对与滑道相通的通孔，所述铰接杆上还开有与通孔相配合的螺纹孔，其中，所述铰接杆穿过矩形孔插接在滑道内，通过插接和螺接结合的方式实现吊舱本体和连接杆的可拆卸连接能够降低螺钉和销钉的数量，方便维护时的拆卸和装配。
在进一步的实施例中，所述连接杆与发动机连接的一端设有插接件，插接件的一侧自上而下开有T形槽，所述T形槽的底端封闭，顶端与外界相通。
所述发动机的基座远离输出轴的一端设有T形块，所述T形槽的顶端两侧开有至少一对对称的螺纹孔，所述T形块的两侧开有与T形槽的螺纹孔相配合的通孔，其中，所述T形块插接在T形槽内，通过插接和螺接结合的方式实现吊舱本体和发动机的可拆卸连接能够降低螺钉和销钉的数量，方便维护时的拆卸和装配。
 有益效果
本实用新型通过插接与螺接相配合的可拆卸连接方式实现气囊、方向舵与吊舱本体的连接，解决了现有技术中，飞艇组件的连接结构使用焊接的形式进行固定连接，以及单纯的使用螺接导致螺钉和定位销数量过多，不利于维护时的装配和拆卸的问题，同时通过插接对气囊、方向舵与吊舱本体进行定位，保证了连接质量。
 附图说明
图1是本实用新型的装配示意图。
图2是本实用新型的吊舱本体示意图。
图3是本实用新型的气囊的底部轴测示意图。
图4是本实用新型的连接杆局部剖视示意图。
图5是本实用新型的方向舵局部剖视示意图。
图1至图5所示附图标记为：吊舱本体1、气囊2、方向舵3、起落架4、凸缘11、槽块21、连接杆31、动力组件32、竖杆42、横杆41、铰接杆311、滑道312、插接件313、发动机321、凹槽211、桨叶322、涵道323、机座3211、输出轴3212、T形块3213。
 本发明的实施方式
飞艇是指由气囊带动吊舱滞留空中的飞行器，其在空中具有良好的稳定性，飞艇的结构主要包括气囊、吊舱和方向舵，现有飞艇的广泛用途之一就是使用无人驾驶技术驾驶飞艇在空中进行环境监测，申请人对飞艇的维护进行研究时发现在上述飞艇的结构中，除吊舱外其余组件均为易损耗组件，然而现有飞艇组件的连接结构是使用焊接的形式进行固定连接，不利于维护时的装配和拆卸，维护工作时间长，劳动强度大。
为了解决上述问题，申请人研发了一种快速拆解的飞艇吊舱包括：吊舱本体1、气囊2、方向舵3、起落架4、凸缘11、槽块21、连接杆31、动力组件32、竖杆42、横杆41、铰接杆311、滑道312、插接件313、发动机321、凹槽211、桨叶322、涵道323、机座3211、输出轴3212、T形块3213。
气囊2安装在吊舱本体1的上方为飞艇提供升力。
两个对称安装在吊舱本体1两侧的方向舵3为飞艇提供动力和转向力。
其中，气囊2与吊舱本体1之间通过连接组件可拆卸连接，方向舵3包括一端与吊舱本体1可拆卸连接的连接杆31，以及与连接杆31的另一端可拆卸连接的动力组件32。
工作原理：在进行飞艇的维护时通过可拆卸连接的方式快速的将气囊2、吊舱本体1和方向舵3拆分开来，分开来同时维护，缩短维护所用时间和劳动强度。
在飞艇的气囊2、吊舱本体1和方向舵3其中一个组件发生损坏时，通过可拆卸连接的方式快速的损坏部分拆下更换上新的组件，使飞艇能够快速的回到工作岗位。
在进一步的实施例中，在现有技术中动力组件32包括与连接杆31可拆卸连接的发动机321，以及与发动机321可拆卸连接的桨叶322，桨叶322旋转工作时容易与外界杂物发生碰撞，需要经常对桨叶322进行维护，所以本实用新型还设有与发动机321可拆卸连接的涵道323，发动机321包括机座3211和输出轴3212，桨叶322与发动机321的输出轴3212可拆卸连接，涵道323与发动机321的基座可拆卸连接，涵道323套接在发动机321和桨叶322的外侧，通过在输出轴3212远离机座3211的一端开有螺纹，在螺纹和机座3211之间的一侧还开有键槽，桨叶322通过键连接与输出轴3212转动连接，在输出轴3212远离机座3211的一端螺接有两个螺母实现桨叶322与发动机321的输出轴3212的可拆卸连接，其中，涵道323的宽度大于桨叶322至连接杆31的距离，通过涵道323避免桨叶322旋转时与外界杂物发生碰撞，提高桨叶322的使用寿命，通过可拆卸连接的方式方便发动机321、桨叶322和涵道323维护时的拆卸与装配。
在进一步的实施例中，在飞艇降落时吊舱本体1经常落在地面上与地面发生摩擦容易发生磨损，所以吊舱本体1的底部两侧还可拆卸安装有相互对称的两个起落架4，起落架4包括一个横杆41，以及固定安装在横杆41上的至少两个竖杆42，竖杆42通过螺钉固定在吊舱本体1的底部，通过起落架4降低吊舱本体1的底部的磨损，提高吊舱本体1的使用寿命，通过螺钉实现起落架4与吊舱本体1的可拆卸连接，方便起落架4损坏时的拆卸、更换与维护。
在进一步的实施例中，增加可拆连接结构会给飞艇带来重量增加的问题，不利于飞艇的正常使用，所以吊舱本体1、连接杆31、涵道323和起落架4均由碳纤维轻木复合材料制成，碳纤维轻木复合材料由轻木板和碳纤维布通过环氧树脂粘合而成，在吊舱本体1、连接杆31、涵道323和起落架4的制作时将轻木片和碳纤维布用环氧树脂粘合后，组成骨架，并在接缝处用环氧树脂粘合，通过外形工装的挤压固定后，待环氧树脂凝固即可完成，其中，起落架4因为需要与地面抵接支撑飞艇受到较大的压力，可能超出轻木片的强度，所以起落架4也可使用重量轻，强度高的铝合金管制成，为了增加起落架4间的间距所以竖杆42还自吊舱本体1的中线向两侧弯曲延伸。通过使用由轻木板和碳纤维布制成的轻木复合材料能够在保证吊舱本体1、连接杆31、涵道323和起落架4自身强度的同时降低自重，解决了增加可拆连接结构带来的重量增加问题，使飞艇能够正常使用。
在进一步的实施例中，在现有技术中大多可拆卸连接都是在连接部位的周围安装较多的螺钉和销钉，这种方法不仅重量大，而且拆卸和装配时间过长，所以连接组件包括吊舱本体1的顶端边缘向外侧延伸的凸缘11，以及固定安装在气囊2的底端与凸缘11相配合的槽块21，所述凸缘11的外形呈椭圆形。
槽块21为一端封闭，另一端与外界相通的U形块，U形块的内侧开有与凸缘11相配合的凹槽211，槽块21的两侧端部还开有至少一对对称的螺纹孔，凸缘11上开有与螺纹孔相配合的通孔，其中，凸缘11插接在槽块21的凹槽211内，通过插接和螺接结合的方式实现吊舱本体1和气囊2的可拆卸连接解决了螺钉和销钉的数量过多的问题，通过凹槽211对凸缘11进行定位后只需在端部安装两个螺钉即可完成气囊2与吊舱本体1之间的固定，极大地降低了螺钉和销钉的数量，方便维护时的拆卸和装配。
在进一步的实施例中，连接杆31与吊舱本体1连接的一端对称安装有一对铰接杆311，铰接杆311对称安装在连接杆31的两侧，并在连接杆31的两侧转动。
吊舱本体1的两侧开有矩形孔，吊舱本体1的内部两侧还开有与铰接杆311相配合的滑道312，矩形孔的两侧还开有至少一对与滑道312相通的通孔，铰接杆311上还开有与通孔相配合的螺纹孔，其中，铰接杆311穿过矩形孔插接在滑道312内，通过滑道312对铰接杆311进行限位，通过插接和螺接结合的方式实现吊舱本体1和连接杆31的可拆卸连接能够降低螺钉和销钉的数量，方便维护时的拆卸和装配。
在进一步的实施例中，连接杆31与发动机321连接的一端设有插接件313，插接件313的一侧自上而下开有T形槽，T形槽的底端封闭，顶端与外界相通。
发动机321的基座远离输出轴3212的一端设有T形块3213，T形槽的顶端两侧开有至少一对对称的螺纹孔，T形块3213的两侧开有与T形槽的螺纹孔相配合的通孔，其中，T形块3213插接在T形槽内，通过插接和螺接结合的方式实现吊舱本体1和发动机321的可拆卸连接能够降低螺钉和销钉的数量，方便维护时的拆卸和装配。

Claims (7)

  1. 一种快速拆解的飞艇吊舱，其特征在于，包括：吊舱本体，安装在吊舱本体上方为飞艇提供升力的气囊，以及安装在吊舱本体两侧为飞艇提供动力和转向力的方向舵；
    所述气囊与吊舱本体之间通过连接组件可拆卸连接；
    所述方向舵包括一端与吊舱本体可拆卸连接的连接杆，以及与连接杆的另一端可拆卸连接的动力组件。
  2. 根据权利要求1所述一种快速拆解的飞艇吊舱，其特征在于，所述动力组件包括与连接杆可拆卸连接的发动机，以及与发动机可拆卸连接的桨叶和涵道，所述发动机包括机座和输出轴，所述桨叶与发动机的输出轴可拆卸连接，所述涵道与发动机的基座可拆卸连接，所述涵道套接在发动机和桨叶的外侧，其中，所述涵道的宽度大于桨叶至连接杆的距离。
  3. 根据权利要求2所述一种快速拆解的飞艇吊舱，其特征在于，还包括可拆卸安装在吊舱本体底部两侧相互对称的两个起落架，所述起落架包括一个横杆，以及固定安装在横杆上的至少两个竖杆，所述竖杆通过螺钉固定在吊舱本体的底部。
  4. 根据权利要求3所述一种快速拆解的飞艇吊舱，其特征在于，所述吊舱本体、连接杆、涵道和起落架均由碳纤维轻木复合材料制成，所述碳纤维轻木复合材料由轻木板和碳纤维布通过环氧树脂粘合而成。
  5. 根据权利要求3所述一种快速拆解的飞艇吊舱，其特征在于，所述连接组件包括吊舱本体的顶端边缘向外侧延伸的凸缘，以及固定安装在气囊的底端与凸缘相配合的槽块，所述凸缘的外形呈椭圆形；
    所述槽块为一端封闭，另一端与外界相通的U形块，所述U形块的内侧开有与凸缘相配合的凹槽，所述槽块的两侧端部还开有至少一对对称的螺纹孔，所述凸缘上开有与螺纹孔相配合的通孔，其中，所述凸缘插接在槽块的凹槽内。
  6. 根据权利要求3所述一种快速拆解的飞艇吊舱，其特征在于，所述连接杆与吊舱本体连接的一端对称安装有一对铰接杆，所述铰接杆对称安装在连接杆的两侧，并在连接杆的两侧转动；
    所述吊舱本体的两侧开有矩形孔，所述吊舱本体的内部两侧还开有与铰接杆相配合的滑道，所述矩形孔的两侧还开有至少一对与滑道相通的通孔，所述铰接杆上还开有与通孔相配合的螺纹孔，其中，所述铰接杆穿过矩形孔插接在滑道内。
  7. 根据权利要求3所述一种快速拆解的飞艇吊舱，其特征在于，所述连接杆与发动机连接的一端设有插接件，插接件的一侧自上而下开有T形槽，所述T形槽的底端封闭，顶端与外界相通；
    所述发动机的基座远离输出轴的一端设有T形块，所述T形槽的顶端两侧开有至少一对对称的螺纹孔，所述T形块的两侧开有与T形槽的螺纹孔相配合的通孔，其中，所述T形块插接在T形槽内。
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