WO2019041068A1 - 一种飞行机器人减震设备 - Google Patents

一种飞行机器人减震设备 Download PDF

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Publication number
WO2019041068A1
WO2019041068A1 PCT/CN2017/099209 CN2017099209W WO2019041068A1 WO 2019041068 A1 WO2019041068 A1 WO 2019041068A1 CN 2017099209 W CN2017099209 W CN 2017099209W WO 2019041068 A1 WO2019041068 A1 WO 2019041068A1
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Prior art keywords
column
fixing
damping device
parachute
fixed
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PCT/CN2017/099209
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English (en)
French (fr)
Inventor
刘哲
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刘哲
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Priority to PCT/CN2017/099209 priority Critical patent/WO2019041068A1/zh
Publication of WO2019041068A1 publication Critical patent/WO2019041068A1/zh

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/50—Glider-type UAVs, e.g. with parachute, parasail or kite
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25J—MANIPULATORS; CHAMBERS PROVIDED WITH MANIPULATION DEVICES
    • B25J11/00—Manipulators not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25J—MANIPULATORS; CHAMBERS PROVIDED WITH MANIPULATION DEVICES
    • B25J19/00—Accessories fitted to manipulators, e.g. for monitoring, for viewing; Safety devices combined with or specially adapted for use in connection with manipulators
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25J—MANIPULATORS; CHAMBERS PROVIDED WITH MANIPULATION DEVICES
    • B25J19/00—Accessories fitted to manipulators, e.g. for monitoring, for viewing; Safety devices combined with or specially adapted for use in connection with manipulators
    • B25J19/06—Safety devices

Definitions

  • the invention relates to the field of robot technology, in particular to a flying robot damping device.
  • a robot is a machine that automatically performs work. It can accept human command, run pre-programmed procedures, or act on principles that are based on artificial intelligence techniques. Its mission is to assist or replace human work, such as production, construction, or other dangerous work. As the times progress, robotic disassembly equipment also increases.
  • the existing flying robot damping device can not effectively use the surrounding environment to save energy, can not provide safety protection during the falling process, and cannot flexibly control the damping device.
  • a flying robot damping device including a damping device body, and a front chest fixing plate and a back fixing plate are mounted on the left and right sides of the damping device body, and An arm fixing post is fixed in a front middle portion of the front chest fixing plate, a signal transmitter is disposed at a top left inner side of the front chest fixing plate, and a parachute slot is disposed at an inner side of the front chest fixing plate, the parachute slot
  • a fixing strap is installed in the middle of the front side, and a buckle base is fixed in the middle of the left side of the parachute slot, a buckle is fixed in the middle of the left side of the buckle base, and a plurality of evenly distributed steel belts are disposed on the buckle.
  • a parachute is fixed on the left side of the steel ribbon, and an arm telescopic column is fixed in the middle of the front side of the rear fixing column, and a plurality of uniformly distributed elastic telescopic columns and elastic telescopic column bases are disposed inside the fixing column, and the opposite of the fixing column a gravity plate is fixed to the side, and the front chest fixing plate is fixed
  • the top of each of the back fixing columns is provided with two head telescopic columns, and the right side of the back fixing column is installed with solar panels, and the solar panels 4 A fixing nut is fixed to each corner.
  • the left end of the arm telescopic column is movably connected with the right end of the arm fixing column
  • the head telescopic column is movably connected with the head fixing column
  • the elastic telescopic column and the elastic telescopic column base are movably connected, and the elastic telescopic column and the elastic telescopic column base are embedded in the back fixing plate.
  • the gravity plate covers the rear side of the back fixing plate, and the weight of the gravity plate is 9 kg.
  • the right side of the parachute is fixedly connected to the left side of the buckle by a steel wire band.
  • the flying robot damping device is provided with an arm telescopic column and a head telescopic column, and the left end of the arm telescopic column is movably connected with the right top end of the arm fixing column.
  • the head telescopic column is movably connected to the head fixing column, because the arm telescopic column and the arm fixing column are telescopically stretched left and right, and the head fixing column and the head telescopic column are telescopically stretched to the left and right, so that any robot of different sizes can be worn well and stably.
  • the shock absorbing device improves the practicality, and the elastic telescopic column is set, the elastic telescopic column and the elastic telescopic column base are movably connected, and the elastic telescopic column and the elastic telescopic column base are embedded in the back fixing plate, during the flight of the robot
  • the impact force in the air is buffered, and the impact force is too large to cause the parts of the shock absorbing device to be misaligned, and the safety is improved.
  • the gravity plate, the gravity plate cover and the back fixed plate are provided.
  • the back side, and the weight of the gravity plate is 9kg, because the gravity plate is placed on the back fixing plate, so that the quality of the back fixing plate is super
  • the front chest fixing plate enables the back fixing plate to land first when the robot is dropped, and the impact force is reduced as much as possible through the buffer column, and the parachute is set.
  • the right side of the parachute is fixedly connected to the left side of the buckle by the steel wire band, because the front A parachute is installed in the chest fixing plate.
  • Figure 1 is a schematic view of the overall structure of the present invention
  • Figure 2 is a cross-sectional view showing the structure of the front chest fixing plate of the present invention.
  • Figure 3 is a cross-sectional view showing the structure of the back fixing plate of the present invention.
  • FIG. 4 is a schematic view showing a partial structure of a parachute slot of the present invention.
  • FIG. 5 is a schematic structural diagram of a structure of a signal transmitter module according to the present invention.
  • a flying robot damping device including 1, a chest fixed plate, 101, a signal transmitter, 102, a parachute slot, 103, a fixed belt, 104, Buckle base, 105, buckle, 106, wire belt, 107, parachute, 2, arm fixed column, 3, arm telescopic column, 4, back fixed plate, 401, elastic telescopic column, 402, elastic telescopic column base, 403, gravity plate, 5, solar panel, 6, fixing nut, 7, head telescopic column, 8, head fixing column, 9, damping device body, the left and right sides of the shock absorbing device body 9 are installed a front chest fixing plate 1 and a back fixing plate 4, and an arm fixing column 2 is fixed in the front surface of the front chest fixing plate 1, and a signal transmitter 101 is disposed at the top left inner side of the front chest fixing plate 1, and the front chest The inner side of the fixed plate 1 is provided A parachute slot 102 is disposed, and a fixing strap 103 is disposed in
  • the left side of the steel belt 106 is fixed with a parachute 107, and a parachute 107 is disposed.
  • the right side of the parachute 107 passes through the steel belt 106 and the buckle 105.
  • the left side is fixedly connected, because the parachute 107 is installed in the front chest fixing plate 1, and when the terminal finds that the robot is faulty, the robot's parachute 107 is opened in time to minimize the damage of the robot falling, thereby improving safety, and the back is fixed.
  • An arm telescopic column 3 is fixed in the middle of the front surface of the column 4, and a plurality of uniformly distributed elastic telescopic columns 401 and an elastic telescopic column base 402 are disposed inside the fixing column 4, and an elastic telescopic column 401, an elastic telescopic column 401 and an elastic telescopic column are disposed.
  • the base 402 is movably connected, and the elastic telescopic column 401 and the elastic telescopic column base 402 are respectively embedded in the back fixing plate 4, and are elastically stretched during the flight of the robot.
  • the expansion and contraction of the column 401 and the elastic telescopic column base 402 will buffer the impact force in the air, avoiding the impact force being too large, causing the parts of the shock absorbing device body 9 to be dislocated, and improving the safety.
  • the opposite side of the fixing column 4 is fixed with the gravity plate 403.
  • a gravity plate 403 is disposed, the gravity plate 403 covers the rear side of the back fixing plate 4, and the weight of the gravity plate 403 is 9 kg, because the gravity plate 403 is disposed on the back fixing plate 4, so that the back fixing plate 4
  • the mass exceeds the front chest fixing plate 1, so that when the robot is dropped, the back fixing plate 4 can be grounded first, and the impact force is relieved as much as possible by buffering.
  • the top of the front chest fixing plate 1 is provided with two head fixing columns. 8.
  • the top end of the back fixing column 4 is fixed with two head telescopic columns 7, and the arm telescopic column 3 and the head telescopic column 7 are disposed.
  • the left end of the arm telescopic column 3 and the right side of the arm fixing column 2 The side top is movably connected, and the head telescopic column 7 is movably connected to the head fixing column 8, because the arm telescopic column 3 and the arm fixing column 2 are telescopically stretched, and the head fixing column 8 and the head telescopic column 7 are telescopically stretched to the left and right to reach any body type.
  • Different robots can be well stabilized Wearing the damping device body 9, to improve the usability, and back right middle column 4 is attached to a fixed solar panels 5, four corners of the solar panel 5 are fixed to a fixing nut 6.
  • a gravity plate 403 is disposed, and the gravity plate 403 covers the rear side of the back fixing plate 4, and the weight of the gravity plate 403 is 9 kg because the gravity plate 403 is disposed on the back fixing plate.
  • the back fixing plate 4 can first land, buffering as much as possible to reduce the impact force, and then, setting the parachute 107, parachute
  • the right side of the 107 is fixedly connected to the left side of the buckle 105 by the steel wire band 106, because the parachute 107 is installed in the front chest fixing plate 1, and the terminal finds that the robot has a fault and promptly hits Robot parachute 107, to minimize the robot falling damage, resulting in improved safety, thus completing the working process of the main damping device 9.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Robotics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Remote Sensing (AREA)
  • Manipulator (AREA)

Abstract

一种飞行机器人减震设备，包括减震设备主体（9），减震设备主体（9）的左右两侧均安装有前胸固定板（1）和后背固定板（4），且前胸固定板（1）的正面中间固定有手臂固定柱（2），前胸固定板（1）的内侧左边的顶端设置有信号传输器（101），且前胸固定板（1）的内侧中间设置有降落伞槽口（102）。该种飞行机器人减震设备，设置了手臂伸缩柱（3）和头部伸缩柱（7），手臂伸缩柱（3）的左侧顶端与手臂固定柱（2）的右侧顶端活动连接，且头部伸缩柱（7）与头部固定柱（8）活动连接，因为手臂伸缩柱（3）与手臂固定柱（2）左右伸缩，头部固定柱（8）和头部伸缩柱（7）左右伸缩，使得任何体型不一的机器人都能够良好稳固地穿戴该减震设备，提高了实用性。

Description

一种飞行机器人减震设备 技术领域
本发明涉及机器人技术领域，具体为一种飞行机器人减震设备。
背景技术
机器人是自动执行工作的机器装置。它既可以接受人类指挥，又可以运行预先编排的程序，也可以根据以人工智能技术制定的原则纲领行动。它的任务是协助或取代人类的工作，例如生产业、建筑业，或是其它危险的工作，随着时代的进步，机器人的拆装设备也随之增多。
现有的飞行机器人减震设备，不能有效利用周围环境进行节能，无法在坠落过程中提供安全保护，不能灵活的控制减震设备。
发明内容
本发明的目的在于提供一种飞行机器人减震设备，以解决上述背景技术中提出不能有效利用周围环境进行节能，无法在坠落过程中提供安全保护，不能灵活的控制减震设备的问题。
为实现上述目的，本发明提供如下技术方案：一种飞行机器人减震设备，包括减震设备主体，所述减震设备主体的左右两侧均安装有前胸固定板和后背固定板，且前胸固定板的正面中间固定有手臂固定柱，所述前胸固定板的内侧左边的顶端设置有信号传输器，且前胸固定板的内侧中间设置有降落伞槽口，所述降落伞槽口的正面中间安装有固定带，且降落伞槽口的左侧中间固定有环扣底座，所述环扣底座的左侧中间固定有环扣，且环扣设置有多个均匀分布的钢丝带，所述钢丝带的左侧固定有降落伞，所述后背固定柱正面中间固定有手臂伸缩柱，且固定柱的内部设置有若干个均匀分布的弹性伸缩柱和弹性伸缩柱底座，所述固定柱的对立侧固定有重力板，所述前胸固定板 的顶端均设置有2个头部固定柱，所述后背固定柱的顶端均固定有2个头部伸缩柱，且后背固定柱的右侧中间安装有太阳能板，所述太阳能板的4个边角均固定有固定螺母。
优选的，所述手臂伸缩柱的左侧顶端与手臂固定柱的右侧顶端活动连接，且头部伸缩柱与头部固定柱活动连接。
优选的，所述弹性伸缩柱和弹性伸缩柱底座活动连接，且弹性伸缩柱和弹性伸缩柱底座均嵌入设置于后背固定板中。
优选的，所述重力板覆盖与后背固定板的后侧，且重力板的重量为9kg。
优选的，所述降落伞右侧通过钢丝带与环扣的左侧固定连接。
与现有技术相比，本发明的有益效果是：该种飞行机器人减震设备，设置了手臂伸缩柱和头部伸缩柱，手臂伸缩柱的左侧顶端与手臂固定柱的右侧顶端活动连接，且头部伸缩柱与头部固定柱活动连接，因为手臂伸缩柱与手臂固定柱左右伸缩，头部固定柱和头部伸缩柱左右伸缩，达到任何体型不一的机器人能够良好稳固的穿戴该减震设备，提高了实用性，设置了弹性伸缩柱，弹性伸缩柱和弹性伸缩柱底座活动连接，且弹性伸缩柱和弹性伸缩柱底座均嵌入设置于后背固定板中，在机器人飞行过程中，通过弹性伸缩柱和弹性伸缩柱底座伸缩将在空中的冲击力缓冲，避免冲击力过大造成减震设备出现零件错位，提高了安全性，设置了重力板，重力板覆盖与后背固定板的后侧，且重力板的重量为9kg，因为重力板设置在后背固定板上，使得后背固定板的质量超过前胸固定板，使得机器人在掉落时，后背固定板能够先着地，通过缓冲柱尽量的减缓冲击力，设置了降落伞，降落伞右侧通过钢丝带与环扣的左侧固定连接，因为前胸固定板中安装了降落伞，终端发现机器人出现故障时，及时的打开机器人的降落伞，尽量减少机器人坠落的伤害，从而提高了安全性。
附图说明
图1为本发明整体结构示意图；
图2为本发明前胸固定板结构剖视图；
图3为本发明后背固定板结构剖视图；
图4为本发明降落伞槽口局部结构示意图；
图5为本发明信号传输器模块结构流程示意图。
图中：1、前胸固定板，101、信号传输器，102、降落伞槽口，103、固定带，104、环扣底座，105、环扣，106、钢丝带，107、降落伞，2、手臂固定柱，3、手臂伸缩柱，4、后背固定板，401、弹性伸缩柱，402、弹性伸缩柱底座，403、重力板，5、太阳能板，6、固定螺母，7、头部伸缩柱，8、头部固定柱，9、减震设备主体。
具体实施方式
下面将结合本发明实施例中的附图，对本发明实施例中的技术方案进行清楚、完整地描述，显然，所描述的实施例仅仅是本发明一部分实施例，而不是全部的实施例。基于本发明中的实施例，本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例，都属于本发明保护的范围。
请参阅图1-5，本发明提供一种技术方案：一种飞行机器人减震设备，包括1、前胸固定板，101、信号传输器，102、降落伞槽口，103、固定带，104、环扣底座，105、环扣，106、钢丝带，107、降落伞，2、手臂固定柱，3、手臂伸缩柱，4、后背固定板，401、弹性伸缩柱，402、弹性伸缩柱底座，403、重力板，5、太阳能板，6、固定螺母，7、头部伸缩柱，8、头部固定柱，9、减震设备主体，所述减震设备主体9的左右两侧均安装有前胸固定板1和后背固定板4，且前胸固定板1的正面中间固定有手臂固定柱2，所述前胸固定板1的内侧左边的顶端设置有信号传输器101，且前胸固定板1的内侧中间设 置有降落伞槽口102，所述降落伞槽口102的正面中间安装有固定带103，且降落伞槽口102的左侧中间固定有环扣底座104，所述环扣底座104的左侧中间固定有环扣105，且环扣105设置有多个均匀分布的钢丝带106，所述钢丝带106的左侧固定有降落伞107，设置了降落伞107，降落伞107右侧通过钢丝带106与环扣105的左侧固定连接，因为前胸固定板1中安装了降落伞107，终端发现机器人出现故障时，及时的打开机器人的降落伞107，尽量减少机器人坠落的伤害，从而提高了安全性，所述后背固定柱4正面中间固定有手臂伸缩柱3，且固定柱4的内部设置有若干个均匀分布的弹性伸缩柱401和弹性伸缩柱底座402，设置了弹性伸缩柱401，弹性伸缩柱401和弹性伸缩柱底座402活动连接，且弹性伸缩柱401和弹性伸缩柱底座402均嵌入设置于后背固定板4中，在机器人飞行过程中，通过弹性伸缩柱401和弹性伸缩柱底座402伸缩将在空中的冲击力缓冲，避免冲击力过大造成减震设备主体9出现零件错位，提高了安全性，所述固定柱4的对立侧固定有重力板403，设置了重力板403，重力板403覆盖与后背固定板4的后侧，且重力板403的重量为9kg，因为重力板403设置在后背固定板4上，使得后背固定板4的质量超过前胸固定板1，使得机器人在掉落时，后背固定板4能够先着地，通过缓冲尽量的减缓冲击力，所述前胸固定板1的顶端均设置有2个头部固定柱8，所述后背固定柱4的顶端均固定有2个头部伸缩柱7，设置了手臂伸缩柱3和头部伸缩柱7，手臂伸缩柱3的左侧顶端与手臂固定柱2的右侧顶端活动连接，且头部伸缩柱7与头部固定柱8活动连接，因为手臂伸缩柱3与手臂固定柱2左右伸缩，头部固定柱8和头部伸缩柱7左右伸缩，达到任何体型不一的机器人能够良好稳固的穿戴该减震设备主体9，提高了实用性，且后背固定柱4的右侧中间安装有太阳能板5，所述太阳能板5的4个边角均固定有固定螺母6。
工作原理：首先，使用者将减震设备主体9套上飞行机器人的身上，设置了手臂伸缩柱3和头部伸缩柱7，手臂伸缩柱3的左侧顶端与手臂固定柱2 的右侧顶端活动连接，且头部伸缩柱7与头部固定柱8活动连接，因为手臂伸缩柱3与手臂固定柱2左右伸缩，头部固定柱8和头部伸缩柱7左右伸缩，达到任何体型不一的机器人能够良好稳固的穿戴该减震设备主体9，提高了实用性，然后，当飞行机器人在阳光地方下飞行，通过后背固定板4能够有效的将太阳能转化成电能，供飞行机器人使用，节约了飞行成本，接着，设置了重力板403，重力板403覆盖与后背固定板4的后侧，且重力板403的重量为9kg，因为重力板403设置在后背固定板4上，使得后背固定板4的质量超过前胸固定板1，使得机器人在掉落时，后背固定板4能够先着地，通过缓冲尽量的减缓冲击力，随后，设置了降落伞107，降落伞107右侧通过钢丝带106与环扣105的左侧固定连接，因为前胸固定板1中安装了降落伞107，终端发现机器人出现故障时，及时的打开机器人的降落伞107，尽量减少机器人坠落的伤害，从而提高了安全性，从而完成了减震设备主体9的工作过程。
尽管已经示出和描述了本发明的实施例，对于本领域的普通技术人员而言，可以理解在不脱离本发明的原理和精神的情况下可以对这些实施例进行多种变化、修改、替换和变型，本发明的范围由所附权利要求及其等同物限定。

Claims (9)

  1. 一种飞行机器人减震设备，包括减震设备主体(9)，其特征在于：所述减震设备主体(9)的左右两侧均安装有前胸固定板(1)和后背固定板(4)，且前胸固定板(1)的正面中间固定有手臂固定柱(2)，所述前胸固定板(1)的内侧左边的顶端设置有信号传输器(101)，且前胸固定板(1)的内侧中间设置有降落伞槽口(102)，所述降落伞槽口(102)的正面中间安装有固定带(103)，且降落伞槽口(102)的左侧中间固定有环扣底座(104)，所述环扣底座(104)的左侧中间固定有环扣(105)，且环扣(105)设置有多个均匀分布的钢丝带(106)，所述钢丝带(106)的左侧固定有降落伞(107)，所述后背固定柱(4)正面中间固定有手臂伸缩柱(3)，且固定柱(4)的内部设置有若干个均匀分布的弹性伸缩柱(401)和弹性伸缩柱底座(402)，所述固定柱(4)的对立侧固定有重力板(403)，所述前胸固定板(1)的顶端均设置有2个头部固定柱(8)，所述后背固定柱(4)的顶端均固定有2个头部伸缩柱(7)，且后背固定柱(4)的右侧中间安装有太阳能板(5)，所述太阳能板(5)的4个边角均固定有固定螺母(6)。
  2. 根据权利要求1所述的一种飞行机器人减震设备，其特征在于：所述手臂伸缩柱(3)的左侧顶端与手臂固定柱(2)的右侧顶端活动连接。
  3. 根据权利要求2所述的一种飞行机器人减震设备，其特征在于：头部伸缩柱(7)与头部固定柱(8)活动连接。
  4. 根据权利要求1所述的一种飞行机器人减震设备，其特征在于：所述弹性伸缩柱(401)和弹性伸缩柱底座(402)活动连接。
  5. 根据权利要求4所述的一种飞行机器人减震设备，其特征在于：弹性伸缩柱(401)和弹性伸缩柱底座(402)均嵌入设置于后背固定板(4)中。
  6. 根据权利要求1所述的一种飞行机器人减震设备，其特征在于：所述重力板(403)覆盖于后背固定板(4)的后侧。
  7. 根据权利要求1所述的一种飞行机器人减震设备，其特征在于：所述 降落伞(107)右侧通过钢丝带(106)与环扣(105)的左侧固定连接。
  8. 根据权利要求1所述的一种飞行机器人减震设备，其特征在于：所述降落伞(107)活动嵌设于降落伞槽口(102)中。
  9. 根据权利要求1所述的一种飞行机器人减震设备，其特征在于：所述飞行机器人减震设备还包括接收装置，在接收到降落伞启用指令时打开降落伞107。
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Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1393374A (zh) * 2001-07-02 2003-01-29 刘慧茹 背包式战斗机
WO2011002517A2 (en) * 2009-07-03 2011-01-06 Jon Kunowski Turbine powered personal flight system
CN102556348A (zh) * 2010-12-23 2012-07-11 马世强 动力悬挂喷气飞行背包
WO2016210252A1 (en) * 2015-06-26 2016-12-29 Nelson Tyler Back mounted flight machine
CN106377848A (zh) * 2016-12-01 2017-02-08 郑州特别有效营销管理咨询有限公司 高层建筑逃生背包
CN206324263U (zh) * 2016-11-25 2017-07-14 深圳沃海森科技有限公司 高空运动飞行服及推进器结构
CN107398927A (zh) * 2017-08-27 2017-11-28 刘哲 一种飞行机器人减震设备
CN107685867A (zh) * 2017-08-27 2018-02-13 刘哲 一种飞行机器人

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1393374A (zh) * 2001-07-02 2003-01-29 刘慧茹 背包式战斗机
WO2011002517A2 (en) * 2009-07-03 2011-01-06 Jon Kunowski Turbine powered personal flight system
CN102556348A (zh) * 2010-12-23 2012-07-11 马世强 动力悬挂喷气飞行背包
WO2016210252A1 (en) * 2015-06-26 2016-12-29 Nelson Tyler Back mounted flight machine
CN206324263U (zh) * 2016-11-25 2017-07-14 深圳沃海森科技有限公司 高空运动飞行服及推进器结构
CN106377848A (zh) * 2016-12-01 2017-02-08 郑州特别有效营销管理咨询有限公司 高层建筑逃生背包
CN107398927A (zh) * 2017-08-27 2017-11-28 刘哲 一种飞行机器人减震设备
CN107685867A (zh) * 2017-08-27 2018-02-13 刘哲 一种飞行机器人

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