WO2013120357A1 - 飞机防坠自救装置 - Google Patents

飞机防坠自救装置 Download PDF

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Publication number
WO2013120357A1
WO2013120357A1 PCT/CN2012/083170 CN2012083170W WO2013120357A1 WO 2013120357 A1 WO2013120357 A1 WO 2013120357A1 CN 2012083170 W CN2012083170 W CN 2012083170W WO 2013120357 A1 WO2013120357 A1 WO 2013120357A1
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WO
WIPO (PCT)
Prior art keywords
hot
aircraft
hot air
connecting plate
parachute
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PCT/CN2012/083170
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English (en)
French (fr)
Inventor
孙磊
Original Assignee
Sun Lei
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Filing date
Publication date
Application filed by Sun Lei filed Critical Sun Lei
Publication of WO2013120357A1 publication Critical patent/WO2013120357A1/zh

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D17/00—Parachutes
    • B64D17/80—Parachutes in association with aircraft, e.g. for braking thereof

Definitions

  • the invention relates to a transportation safety device, in particular to an aircraft anti-falling self-rescue device.
  • the utility model patent of the utility model discloses an aircraft anti-falling self-rescue device and solves the above technical problems.
  • the patented technology also has the following technical problems: the airbag is easy to explode due to the impact of the huge impact force when the aircraft is falling. It has a destructive effect on the body; at the same time, the stability of the connection between the umbrella stand and the aircraft body needs to be improved.
  • the present invention is to solve the above technical problem, and to provide an aircraft anti-falling self-rescue device, which has a simple structure, and the protection structure does not damage the aircraft body when the aircraft is falling, and the stability of the connection between the aircraft platform and the aircraft body is relatively high.
  • the present invention is achieved by the following technical solutions.
  • the aircraft anti-falling self-rescue device has an upper connecting plate connected to the outer wall of the upper end of the aircraft body; the upper connecting plate is connected with the hot air umbrella column, the hot air umbrella column is connected with the hair umbrella stand; the sending umbrella stand is arranged at the upper end of the hot air umbrella column; the lower connecting plate is installed at the upper end The lower end of the aircraft body; the connecting belt connects the upper connecting plate and the lower connecting plate with the aircraft body, and the lower end of the lower connecting plate is connected with a retractable spring; the sending stand has a hot air parachute and provides hot air energy for the hot air parachute; A plurality of hot gas stations, each of which is connected to the hot gas transfer main pipe through a respective branch hot gas transfer pipe, and the hot gas transfer main pipe is connected with a hot gas source provided in the aircraft body.
  • the above-mentioned hot gas source is an electric start heat source.
  • the lower connecting plate mentioned above is two pieces, and the upper connecting plate is one piece.
  • the above-mentioned hair umbrella stand is equipped with a controller for controlling the hair stand and spring opening.
  • the above hot air stations are 3-10.
  • the above hot air umbrella column has a height of 1-5 meters.
  • the lower end of the spring above is 15-30 cm above the bottom wheel of the aircraft.
  • the present invention has the following advantages and effects:
  • the invention has simple structure and adopts the principle of hot air balloon.
  • the controller When an accident occurs in the aircraft, the controller is turned on, the umbrella stand is activated, and the hot air parachute in the umbrella stand is started by the heat source, rises upward, gives the aircraft an upward force, and makes the aircraft slow. Falling and landing safely, effectively preventing the plane from crashing into an air crash.
  • a connecting plate is installed on the upper and lower sides of the aircraft body, and is connected by a connecting belt, and the transmitting umbrella stand is connected to the upper connecting plate, so that the stability of the connection between the transmitting umbrella stand and the aircraft body is greatly improved, and the spring is used for shock absorption.
  • the aircraft protects the structure from damage to the aircraft's body when it falls.
  • Figure 1 is a schematic side view showing the structure of the present invention.
  • the aircraft anti-dropping self-rescue device of the present invention has the following structure: the upper end wall of the aircraft body 1 is connected with the upper connecting plate 8; the upper connecting plate 8 connected to the hot air umbrella column 2, the hot air umbrella column 2 is connected with the hair umbrella stand 3; the hair stand 3 is arranged at the upper end of the hot air umbrella column 2; the two lower connecting plates 9 are installed on the outer wall of the lower end of the aircraft body 1; 7 Connect to the upper connecting plate 8, the aircraft body 1 and the lower connecting plate 9; the connecting belt 7 connects the upper connecting plate 8 and the lower connecting plate 9 to the aircraft body 1; the lower connecting plate 9 The lower end is connected with a retractable spring 10; the umbrella stand 3 is provided with a hot air parachute 4 and a plurality of hot air tables 5 for supplying hot air energy to the hot air parachute 4, each hot air table 5
  • the hot gas delivery manifold 11 is connected to the hot gas delivery manifold 11 through a respective branch hot gas delivery conduit 11 which is connected to a hot
  • a controller 6 for controlling the umbrella stand 3 and the spring 10 is mounted on the umbrella stand 3 .
  • the above-mentioned hot air table 5 is 3-10.
  • the hot air column 2 has a height of 1-5 meters.
  • the lower end of the spring above is 15-30 cm above the bottom wheel of the aircraft.
  • the controller When an accident occurs in the aircraft, the controller is turned on, the umbrella is activated, and the hot air parachute in the umbrella stand is started by the heat source, rising upwards, giving the aircraft an upward force, causing the aircraft to slowly descend and land safely, effectively preventing the flight opportunity. It’s hard to crash in the air.

Abstract

一种飞机防坠自救装置，飞机机体（1）上端外壁连接有上连接板（8，9）；上连接板（8）与热气伞柱（2）连接，热气伞柱（2）与发伞台（3）连接；发伞台（3）设置在热气伞柱（2）的上端；下连接板（9）安装在飞机机体（1）下端外壁上；连接带（7）将上连接板（8）和下连接板（9）与飞机机体（1）连接在一起，下连接板（9）的下端连接有可伸缩弹簧（10）；发伞台（3）内设有热气降落伞（4）和为热气降落伞（4）提供热气能源的多个热气台（5），每个热气台（5）通过各自的分支热气输送管路与热气输送总管（11）连接，热气输送总管（11）与飞机机体（1）内设置的热气源连接。本发明结构简单，增强了发伞台和飞机机体连接的稳定性，在飞机坠落时保护结构不破坏飞机机体。

Description

飞机防坠自救装置
技术领域
本发明涉及一种交通运输安全装置，尤其涉及一种飞机防坠自救装置。
背景技术
随着科技的发展，飞机已经逐渐成为人们出行的重要交通工具。乘飞机出行具有方便、快捷的特点。民用飞机乘坐的人比较多，一旦飞机遇到危险，很难用跳伞的方式施救。由于气候等因素的影响，飞机出现空难的事故时有发生。当飞机遇到不能排除的事故时，就会导致机毁、人亡，据统计，每年平均有 1500 人由于飞机事故而遇难。这给人们生命及财产带来巨大损失。如何解决飞机遇到事故时能安全降落地面，是本领域技术人员急需解决的技术问题。为了解决上述技术问题，本专利申请人于 2010 年 2 月 4 日申请了专利号为 ZL201020108039.2 的中国实用新型专利，此专利中公开了一种飞机防坠自救装置，解决了上述技术问题，但此专利技术还存在如下技术问题：飞机在坠落时由于巨大冲击力的作用，气囊容易爆炸，对机体产生破坏作用；同时发伞台和飞机机体连接的稳定性还有待提高。
发明内容
本发明就是为了解决上述技术问题，而提供一种飞机防坠自救装置，其结构简单，飞机在坠落时保护结构不破坏飞机机体，发伞台和飞机机体连接的稳定性较高。
为了解决上述技术问题，本实用新型是通过如下技术方案实现的。
飞机防坠自救装置，飞机机体上端外壁连接有上连接板；上连接板与热气伞柱连接，热气伞柱与发伞台连接；发伞台设置在热气伞柱的上端；下连接板安装在飞机机体下端外壁上；连接带将上连接板和下连接板与飞机机体连接在一起，下连接板的下端连接有可伸缩弹簧；发伞台内设有热气降落伞和为热气降落伞提供热气能源的多个热气台，每个热气台通过各自的分支热气输送管路与热气输送总管连接，热气输送总管与飞机机体内设置的热气源连接。
上述的热气源为电启动热气源。
上述的下连接板为两块，上连接板为 1 块。
上述的发伞台上安装有控制发伞台和弹簧开启的控制器。
上述的热气台为 3-10 个。
上述的热气伞柱的高度为 1-5 米。
上述的弹簧下端高于飞机底轮 15-30 厘米。
本发明的优点和效果如下：
由于采用上述结构，使得本发明具有如下优点和效果：
本发明结构简单，采用热气球原理，当飞机发生事故时，开启控制器，启动发伞台，发伞台内的热气降落伞经热源启动，向上升起，给飞机一个向上的力，使飞机缓慢下降，并平安着陆，有效防止飞机遇到空难坠毁。在飞机机体的上下安装了连接板，并通过连接带连接，发伞台连接在上连接板上，使得发伞台和飞机机体连接的稳定性有了较大的提高，采用弹簧进行减震使得飞机在坠落时保护结构不破坏飞机机体。
附图说明
图1是本发明的 侧视结构示意图。
图中， 1 、飞机机体， 2 、热气伞柱， 3 、发伞台， 4 、热气降落伞， 5 、热气台， 6 、控制器， 7 、连接带； 8 、上连接板； 9 、下连接板； 10 、弹簧； 11 、热气输送总管。
具体实施方式
下面结合实施例对本发明做进一步详细说明，但本发明的保护范围不受实施例所限制。
如图 1 所示，本发明飞机防坠自救装置，其结构如下：飞机机体 1 上端外壁连接有上连接板 8 ；上连接板 8 与热气伞柱 2 连接，热气伞柱 2 与发伞台 3 连接；发伞台 3 设置在热气伞柱 2 的上端；两块下连接板 9 安装在飞机机体 1 下端外壁上；连接带 7 与上连接板 8 、飞机机体 1 及下连接板 9 连接；连接带 7 将上连接板 8 和下连接板 9 与飞机机体 1 连接在一起；下连接板 9 的下端连接有可伸缩弹簧 10 ；发伞台 3 内设有热气降落伞 4 和为热气降落伞 4 提供热气能源的多个热气台 5 ，每个热气台 5 通过各自的分支热气输送管路与热气输送总管 11 连接，热气输送总管 11 与飞机机体 1 内设置的热气源连接，热气源为电启动热气源。
发伞台 3 上安装有控制发伞台 3 和弹簧 10 开启的控制器 6 。
上述的热气台 5 为 3-10 个。热气伞柱 2 的高度为 1-5 米。
上述弹簧下端高于飞机底轮 15-30 厘米。
本发明的工作原理如下：
当飞机发生事故时，开启控制器，启动发伞台，发伞台内的热气降落伞经热源启动，向上升起，给飞机一个向上的力，使飞机缓慢下降，并平安着陆，有效防止飞机遇到空难坠毁。

Claims (7)

  1. 飞机防坠自救装置，其特征在于结构如下：飞机机体上端外壁连接有上连接板；上连接板与热气伞柱连接，热气伞柱与发伞台连接；发伞台设置在热气伞柱的上端；下连接板安装在飞机机体下端外壁上；连接带将上连接板和下连接板与飞机机体连接在一起，下连接板的下端连接有可伸缩弹簧；发伞台内设有热气降落伞和为热气降落伞提供热气能源的多个热气台，每个热气台通过各自的分支热气输送管路与热气输送总管连接，热气输送总管与飞机机体内设置的热气源连接 。
  2. 根据权利要求1所述的飞机防坠自救装置，其特征在于所述的热气源为电启动热气源。
  3. 根据权利要求 1 所述的飞机防坠自救装置，其特征在于所述的下连接板为两块，上连接板为 1 块。
  4. 根据权利要求 1 所述的飞机防坠自救装置，其特征在于所述的发伞台上安装有控制发伞台和弹簧开启的控制器。
  5. 根据权利要求 1 所述的飞机防坠自救装置，其特征在于所上述的热气台为 3-10 个。
  6. 根据权利要求 1 所述的飞机防坠自救装置，其特征在于所述的热气伞柱的高度为 1-5 米。
  7. 根据权利要求 1 所述的飞机防坠自救装置，其特征在于所述的弹簧下端高于飞机底轮 15-30 厘米。
PCT/CN2012/083170 2012-02-17 2012-10-19 飞机防坠自救装置 WO2013120357A1 (zh)

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Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN202491924U (zh) * 2012-02-17 2012-10-17 孙磊 飞机防坠自救装置
CN104118565A (zh) * 2014-08-04 2014-10-29 陈世文 飞机降落伞

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6164595A (en) * 1999-04-29 2000-12-26 Williams; Charles Helium actuated airplane parachute
KR20020048139A (ko) * 2000-12-16 2002-06-22 백병룡 비행기용 추락방지장치
US20100127115A1 (en) * 2007-05-08 2010-05-27 Yigal Adir "power jet controller" ball taype
CN201604799U (zh) * 2010-02-04 2010-10-13 孙磊 飞机防坠自救装置
CN201784799U (zh) * 2010-02-04 2011-04-06 孙磊 轮船安全防沉器
CN201793013U (zh) * 2010-07-05 2011-04-13 李轩 自动充气气球热气球降落伞
CN202481272U (zh) * 2012-02-17 2012-10-10 孙磊 轮船防沉装置
CN202491924U (zh) * 2012-02-17 2012-10-17 孙磊 飞机防坠自救装置

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6164595A (en) * 1999-04-29 2000-12-26 Williams; Charles Helium actuated airplane parachute
KR20020048139A (ko) * 2000-12-16 2002-06-22 백병룡 비행기용 추락방지장치
US20100127115A1 (en) * 2007-05-08 2010-05-27 Yigal Adir "power jet controller" ball taype
CN201604799U (zh) * 2010-02-04 2010-10-13 孙磊 飞机防坠自救装置
CN201784799U (zh) * 2010-02-04 2011-04-06 孙磊 轮船安全防沉器
CN201793013U (zh) * 2010-07-05 2011-04-13 李轩 自动充气气球热气球降落伞
CN202481272U (zh) * 2012-02-17 2012-10-10 孙磊 轮船防沉装置
CN202491924U (zh) * 2012-02-17 2012-10-17 孙磊 飞机防坠自救装置

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