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JPS59209999A - Device for relaxing shock on emergency drop of aircraft - Google Patents

Device for relaxing shock on emergency drop of aircraft

Info

Publication number
JPS59209999A
JPS59209999A JP16513981A JP16513981A JPS59209999A JP S59209999 A JPS59209999 A JP S59209999A JP 16513981 A JP16513981 A JP 16513981A JP 16513981 A JP16513981 A JP 16513981A JP S59209999 A JPS59209999 A JP S59209999A
Authority
JP
Japan
Prior art keywords
rocket
aircraft
parachute
emergency drop
emergency
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP16513981A
Other languages
Japanese (ja)
Inventor
且元 原村
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to JP16513981A priority Critical patent/JPS59209999A/en
Publication of JPS59209999A publication Critical patent/JPS59209999A/en
Pending legal-status Critical Current

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  • Tires In General (AREA)
  • Alarm Systems (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 現在の航空機に於ては離着陸時の事故に対しての救命対
策は色々あるが離陸直後飛行不能、高空エンジンストツ
プ、空中衝突等の対策は皆無である。今日の様に広く航
空機が日常利用されている時乗客の生命をただ経済性や
快適性の様な生命の重さに比べればとるに足りない問題
に固執することなく万人が求める人命の安全の保障をも
たらすことを目的とする。事故を起こさないというパイ
ロツトの安全対策は勿論必要であるがそれぞれでは不十
分であるから非常時物理的に人命の救命装置たることを
本発明は目的とする。
DETAILED DESCRIPTION OF THE INVENTION There are various life-saving measures for current aircraft in the event of an accident during take-off or landing, but there are no measures for situations such as inability to fly immediately after take-off, high-altitude engine stop, mid-air collision, etc. When airplanes are widely used on a daily basis as they are today, the safety of human life is what everyone seeks, without fixating on issues such as economy and comfort, which are trivial compared to the weight of life. The purpose is to provide security. Although safety measures for pilots to prevent accidents are of course necessary, they are insufficient, so the present invention aims to provide a device that physically saves lives in emergencies.

次に図面に基づく実例に基づいてこの発明を説明する。Next, the present invention will be explained based on an example based on the drawings.

第1,2,3図が本発明の装置である。本発明では離陸
直後飛行不可能時の為特に極小ロケツトbを用いる。そ
れはロケツトでパラシユートeを開花可能な位置迄上げ
る為である.これは高空に於いても用いてもさしつかえ
ないから非常時はいつでもこのソケツトを作動させるも
のとする。パラシユートをジエラルミン製の流線形の人
物第1〜3図に大型パラシユート数個を入れ仕切り入の
右側に細長いワイヤーfを入れる。これは各パラシユー
トとロケツトにつながれておりロケツトでパラシユート
開花可能位置迄引つぱることによつてパラシユートを開
花させる。その際パラシユートにロケツト噴射で破損を
与えぬ為ワイヤーはかなり長くする。ボタン操作により
ロケツト発射と同時に第3図のgの様に人物の上半分が
半開きになりワイヤーとパラシユートが外に出現する。
Figures 1, 2 and 3 show the apparatus of the present invention. In the present invention, a very small rocket b is especially used for when flight is impossible immediately after takeoff. The reason for this is to use a rocket to raise Parachute e to a position where it can bloom. Since this can be used even at high altitudes, this socket shall be activated at any time in an emergency. Place several large parachutes into the streamlined figures 1 to 3 made of Dierarmine, and insert a long thin wire f into the right side of the partition. This is connected to each parachute and a rocket, and the rocket causes the parachute to bloom by pulling it to a position where the parachute can bloom. At that time, the wire should be quite long so that the parachute will not be damaged by the rocket jet. By pressing the button, the rocket launches, and at the same time, the upper half of the person opens half-way, and the wire and parachute appear outside, as shown in Figure 3 (g).

スロケツト部分は翼の場合は発射は容易だがロケツトが
操縦帯のすぐ後方の飛行機の天井部分にとりつけられて
いる場合はロケツト噴射部分の機体はそれによつて機体
に穴などのあくことのない様に強度の金属をあてるもの
とする。緊急時はパイロツトが全パラシユートの操作を
手許のボタン等で操作するものとするが方一これが不可
能の場合及び空中衝突時、空中分解時の為乗客用の爲非
常ボタンを取りつけ付近のパラシユートが開く様にする
。なおバランス等は生死を問題にする時には問題ではな
く例えさかさまであろうと無事地上に着地出来ればよい
のである。流線形カプセルの中に大型パラシユートを納
入することにより機内のスペースは従来通りで乗客貨物
運行に支障はなくこのカプセルは航空機の重量に応じて
大きさを変え個数をふやすことにより数百トンの重量に
も耐えられる等の効果がある.又付ける場所はバランス
を考え適当に付ける。この発明は以上説明した様に離陸
以後着地迄の空中に於ける飛行可能時の為地上への航空
機着地の衝撃を緩和することによつて乗客の生命を救う
ことに効果がある。
If the rocket part is on the wing, it is easy to launch, but if the rocket is attached to the ceiling of the airplane just behind the control zone, the rocket injection part of the fuselage must be mounted to prevent holes from being made in the fuselage. It shall be made of strong metal. In the event of an emergency, the pilot shall operate all parachutes using buttons at hand, but if this is not possible, or in the event of a mid-air collision or disintegration, an emergency button for passengers will be installed and parachutes nearby Let it open. Note that balance is not an issue when it comes to life and death; it is just a matter of being able to land safely on the ground, even if you are upside down. By delivering a large parachute inside a streamlined capsule, the space inside the aircraft remains the same as before, and there is no problem with passenger cargo operations.The capsule can be changed in size according to the weight of the aircraft and the number of pieces can be increased, allowing it to weigh several hundred tons. It has the effect of being able to withstand Also, consider the balance and attach it appropriately. As explained above, this invention is effective in saving the lives of passengers by alleviating the impact of an aircraft landing on the ground during the time when it is possible to fly in the air after takeoff until landing.

図面の簡単な説明 A図は本発明装置を航空機に取りつ
ける時の見取図。B図はヘリコプターへの応用の見取図
.第1図は側面図、第2図は平面図、第3図は立面図。
BRIEF DESCRIPTION OF THE DRAWINGS Figure A is a sketch when the device of the present invention is installed on an aircraft. Figure B is a sketch of the application to a helicopter. Figure 1 is a side view, Figure 2 is a plan view, and Figure 3 is an elevation view.

b…極小ロケツト、c…機体への取付け部分、d…仕切
り、e…パラシユート、f…ワイヤー、g…使用時開い
た時の見取図。
b...minimum rocket, c...attachment part to the fuselage, d...partition, e...parachute, f...wire, g...schematic diagram when opened during use.

Claims (2)

【特許請求の範囲】[Claims] 1.極小ロケツトを設置した流線形カプセルの中にパラ
シユートとこのパンシユートとロケツトをつなぐ細長い
ワイヤーを入れパイロツトが手許のボタンを押すことに
よりロケツトと装置が作動しパラシユートが開く装置。
1. A device in which a parachute and a long thin wire connecting the panchute and the rocket are placed inside a streamlined capsule in which an extremely small rocket is installed, and when the pilot presses a button in his hand, the rocket and device are activated and the parachute opens.
2.パイロツトが操作不能の時乗客用に非常ボタンを数
個所に設置する.
2. Emergency buttons will be installed in several places for passengers to use when the pilot is inoperable.
JP16513981A 1981-10-16 1981-10-16 Device for relaxing shock on emergency drop of aircraft Pending JPS59209999A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP16513981A JPS59209999A (en) 1981-10-16 1981-10-16 Device for relaxing shock on emergency drop of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP16513981A JPS59209999A (en) 1981-10-16 1981-10-16 Device for relaxing shock on emergency drop of aircraft

Publications (1)

Publication Number Publication Date
JPS59209999A true JPS59209999A (en) 1984-11-28

Family

ID=15806630

Family Applications (1)

Application Number Title Priority Date Filing Date
JP16513981A Pending JPS59209999A (en) 1981-10-16 1981-10-16 Device for relaxing shock on emergency drop of aircraft

Country Status (1)

Country Link
JP (1) JPS59209999A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03118196U (en) * 1990-03-20 1991-12-05

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4004764A (en) * 1974-05-13 1977-01-25 The United States Of America As Represented By The Secretary Of The Navy Drogue chute extraction

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4004764A (en) * 1974-05-13 1977-01-25 The United States Of America As Represented By The Secretary Of The Navy Drogue chute extraction

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03118196U (en) * 1990-03-20 1991-12-05

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