JPS5839598A - Safety device for aircraft - Google Patents

Safety device for aircraft

Info

Publication number
JPS5839598A
JPS5839598A JP13777781A JP13777781A JPS5839598A JP S5839598 A JPS5839598 A JP S5839598A JP 13777781 A JP13777781 A JP 13777781A JP 13777781 A JP13777781 A JP 13777781A JP S5839598 A JPS5839598 A JP S5839598A
Authority
JP
Japan
Prior art keywords
center
aircraft
tie
container
safety device
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
JP13777781A
Other languages
Japanese (ja)
Inventor
岩本 孝治
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 JP13777781A priority Critical patent/JPS5839598A/en
Publication of JPS5839598A publication Critical patent/JPS5839598A/en
Pending legal-status Critical Current

Links

Landscapes

  • Emergency Protection Circuit Devices (AREA)
  • Air Bags (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】 図面第1図に示す鉄板製円筒形固定容器2に可動容器1
を摺合し、環状鍔6で固定すれば下部に空$15が出来
る。ここに火薬Kを装置し、これに電熱器を挿入し、電
線で操縦席に結線し。
[Detailed description of the invention] A movable container 1 is attached to a cylindrical fixed container 2 made of iron plate as shown in FIG.
By sliding them together and fixing them with the annular collar 6, an empty space of $15 is created at the bottom. We installed gunpowder K here, inserted an electric heater into it, and connected it to the cockpit with electric wires.

電源及び押ボタンを接続する。可動円筒容器1及び固定
容器2の内面中心部に鉄製環3.3′を溶接し、これに
大小2個の落下傘A、Bの中心紐4.4′を結び付ける
。更に大小二つの傘の外 、側中心゛頂点を短い紐7.
7′で結び中心部Xと弱めの紐Xで結ぶ。次に本装置が
航空機のエンジンの不凋其他の理由で墜落の危険のあっ
た場合。
Connect the power supply and pushbutton. An iron ring 3.3' is welded to the center of the inner surface of the movable cylindrical container 1 and fixed container 2, and the center strings 4.4' of two large and small parachutes A and B are tied to this ring. Furthermore, attach a short string to the outside of the two umbrellas, one large and one small, and the top of the center of the side.
Tie at 7' and tie with a weak string X to the center X. Next, if this device is at risk of crashing due to failure of the aircraft engine or other reasons.

操縦席の押ボタンを押せば火薬が爆発し、可動円筒1は
空中に飛び出し、第2図のA図に示す状態となり、更に
次の!間に紐7.7′は引張られ、X点で切断し、第2
図のB図の状態となり可動円筒1は穏かに落下するJ′
伺木本装置利用例を籏3図に示す。
When the push button on the cockpit is pressed, the gunpowder explodes and the movable cylinder 1 flies into the air, resulting in the state shown in Figure 2 A, and then the next one! In between, the string 7.7' is pulled, cut at the X point, and the second
The state shown in figure B is reached and the movable cylinder 1 falls gently J'
An example of the use of this device is shown in Figure 3.

第3図のA図はヘリコプタ−の場合を示しB図は小型航
空機の場合を示し。
Diagram A in FIG. 3 shows the case of a helicopter, and diagram B shows the case of a small aircraft.

6図は大型航空機の場合であって。Figure 6 shows the case of a large aircraft.

大型機の場合は落下傘を三つ以上とし中心の金は大型と
し紐を長くして傘相互の接触を防ぐ事としたもので、そ
れぞれの傘の大きさは航空機の重重と安全落下速度の設
定により傘の設計をすべきである。
In the case of large aircraft, there are three or more parachutes, the gold in the center is large, and the string is long to prevent the umbrellas from touching each other, and the size of each umbrella is determined by the weight of the aircraft and the safe falling speed. The umbrella should be designed accordingly.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本発明の縦断面図 第2図は本発明の使用状態図 A図は爆発直後の作動図 B図は紐7,7′がX点で切断後の作勧図第3図は本発
明の各航空機の使用状態図1 可動円筒  2. 固定
円筒 3.3′  鉄製環 −4,4′  傘の中心紐5、空
洞 6 可動円筒1の固定釘 7.7′  傘頂点紐 X 弱紐 K 火薬ヤJi出 才2図 手続補正書 昭和56年10月31日 特許庁長官       殿 (特許庁審査官         殿)1、事件の表示 昭和56年字p曝  特許願 第137777号指定面
品および商品の区分 第     類 3、補正をする者 事件との関係         出願人(+所    
       郵便番号 国同同−ロロ4、補正命令の
84寸   昭和  年  月  日507−
Figure 1 is a longitudinal sectional view of the present invention. Figure 2 is a diagram of the present invention in use. Usage state diagram of each aircraft of the present invention 1 Movable cylinder 2. Fixed cylinder 3.3' Iron ring -4,4' Umbrella center string 5, hollow 6 Fixed nail of movable cylinder 1 7.7' Umbrella top string October 31, 2016, Director General of the Patent Office (Dear Examiner of the Patent Office) 1, Indication of the case 1981 character p exposure Patent Application No. 137777 Classification of designated surface goods and goods Category 3, person making the amendment Related applicant (+ place)
Postal code Kuni Dodo - Roro 4, 84 sun of amendment order Showa year month day 507 -

Claims (1)

【特許請求の範囲】 鉄板製円筒形容器1.2を上部より摺合させ。 容器1.2の内部の中心部に鉄製環3.3′を溶接し、
これに大小2個の落下傘A、Bの中心紐4.4′を結び
、又それぞれの傘の外側中心頂点に中心部の弱い短い紐
で7.7′を結んだものを円筒形容器に収納する。鉄板
製円筒容器1.2の摺合した下部の空洞5の下部−に火
薬Kを装置し、これに電熱器を挿入、非常の時、押ボタ
ンを押せば電源に接続火薬が爆発9円筒1は空中に飛び
出し落下傘が開く航空機の安全装置。
[Claims] Cylindrical containers 1.2 made of iron plates are slid together from above. A steel ring 3.3' is welded to the center of the interior of the container 1.2,
Tie the center strings 4.4' of two large and small parachutes A and B to this, and tie 7.7' to the outer center apex of each umbrella with a short, weak string at the center and store them in a cylindrical container. do. Explosive powder K is installed in the lower part of the cavity 5 at the bottom of the iron plate cylindrical container 1.2 that is slid together, and an electric heater is inserted into this.In an emergency, when the push button is pressed, the gunpowder is connected to the power source and the cylinder 1 explodes. An aircraft safety device that launches into the air and opens a parachute.
JP13777781A 1981-09-03 1981-09-03 Safety device for aircraft Pending JPS5839598A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13777781A JPS5839598A (en) 1981-09-03 1981-09-03 Safety device for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13777781A JPS5839598A (en) 1981-09-03 1981-09-03 Safety device for aircraft

Publications (1)

Publication Number Publication Date
JPS5839598A true JPS5839598A (en) 1983-03-08

Family

ID=15206588

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13777781A Pending JPS5839598A (en) 1981-09-03 1981-09-03 Safety device for aircraft

Country Status (1)

Country Link
JP (1) JPS5839598A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03118196U (en) * 1990-03-20 1991-12-05
WO2018216531A1 (en) * 2017-05-26 2018-11-29 ソフトバンク株式会社 Parachute device and flight vehicle

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03118196U (en) * 1990-03-20 1991-12-05
WO2018216531A1 (en) * 2017-05-26 2018-11-29 ソフトバンク株式会社 Parachute device and flight vehicle
JP2018199385A (en) * 2017-05-26 2018-12-20 ソフトバンク株式会社 Parachute device and flying object

Similar Documents

Publication Publication Date Title
JPS5839598A (en) Safety device for aircraft
GB1383512A (en) Detonating cord for aircraft canpoy emergency break-up systems
US2535309A (en) Rocket
US2408246A (en) Aerial cargo landing container
Ottersen et al. X-ray structure of cannabispiran: A novel cannabis constituent
US3187712A (en) Lifesaving device
Ochi et al. Structure of linearol, a novel ditrepenoid from the brown seaweed Dictyota linearis
US3642237A (en) Spiral reefed variable drag parachute
Jones Probabilistic design and reliability(strength and load aspects for composite material structures)
US2950882A (en) Balloon gondola
US3291047A (en) Projectile apparatus for flying objects
SCHATT Flight safety work of the German Aviation and Space Research Institute
Johnson Sounding Rocket Payload Recovery Systems
Ternay et al. 9-Oxothioxanthenium methylides
Landholt et al. Dissection of Hatch Actuator Breech Cartridge, P/N A218-10 (15-1006)
LEWIS Apparatus, techniques and physical parameters of sounding-rocket flights(noting Skylark rocket, for space manufacturing development)
Rothe et al. Development of encasement for emergency dental kit for use on space missions
MORLAN Applications of pyrotechniques in aviation
GABRIELLI Expression for the ideal weight of shell fuselages(Ideal weight of axisymmetric fuselage shells, taking into account load distribution and cabin pressurization)
MORLAN Pyrotechnic applications in aeronautics
KATSIKAS et al. Manned spacecraft nonmetallic-materials flammability selection criteria and requirements(Criteria and requirements governing selection of nonmetallic materials for use in manned spacecraft to control potential fire hazards)
MULLER et al. Factor of safety- USAF design practice(conferences)[Final Report, Jan.- Sep. 1977]
COOPER et al. Resource management on the flight deck(conferences)
Rabenhorst et al. Rocket Escape System with Cruise Using Electric Rotors (Rescuer).
Galyer et al. The photoelectron spectra of hexamethyltungsten and pentamethyltantalum