JPS60174393A - Parachute device for gyrocopter - Google Patents
Parachute device for gyrocopterInfo
- Publication number
- JPS60174393A JPS60174393A JP2869984A JP2869984A JPS60174393A JP S60174393 A JPS60174393 A JP S60174393A JP 2869984 A JP2869984 A JP 2869984A JP 2869984 A JP2869984 A JP 2869984A JP S60174393 A JPS60174393 A JP S60174393A
- Authority
- JP
- Japan
- Prior art keywords
- parachute
- gyrocopter
- parachute device
- pressure gas
- accident
- 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
Links
Landscapes
- Gyroscopes (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】
（唾東上の利用分野）
この発明は超駐緻オートジャイロ、特にパラシュ−トｋ
ＩＩ！＋１えた超転既オートジャイロにｌＮｆる。[Detailed Description of the Invention] (Field of Application of the Invention) This invention relates to a super-tight autogyro, especially a parachute k.
II! +1 to the super-turned autogyro.
（従来技術）
プロペラによる推進装誼を持ち、回転具で浮力を得る超
軽量オートジャイロ、いわゆるジャイロコブターは狭い
場所からの１ＩＩｉ着陸が可能であシ、近年、新しいス
ポーツとして普及しつつ〜ある〇
しかし、ジャイロコブターは風によってバランスを崩し
易く、突風等によシ墜洛事故や接触事故を起こす場合が
ある。しかも、飛行高駅か低く、事故を起こした場診に
操縦者が脱出しても、従来のパラシュートをオリ用して
安全に降下するには尚変が不足し、事故は直ちに操縦者
の死亡につながることも多い口
（発明の目的）
この発Ｅ！ＡＦｉジャイロコブター自体にバラシューｌ
ｋｌ＆付け、事故を生じた場合にはジャイロコツターご
とパラシュートによって降下させることにより死亡番数
を防ごうとするものである。(Prior art) The so-called gyrocopter, an ultra-light autogyro that has a propulsion system using a propeller and obtains buoyancy using a rotating device, is capable of 1IIIi landing from a narrow space, and has become popular as a new sport in recent years. 〇However, gyrocopters tend to lose their balance due to wind, and gusts of wind can cause crashes or collisions. Moreover, the height of the flight was low, and even if the pilot escaped to the scene of the accident, he would not be able to descend safely using a conventional parachute, and the accident would immediately result in the pilot's death. Mouth that is often connected to (purpose of invention) This E! AFi Gyrocopter itself has a rose
This is to prevent fatalities by lowering the gyrocotter with a parachute in the event of an accident.
（発明の構成） 以下図画を鯵照して詳細に説明する。(Structure of the invention) A detailed explanation will be given below with reference to the drawings.
ジャイロコブター１は、プロペラによる推進装置２及び
（ロ）１興３を備えておシ、回転具３の軸４はほぼジャ
イロブタ−全体ｖ）重心位置にあシ、回転翼の浮力によ
ってジャイロブタ−を空中に支える。The gyrocopter 1 is equipped with a propeller-based propulsion device 2 and (b) 1 propulsion 3, and the shaft 4 of the rotating tool 3 is located almost at the center of gravity of the gyrocopter, and the gyro is propelled by the buoyancy of the rotor blades. Support the pig in the air.
この発明においては、回転翼０ｍ１４’ｏ上端にパラシ
ュートを収納した容器５を固定し、事故の際はこのパラ
シュートによって機体ごと安全に降下させる。In this invention, a container 5 containing a parachute is fixed to the upper end of the rotary wing 0m14'o, and in the event of an accident, the entire aircraft is safely lowered using this parachute.
こＯ／＜ラシュート６は、吐富のように先ずパイロット
シュートが開き、これによって主傘が谷詣５から引出さ
れ、Ｋをはらんで開くＩし式のものを月Ｊいてもよいが
、前記のように、ジャイロコブターの飛行褐変が低い点
を４膨、すると、主傘が−く迫の時１ｈ」がなるべく短
いことが電ましい。La Chute 6 may be of the I-style type, where the pilot chute opens first, as in Totomi, and the main umbrella is pulled out from the valley 5, and opens with a K. As mentioned above, if the point at which the flight browning of the gyrocopter is low is set to 4, it is desirable that the period of 1 hour when the main umbrella approaches is as short as possible.
このパラシュート６が開く時間を短かくするためには、
パラシュート６を谷ｂ５からバネ或いは尚圧力スによっ
て別出し、同時に主傘の下縁等、ＩＭｉの位置に配叙し
、収納時は傘と共に折たたまれている柔軟なバ１グ６′
にｄ宜のカス源７からこのバイブロ′に概圧力スを供給
し、バを利用して強制的に開傘させるようにする■がよ
い。この高圧力ス供給には火薬の燃焼ガスの利用等、容
積の方法が利用出来るが、容器５中、〃
のカス源からバイン６によって供給してもよい。In order to shorten the time for this parachute 6 to open,
The parachute 6 is separated from the valley b5 by a spring or a force, and at the same time it is placed at the lower edge of the main umbrella, etc., at the position of IMi, and when stored, a flexible bag 1 6' is folded together with the umbrella.
It is preferable to supply a pressure gas to this vibro' from the scum source 7 and force it to open using a bar. This high-pressure gas can be supplied by a volumetric method such as using the combustion gas of gunpowder, but it may also be supplied from the waste source in the container 5 through the binder 6.
これによって開傘操作から一雄迄の時間を＠Ｌ７〈短縮
することが出来る。As a result, the time from the opening operation to Kazuo can be shortened by @L7.
（発明の幼果）
こυ発明は上記の鉤成を有するので、以下のような顕著
な効果を奏する。(Effects of the Invention) Since this invention has the features described above, it has the following remarkable effects.
■ ジャイロコグター自犀にパラシュートを敗付けたの
で、事故発生時には機体こと、パラシュートによって安
全に降下出来る。■ Since the parachute was defeated by the Gyrocogter Scythe, in the event of an accident, the aircraft can descend safely using the parachute.
■ パラシュートを回転翼の軸頂部に嘔付けたので、既
存のジャイロコグターにびんに取付けることが出来る。■ Since the parachute is attached to the top of the shaft of the rotor, it can be attached to the existing gyrocogter.
■ パラシュートをジャイロコグターＱ服心近くに収け
られた回転Ａ＠に嘔付けたので、機体を安矩して吊るこ
とが出来、安全カバラシニート降下？Ｉ−町舵とする口
■ 高圧ガスによって強制的に開傘させると、パラシュ
ートが開く迄の時間が短縮され、低壁からの降下を可能
とし、特に飛行間ｋを高くとれないジャイロコグターの
安全を高める口４、 図面’７）簡鵬な説明
図はこの発明のパラシュート装置の１夾施し□を示し、
パラシュートが開傘した状態の概念図である１
特ｈト出願人 香 内 登
出願人代理人 弁理士 性 藤 文 彬（ｆユか１名ン■ I put the parachute in the rotating A @ stored near the center of Gyrocogter Q, so I was able to safely hang the aircraft and descend safely. ■ Forcibly opening the parachute using high-pressure gas shortens the time it takes for the parachute to open, making it possible to descend from a low wall, especially for gyrocoggers that cannot maintain a high distance between flights. 4.Drawing '7) A simple explanatory drawing shows one implementation of the parachute device of this invention,
This is a conceptual diagram of the state in which the parachute is opened.
Claims (1)
ための回転具を封するＨｉ軽軽舟飛行機おいて、回転Ｘ
’７）回転軸境部にパラシュート’ｔｔｉ！！Ｊ嚇した
ジャイロコブターのパラシュート装置 ２）上ｇ（Ｈパラシュートは、主傘に沿って来秋なパイ
プ゛を配置し、該パイプに筒圧力スを送入して強制的に
開傘させることを％畝とするジャイロコブターのバラシ
ュ〜１１[Claims] 1) In a Hi light boat airplane that seals a 7° lobera device for obtaining propulsive force and a rotating device for borrowing buoyancy, rotation
'7) Parachute 'tti at the boundary of the rotation axis! ! Parachute device for the threatened Gyrocopter 2) Upper g (H parachute consists of arranging a pipe along the main umbrella and forcing it to open by sending pressure gas into the pipe. Barash of Gyrocopter with % furrow ~ 11
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2869984A JPS60174393A (en) | 1984-02-20 | 1984-02-20 | Parachute device for gyrocopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2869984A JPS60174393A (en) | 1984-02-20 | 1984-02-20 | Parachute device for gyrocopter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS60174393A true JPS60174393A (en) | 1985-09-07 |
Family
ID=12255716
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2869984A Pending JPS60174393A (en) | 1984-02-20 | 1984-02-20 | Parachute device for gyrocopter |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS60174393A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0487382U (en) * | 1990-12-06 | 1992-07-29 | ||
| WO2017036080A1 (en) * | 2015-09-02 | 2017-03-09 | 河南三和航空工业有限公司 | Parachute equipped autogyro and manufacturing method |
| JP2018154249A (en) * | 2017-03-17 | 2018-10-04 | 東芝電波プロダクツ株式会社 | Safety device and method for drone and drone |
| WO2018190319A1 (en) * | 2017-04-11 | 2018-10-18 | 日本化薬株式会社 | Flight vehicle and method for controlling flight vehicle |
| JP2020049972A (en) * | 2018-09-21 | 2020-04-02 | 日本化薬株式会社 | Flying body with expansion device of parachute or paraglider |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS48104300A (en) * | 1972-04-13 | 1973-12-27 | ||
| JPS5041300A (en) * | 1973-06-02 | 1975-04-15 |
-
1984
- 1984-02-20 JP JP2869984A patent/JPS60174393A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS48104300A (en) * | 1972-04-13 | 1973-12-27 | ||
| JPS5041300A (en) * | 1973-06-02 | 1975-04-15 |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0487382U (en) * | 1990-12-06 | 1992-07-29 | ||
| WO2017036080A1 (en) * | 2015-09-02 | 2017-03-09 | 河南三和航空工业有限公司 | Parachute equipped autogyro and manufacturing method |
| JP2018154249A (en) * | 2017-03-17 | 2018-10-04 | 東芝電波プロダクツ株式会社 | Safety device and method for drone and drone |
| WO2018190319A1 (en) * | 2017-04-11 | 2018-10-18 | 日本化薬株式会社 | Flight vehicle and method for controlling flight vehicle |
| JPWO2018190319A1 (en) * | 2017-04-11 | 2020-03-05 | 日本化薬株式会社 | Flying object and control method of flying object |
| JP2020049972A (en) * | 2018-09-21 | 2020-04-02 | 日本化薬株式会社 | Flying body with expansion device of parachute or paraglider |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Chambers et al. | Aerodynamic characteristics of airplanes at high angles of attack | |
| US6373521B1 (en) | Aircraft incident surveillance system | |
| CN109204834A (en) | Flapping wing landing knapsack | |
| JPS60174393A (en) | Parachute device for gyrocopter | |
| CN108163179A (en) | A kind of near space aerostatics distribution method and dispensing apparatus | |
| Burk Jr et al. | Radio-controlled model design and testing techniques for stall/spin evaluation of general-aviation aircraft | |
| CN206900650U (en) | A kind of vertical coaxial dual-rotor helicopter | |
| JPS59100098A (en) | Stabilizer for injected seat | |
| RU2152891C1 (en) | Helicopter | |
| Bowman | Dynamic Model Tests at Low Subsonic Speeds of Project Mercury Capsule Configurations with and without Drogue Parachutes | |
| Darcy | Russian-English aerospace dictionary | |
| GB1501685A (en) | Flying toy | |
| JPS5927213A (en) | Method for performing photographing and measurement from up in the air | |
| Blackburn | Aces Wild: The Race for Mach 1 | |
| Peterson | High-performance parachutes | |
| Davidson et al. | Air | |
| Bond | Fleet Air Arm Boys: Helicopters: True Tales from Royal Navy Men and Women Air and Ground Crew | |
| Labun et al. | Progress in sealed parachute development | |
| Maurer et al. | Project Hummingbird: recovery of a rocket using autorotation | |
| Kerr et al. | SPINNING | |
| Burgess et al. | Fifteen minutes that stopped a nation | |
| Celniker et al. | Stopped and Slow Rotor Aircraft Configuration | |
| JP4019165B2 (en) | High altitude return and aerial powered balloon and its operation method | |
| Whitlock et al. | Performance Characteristics of a Preformed Elliptical Parachute at Altitudes Between 200,000 and 100,000 Feet Obtained by In-flight Photography | |
| Klinar et al. | Supplementary Investigation in the Free-Spinning Tunnel of a 1/24-Scale Model of the Grumman F9F-6 Airplane Incorporating only Flaperons for Lateral Control, TED No. NACA DE 364 |