JP2015131504A - parachute - Google Patents

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JP2015131504A
JP2015131504A JP2014002429A JP2014002429A JP2015131504A JP 2015131504 A JP2015131504 A JP 2015131504A JP 2014002429 A JP2014002429 A JP 2014002429A JP 2014002429 A JP2014002429 A JP 2014002429A JP 2015131504 A JP2015131504 A JP 2015131504A
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fixed
parachute
umbrella
tank
airflow
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廖學志
Shueh-Chih Liao
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Abstract

PROBLEM TO BE SOLVED: To provide a parachute which hardly makes injuries even by receiving no prolonged period of operation training with no high specialty of operation charts.SOLUTION: A guide ring 30 is provided in the outer periphery of a spherical type shade 20. Since the guide ring has the effect of collecting air streams and enables an auxiliary shade 40 located above the guide ring to smoothly be developed with collected air streams, even a user with no operation experience can smoothly open the auxiliary shade. Further, the structure shows a symmetry of revolution on the axis of the center axis of the spherical type shade and has the effect of taking a balance when falling.

Description

本発明は、人や物が高所から降下する際の緩速降下装置に関する。   The present invention relates to a slow descent device when a person or an object descends from a high place.

一般的なパラシュートは、開いた傘布を主体とし、周囲に複数の接続ロープを固設し、接続ロープの他端とユーザとを固定し、使用する際、傘布に降下時の風抵抗が増大して降下速度が減速する効果を奏する。
しかし、従来のパラシュートの改良の多くがさらに降下速度を減速させるために、パラシュートの形状を変更して、パラシュートの風抵抗を増大させることに重点が置かれていた。
A general parachute is mainly composed of an open umbrella cloth, a plurality of connection ropes are fixed around it, and the other end of the connection rope and the user are fixed. This increases the speed of descent and slows down.
However, many of the improvements in the conventional parachute have focused on changing the shape of the parachute to increase the wind resistance of the parachute in order to further reduce the descending speed.

米国特許出願公開第US1185537号公報US Patent Application Publication No. US1185537

然しながら、前述した従来のパラシュートでは、使用前に長時間の操作訓練が必須であり、さもなければ使用面で極めて怪我をし易いため、訓練を受けたことのないユーザでもどのようにしてパラシュートで高所から降下することができるかが本発明の創作の動機である。
この目的の達成が可能な従来のパラシュートは(特許文献1参照)、自動オープン機能を備え、操作経験のないユーザでもスムーズにパラシュートを開くことができる旨開示しているが、降下の際になおもアンバランスとなる問題があった。
However, the above-mentioned conventional parachute requires long-time operation training before use, and it is extremely easy to get injured in terms of use. The motive of creation of the present invention is to be able to descend from a high place.
A conventional parachute capable of achieving this object (see Patent Document 1) discloses that it has an automatic opening function, and even a user with no operating experience can open the parachute smoothly. There was also an unbalanced problem.

そこで、本発明者は上記の欠点が改善可能と考え、鋭意検討を重ねた結果、合理的かつ効果的に課題を改善する本発明の提案に到った。   Therefore, the present inventor considered that the above-mentioned drawbacks can be improved, and as a result of intensive studies, the present inventor has arrived at the proposal of the present invention for improving the problem reasonably and effectively.

本発明は、このような従来の問題に鑑みてなされたものである。上記課題解決のため、本発明は、操作経験のないユーザでも安全且つ安定して降下することができるパラシュートを提供することを主目的とする。   The present invention has been made in view of such conventional problems. In order to solve the above problems, it is a main object of the present invention to provide a parachute that can be safely and stably lowered even by a user who has no operation experience.

上述した課題を解決し、目的を達成するための本発明に係るパラシュートは、下降物の降下速度を減速させるパラシュートであって、中心軸を備え、空気注入孔を開設し、前記空気注入孔に栓部を設け、底部に前記中心軸を囲繞して複数の連接部に固設し、前記連接部の他端は前記下降物と結合する球状傘と、前記中心軸を囲繞して前記球状傘の周囲に固設し、リングと前記球状傘の下方に延在するすそ部を備え、前記リングの底端面に少なくとも3つの気流案内用凹部を成型し、各気流案内用凹部は前記球状傘の上方に気流ダクトを突設して成型し、前記気流ダクトの末端に案内孔を開設し、前記気流ダクトの頂部に少なくとも3つのタンクを成型し、前記タンクの下端面は前記案内孔と連通し、前記案内用リングは前記中心軸を軸とする回転対称構造とする案内用リングと、それぞれ複数の固定部で各タンク内部と固着する少なくとも3つの補助用傘と、を備えることを特徴とする。   The parachute according to the present invention for solving the above-described problems and achieving the object is a parachute for decelerating the descending speed of a descending object, comprising a central axis, opening an air injection hole, A stopper is provided, the bottom is surrounded by the central axis and fixed to a plurality of connecting parts, and the other end of the connecting part is connected to the descending object, and the central axis is surrounded by the spherical umbrella. A ring and a skirt extending below the spherical umbrella, and forming at least three airflow guide recesses on the bottom end surface of the ring, and each airflow guide recess is formed on the spherical umbrella. An airflow duct is formed by projecting upward, a guide hole is formed at the end of the airflow duct, at least three tanks are formed at the top of the airflow duct, and the lower end surface of the tank communicates with the guide hole The guide ring is centered on the central axis. A guide ring for the rolling symmetrical structure, each of at least three auxiliary bevel fixed with each tank interior at a plurality of fixing portions, characterized in that it comprises a.

なお、本発明の案内用リングは気流を集める効果を有し、積載した下降物が降下する際、気体は案内用リング下方のすそ部で集められ、気流案内用凹部から気流ダクトに流入し、最終的にタンクから吹き出すため、タンク内の補助用傘は始動時にどんな形態であっても、タンクから吹き出す気流によってスムーズに開く。
また、案内用リングは中心軸を軸とする回転対称構造であることから、降下する際、安定してバランスを取る効果があるので、ユーザは訓練の有無に関係なく、安全且つ安定して降下する目的を達成することができる。
The guide ring of the present invention has an effect of collecting the airflow, and when the loaded falling object descends, the gas is collected at the skirt portion below the guide ring, flows into the airflow duct from the airflow guide recess, In order to finally blow out from the tank, the auxiliary umbrella in the tank is smoothly opened by the air flow blown out of the tank in any form at the time of starting.
In addition, since the guide ring has a rotationally symmetric structure with the central axis as the axis, it has the effect of balancing stably when descending, so the user can descend safely and stably regardless of whether or not they are trained. Can achieve the purpose.

本発明によれば、操作経験のないユーザでも安全且つ安定して降下することができる。   According to the present invention, even a user who has no operation experience can descend safely and stably.

本発明の第1実施形態によるパラシュートが開く時の傾斜の模式図である。It is a schematic diagram of the inclination when the parachute by 1st Embodiment of this invention opens. 本発明の第1実施形態によるパラシュートの断面模式図である。It is a cross-sectional schematic diagram of the parachute by 1st Embodiment of this invention. 本発明の第1実施形態によるパラシュートのタンク構造を示す一部の断面図である。It is a partial sectional view showing the tank structure of the parachute according to the first embodiment of the present invention. 本発明の第2実施形態によるパラシュートの傾斜の外観図である。It is an external view of the inclination of the parachute by 2nd Embodiment of this invention.

以下に図面を参照して、本発明を実施するための形態について、詳細に説明する。なお、本発明は、以下に説明する実施形態に限定されるものではない。   Hereinafter, embodiments for carrying out the present invention will be described in detail with reference to the drawings. Note that the present invention is not limited to the embodiments described below.

本発明の第1実施形態の構成を図1から図3に示す。なお、本発明に係るパラシュートの好適な実施形態は図1から4のように、下降物60の降下速度を減速させ、球状傘20、案内用リング30、及び4つの補助用傘40からなり、球状傘20は複合纖維素材で製造された可撓性構造で、その内部に密度の低い気体を充満させる。
球状傘20は中心軸a1を備え、球状傘20の内部は中心軸a1の方向に収納用チャンネル21があり、収納用チャンネル21は球状傘20の頂部と底部にそれぞれ頂部開口部211と底部開口部212がある。収納用チャンネル21内に貫通柱22を穿設し、貫通柱22はそれぞれ頂部クランプ221と底部クランプ222で頂部開口部211と底部開口部212を密閉して球状傘20を固定することによって、球状傘20が過大な気圧で捻じ曲がって変形するのを防止する。
貫通柱22は球状傘20が風抵抗に耐え得る能力を強化し、球状傘20の底部開口部212の周囲に空気注入孔23を開設する。空気注入孔23は球状傘20と底部クランプ222を貫通して、空気注入孔23を密閉する栓部24を設ける。球状傘20の底部に中心軸a1を囲繞して複数の連接部25を固設し、連接部25は高い張力を有するナイロンロープで、他端で下降物60と結合させる。
The configuration of the first embodiment of the present invention is shown in FIGS. 1 to 4, the preferred embodiment of the parachute according to the present invention comprises a spherical umbrella 20, a guide ring 30, and four auxiliary umbrellas 40, which reduce the descending speed of the descending object 60, The spherical umbrella 20 is a flexible structure made of a composite fiber material, and the inside thereof is filled with a low density gas.
The spherical umbrella 20 has a central axis a1, and the inside of the spherical umbrella 20 has a storage channel 21 in the direction of the central axis a1, and the storage channel 21 has a top opening 211 and a bottom opening at the top and bottom of the spherical umbrella 20, respectively. There is a section 212. A through pillar 22 is drilled in the storage channel 21, and the through pillar 22 is formed into a spherical shape by fixing the spherical umbrella 20 by sealing the top opening 211 and the bottom opening 212 with the top clamp 221 and the bottom clamp 222, respectively. The umbrella 20 is prevented from being twisted and deformed by excessive atmospheric pressure.
The through column 22 reinforces the ability of the spherical umbrella 20 to withstand wind resistance, and opens an air injection hole 23 around the bottom opening 212 of the spherical umbrella 20. The air injection hole 23 penetrates the spherical umbrella 20 and the bottom clamp 222 and is provided with a plug portion 24 that seals the air injection hole 23. A plurality of connecting portions 25 are fixed to the bottom of the spherical umbrella 20 so as to surround the central axis a1, and the connecting portions 25 are nylon ropes having high tension and are connected to the descending object 60 at the other end.

案内用リング30は中心軸a1を囲繞して球状傘20の周囲に固設し、リング31と球状傘20下方に延在するすそ部32を備え、リング31の底端面に4つの気流案内用凹部311を成型し、各気流案内用凹部311は球状傘20の上方に気流ダクト33を突設して成型する。気流ダクト33は可撓性材料で製造された構造で、上方に次第に収縮する錐形であり、気流ダクト33の末端に案内孔331を開設して4つのタンク34を成型し、その中央に補助軸a2を備える。
タンク34の上下は開口部341のある円柱形で、タンク34の中央部に底部環状台座346を突設して成型し、底部環状台座346の周囲に円柱空間347を空け、気流ダクト33を円柱空間347内に設けることで、底部環状台座346の頂部の中央部と案内孔331とを連通させる。
タンク34内に複数の滑り柱35、クランプ342、及び移動ブロック343を設け、滑り柱35は底部環状台座346の頂部周囲に穿設し、滑り柱35を移動端351で底部環状台座346の上方に位置させ、作動端352で底部環状台座346の下方に位置させる。クランプ342の一端は回転点348で弾性部材344と結合させ、弾性部材344の他端は作動端352に固設し、クランプ342の他端は気流ダクト33の周囲に位置させる。移動ブロック343は各滑り柱35の移動端351に固設する。
案内用リング30は中心軸a1を軸とする回転対称構造で、各タンク34も補助軸a2を軸とする回転対称構造である。案内用リング30の頂部に固定リング36を成型し、固定リング36は中心軸a1を囲繞して球状傘20の周囲に固設する。固定リング36は球状傘20が風抵抗に耐え得る能力を強化して、球状傘20が過大な気圧で捻じ曲がって変形するのを防止する。固定リング36上に4つの補助孔361を開設し、各タンク34は穿設した上で各補助孔361内に位置決めする。
The guide ring 30 surrounds the central axis a 1 and is fixed around the spherical umbrella 20, and includes a ring 31 and a skirt portion 32 extending below the spherical umbrella 20, and four airflow guides are provided on the bottom end surface of the ring 31. The recesses 311 are formed, and each of the airflow guide recesses 311 is formed by projecting an airflow duct 33 above the spherical umbrella 20. The airflow duct 33 is a structure made of a flexible material and has a conical shape that gradually contracts upward. A guide hole 331 is formed at the end of the airflow duct 33 to form four tanks 34, and an auxiliary is provided at the center. An axis a2 is provided.
The upper and lower sides of the tank 34 have a cylindrical shape with an opening 341, and a bottom annular pedestal 346 is formed projecting from the center of the tank 34, a cylindrical space 347 is formed around the bottom annular pedestal 346, and the airflow duct 33 is formed into a cylinder. By providing in the space 347, the center part of the top part of the bottom part annular base 346 and the guide hole 331 are connected.
A plurality of sliding columns 35, clamps 342, and moving blocks 343 are provided in the tank 34, and the sliding columns 35 are drilled around the top of the bottom annular pedestal 346, and the sliding columns 35 are positioned above the bottom annular pedestal 346 at the moving end 351. At the working end 352 and below the bottom annular pedestal 346. One end of the clamp 342 is coupled to the elastic member 344 at the rotation point 348, the other end of the elastic member 344 is fixed to the operating end 352, and the other end of the clamp 342 is positioned around the airflow duct 33. The moving block 343 is fixed to the moving end 351 of each sliding column 35.
The guide ring 30 has a rotationally symmetric structure with the central axis a1 as an axis, and each tank 34 also has a rotationally symmetric structure with the auxiliary axis a2 as an axis. A fixing ring 36 is molded on the top of the guide ring 30, and the fixing ring 36 is fixed around the spherical umbrella 20 so as to surround the central axis a <b> 1. The fixing ring 36 reinforces the ability of the spherical umbrella 20 to withstand wind resistance, and prevents the spherical umbrella 20 from being twisted and deformed by excessive atmospheric pressure. Four auxiliary holes 361 are opened on the fixing ring 36, and each tank 34 is drilled and positioned in each auxiliary hole 361.

補助用傘40はそれぞれ複数の高い張力のナイロンロープを固定部41とし、滑り柱35の移動端351に固設して、各固定部41は等分に移動端351上に固設する。   The auxiliary umbrellas 40 each have a plurality of high-strength nylon ropes as fixed portions 41 and fixed to the moving end 351 of the sliding column 35, and each fixed portion 41 is equally fixed on the moving end 351.

図1は本発明のパラシュートが降下する際、各補助用傘40が完全に開いた状態である。ユーザが高所から降下する際、重力により下方へ落下すると、このとき空気が本発明の球状傘20と案内用リング30の底部にぶつかることで、降下方向と反対の空気浮力を生じて、減速降下する効果を奏する。
また、図2に示すように、本発明における特設の案内用リング30には気流を集める効果があり、本発明では積載された下降物60が下降する際、気体が案内用リング30下方のすそ部32で收集され、気流案内用凹部311を経て気流ダクト33に流入して、最終的にタンク34から吹き出されることから、タンク34内の補助用傘40が始動時にどのような形態であっても、タンク34から吹き出す気流によりスムーズに開いて、空気の浮力が一層増大し、ユーザの降下速度が減速されて、安全に降下する効果が達成される。
FIG. 1 shows a state in which each auxiliary umbrella 40 is fully opened when the parachute of the present invention is lowered. When the user descends from a high place and falls downward due to gravity, the air collides with the bottom of the spherical umbrella 20 and the guide ring 30 of the present invention, thereby generating an air buoyancy opposite to the descending direction and decelerating. Has the effect of descending.
Further, as shown in FIG. 2, the special guide ring 30 in the present invention has an effect of collecting an air flow. In the present invention, when the loaded descending object 60 is lowered, the gas is placed under the guide ring 30. Since it is collected by the section 32, flows into the airflow duct 33 through the airflow guide recess 311 and is finally blown out of the tank 34, the auxiliary umbrella 40 in the tank 34 is in any form at the time of starting. However, it opens smoothly by the air flow blown out from the tank 34, the buoyancy of the air is further increased, the descent speed of the user is reduced, and the effect of safely descending is achieved.

案内用リング30は中心軸a1を軸とする回転対称構造であり、補助用傘40が移動端351に固設されても、なおも中心軸a1を軸とする回転対称を維持し、各タンク34と補助用傘40も補助軸a2を軸とする回転対称構造であることから、降下する際、本発明は全体的に安定したバランス効果がある(図1から図3参照)。
また、本発明のタンク34内には収納空間345があるため、補助用傘40は未使用の際は畳んで、タンク34の収納空間345に收納することができ、見栄えが良いだけでなく、効果的に收納する体積を縮小させる。さらに、本発明は使用面で完全に操作不要なため、下降物60が生命のない物品でもスムーズに本発明を利用して降下する目的を達することができる。
The guide ring 30 has a rotationally symmetric structure with the central axis a1 as the axis, and even if the auxiliary umbrella 40 is fixed to the moving end 351, it still maintains rotational symmetry with the central axis a1 as the axis, and each tank Since 34 and the auxiliary umbrella 40 also have a rotationally symmetric structure with the auxiliary axis a2 as an axis, the present invention has an overall stable balance effect when descending (see FIGS. 1 to 3).
In addition, since the storage space 345 is provided in the tank 34 of the present invention, the auxiliary umbrella 40 can be folded when not in use and stored in the storage space 345 of the tank 34. Effectively reduce the volume to be stored. In addition, since the present invention does not require any operation in terms of use, the object of the descending object 60 to smoothly descend even if it is a lifeless article can be achieved using the present invention.

補助用傘40が開くと、補助用傘40の固定部41に固設された移動端351が上方へ移動し、このとき作動端352が弾性部材344を押し開いて、クランプ342が気流ダクト33を束縮させて、気流ダクト33を通過する気体が減少するため、本発明のパラシュートの浮力が増大して、降下速度を減速する(図2及び図3参照)。   When the auxiliary umbrella 40 is opened, the moving end 351 fixed to the fixing portion 41 of the auxiliary umbrella 40 moves upward. At this time, the operating end 352 pushes open the elastic member 344, and the clamp 342 is connected to the airflow duct 33. Since the gas passing through the airflow duct 33 is reduced, the buoyancy of the parachute of the present invention is increased and the descending speed is reduced (see FIGS. 2 and 3).

図4は本発明の第2実施形態の傾斜外観図である。本例では、パラシュートの外観に若干の相違が見られるに留まり、補助用傘40Bの数は3つである。
本発明の特徴は案内用リング30Bで気流を集める効果であり、補助用傘40Bが吹き出す気流によりスムーズに開いて、案内用リング30Bを中心軸a1を軸とする回転対称構造とする。本発明には、降下する際、安定したバランス効果があることから、図のような別の実施形態でも本発明の創作目的を達成することができる。
FIG. 4 is an inclined external view of the second embodiment of the present invention. In this example, only a slight difference is seen in the appearance of the parachute, and the number of auxiliary umbrellas 40B is three.
A feature of the present invention is the effect of collecting the airflow by the guide ring 30B, which is smoothly opened by the airflow blown by the auxiliary umbrella 40B, so that the guide ring 30B has a rotationally symmetric structure about the central axis a1. Since the present invention has a stable balance effect when descending, the creative object of the present invention can be achieved in another embodiment as shown in the figure.

上述の実施形態は本発明の技術思想及び特徴を説明するためのものにすぎず、当該技術分野を熟知する者に本発明の内容を理解させると共にこれをもって実施させることを目的とし、本発明の特許請求の範囲を限定するものではない。従って、本発明の精神を逸脱せずに行う各種の同様の効果をもつ改良又は変更は、後述の請求項に含まれるものとする。   The above-described embodiments are merely for explaining the technical idea and features of the present invention, and are intended to allow those skilled in the art to understand the contents of the present invention and to carry out the same with the present invention. It is not intended to limit the scope of the claims. Accordingly, improvements or modifications having various similar effects made without departing from the spirit of the present invention shall be included in the following claims.

20 球状傘
21 収納用チャンネル
211 頂部開口部
212 底部開口部
22 貫通柱
221 頂部クランプ
222 底部クランプ
23 空気注入孔
24 栓部
25 連接部
30 案内用リング
30B 案内用リング
31 リング
311 気流案内用凹部
32 すそ部
33 気流ダクト
331 案内孔
34 タンク
341 開口部
342 クランプ
343 移動ブロック
344 弾性部材
345 収納空間
346 底部環状台座
347 円柱空間
348 回転点
35 滑り柱
351 移動端
352 作動端
36 固定リング
361 補助孔
40 補助用傘
40B 補助用傘
41 固定部
60 下降物
a1 中心軸
a2 補助軸
20 spherical umbrella
21 Storage channel
211 Top opening
212 Bottom opening
22 Through pillars
221 Top clamp
222 Bottom clamp
23 Air injection hole
24 stopper
25 articulated parts
30 Guide ring
30B Guide ring
31 rings
311 Concave for airflow guidance
32 bottom
33 Airflow duct
331 Guide hole
34 tanks
341 opening
342 Clamp
343 Moving block
344 Elastic member
345 storage space
346 Bottom annular pedestal
347 cylindrical space
348 Rotation point
35 sliding pillar
351 Moving end
352 working end
36 Fixing ring
361 Auxiliary hole
40 Auxiliary umbrella
40B Auxiliary umbrella 41 Fixed part
60 Falling objects
a1 Center axis
a2 Auxiliary shaft

Claims (6)

下降物の降下速度を減速させるパラシュートであって、
中心軸を備え、空気注入孔を有し、前記空気注入孔に栓部を設け、底部は前記中心軸を囲繞して複数の連接部に固設し、前記連接部の他端は前記下降物と結合する球状傘と、
前記中心軸を囲繞して前記球状傘の周囲に固設し、リングと前記球状傘の下方に延在するすそ部を備え、前記リングの底端面に少なくとも3つの気流案内用凹部を成型し、各気流案内用凹部は前記球状傘の上方に気流ダクトを突設して成型し、前記気流ダクトの末端に案内孔を開設し、前記気流ダクトの頂部に少なくとも3つのタンクを成型し、前記タンクの下端面は前記案内孔と連通し、前記案内用リングは前記中心軸を軸とする回転対称構造とする案内用リングと、
それぞれ複数の固定部で各タンク内部と固着する少なくとも3つの補助用傘と、を備えることを特徴とする、
パラシュート。
A parachute that decelerates the descending speed of falling objects,
A central axis, an air injection hole, a plug portion provided in the air injection hole, a bottom portion surrounding the central axis and fixed to a plurality of connecting portions, the other end of the connecting portion being the descending object A spherical umbrella combined with
Surrounding the central axis, fixed around the spherical umbrella, provided with a ring and a skirt portion extending below the spherical umbrella, molding at least three airflow guiding recesses on the bottom end surface of the ring, Each airflow guide recess is formed by projecting an airflow duct above the spherical umbrella, opening a guide hole at the end of the airflow duct, molding at least three tanks at the top of the airflow duct, A lower end surface of the guide ring communicates with the guide hole, and the guide ring has a rotationally symmetric structure about the central axis;
Each comprising at least three auxiliary umbrellas that are fixed to the inside of each tank by a plurality of fixing portions,
parachute.
前記案内用リングの頂部にさらに固定リングを増設し、前記固定リングは前記中心軸を囲繞して前記球状傘の周囲に固設され、前記固定リング上に少なくとも3つの補助孔を開設し、前記タンクは前記補助孔内に穿設して位置決めをし、前記固定リングは前記球状傘が風抵抗に耐え得る能力を強化することによって、前記球状傘が気圧によって捻じ曲がって変形するのを防止することを特徴とする請求項1に記載のパラシュート。   A fixing ring is further added to the top of the guide ring, the fixing ring is fixed around the spherical umbrella around the central axis, and at least three auxiliary holes are opened on the fixing ring, The tank is drilled in the auxiliary hole for positioning, and the fixing ring strengthens the ability of the spherical umbrella to withstand wind resistance, thereby preventing the spherical umbrella from being twisted and deformed by atmospheric pressure. The parachute according to claim 1. 前記気流ダクトは可撓性材料で製造された構造であり、前記タンク内にさらに複数の滑り柱、クランプ、及び移動ブロックを増設し、前記滑り柱は前記タンクに穿設され、前記滑り柱は移動端がタンク内に位置し、作動端がタンク外に位置し、前記クランプの一端は弾性部材で前記作動端に固設され、他端は前記気流ダクト周囲に位置し、前記移動ブロックは各前記滑り柱の移動端に固設することを特徴とする請求項1に記載のパラシュート。   The airflow duct is a structure made of a flexible material, and further includes a plurality of sliding columns, clamps, and moving blocks in the tank, the sliding column is drilled in the tank, and the sliding column is The moving end is located inside the tank, the working end is located outside the tank, one end of the clamp is fixed to the working end by an elastic member, the other end is located around the air flow duct, The parachute according to claim 1, wherein the parachute is fixed to a moving end of the sliding column. 前記補助用傘の固定部は前記滑り柱の移動端に固設され、気流が作動すると、前記固定部は上方向に前記移動端を牽引し、前記作動端が前記弾性部材を押し開いて、前記クランプを動かして前記気流ダクトを収縮させて、気流の通過量を減少させることを特徴とする請求項3に記載のパラシュート。   The fixing portion of the auxiliary umbrella is fixed to the moving end of the sliding column, and when the airflow is activated, the fixing portion pulls the moving end upward, and the operating end pushes the elastic member open, The parachute according to claim 3, wherein the airflow duct is contracted by moving the clamp to reduce a passing amount of the airflow. 前記タンクの中央部にさらに底部環状台座を突設して成型し、前記底部環状台座の周囲に円柱空間を空け、前記気流ダクトを前記円柱空間内に設けることで、前記底部環状台座の頂部の中央が前記案内孔と連通し、前記タンク内に複数の滑り柱、クランプ、及び移動ブロックを設け、前記滑り柱は前記底部環状台座の頂部周囲に穿設され、前記滑り柱の移動端は底部環状台座の上方に位置し、作動端は前記底部環状台座の下方に位置し、前記クランプの一端は回転点により弾性部材と結合させ、前記弾性部材の他端は前記作動端に固設し、前記クランプの他端は前記気流ダクトの周囲に位置させ、前記移動ブロックは各前記滑り柱の移動端に固設することを特徴とする請求項1に記載のパラシュート。   A bottom annular pedestal is further projected and formed at the center of the tank, a cylindrical space is formed around the bottom annular pedestal, and the airflow duct is provided in the cylindrical space, so that the top of the bottom annular pedestal is formed. The center communicates with the guide hole, and a plurality of sliding columns, clamps, and moving blocks are provided in the tank. The sliding columns are perforated around the top of the bottom annular pedestal, and the moving end of the sliding column is the bottom. Located above the annular pedestal, the working end is located below the bottom annular pedestal, one end of the clamp is coupled to the elastic member by a rotation point, the other end of the elastic member is fixed to the working end, 2. The parachute according to claim 1, wherein the other end of the clamp is positioned around the airflow duct, and the moving block is fixed to a moving end of each sliding column. 前記球状傘は可撓性材料で製造された構造であり、その内部に収納用チャンネルを有し、前記収納用チャンネルの球状傘の頂部と底部にそれぞれ頂部開口部と底部開口部を備え、前記パラシュートはさらに貫通柱を増設し、前記貫通柱は前記収納用チャンネルに穿設され、それぞれ頂部クランプと底部クランプで前記頂部開口部と前記底部開口部を密閉して、前記球状傘を固定することで、前記球状傘が気圧によって捻じ曲がって変形するのを防止することを特徴とする請求項1に記載のパラシュート。   The spherical umbrella is a structure made of a flexible material, has a storage channel therein, and has a top opening and a bottom opening at the top and bottom of the spherical umbrella of the storage channel, The parachute further includes a penetrating column, the penetrating column is formed in the storage channel, the top opening and the bottom opening are sealed with a top clamp and a bottom clamp, respectively, and the spherical umbrella is fixed. The parachute according to claim 1, wherein the spherical umbrella is prevented from being twisted and deformed by atmospheric pressure.
JP2014002429A 2014-01-09 2014-01-09 parachute Ceased JP2015131504A (en)

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Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1185537A (en) * 1915-08-31 1916-05-30 Andrew Raffa Parachute.
JPH0519096U (en) * 1991-08-22 1993-03-09 阪口 盛彦 Parasail with balloon
EP0879758A2 (en) * 1997-05-19 1998-11-25 Masahiko Hyashi Parachute balloon

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1185537A (en) * 1915-08-31 1916-05-30 Andrew Raffa Parachute.
JPH0519096U (en) * 1991-08-22 1993-03-09 阪口 盛彦 Parasail with balloon
EP0879758A2 (en) * 1997-05-19 1998-11-25 Masahiko Hyashi Parachute balloon

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