JPH01195200A - Ram pressure type darablider with small wing - Google Patents

Ram pressure type darablider with small wing

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Publication number
JPH01195200A
JPH01195200A JP1923088A JP1923088A JPH01195200A JP H01195200 A JPH01195200 A JP H01195200A JP 1923088 A JP1923088 A JP 1923088A JP 1923088 A JP1923088 A JP 1923088A JP H01195200 A JPH01195200 A JP H01195200A
Authority
JP
Japan
Prior art keywords
wing
small
ram
pressure type
attached
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
JP1923088A
Other languages
Japanese (ja)
Inventor
Masato Kobayashi
正登 小林
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 JP1923088A priority Critical patent/JPH01195200A/en
Publication of JPH01195200A publication Critical patent/JPH01195200A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To prevent reduction of a lift following deformation of a wing body by attaching a bag-shaped small wing tip having an opening on its front to a wing body including a main wing and making flight control by means of a control cable connected to the small wing. CONSTITUTION:An eilron 32 that is, a vertically swingable small wing and a spoiler 37 are attached in each of right and left two positions in the rear and central areas of a main wing 22 respectively. The ailron 32 and the spoiler 27 are formed of small bag bodies 33, 38 respectively and provided with respectively openings 35, 40 in their front areas. In the similar way, an elevator 42, that is, a vertically swingable small wing is attached in each of right and left two positions in the rear area of a horizontal tail wing 30. Hereat, flight control such as climb/deceleration, etc., may be carried out by operating the eilrons 32, the spoiler 37 and the elevators 42 by means of control cables 34a, 43, but its controllability and stability can be improved without any deformation of the wing body because those flight control means are formed of small bag bodies independent from the wing body.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、操縦性が良く、しかも安全なラム圧式小翼付
パラグライダ−に関する。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a ram pressure type small-winged paraglider that has good maneuverability and is safe.

〔従来の技術〕[Conventional technology]

第5図に示すように、従来のパラシュートグライダ−1
0は前部に開口部11が設けられた複数の袋体12を横
方向に連接した翼体13と、該翼体13の下部にその一
端が接続される複数の支持索14と、該支持索14の下
部に設けられたハーネス15とを有して構成されていた
As shown in Figure 5, a conventional parachute glider-1
Reference numeral 0 denotes a wing body 13 in which a plurality of bags 12 each having an opening 11 in the front part are connected in the transverse direction, a plurality of support cables 14 having one end connected to the lower part of the wing body 13, and the supporting cables 14. The harness 15 was provided at the bottom of the cable 14.

このパラシュートグライダ−10を使用する場合には、
予め人16の体にハーネス15を装着して、適当な風の
あるときに上記パラシュートグライダ−10の前部の開
口部11から袋体12内に風を入れることによって膨張
させて翼体13を成形し、この翼体13の揚力によって
上昇あるいは滑空させるようにしていた。
When using this parachute glider 10,
The harness 15 is attached to the body of the person 16 in advance, and when there is a suitable wind, air is introduced into the bag body 12 from the front opening 11 of the parachute glider 10 to inflate the wing body 13. The wing body 13 was shaped so that it could rise or glide using the lift force of the wing body 13.

そして、上記支持索14のうち袋体12の後部に接続さ
れた支持索14は特に操縦索17としての役目を有して
おり、該操縦索17を操作して翼体を変形させることに
よって方向、昇降、減速等のあらゆる操作を行っていた
Of the support cables 14, the support cable 14 connected to the rear part of the bag body 12 has a particular role as a control cable 17, and by operating the control cable 17 to deform the wing body, He performed all kinds of operations such as lifting, lowering, and decelerating.

〔発明が解決しようとする問題点〕[Problem that the invention seeks to solve]

ところが、上記従来例に係るパラシュートグライダ−1
0においては、袋体12は通常軽い布材からなっており
、風が袋体12の前部に形成された開口部11から入っ
て翼体13が成形されているので、操縦索17の操作に
よっては翼体13が潰れることもあり、揚力を失って落
下する危険性があった。
However, the parachute glider 1 according to the above conventional example
0, the bag body 12 is usually made of a light cloth material, and the wind enters through the opening 11 formed in the front part of the bag body 12, and the wing body 13 is formed, so that the control line 17 cannot be operated. In some cases, the wing body 13 could collapse, posing a risk of losing lift and falling.

また、上記危険を回避するためには、翼体13が潰れな
いように操縦索17を操作しなければならず、そのため
には急激な方向転換、急激な昇降、急激な減速等の操作
を控える必要があった。
In addition, in order to avoid the above-mentioned danger, it is necessary to operate the control cables 17 so as not to crush the wing body 13, and for this purpose, refrain from operations such as sudden direction changes, sudden elevations, sudden decelerations, etc. There was a need.

一方、主翼13の後部に単なる布状片を延設し、該布状
片の後部に操縦索17を接続する試みも成されたが、上
記布状片がフラッタ−現象(風によって旗が揺れ動くよ
うな現象)を起こし、実際には採用するにはまだ多くの
課題が残されていた本発明は上記事情に鑑みてなされた
もので、方向転換、昇降、減速等の操作が容易で、しか
も、翼体を殆ど変形させないで操縦できるラム圧式小翼
付パラグライダ−を提供することを目的とする〔問題点
を解決するための手段〕 上記問題点を解決する本発明に係るラム圧式小翼付パラ
グライダ−は、少なくとも複数の袋体が横方向に連接さ
れて翼状に形成される主翼と、該主翼の下部にその一端
が接続される複数の支持索と、該支持索の下部に設けら
れたハーネスとを有してなるパラシュートグライダ−に
おいて、上記主翼を含む翼体に前部に開口部が形成され
た袋状の小翼の先部を取付け、該小翼に接続された操縦
索によって操縦を行うようにして構成されているここに
、小翼が操縦索によって引っ張られると上下動する上下
動小翼と、左右動する左右動小翼とで構成されることが
好ましい。
On the other hand, an attempt was also made to extend a simple cloth piece to the rear of the main wing 13 and connect the control cable 17 to the rear of the cloth piece. The present invention was developed in view of the above circumstances, and it is easy to perform operations such as changing direction, ascending and descending, decelerating, etc. It is an object of the present invention to provide a ram-pressure type small-winged paraglider that can be operated with almost no deformation of the wing body. A paraglider has a main wing formed into a wing shape by connecting at least a plurality of bags in the lateral direction, a plurality of support cables having one end connected to the lower part of the main wing, and a plurality of support cables provided at the lower part of the support cables. In a parachute glider having a harness, the tip of a bag-shaped winglet with an opening formed in the front part is attached to the wing body including the main wing, and the parachute glider is operated by a control cable connected to the winglet. It is preferable that the winglet is configured to include a vertically movable winglet that moves up and down when the winglet is pulled by a control cable, and a leftward and rightward movable winglet that moves left and right.

また、小翼の前部に形成された開口部が翼体に連接され
ると共に、該翼体には開口部から小翼へ空気の導入が行
える孔が形成されているものも本発明に含まれるもので
ある。
The present invention also includes a structure in which an opening formed in the front part of a small wing is connected to a wing body, and a hole is formed in the wing body through which air can be introduced from the opening to the small wing. It is something that can be done.

〔作用〕[Effect]

本発明に係るラム圧式小翼付パラグライダ−は、主翼を
含む翼体に前部に開口部が形成された袋状の小翼の先部
を取付け、該小翼には操縦索が接続されているので、翼
体を殆ど変形させることなく操縦索を操作して小翼を動
かすことによって操縦することができる。
The ram-pressure type small-winged paraglider according to the present invention has a bag-shaped small wing tip with an opening formed in the front part attached to the wing body including the main wing, and a control cable is connected to the small wing. Because of this, it is possible to control the aircraft by operating the control cables and moving the winglet without substantially deforming the wing body.

〔実施例〕〔Example〕

続いて、添付した図面を参照しつつ、本発明を具体化し
た一実施例につき説明し、本発明の理解に供する。
Next, an embodiment embodying the present invention will be described with reference to the attached drawings to provide an understanding of the present invention.

ここに、第1図は本発明の一実施例に係るラム圧式小翼
付パラグライダ−の斜視図、第2図は上記ラム圧式小翼
付パラグライダ−の一部省略側断面図、第3図は本発明
の他の実施例に係るラム圧式小翼付パラグライダ−の一
部省略斜視図、第4図は上記他のラム圧式小翼付パラグ
ライダ−の平面図である。
Here, FIG. 1 is a perspective view of a ram pressure type paraglider with small wings according to an embodiment of the present invention, FIG. 2 is a partially omitted side sectional view of the ram pressure type paraglider with small wings, and FIG. FIG. 4 is a partially omitted perspective view of a ram pressure type paraglider with small wings according to another embodiment of the present invention, and FIG. 4 is a plan view of the other ram pressure type paraglider with small wings.

第1図に示すように本発明の一実施例に係るラム圧式小
翼付パラグライダ−20は、複数の袋体21を横方向に
連接してなる主翼22と、該主翼22の後部に連接して
設けられた胴体23及び尾翼24と、該主翼22、胴体
23及び尾翼24の下部に取付けられた複数の支持索2
5と、該支持索25の下部に設けられたハーネス26と
を有して構成されている。以下、これらについて詳しく
説明する。
As shown in FIG. 1, a ram pressure type paraglider 20 with small wings according to an embodiment of the present invention has a main wing 22 formed by connecting a plurality of bags 21 in the lateral direction, and a main wing 22 connected to the rear part of the main wing 22. A fuselage 23 and a tail 24 are provided, and a plurality of support cables 2 are attached to the lower parts of the main wings 22, the fuselage 23, and the tail 24.
5 and a harness 26 provided at the bottom of the support rope 25. These will be explained in detail below.

上記袋体21は合成樹脂等からなる軽い布材(ナイロン
、ビニロン、テトロン等)からなり、第第2図に示すよ
うに、先部に開口部27が形成されていると共に、ある
程度の丸みを帯びて、しかも開口部27には布材からな
る空気導入管28が取付けられているので、開口部27
からの空気を袋体21に詰めることができ、複数個横方
向に連接された袋体21が全体として流線型の主翼22
を構成することになる。
The bag body 21 is made of a light cloth material (nylon, vinylon, Tetron, etc.) made of synthetic resin, etc., and as shown in FIG. Furthermore, since the air introduction pipe 28 made of cloth is attached to the opening 27, the opening 27
air can be filled into the bag body 21, and a plurality of bags 21 connected laterally form a streamlined main wing 22 as a whole.
This will constitute the following.

上記胴体23は主翼22の中心後部に取付けられ円筒状
又は角筒状の袋体からなって、孔が形成されたリブ(図
示せず)が複数個設けられていると共に、上記主翼22
及び尾翼24との取付は壁面にも孔が形成されて、開口
部27か6導入された空気が主翼22、胴体23及び尾
翼24に導入されるようになっている。
The fuselage 23 is attached to the center rear part of the main wing 22 and is made of a cylindrical or square tubular bag body, and is provided with a plurality of ribs (not shown) having holes formed therein.
For attachment to the tail wing 24, holes are also formed in the wall surface so that the air introduced through the openings 27 or 6 is introduced into the main wing 22, the fuselage 23, and the tail wing 24.

上記尾翼24は胴体23に連接する袋状の垂直尾翼29
と、該垂直尾翼29の上部に取付けられた袋状の水平尾
翼30とからなっている。
The tail 24 is a bag-shaped vertical tail 29 connected to the fuselage 23.
and a bag-shaped horizontal stabilizer 30 attached to the upper part of the vertical stabilizer 29.

上記垂直尾翼29は胴体23と連接して取付けられ、そ
の上部に水平尾翼30の中央部が設けられており、しか
も内部には孔が形成されたりプ(図示せず)が複数個設
けられているので、上記胴体23からの空気を垂直尾翼
29に導入できるものである。
The vertical stabilizer 29 is attached to be connected to the fuselage 23, and the center portion of the horizontal stabilizer 30 is provided on the upper part of the vertical stabilizer 29, and a plurality of holes (not shown) are formed inside the vertical stabilizer 29. Therefore, air from the fuselage 23 can be introduced into the vertical stabilizer 29.

上記水平尾翼30は袋状からなって、内部に孔が形成さ
れたリブ(図示せず)が設けられていると共に、垂直尾
翼29との取付は壁面にも図示しない孔が形成されてい
るので、垂直尾翼29に導入された空気は水平尾翼30
まで導入されることになる。
The horizontal stabilizer 30 has a bag-like shape and is provided with a rib (not shown) with a hole formed inside, and a hole (not shown) is also formed in the wall surface for attachment to the vertical stabilizer 29. , the air introduced into the vertical stabilizer 29 is transferred to the horizontal stabilizer 30.
It will be introduced until then.

上記主翼22、胴体23及び尾翼24の下部には複数の
合成樹脂繊維からなる支持索25が取付けられているが
、該支持索25は主翼22に吊下される人31の荷重が
分散されるように、複数個所に取付けられ、しかも該支
持索25は左右2系統に分割されて、下部のハーネス2
6に連結されている。
Support cables 25 made of a plurality of synthetic resin fibers are attached to the lower portions of the main wing 22, fuselage 23, and tail 24, and the support cables 25 distribute the load of the person 31 suspended from the main wing 22. As shown in FIG.
6.

上記ハーネス26は周知の構造となって、人31の体を
吊下するベルト体からなっている。
The harness 26 has a well-known structure and consists of a belt body for suspending the body of the person 31.

上記主翼22の後部及び中央部には第1図及び第2図に
示すように、左右2個所に上下動小翼の一例であるエル
ロン32及びスポイラ−37が取付けられている。上記
エルロン32は第2図に示すように、小袋体33によっ
てなり、その前部には小袋体33の上部から延設された
接合片34が取付けられ、該接合片34が主翼22の底
部に接合されていて、エルロン32の後部に接続された
操縦索34aを操作することによって翼体を左右に傾け
ることができる。
As shown in FIGS. 1 and 2, an aileron 32 and a spoiler 37, which are examples of vertically movable small wings, are attached to the rear and center portions of the main wing 22 at two locations on the left and right. As shown in FIG. 2, the aileron 32 is made up of a pouch body 33, and a joint piece 34 extending from the top of the pouch body 33 is attached to the front part of the pouch body 33, and the joint piece 34 is attached to the bottom of the main wing 22. By operating a control cable 34a connected to the rear of the aileron 32, the wing body can be tilted to the left or right.

また、小袋体33の前部は風抵抗の減少を図って流線型
となっていると共に開口部35が形成され、空気導入管
36を通って小袋体33の中に風が導入されるようにな
っている。
Further, the front part of the pouch body 33 is streamlined to reduce wind resistance, and an opening 35 is formed so that wind can be introduced into the pouch body 33 through an air introduction pipe 36. ing.

上記スポイラ−37もエルロン32と同様に小袋体38
によってなり、その前部には小袋体38の上部から延設
された接合片39が取付けられ、該接合片39が主翼2
2の底部に接合されていると共に、小袋体38の前部は
風抵抗の減少を図って流線型となって、前部に形成され
た開口部40の空気導入管41を通って小袋体3日の中
に風が導入されるようになっていて、スポイラ−37の
後部に接続される概縦索(図示しない)を操作すること
によってエアーブレーキの役目をすることができる。
The spoiler 37 also has a small bag body 38 like the aileron 32.
A joint piece 39 extending from the upper part of the pouch body 38 is attached to the front part of the pouch body 38, and the joint piece 39 is attached to the main wing 2.
2, and the front part of the pouch body 38 has a streamlined shape to reduce wind resistance. Wind is introduced into the spoiler 37, and by operating a longitudinal cable (not shown) connected to the rear of the spoiler 37, it can serve as an air brake.

ここで、小袋体33.38の内部に孔が形成されたリブ
を複数個取付けて、小袋体33及び38を補強した方が
好ましい。
Here, it is preferable to reinforce the pouches 33 and 38 by attaching a plurality of ribs each having a hole inside the pouches 33 and 38.

更に、第1図に示すように、水平尾翼30の後部にも左
右2個所に上下動小翼の一例であるエレベータ−42が
取付けられており、該エレベータ−42はエルロン32
、スポイラ−37と同じ構成になっているのでその説明
は省略するが、エレベータ−42の後部に接続された操
縦索43を操作することによって、翼体全体を上下に向
けることができるものである。
Furthermore, as shown in FIG. 1, elevators 42, which are examples of vertically movable small wings, are attached to the rear of the horizontal stabilizer 30 at two locations on the left and right.
Since it has the same structure as the spoiler 37, its explanation will be omitted, but by operating the control cable 43 connected to the rear of the elevator 42, the entire wing body can be directed up or down. .

なお、上下動小翼の一例であるエルロン32、スポイラ
−37及びエレベータ−42は自然な滑空状態では風抵
抗によって主翼22と略平行になっていて、操縦索を引
いて風抵抗を増加させるものである。
Note that the aileron 32, spoiler 37, and elevator 42, which are examples of vertically movable small wings, are approximately parallel to the main wing 22 due to wind resistance in a natural gliding state, and the wind resistance is increased by pulling the control cable. It is.

また、主翼22の後部であってエルロン32の内側部分
に上下動小翼の一例であるフラップ(図示せず)を取付
けたり、もしくは主翼22の前部にスラット(図示せず
)を取付けることも可能でである。
Furthermore, a flap (not shown), which is an example of a vertically movable wing, may be attached to the rear part of the main wing 22 and inside the aileron 32, or a slat (not shown) may be attached to the front part of the main wing 22. It is possible.

続いて、上記ラム圧式小翼付パラグライダ−20の使用
方法及びその作用について詳しく説明する。
Next, the method of using the ram pressure type paraglider 20 with small wings and its operation will be explained in detail.

まず、ハーネス26を装着した状態で、該ラム圧式小翼
付パラグライダ−20の前部を風の方向に向けると、空
気が袋体21の前部の開口部27がら空気導入管28を
通って袋体21の内部に入り、更に、胴体23、垂直尾
翼29及び水平尾翼30と導入されて翼体を構成するこ
とになる。
First, when the front part of the ram-pressure small-winged paraglider 20 is turned in the direction of the wind with the harness 26 attached, air flows through the opening 27 at the front part of the bag body 21 and through the air introduction pipe 28. It enters the inside of the bag 21 and is further introduced with the fuselage 23, vertical tail 29, and horizontal tail 30 to form a wing body.

これによって、該ラム圧式小翼付パラグライダ−20の
ハーネス26の部分に紐を付けて引くか、あるいは上記
ハーネス26の付いた所定長の紐の端を固定して上記主
翼22及び水平尾翼30に風に当てると、凧の原理によ
ってラム圧式小翼付パラグライダ−20は上昇するが、
主翼22の先部は全体として流線型となっているので風
抵抗の減少から揚力が増加することになる。
Accordingly, a string can be attached to the harness 26 of the ram-pressure winged paraglider 20 and pulled, or the end of a predetermined length of string attached to the harness 26 can be fixed to the main wing 22 and horizontal stabilizer 30. When exposed to the wind, the ram-pressure small-winged paraglider 20 rises due to the principle of a kite, but
Since the tip of the main wing 22 has a streamlined shape as a whole, lift is increased by reducing wind resistance.

そして、下部のハーネス26に接続された紐を外すと、
該ラム圧式小翼付パラグライダ−20は滑空することに
なる。
Then, when you remove the string connected to the lower harness 26,
The ram-pressure winged paraglider 20 will glide.

ここで、上記エルロン32、スポイラ−37、エレベー
タ−42を自在に操作して、昇降、減速等の操縦を行う
が、これらは翼体とは独立した小袋体によって構成され
ているので、翼体を殆ど変形させることなく、操縦性及
び安定性が向上する続いて、第3図及び第4図に示す本
発明の他の実施例に係るラム圧式小翼付パラグライダ−
44について説明するが、該ラム圧式小翼付パラグライ
ダ−44は、前部に開口部45が形成された袋体46を
横方向に連接してなる翼体47の両側部に、前部が閉塞
となった袋体48を縦方向に連接してなる翼端質49を
取付け、該翼端質49の後部に前部に開口部50が形成
され左右方向に回動する左右動小翼の一例であるラダー
51を取付けて構成されている。
Here, the aileron 32, spoiler 37, and elevator 42 are freely operated to perform maneuvers such as elevation, descent, deceleration, etc., but since these are composed of a pouch body independent of the wing body, the wing body Next, a ram-pressure small-winged paraglider according to another embodiment of the present invention shown in FIGS. 3 and 4 has improved maneuverability and stability without substantially deforming the
44, the ram-pressure small-winged paraglider 44 has a wing body 47 which is formed by connecting a bag body 46 in the lateral direction with an opening 45 formed in the front part, and has a closed front part on both sides of the wing body 47. An example of a left-right movable small wing in which a wing tip material 49 formed by vertically connecting the bag bodies 48, and an opening 50 formed in the front part at the rear of the wing tip material 49, rotates in the left-right direction. It is constructed by attaching a ladder 51.

上記ラダー51の後部に接続された操縦索52を操作す
ることによってラダー51を第4図に2点鎖線で示すよ
うに、左右方向に動かすことができ方向舵の役目をする
ことができる。
By operating the control cable 52 connected to the rear of the rudder 51, the rudder 51 can be moved left and right as shown by the two-dot chain line in FIG. 4, and can serve as a rudder.

また、上記ラム圧式小翼付パラグライダ−20及び44
においては小翼の前部に形成された開口部から直接外部
の空気を導入しているが、小翼の前部に形成された開口
部を翼体と連接し、該翼体に形成された孔から小翼内へ
空気を導入することも可能で、これによって小翼の開口
部に掛かる風抵抗を減少させることができる。
In addition, the above-mentioned ram pressure type paragliders with small wings - 20 and 44
In this method, external air is introduced directly from the opening formed in the front part of the small wing, but the opening formed in the front part of the small wing is connected to the wing body, and the It is also possible to introduce air into the winglet through the holes, thereby reducing wind resistance on the winglet opening.

〔発明の効果〕〔Effect of the invention〕

本発明に係るラム圧式小翼付パラグライダ−は、操縦の
際に翼体を殆ど変形させることなく、翼体の変形に伴っ
て揚力が低下する虞が無くなり、操縦性及び安定性の向
上に繋がるようになると共に、急激な方向転換、急激な
昇降、急激な減速等の操作が初心者でさえも容易に行え
るようになった。
The ram pressure type paraglider with small wings according to the present invention hardly deforms the wing body during maneuvering, and there is no fear that the lift force will decrease due to the deformation of the wing body, leading to improved maneuverability and stability. With this development, even beginners can easily perform operations such as sudden direction changes, sudden elevations and sudden decelerations.

また、小翼にはラム圧が利用されているので、フラッタ
−現象を引き起こす心配もなくなった。
In addition, since ram pressure is used in the winglet, there is no need to worry about flutter.

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

第1図は本発明の一実施例に係るう、ム圧式小翼付パラ
グライダ−の斜視図、第2図は上記ラム圧式小翼付パラ
グライダ−の一部省略側断面図、第3図は本発明の他の
実施例に係るラム圧式小翼付パラグライダ−の一部省略
斜視図、第4図は上記他のラム圧式小翼付パラグライダ
−の平面図、第5図は従来のパラシュートグライダ−の
斜視図である。 〔符号の説明〕 20.44・・・ラム圧式小翼付パラグライダ−121
,46,48・・・袋体、22・・・主翼、23・・・
胴体、24・・・尾翼、25・・・支持索、26・・・
ハーネス、27,35,40.45.50・・・開口部
、2B、36.41・・・空気導入管、29・・・垂直
尾翼、30・・・水平尾翼、31・・・人、32・・・
エルロン、33.38・・・小袋体、34.39・・・
接合片、34a、43.52・・・操縦索、37・・・
スポイラ−142・・・エレベータ−147・・・翼体
、49・・・翼端翼、51・・・ラダー 代理人  弁理士 中部 富士男
Fig. 1 is a perspective view of a ram-pressure type paraglider with small wings according to an embodiment of the present invention, Fig. 2 is a partially omitted side sectional view of the ram-pressure type paraglider with small wings, and Fig. 3 is a side view of the ram-pressure type paraglider with small wings. A partially omitted perspective view of a ram pressure type paraglider with small wings according to another embodiment of the invention, FIG. 4 is a plan view of the other ram pressure type paraglider with small wings, and FIG. 5 is a view of a conventional parachute glider. FIG. [Explanation of symbols] 20.44... Ram pressure type paraglider with small wings - 121
, 46, 48...bag body, 22...main wing, 23...
Fuselage, 24... Tail, 25... Support rope, 26...
Harness, 27, 35, 40. 45. 50... Opening, 2B, 36. 41... Air introduction pipe, 29... Vertical stabilizer, 30... Horizontal stabilizer, 31... Person, 32 ...
Aileron, 33.38... Bag body, 34.39...
Joint piece, 34a, 43.52... Control rope, 37...
Spoiler-142...Elevator-147...Wing body, 49...Wing tip wing, 51...Rudder agent Patent attorney Fujio Chubu

Claims (4)

【特許請求の範囲】[Claims] (1)少なくとも複数の袋体が横方向に連接されて翼状
に形成される主翼と、該主翼の下部にその一端が接続さ
れる複数の支持索と、該支持索の下部に設けられたハー
ネスとを有してなるパラシュートグライダーにおいて、
上記主翼を含む翼体に前部に開口部が形成された袋状の
小翼の先部を取付け、該小翼に接続された操縦索によっ
て操縦を行うことを特徴とするラム圧式小翼付パラグラ
イダー。
(1) A main wing formed into a wing shape by connecting at least a plurality of bags in the lateral direction, a plurality of support cables having one end connected to the lower part of the main wing, and a harness provided at the lower part of the support cables. In a parachute glider comprising:
A ram-pressure type small wing characterized in that a tip of a bag-shaped small wing with an opening formed in the front part is attached to the wing body including the main wing, and the control is performed by a control cable connected to the small wing. Paragliding.
(2)小翼の前部に形成された開口部が翼体と連接され
ると共に、該翼体には開口部から小翼へ空気の導入が行
える孔が形成されている特許請求の範囲第1項記載のラ
ム圧式小翼付パラグライダー。
(2) The opening formed in the front part of the winglet is connected to the wing body, and the wing body is formed with a hole through which air can be introduced from the opening to the winglet. The ram-pressure small-winged paraglider described in item 1.
(3)小翼が操縦索によって引っ張られると上下動する
上下動小翼である特許請求の範囲第1項または第2項記
載のラム圧式小翼付パラグライダー。
(3) The ram-pressure type small-winged paraglider according to claim 1 or 2, wherein the small wing is a vertically movable small wing that moves up and down when pulled by a control cable.
(4)小翼が操縦索によって引っ張られると左右動する
左右動小翼である特許請求の範囲第1項または第2項記
載のラム圧式小翼付パラグライダー。
(4) The ram-pressure type small-winged paraglider according to claim 1 or 2, wherein the small wing is a left-right movable small wing that moves left and right when pulled by a control cable.
JP1923088A 1988-01-28 1988-01-28 Ram pressure type darablider with small wing Pending JPH01195200A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1923088A JPH01195200A (en) 1988-01-28 1988-01-28 Ram pressure type darablider with small wing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1923088A JPH01195200A (en) 1988-01-28 1988-01-28 Ram pressure type darablider with small wing

Publications (1)

Publication Number Publication Date
JPH01195200A true JPH01195200A (en) 1989-08-07

Family

ID=11993580

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1923088A Pending JPH01195200A (en) 1988-01-28 1988-01-28 Ram pressure type darablider with small wing

Country Status (1)

Country Link
JP (1) JPH01195200A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6508436B2 (en) * 2000-07-17 2003-01-21 Chih-Yu Hsia Inflatable airfoils, and elevated and propulsion driven vehicles
US6688553B2 (en) * 2002-01-04 2004-02-10 Chih-Yu Hsia Inflatable airfoils, and elevated and propulsion driven vehicles
JP2005242388A (en) * 2005-05-06 2005-09-08 Mitsubishi Electric Corp Technical education system using flying object and flying object
JP2020097381A (en) * 2018-12-18 2020-06-25 好包 生武 Airfoil profile fuselage wingless aircraft

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6508436B2 (en) * 2000-07-17 2003-01-21 Chih-Yu Hsia Inflatable airfoils, and elevated and propulsion driven vehicles
US6659403B2 (en) * 2000-07-17 2003-12-09 Chih-Yu Hsia Inflatable airfoils, and elevated and propulsion driven vehicles
US6688553B2 (en) * 2002-01-04 2004-02-10 Chih-Yu Hsia Inflatable airfoils, and elevated and propulsion driven vehicles
JP2005242388A (en) * 2005-05-06 2005-09-08 Mitsubishi Electric Corp Technical education system using flying object and flying object
JP2020097381A (en) * 2018-12-18 2020-06-25 好包 生武 Airfoil profile fuselage wingless aircraft

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