JPH11198621A - Winged air-body vehicle - Google Patents

Winged air-body vehicle

Info

Publication number
JPH11198621A
JPH11198621A JP4275698A JP4275698A JPH11198621A JP H11198621 A JPH11198621 A JP H11198621A JP 4275698 A JP4275698 A JP 4275698A JP 4275698 A JP4275698 A JP 4275698A JP H11198621 A JPH11198621 A JP H11198621A
Authority
JP
Japan
Prior art keywords
attached
engine
denotes
air
fuselage
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
JP4275698A
Other languages
Japanese (ja)
Inventor
Akira Sakamoto
暁 坂本
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 JP4275698A priority Critical patent/JPH11198621A/en
Publication of JPH11198621A publication Critical patent/JPH11198621A/en
Pending legal-status Critical Current

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  • Body Structure For Vehicles (AREA)

Abstract

PROBLEM TO BE SOLVED: To travel all the space of land, sea and air by means of one vehicle alone. SOLUTION: An extensible wing 2 is attached to a fuselage 1 consisting of a tube, where air is pressed-in, and thereby two wheels are rotated by an engine to run on the ground, to navigate on the sea and to get into the air with a propeller 41 rotated in combination.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【産業上の利用分野】[Industrial applications]

【0002】 乗り物に関するものである。[0002] It relates to vehicles.

【従来の技術】[Prior art]

【0003】 エヤーボデーの車(公開63−2229
92)本出願人保有の特許第2717197号がある。
クレームは「シャーシーと、空気を圧入した環状チュー
ブからなる胴体と、空気を圧入した複数のチューブから
それぞれなる複数の屋根支柱と、柔軟性のある合成樹脂
又はこれに類するものからなる屋根とを有するエヤーボ
デー車において、バインダーにて前記シャーシーと前記
胴体とをくみつけると共に、前記胴体の両側部に前記各
屋根支柱の両端部を取付け、さらに、これら屋根支柱で
前記屋根を支持したことを特徴とするエヤーボデー車」
である。
[0003] Ayerbody's car (Publication 63-2229)
92) There is Japanese Patent No. 2717197 owned by the present applicant.
The claim `` has a chassis, a body consisting of an annular tube pressurized with air, a plurality of roof supports each consisting of a plurality of tubes pressurized with air, and a roof made of flexible synthetic resin or the like. In the air body vehicle, the chassis and the body are attached together with a binder, and both ends of the roof pillars are attached to both sides of the body, and the roof is supported by the roof pillars. Airy Body Car "
It is.

【発明が解決しようとする課題】[Problems to be solved by the invention]

【0004】 前記の乗り物に翼を付け陸・海・空を一
つの乗り物で行動出来るようにする。
[0004] The vehicle is provided with wings so that land, sea, and air can be operated by one vehicle.

【課題を解決する為の手段】[Means for solving the problem]

【0005】 空気を圧入したチューブからなる胴体
に、、伸縮出来る桁と、その伸縮に伴い折畳み出来るよ
うにした羽布よりなる翼を取り付け、上下に突出した支
軸を有するエンジンを、支軸を中心に、水平方向に回す
事の出来るように、前記胴体にバインダーで付設したシ
ヤーシーに取付け、そのエンジンで車輪を回して地上走
行し、水上ではその車輪が水掻きとなり、空をとぶ場合
はエンジンの駆動軸を前後方向に変え、その駆動軸にプ
ロペラ軸を取りつける。
An engine having a support shaft protruding up and down is attached to a body made of a tube into which air is press-fitted, with an expandable and contractible girder and wings made of a feather cloth which can be folded along with the expansion and contraction. At the center, it is attached to a chassis attached to the fuselage with a binder so that it can be turned in the horizontal direction, the wheel is turned by the engine, and the vehicle runs on the ground. Change the drive shaft in the front-rear direction, and attach the propeller shaft to the drive shaft.

【作用】[Action]

【0006】 軽いので小さなエンジンで飛び、離着陸
距離も短く、水上離着陸が出来、墜落・衝突事故に際し
てボデーはクッションとなる。
Since it is light, it flies with a small engine, the take-off and landing distance is short, it can take off and land on water, and the body becomes a cushion in the event of a crash or collision.

【実施例】【Example】

【0007】 図に於いて1は空気を圧入した気密なチ
ューブからなる胴体、2は翼、3は翼桁、4は羽布、5
は垂直安定板、6は方向舵、7は水平安定板、8は昇降
舵である。これら翼類に必要な翼桁・支柱・各安定板と
方向舵・昇降舵を繋ぐ蝶番軸等棒状の物は、釣り竿の様
に伸縮出来る構造とし、翼桁は中央部をシャシーに、支
柱も適宜の方法で胴体に固定する。羽布は炭素繊維・ガ
ラス繊維・化学繊維等の極細糸織物を、気密処理した物
を用いて、翼桁・支柱・蝶番軸の伸縮に従って展開・折
り畳み出来る構造とする。翼の小骨は図では省略した
が、釣り竿の道糸ガイドと同様の方法で翼桁に取付け
る。9は前輪、10は半皿型の補強部、11は尾輪、1
2はプロペラ軸、13はシャーシーで前記胴体の上下に
渡してバインダー14で胴体1に接着する。シヤーシー
は必要に応じ、組立型の六面体や四面体としてもよい、
この場合後述するエンジンの旋回に不都合の無いように
する。素材は翼桁3支柱類と同様の、軽くて強い炭素繊
維補強材等を用いる。15は旋回軸穴、16は翼を折り
畳んだ場合の翼カバー、17は操縦席、18は底で、胴
体と同様の軽くて強く気密で、防水性のある布を用いて
胴体の底面に気密に張つける。上面も同様にし、操縦席
背凭れとの関係も気密にし、シヤーシーの前の空間も同
様にして空気を圧入し、上下面の流線型を整える。燃料
タンクは操縦席の下等適宜の空間に設ける。19は操縦
棹で、地上・海上走行の場合は球関接手20を締めて、
普通のハンドルとなる。21はハンドル棒、22は操縦
索を示し飛行の場合以外は外す。23はエンジン、24
は支軸、25はエンジンの駆動軸、26は車軸、27は
ガイド、28は止金で着脱出来るようにする。29はク
ラッチ、30は滑り軸で駆動軸25と滑り結合とする。
31はその滑り部分、35は車輪を示す。32は反発バ
ネで滑り軸30を押してクラッチ29を結合させる。第
5図は31の滑り部分の一部断面図である。33、34
はクラッチ29の開閉機構の一部で、33は開閉バネ、
34は中心に向かって図の様に傾斜した面より成るバネ
ガイドである。その作動機構は第6図に示す。36はク
ラッチペダル、37・38は支点、39は自由結合点を
示す。飛行する場合は滑り軸30を駆動軸から外し、エ
ンジン23を回して駆動軸25をプロペラ軸12にネジ
40で結合する。41はプロペラを示す。車軸・プロペ
ラ軸・翼桁・操縦索等胴体を貫通する必要のある部分
は、気密な筒貼りとし、回転・滑り等の摩擦部分にはフ
ッソ樹脂等の管を保護装置として挿入する。翼を耐熱素
材で作った場合、排気を導入し、翼端から放出するよう
にして、熱気球のような効果を期待することも出来る。
光り発電の幕が進歩し、強度と発電効率が良くなればエ
ンジンをモーターに変える事も可能となる。
In the figure, 1 is a fuselage composed of an airtight tube into which air is injected, 2 is a wing, 3 is a spar, 4 is a blanket, 5
Is a vertical stabilizer, 6 is a rudder, 7 is a horizontal stabilizer, and 8 is an elevator. Necessary wing spars, struts, and rod-like objects such as hinge shafts that connect the stabilizers and rudder / elevator to the wings have a structure that can expand and contract like fishing rods. To the fuselage in the manner described above. The feather cloth has a structure that can be expanded and folded according to the expansion and contraction of the spar, the strut, and the hinge axis, using an airtightly treated material of ultra-fine yarn fabric such as carbon fiber, glass fiber, and chemical fiber. Although the small bones of the wing are omitted in the figure, they are attached to the spar in the same manner as the fishing line guide. 9 is a front wheel, 10 is a half-plate-shaped reinforcement, 11 is a tail wheel, 1
Reference numeral 2 denotes a propeller shaft, and reference numeral 13 denotes a chassis, which is provided above and below the body, and adheres to the body 1 with a binder 14. The shears may be assembled hexahedrons or tetrahedrons if necessary.
In this case, there is no inconvenience in turning the engine, which will be described later. As the material, a light and strong carbon fiber reinforcing material similar to the three spar columns is used. 15 is a pivot hole, 16 is a wing cover when the wing is folded, 17 is a cockpit, and 18 is a bottom, which is airtight on the bottom of the fuselage using a light, strong, airtight and waterproof cloth similar to the fuselage. Stick to. The upper surface is made the same, the relationship with the cockpit backrest is made airtight, and air is similarly injected into the space in front of the chassis to form a streamlined upper and lower surface. The fuel tank will be provided in an appropriate space such as below the cockpit. Reference numeral 19 denotes a control rod. In the case of running on the ground or at sea, tighten the ball joint 20 and
It becomes an ordinary handle. Reference numeral 21 denotes a handle bar, and 22 denotes a steering cable, which is removed except for flight. 23 is an engine, 24
Is a support shaft, 25 is a drive shaft of an engine, 26 is an axle, 27 is a guide, and 28 is a stopper so that it can be attached and detached. Reference numeral 29 denotes a clutch, and reference numeral 30 denotes a slide shaft which is slidably connected to the drive shaft 25.
Reference numeral 31 denotes the sliding portion, and reference numeral 35 denotes wheels. Reference numeral 32 denotes a rebound spring that pushes the slide shaft 30 to connect the clutch 29. FIG. 5 is a partial sectional view of a sliding portion 31. 33, 34
Is a part of the opening / closing mechanism of the clutch 29, 33 is an opening / closing spring,
Reference numeral 34 denotes a spring guide having a surface inclined toward the center as shown in the figure. The operating mechanism is shown in FIG. 36 is a clutch pedal, 37 and 38 are fulcrums, and 39 is a free connection point. When flying, the slide shaft 30 is removed from the drive shaft, and the engine 23 is turned to connect the drive shaft 25 to the propeller shaft 12 with the screw 40. Reference numeral 41 denotes a propeller. Parts that need to penetrate the fuselage, such as axles, propeller shafts, wing spars, and steering ropes, should be airtightly attached to cylinders, and tubes such as fluorine resin should be inserted as protective devices into frictional parts such as rotation and slippage. When the wing is made of heat-resistant material, exhaust gas is introduced and discharged from the wing tip, so that an effect like a hot air balloon can be expected.
As the curtain of light generation progresses and strength and power generation efficiency improve, it will be possible to change the engine to a motor.

【発明の効果】【The invention's effect】

【0008】 一つの車で陸海空を行動出来楽しいもの
になる。目的地への経路の短縮が可能で交通緩和にも役
立つ。そのため車が軽い事と共にエネルギー消費が少な
くなり、有害排気ガスの減少にも役立つ。高価な橋梁・
トンネルの必要が少なくなり、それの無い部分も自由に
往来可能となる。
[0008] A single car can travel on land, sea and air, making it fun. It is possible to shorten the route to the destination and it is also useful for traffic mitigation. As a result, lighter cars consume less energy and help reduce harmful emissions. Expensive bridges
The need for tunnels is reduced, and parts without tunnels can be freely moved.

【図面の簡単な説明】[Brief description of the drawings]

【図1】 機体の側面図で翼は断面を示す。FIG. 1 is a side view of a fuselage showing wings in cross section.

【図2】 機体の平面図で右翼を縮めて収納した場合を
示す。
FIG. 2 is a plan view of the fuselage showing a case where the right wing is retracted and stored.

【図3】 操縦稈とハンドル棒の結合部分を示す。FIG. 3 shows a connecting portion between a control culm and a handle bar.

【図4】 右側の大部を省略した動力伝達機構を示す。FIG. 4 shows a power transmission mechanism in which most of the right side is omitted.

【図5】 駆動軸と滑り軸の組合せ滑り部分の一部を示
す。
FIG. 5 shows a part of a combined sliding portion of a drive shaft and a sliding shaft.

【図6】 クラッチ機構の側面図を示す。FIG. 6 shows a side view of the clutch mechanism.

【符号の説明】[Explanation of symbols]

1 胴体 2 翼 3 翼桁 4 羽布 5 垂直安定板 6 方向舵 7 水平安定板 8 昇降舵 9 前輪 10 半皿型の捕強部 11 尾輪 12 プロペラ軸 13 シャーシー 14 バインダー 15 旋回軸穴 16 翼カバー 17 操縦席 18 底 19 操縦稈 20 球関接手 21 ハンドル棒 22 操縦索 23 エンジン 24 支軸 25 駆動軸 26 車軸 27 ガイド 28 止金 29 クラッチ 30 滑り軸 31 滑り部分 32 反発バネ 33 開閉バネ 34 バネガイド 35 車輪 36 クラッチペダル 37 支点 38 支点 39 自由結合点 40 ネジ 41 プロペラ DESCRIPTION OF REFERENCE NUMERALS 1 fuselage 2 wing 3 spar 4 feather 5 vertical stabilizer 6 rudder 7 horizontal stabilizer 8 elevator 9 front wheel 10 semi-dish type forcing part 11 tail wheel 12 propeller shaft 13 chassis 14 binder 15 turning shaft hole 16 blade cover 17 cockpit 18 bottom 19 steering culm 20 ball joint 21 handle rod 22 steering cable 23 engine 24 support shaft 25 drive shaft 26 axle 27 guide 28 stopper 29 clutch 30 slide shaft 31 sliding portion 32 rebound spring 33 opening and closing spring 34 spring guide 35 Wheel 36 clutch pedal 37 fulcrum 38 fulcrum 39 free connection point 40 screw 41 propeller

【手続補正書】[Procedure amendment]

【提出日】平成10年12月25日[Submission date] December 25, 1998

【手続補正1】[Procedure amendment 1]

【補正対象書類名】図面[Document name to be amended] Drawing

【補正対象項目名】全図[Correction target item name] All figures

【補正方法】変更[Correction method] Change

【補正内容】[Correction contents]

【図1】 FIG.

【図2】 FIG. 2

【図3】 FIG. 3

【図4】 FIG. 4

【図5】 FIG. 5

【図6】 FIG. 6

【図7】 FIG. 7

【手続補正書】[Procedure amendment]

【提出日】平成10年12月25日[Submission date] December 25, 1998

【手続補正1】[Procedure amendment 1]

【補正対象書類名】明細書[Document name to be amended] Statement

【補正対象項目名】全文[Correction target item name] Full text

【補正方法】変更[Correction method] Change

【補正内容】[Correction contents]

【書類名】 明細書[Document Name] Statement

【発明の名称】 翼付きエヤーボデー車[Title of the Invention] Aircraft body with wings

【特許請求の範囲】[Claims]

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【産業上の利用分野】[Industrial applications]

【0002】 乗り物に関するものである。[0002] It relates to vehicles.

【従来の技術】[Prior art]

【0003】 エヤーボデーの車(公開63−2229
92)本出願人保有の特許第2747197号がある。
クレームは「シャーシーと、空気を圧入した環状チュー
ブからなる胴体と、空気を圧入した複数のチューブから
それぞれなる複数の屋根支柱と、柔軟性のある合成樹脂
又はこれに類するものからなる屋根とを有するエヤーボ
デー車において、バインダーにて前記シャーシーと前記
胴体とをくみつけると共に、前記胴体の両側部に前記各
屋根支柱の両端部を取付け、さらに、これら屋根支柱で
前記屋根を支持したことを特徴とするエヤーボデー車」
である。
[0003] Ayerbody's car (Publication 63-2229)
92) There is Japanese Patent No. 2747197 owned by the present applicant.
The claim `` has a chassis, a body consisting of an annular tube pressurized with air, a plurality of roof supports each consisting of a plurality of tubes pressurized with air, and a roof made of flexible synthetic resin or the like. In the air body vehicle, the chassis and the body are attached together with a binder, and both ends of the roof pillars are attached to both sides of the body, and the roof is supported by the roof pillars. Airy Body Car "
It is.

【発明が解決しようとする課題】[Problems to be solved by the invention]

【0004】 前記の乗り物に翼とプロペラを付け陸・
海・空を一つの乗り物で行動出来るようにする。
[0004] Attaching wings and propellers to the vehicle
Make the sea and sky moveable with one vehicle.

【課題を解決する為の手段】[Means for solving the problem]

【0005】 空気を圧入したチューブからなる胴体
に、、伸縮可能な桁や、支柱等棒状のものと、その伸縮
に伴い折畳み出来るようにした羽布よりなる翼を取り付
け、上下に突出した支軸を有するエンジンを、支軸を中
心に、水平方向に回す事の出来るように、前記胴体にバ
インダーで付設したシヤーシーに取付け、そのエンジン
で車輪を回して地上走行し、水上ではその車輪が水掻き
となり、空をとぶ場合はエンジンの駆動軸を前後方向に
変え、その駆動軸にプロペラ軸を取りつける。
A body made of a tube into which air is press-fitted is attached with a bar-shaped thing such as an expandable girder or a strut and a wing made of a feather cloth that can be folded along with the expansion and contraction, and a vertically protruding spindle. Is mounted on a chassis attached to the fuselage with a binder so that the engine can be turned horizontally around the support shaft, and the engine turns the wheels to run on the ground. When flying in the sky, change the drive shaft of the engine in the front-rear direction and attach the propeller shaft to the drive shaft.

【作用】[Action]

【0006】 1っの乗り物で水陸空の行動が可能、軽
いので離着陸距離が短く、水上離着陸が可能で、陸上で
は飛行場でなくても、小さな空き地、路上でも離着陸が
出来る。墜落・衝突事故に際してボデーはクッションと
なる。
[0006] A single vehicle can act on land, land and air, and since it is light, the take-off and landing distance is short, and it is possible to take off and land on water. The body becomes a cushion in the event of a crash or collision.

【実施例】【Example】

【0007】 図に於いて1は空気を圧入した気密なチ
ューブからなる胴体、2は翼、3は翼桁、4は羽布、5
は垂直安定板、6は方向舵、7は水平安定板、8は昇降
舵である。これら翼類に必要な翼桁・支柱・各安定板と
方向舵・昇降舵を繋ぐ蝶番軸等棒状の物は、釣り竿の様
に伸縮出来る構造とし、使用しない場合は、翼桁は中央
部のシャシー内に、他の支柱類は適宜の方法で胴体に収
納するか、取り外す。羽布は炭素繊維・ガラス繊維・化
学繊維等の極細糸織物を、気密処理した物を用いて、翼
桁・支柱・蝶番軸等の伸縮に従って展開・折り畳み出来
る構造とする。翼の小骨は図では省略したが、釣り竿の
道糸ガイドを横にした状態のものを基準にして付けるの
が簡単であるが、その他既知の適宜な方法で翼桁に取付
ける。9は前輪、10は半皿型の補強部、11は尾輪、
42は地上走行時の、旋回差動調整の索を示す。、12
はプロペラ軸、13はシャーシーで前記胴体の上下に渡
してバインダー14で胴体1に接着する。シヤーシーは
必要に応じ、六面体や四面体としてもよい、この場合後
述するエンジンの旋回に不都合の無いようにする。素材
は翼桁3や支柱類と同様の、軽くて強い炭素繊維補強材
等を用いる。15は旋回軸穴、16は翼を折り畳んだ場
合の翼カバー、17は操縦席、18は底で、胴体と同様
の軽くて強く気密で、防水性のある布を用いて胴体に気
密に張つける。操縦席背凭れ、その後ろの空間、シヤー
シーの前の空間も同様にして空気を圧入し、上下面の流
線型を整える。燃料タンクは操縦席の下等適宜の空間に
設ける。19は操縦棹で、地上・海上走行の場合は球関
接手20を締め、21の止ネジを緩めて普通のハンドル
となる。43はハンドルの鞘、44はハンドル、45は
ハンドルの鞘と車軸との繋でハンドルの操作を車軸に伝
える。ハンドルの動きを走行装置に伝えるには既知の方
法が色々ある。46は止ネジ、47は尾輪の振棒を示
す。22は操縦索を示し飛行の場合以外は外す。23は
エンジン、24は支軸、25はエンジンの駆動軸、26
は車軸、27はガイド、28は止金で着脱出来るように
する。29はクラッチ、30は滑り軸で駆動軸25と滑
り結合とする。31はその滑り部分、35は車輪を示
す。32は反発バネで滑り軸30を押してクラッチ29
を結合させる。第5図は31の滑り部分の一部断面図で
ある。33、34はクラッチ29の開閉機構の一部で、
33は開閉バネ、34は中心に向かって図の様に傾斜し
た面より成るバネガイドである。その作動機構は第6図
に示す。36はクラッチペダル、37・38は支点、3
9は自由結合点を示す。飛行する場合は滑り軸30を駆
動軸から外し、エンジン23を回して駆動軸25をプロ
ペラ軸12にネジ40で結合する。41はプロペラを示
す。車軸・プロペラ軸・翼桁・操縦索等胴体を貫通する
必要のある部分は、気密な筒貼りとし、回転・滑り等の
摩擦部分にはフッソ樹脂等の管を保護装置として挿入す
る。翼を耐熱素材で作った場合、排気を導入し、翼端か
ら放出するようにして、熱気球のような効果を期待する
ことも出来る。光り発電の幕が進歩し、強度と発電効率
が良くなればエンジンをモーターに変える事も可能とな
る。水上航行の為には、車輪の側面に魚の胸鰭類似の物
を付けると効率的である。その他の場合は鰭は振れ止め
とする。図では胴体全体を流線型としたが、尾部は翼桁
と同構造の骨材の露出として、胴体部分は円形や楕円形
としてもよい。
In the figure, 1 is a fuselage composed of an airtight tube into which air is injected, 2 is a wing, 3 is a spar, 4 is a blanket, 5
Is a vertical stabilizer, 6 is a rudder, 7 is a horizontal stabilizer, and 8 is an elevator. Necessary bar-shaped objects such as hinge shafts that connect the spar, strut, and stabilizers to the rudder / elevator are required to be able to expand and contract like fishing rods. Inside, the other struts are housed in the fuselage or removed in an appropriate manner. The feather cloth has a structure that can be expanded and folded according to expansion and contraction of a spar, a strut, a hinge shaft, and the like by using an airtightly treated material of ultra-fine yarn fabric such as carbon fiber, glass fiber, and chemical fiber. Although the wing small bones are not shown in the figure, it is easy to attach them based on the fishing rod with the road line guide laid down, but it is attached to the spar by any other known appropriate method. 9 is a front wheel, 10 is a half-plate-shaped reinforcement, 11 is a tail wheel,
Reference numeral 42 denotes a cable for turning differential adjustment during taxiing. , 12
Is a propeller shaft, and 13 is a chassis which is passed over and under the body and adheres to the body 1 with a binder 14. The shear may be a hexahedron or a tetrahedron if necessary. In this case, there is no inconvenience in turning the engine described later. As the material, a light and strong carbon fiber reinforcing material similar to the spar 3 and the struts is used. Reference numeral 15 denotes a pivot hole, 16 denotes a wing cover when the wing is folded, 17 denotes a cockpit, and 18 denotes a bottom, which is airtightly attached to the fuselage using a light, strongly airtight and waterproof cloth similar to the fuselage. Put on. In the same way, air is injected into the cockpit backrest, the space behind it, and the space in front of the chassis to adjust the upper and lower streamlines. The fuel tank will be provided in an appropriate space such as below the cockpit. Reference numeral 19 denotes a control rod. In the case of running on the ground or at sea, the ball joint 20 is tightened, and the set screw 21 is loosened to form a normal handle. Reference numeral 43 denotes a handle sheath, reference numeral 44 denotes a handle, and reference numeral 45 denotes a connection between the handle sheath and the axle to transmit operation of the handle to the axle. There are various known methods for transmitting the movement of the steering wheel to the traveling device. 46 is a set screw, and 47 is a tail rod. Reference numeral 22 denotes a steering cable, which is removed except for flight. 23 is an engine, 24 is a support shaft, 25 is a drive shaft of the engine, 26
Is an axle, 27 is a guide, and 28 is removable with a stopper. Reference numeral 29 denotes a clutch, and reference numeral 30 denotes a slide shaft which is slidably connected to the drive shaft 25. Reference numeral 31 denotes the sliding portion, and reference numeral 35 denotes wheels. 32 is a rebound spring that pushes the slide shaft 30 and pushes the clutch 29
To combine. FIG. 5 is a partial sectional view of a sliding portion 31. 33 and 34 are a part of the opening and closing mechanism of the clutch 29,
Reference numeral 33 denotes an opening / closing spring, and reference numeral 34 denotes a spring guide having a surface inclined toward the center as shown. The operating mechanism is shown in FIG. 36 is a clutch pedal, 37 and 38 are fulcrums, 3
9 indicates a free bonding point. When flying, the slide shaft 30 is removed from the drive shaft, and the engine 23 is turned to connect the drive shaft 25 to the propeller shaft 12 with the screw 40. Reference numeral 41 denotes a propeller. Parts that need to penetrate the fuselage, such as axles, propeller shafts, wing spars, and steering cables, should be sealed in airtight cylinders, and pipes made of fluororesin or the like should be inserted as protective devices into frictional parts such as rotation and slippage. When the wing is made of heat-resistant material, exhaust gas is introduced and discharged from the wing tip, so that an effect like a hot air balloon can be expected. As the curtain of light generation progresses and strength and power generation efficiency improve, it will be possible to change the engine to a motor. For water navigation, it is effective to attach a pectoral fin-like object to the side of the wheel. In other cases, the fins should be steady. In the figure, the entire fuselage is streamlined, but the tail may be exposed to the aggregate having the same structure as the spar and the fuselage may be circular or elliptical.

【発明の効果】【The invention's effect】

【0008】 一つの車で陸海空を行動出来楽しいもの
になる。目的地への経路の短縮が可能で交通緩和にも役
立つ。そのため車が軽い事と共にエネルギー消費が少な
くなり、有害排気ガスの減少にも役立つ。高価な飛行場
・橋梁・トンネルの必要が少なくなり、それの無い高地
・ローカル地域も自由に往来可能となる。
[0008] A single car can travel on land, sea and air, making it fun. It is possible to shorten the route to the destination and it is also useful for traffic mitigation. As a result, lighter cars consume less energy and help reduce harmful emissions. The need for expensive airfields, bridges and tunnels is reduced, and highlands and local areas without them can be freely moved.

【図面の簡単な説明】[Brief description of the drawings]

【図1】 機体の側面図で翼は断面を示す。FIG. 1 is a side view of a fuselage showing wings in cross section.

【図2】 機体の平面図で右翼を縮めて収納した場合を
示す。
FIG. 2 is a plan view of the fuselage showing a case where the right wing is retracted and stored.

【図3】 操縦稈とハンドル棒の結合部分を示す。FIG. 3 shows a connecting portion between a control culm and a handle bar.

【図4】 右側の大部を省略した動力伝達機構を示す。FIG. 4 shows a power transmission mechanism in which most of the right side is omitted.

【図5】 駆動軸と滑り軸の組合せ滑り部分の一部を示
す。
FIG. 5 shows a part of a combined sliding portion of a drive shaft and a sliding shaft.

【図6】 クラッチ機構の側面図を示す。FIG. 6 shows a side view of the clutch mechanism.

【図7】 地上旋回差動調整機構を示す。FIG. 7 shows a ground swing differential adjustment mechanism.

【符号の説明】 1 胴体 2 翼 3 翼桁 4 羽布 5 垂直安定板 6 方向舵 7 水平安定板 8 昇降舵 9 前輪 10 半皿型の補強部 11 尾輪 12 プロペラ軸 13 シャーシー 14 バインダー 15 旋回軸穴 16 翼カバー 17 操縦席 18 底 19 操縦稈 20 球関接手 21 ハンドル棒 22 操縦索 23 エンジン 24 支軸 25 駆動軸 26 車軸 27 ガイド 28 止金 29 クラッチ 30 滑り軸 31 滑り部分 32 反発バネ 33 開閉バネ 34 バネガイド 35 車輪 36 クラッチペダル 37 支点 38 支点 39 自由結合点 40 ネジ 41 プロペラ 42 索 43 鞘 44 ハンドル 45 繋ぎ 46 止ネジ 47 振棒[Description of Signs] 1 fuselage 2 wing 3 spar 4 feather 5 vertical stabilizer 6 rudder 7 horizontal stabilizer 8 elevator 9 front wheel 10 semi-dish-shaped reinforcement 11 tail wheel 12 propeller shaft 13 chassis 14 binder 15 turning shaft Hole 16 wing cover 17 cockpit 18 bottom 19 steering culm 20 ball joint 21 handlebar 22 steering cable 23 engine 24 support shaft 25 drive shaft 26 axle 27 guide 28 stopper 29 clutch 30 slide shaft 31 sliding portion 32 rebound spring 33 opening and closing Spring 34 Spring guide 35 Wheel 36 Clutch pedal 37 Support point 38 Support point 39 Free connection point 40 Screw 41 Propeller 42 Cable 43 Sheath 44 Handle 45 Connection 46 Set screw 47 Shake rod

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 空気を圧入したチューブからなる胴体
に、、伸縮出来る桁と、その伸縮に伴い折畳み出来るよ
うにした羽布よりなる翼を取り付け、上下に突出した支
軸を有するエンジンを、支軸を中心に、水平方向に回す
事の出来るように、前記胴体にバインダーで付設したシ
ヤーシーに取付け、そのエンジンで車輪を回して地上走
行し、水上ではその車輪が水掻きとなり、空をとぶ場合
はエンジンの駆動軸を前後方向に変え、その駆動軸にプ
ロペラ軸を取りつけるようにした構造物。
An engine having a vertically protruding support shaft is attached to a body made of a tube into which air is press-fitted, and an expandable girder and a wing made of a feather cloth which can be folded along with the expansion and contraction are attached to the body. Attached to the chassis attached to the fuselage with a binder so that it can be turned in the horizontal direction around the axis, running the wheel with the engine and running on the ground, on the water the wheel becomes a webbed, and when flying in the sky A structure in which the drive shaft of the engine is changed in the front-rear direction, and the propeller shaft is attached to the drive shaft.
JP4275698A 1998-01-19 1998-01-19 Winged air-body vehicle Pending JPH11198621A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4275698A JPH11198621A (en) 1998-01-19 1998-01-19 Winged air-body vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4275698A JPH11198621A (en) 1998-01-19 1998-01-19 Winged air-body vehicle

Publications (1)

Publication Number Publication Date
JPH11198621A true JPH11198621A (en) 1999-07-27

Family

ID=12644849

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4275698A Pending JPH11198621A (en) 1998-01-19 1998-01-19 Winged air-body vehicle

Country Status (1)

Country Link
JP (1) JPH11198621A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103287521A (en) * 2013-06-14 2013-09-11 浙江理工大学 Double-spiral-groove-channel cam drive type wheel paddle leg integrated vehicle wheel structure
US9259984B2 (en) 2008-07-28 2016-02-16 Fleck Future Concepts Gmbh Combined air, water and road vehicle

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9259984B2 (en) 2008-07-28 2016-02-16 Fleck Future Concepts Gmbh Combined air, water and road vehicle
CN103287521A (en) * 2013-06-14 2013-09-11 浙江理工大学 Double-spiral-groove-channel cam drive type wheel paddle leg integrated vehicle wheel structure

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