JPH07251798A - Aircraft - Google Patents
AircraftInfo
- Publication number
- JPH07251798A JPH07251798A JP8218794A JP8218794A JPH07251798A JP H07251798 A JPH07251798 A JP H07251798A JP 8218794 A JP8218794 A JP 8218794A JP 8218794 A JP8218794 A JP 8218794A JP H07251798 A JPH07251798 A JP H07251798A
- Authority
- JP
- Japan
- Prior art keywords
- airframe
- air
- upward
- motion
- aircraft
- 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
- Toys (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】大気中を飛行するための機械に関
する。[Field of Industrial Application] A machine for flying in the atmosphere.
【0002】[0002]
【従来の技術】従来の飛行機は左右の主翼で揚力を得て
いた。しかし左右に長い主翼は空気抵抗、構造的強度、
製造工程、速さ、燃料消費、格納のいずれにおいても従
来の飛行機を不利なものにしている。2. Description of the Related Art In a conventional airplane, lift is obtained from the left and right main wings. However, the left and right long wings have air resistance, structural strength,
The manufacturing process, speed, fuel consumption, and storage all make the conventional aircraft disadvantageous.
【0003】[0003]
【発明が解決しようとする課題】前後に長く左右に短い
飛行機を提供することにある。An object of the present invention is to provide an airplane that is long in the front and rear and short in the left and right.
【0004】[0004]
【課題を解決するための手段】機体を平面的にし、主翼
をなくし機体平面を進行方向に対して上向きに傾けるこ
とで揚力を得る。Lifting force is obtained by flattening the fuselage, eliminating the main wing, and tilting the plane of the fuselage upward with respect to the traveling direction.
【0005】[0005]
【作用】図1のように機体平面と進行方向の傾きによっ
て、東洋の凧のようにして揚力を得る。上向きの力が必
要ないときは図2のように進行方向に対して機体平面の
傾きをほとんどなくしてもよい。図1、図2共に矢印の
向きが進行方向を表している。The lift is obtained like an oriental kite by the inclination of the plane and the traveling direction as shown in FIG. When the upward force is not necessary, the inclination of the plane of the body with respect to the traveling direction may be almost eliminated as shown in FIG. In both FIGS. 1 and 2, the direction of the arrow indicates the traveling direction.
【0006】[0006]
【実施例】巡航ミサイルや飛行機、グライダー、フライ
トモデルなどが考えられる。図3は飛行機としての好適
な実施例の一つをあらわしたものである。[Examples] Cruise missiles, airplanes, gliders, flight models, etc. are conceivable. FIG. 3 shows one of the preferred embodiments as an airplane.
【0007】[0007]
【発明の効果】左右に短い飛行機が生まれた。[Effects of the Invention] A short plane is born on the left and right.
図1、図2、図3共に本発明の斜視図である。 1, 2 and 3 are perspective views of the present invention.
Claims (1)
いた面が空気と衝突して受ける上向きの力の合計が、真
上及び斜め上を向いた面が空気から受ける下向きの力と
重力の合計より大きくなることで大気中を飛行すること
ができる機械で、重さにしたがって機体を分けたとき
に、左右方向及び前後方向共に中心の相対的に前後に長
く左右に短い部分で空気との衝突によって上向きの力を
得ることができる形状的特徴をもった機械。1. When advancing in the atmosphere, the total of the upward forces received by the surfaces facing downward and obliquely downward when colliding with air is the downward force and gravity received from the air by the surfaces facing upward and obliquely upward. A machine that can fly in the atmosphere by becoming larger than the total of A machine with a geometrical characteristic that can obtain upward force by collision of.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP8218794A JPH07251798A (en) | 1994-03-15 | 1994-03-15 | Aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP8218794A JPH07251798A (en) | 1994-03-15 | 1994-03-15 | Aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH07251798A true JPH07251798A (en) | 1995-10-03 |
Family
ID=13767441
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP8218794A Pending JPH07251798A (en) | 1994-03-15 | 1994-03-15 | Aircraft |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH07251798A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2611297A (en) * | 2021-09-27 | 2023-04-05 | Isaksen Guttorm | A light aircraft with a dual wedge fuselage |
-
1994
- 1994-03-15 JP JP8218794A patent/JPH07251798A/en active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2611297A (en) * | 2021-09-27 | 2023-04-05 | Isaksen Guttorm | A light aircraft with a dual wedge fuselage |
GB2611297B (en) * | 2021-09-27 | 2024-09-18 | Isaksen Guttorm | A light aircraft with a dual wedge fuselage |
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