JPH07251798A - Aircraft - Google Patents

Aircraft

Info

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
Application number
JP8218794A
Other languages
Japanese (ja)
Inventor
Akira Watanabe
晃 渡邉
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 JP8218794A priority Critical patent/JPH07251798A/en
Publication of JPH07251798A publication Critical patent/JPH07251798A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To provide lift by making an airframe planar, eliminating a wing, and inclining the airframe plane upwards with respect to the direction of motion. CONSTITUTION:An aircraft going forward in the air is allowed to fly in the air because the sum of upward forces exerted on its bottom and diagonally downward side by collision with air exceeds that of downward forces exerted on its top and diagonally upward side from air and gravity. When the airframe is sectioned in terms of weight, the horizontal and longitudinal center parts of the airframe which are relatively great in length and small in width collide with air to provide upward forces. The aircraft is given lift like an Oriental kite by the inclination of the airframe plane relative to the direction of motion. When upward forces are not required, the airframe plane need not be inclined at all relative to the direction of motion.

Description

【発明の詳細な説明】Detailed Description of the Invention

【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.

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

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)

【特許請求の範囲】[Claims] 【請求項1】 大気中を前進すると真下及び斜め下を向
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.
JP8218794A 1994-03-15 1994-03-15 Aircraft Pending JPH07251798A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (2)

* Cited by examiner, † Cited by third party
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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