JPH03292300A - Lift generating device - Google Patents
Lift generating deviceInfo
- Publication number
- JPH03292300A JPH03292300A JP9435190A JP9435190A JPH03292300A JP H03292300 A JPH03292300 A JP H03292300A JP 9435190 A JP9435190 A JP 9435190A JP 9435190 A JP9435190 A JP 9435190A JP H03292300 A JPH03292300 A JP H03292300A
- Authority
- JP
- Japan
- Prior art keywords
- lift
- air
- generating device
- wing
- 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
- 239000000446 fuel Substances 0.000 abstract description 2
- 230000001105 regulatory effect Effects 0.000 abstract 1
- 230000005484 gravity Effects 0.000 description 1
- 230000029305 taxis Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Landscapes
- Vibration Prevention Devices (AREA)
Abstract
Description
【発明の詳細な説明】
この発明は、翼に人工的に気流を起こし、揚力を発生さ
せる装置に関するものである。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a device that generates lift by artificially creating airflow on a wing.
1、揚力発生装置の説明
揚力発生装置は、第1図に示すように、真の上側全面に
空気の流れが起こるように風を送り、真の上側の垂直方
向に対する気圧を下げ、その上下の気圧差により揚力を
発生させる装置である。1. Description of Lift Generation Device As shown in Figure 1, the lift generation device sends wind so that air flows over the entire surface of the true upper side, lowers the atmospheric pressure in the vertical direction of the true upper side, and increases the air pressure above and below it. This is a device that generates lift using a pressure difference.
2、揚力発生装置を付加した航空機
従来の飛行機は、静止した空気に対して機体をある程度
の速度で進め、真に空気の流れを第2図のように起こし
、翼の上下での気流の違いから気圧差を生じ、揚力を発
生させていた。したがって機体の速度を上げなければ揚
力が発生しないため長い滑走路を必要とし、離着陸時が
高速なため′・操縦が難しく危険であった。その上、離
着陸時の騒音・振動も問題にされていた。2. Aircraft equipped with a lift generating device Conventional airplanes advance the aircraft at a certain speed against still air, creating true airflow as shown in Figure 2, and creating a difference in airflow above and below the wing. This creates a pressure difference, which generates lift. Therefore, lift cannot be generated unless the aircraft speed is increased, requiring a long runway, and the high speeds of takeoff and landing made maneuvering difficult and dangerous. In addition, noise and vibration during takeoff and landing were also a problem.
また、本発明と同様な機構で揚力を発生させる短距離離
着陸機もあるが、飛行用エンジンと揚力発生装置が兼用
しているため、主翼の一部に揚力を発生させることしか
できながった。There are also short-range takeoff and landing aircraft that generate lift using a mechanism similar to the present invention, but because the flight engine and lift generator are both used, lift can only be generated on a portion of the main wing. Ta.
尚、従来の垂直離着陸機は、推進力により垂直上昇させ
るためエネルギー的に効率が悪く、バランスを保つため
には高度の技術を要した。Conventional vertical take-off and landing aircraft use propulsion to lift vertically, which is inefficient in terms of energy, and requires advanced technology to maintain balance.
(ア)本発明の揚力発生装置を第3図のように飛行機に
取り付け、装置を作動させると第4図に示すように、機
体が滑走するとすぐに上昇する。ある程度の高度になっ
たとき、ジェットエンジンを噴射し、揚力発生装置を停
止して通常の飛行に移る0着陸時には、揚力発生装置を
作動し揚力を発生させた後、ジェットエンジンを停止し
て速度をおとし、第4図のように着陸する。よって、離
着陸時の騒音・振動が低く、滑走路が短縮できる。また
、離着陸時が低速なため容易に操縦ができ、安全である
。(a) When the lift generating device of the present invention is attached to an airplane as shown in FIG. 3 and the device is activated, the airplane will rise as soon as it taxis, as shown in FIG. 4. When a certain altitude is reached, the jet engine is injected, the lift generator is stopped, and normal flight begins.During landing, the lift generator is activated to generate lift, then the jet engine is stopped and the speed is increased. and land as shown in Figure 4. Therefore, noise and vibration during takeoff and landing are low, and the runway can be shortened. In addition, the aircraft takes off and lands at low speeds, making it easy to maneuver and safe.
(イ)第5図は、翼を円形にした揚力発生装置を付加し
た垂直離着陸機である。装置を作動させると、翼に揚力
が生じ垂直上昇する。揚力で上昇させるため、エネルギ
ー効率がよく、重心を下方にとれるのでバランスを保ち
やすい、その上、装置が故障しても翼が落下重代わりに
なるので、バランスを保ちながら低速で降下していく、
墜落直前で逆噴射をすれば安全に着陸できる。(a) Figure 5 shows a vertical takeoff and landing aircraft with circular wings and a lift generator. When the device is activated, lift is generated on the wings, causing them to rise vertically. Since it lifts up using lift, it is energy efficient, and it is easy to maintain balance because the center of gravity is lowered.Furthermore, even if the device fails, the wings will replace the falling weight, so it descends at a low speed while maintaining balance. ,
If you reverse thrust just before crashing, you can land safely.
このように、航空機に揚力発生装置を付加することは、
安全に航行でき、消費燃料の節約になるまた、騒音・振
動の対策にもなる。尚、翼の形状気流発生方法は、その
他にも色々考えられる。In this way, adding a lift generating device to an aircraft
It allows for safe navigation, saves fuel consumption, and also acts as a countermeasure against noise and vibration. It should be noted that various other methods for generating airflow based on the shape of the wing can be considered.
3、揚力発生装置を取り付けた運搬用機械物体を移動す
る場合、鉛直方向の移動は困難であるが、水平方向に移
動することは易しい、したがって、運搬用機械に第6図
のような揚力発生装置を取り付けると、物体を容易に運
ぶことができる。3. When moving a transporting machine equipped with a lift generating device, it is difficult to move vertically, but it is easy to move horizontally. Therefore, the transporting machine has a lift generating device as shown in Figure 6. Once the device is attached, objects can be easily transported.
また、小型の揚力発生装置は、小荷物の運搬用にも使え
る。The small lift generator can also be used to transport small items.
4、その他の応用
揚力発生装置を体に取り付けることにより、人間を飛行
させることもできる。tた、玩具や模型にも応用できる
。4. Other applications Humans can also be made to fly by attaching lift generating devices to their bodies. It can also be applied to toys and models.
尚、水中でも同様に、揚力発生装置で水流を起こし、揚
力を発生させることができる。Note that even underwater, the lift generating device can generate water flow to generate lift.
以上のように、揚力発生装置は幅広く応用できる。As mentioned above, the lift generating device can be widely applied.
第1図は、揚力発生装置を作動させたときの空気の流れ
の断面図。
第2図は、従来の飛行機の翼に対する空気の流れの断面
図。
第3図は、揚力発生装置を付加した飛行機の視斜図、お
よび、離着陸時・ジェット飛行時における主翼の断面図
。
第4図は、飛行機の飛行径路の左側面図。
第5図は、本発明の垂直離着陸機の視斜図・正面図、お
よび、縦断面・横断面の断面図。
第6図は、運搬用揚力発生装置の左側面図。
第1図
第2図
図面
断面図
く真tel呼〉
第3図
視斜図
第4図
〈離陸時〉
左側面図
〈着陸時〉
左側面図
第5図
視斜図
縦断面図
正面図
横断面図
第6図
左側面図FIG. 1 is a cross-sectional view of the air flow when the lift generating device is operated. FIG. 2 is a cross-sectional view of air flow through a conventional airplane wing. FIG. 3 is a perspective view of an airplane equipped with a lift generating device, and a sectional view of the main wing during takeoff and landing and during jet flight. Figure 4 is a left side view of the airplane's flight path. FIG. 5 is a perspective view, a front view, and longitudinal and transverse cross-sectional views of the vertical take-off and landing aircraft of the present invention. FIG. 6 is a left side view of the lift generating device for transportation. Fig. 1 Fig. 2 Drawing sectional view (tel) Fig. 3 Perspective view Fig. 4 <At the time of takeoff> Left side view <At the time of landing> Left side view Fig. 5 Perspective view Longitudinal sectional view Front view Cross section Figure 6 Left side view
Claims (1)
装置。 2、揚力発生装置を付加した航空機。 3、揚力発生装置を取り付けた運搬用機械。[Claims] 1. A lift generation device that generates lift by artificially creating airflow. 2. Aircraft equipped with a lift generator. 3. A transportation machine equipped with a lift generator.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP9435190A JPH03292300A (en) | 1990-04-10 | 1990-04-10 | Lift generating device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP9435190A JPH03292300A (en) | 1990-04-10 | 1990-04-10 | Lift generating device |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH03292300A true JPH03292300A (en) | 1991-12-24 |
Family
ID=14107864
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP9435190A Pending JPH03292300A (en) | 1990-04-10 | 1990-04-10 | Lift generating device |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH03292300A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7726609B2 (en) * | 2007-03-16 | 2010-06-01 | The Boeing Company | High-performance low-noise aircraft exhaust systems and methods |
-
1990
- 1990-04-10 JP JP9435190A patent/JPH03292300A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7726609B2 (en) * | 2007-03-16 | 2010-06-01 | The Boeing Company | High-performance low-noise aircraft exhaust systems and methods |
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