JPH10167192A - Large heli-plane of parallel engine type - Google Patents
Large heli-plane of parallel engine typeInfo
- Publication number
- JPH10167192A JPH10167192A JP35990896A JP35990896A JPH10167192A JP H10167192 A JPH10167192 A JP H10167192A JP 35990896 A JP35990896 A JP 35990896A JP 35990896 A JP35990896 A JP 35990896A JP H10167192 A JPH10167192 A JP H10167192A
- Authority
- JP
- Japan
- Prior art keywords
- plane
- heli
- engine type
- providing
- parallel engine
- 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
- 230000005540 biological transmission Effects 0.000 claims description 4
- 230000001174 ascending effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
Landscapes
- Toys (AREA)
Abstract
Description
【０００１】〔発明の属する技術分野〕この発明は四基
以上のヘリ用エンジンを並べてその動力を一本のシャフ
トに連結して四隅に設定した回転翼を同期に回して上昇
させ更に同じ動力を使用して変速機を介して前進用プロ
ペラを回して飛行させる航空機である（変速機は前進・
Ｎ・後退の三段）（各エンジンには自動連結器を付け
る）[0001] The present invention relates to a helicopter engine having four or more helicopters arranged side by side, connecting the power of the engines to one shaft, rotating the rotors set at the four corners synchronously, and raising the same power. This is an aircraft that uses a transmission to rotate a forward propeller through a transmission to fly.
N ・ Reverse three stages) (Each engine is equipped with an automatic coupler)
【０００２】〔発明が解決しようとする課題〕 （ニ）近距離旅行をする場合飛行場までのアクセスが十
分でないため時間がかかりスピードのメリットがあまり
ない （ホ）中、小型のヘリを利用したとき他の交通機関より
もコストが高すぎること本発明はこれらの欠点を改善す
るためになされたものである。[Problems to be Solved by the Invention] (d) When traveling short distances The access to the airfield is not sufficient and it takes a long time and there is not much merit of speed. (E) When a small helicopter is used in the middle The present invention has been made to remedy these drawbacks in that the cost is too high compared to other means of transportation.
【０００３】〔課題を解決するための手段〕四基の並列
されたエンジン１の動力をシャフト２にまとめて一方で
は垂直上昇用回転翼３に、またもう一方では前進用プロ
ペラ４に利用、前・後翼、同じ長さのこの航空機をバラ
ンスを保ちながら飛行をさせる本発明は以上のような構
成よりなる大型の航空機である。[Means for Solving the Problems] The power of four paralleled engines 1 is collected on a shaft 2 and used for a vertical ascending rotor 3 on the one hand and a forward propeller 4 on the other hand. The rear wing, which makes this aircraft of the same length fly while maintaining balance, is a large aircraft having the above configuration.
【０００４】〔発明の効果〕 （ヘ）大量の人員・貨物を便利に運ぶことができる。 （ト）構造が簡単で操縦が易しい。[Effect of the Invention] (f) A large amount of personnel and cargo can be conveniently carried. (G) Simple structure and easy operation.
【図１】本発明の平面図であるFIG. 1 is a plan view of the present invention.
【図２】本発明の正面図であるFIG. 2 is a front view of the present invention.
１ エンジン ２ シャフト ３ 回転翼 ４ プロペラ ５ 変速機 DESCRIPTION OF SYMBOLS 1 Engine 2 Shaft 3 Rotor 4 Propeller 5 Transmission
Claims (1)
（ロ）前・後両翼の両端に四基の回転翼さ３を設ける。
（ハ）変速機５を介してプロペラ４を設けるエンジン１
の動力をシャフト２を通じて回転翼３とプロペラ４を共
に回すようにした大型の航空機(1) Four parallel engines 1 are provided.
(B) Four rotor blades 3 are provided at both ends of the front and rear blades.
(C) Engine 1 in which propeller 4 is provided via transmission 5
Large aircraft that rotates the rotor 3 and the propeller 4 together through the shaft 2
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP35990896A JPH10167192A (en) | 1996-12-16 | 1996-12-16 | Large heli-plane of parallel engine type |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP35990896A JPH10167192A (en) | 1996-12-16 | 1996-12-16 | Large heli-plane of parallel engine type |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH10167192A true JPH10167192A (en) | 1998-06-23 |
Family
ID=18466916
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP35990896A Pending JPH10167192A (en) | 1996-12-16 | 1996-12-16 | Large heli-plane of parallel engine type |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH10167192A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2010023820A (en) * | 2008-07-22 | 2010-02-04 | Keiichi Aoyanagi | Vertical taking-off and landing aircraft |
| CN103721421A (en) * | 2012-10-16 | 2014-04-16 | 田瑜 | Aircraft with a plurality of rotors |
| CN105438461A (en) * | 2016-01-11 | 2016-03-30 | 成都学尚科技有限公司 | Power system for constructing aircraft and aircraft |
| CN105460214A (en) * | 2015-12-25 | 2016-04-06 | 天津全华时代航天科技发展有限公司 | Vertical take-off and landing tandem wing unmanned aerial vehicle |
-
1996
- 1996-12-16 JP JP35990896A patent/JPH10167192A/en active Pending
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2010023820A (en) * | 2008-07-22 | 2010-02-04 | Keiichi Aoyanagi | Vertical taking-off and landing aircraft |
| CN103721421A (en) * | 2012-10-16 | 2014-04-16 | 田瑜 | Aircraft with a plurality of rotors |
| CN105460214A (en) * | 2015-12-25 | 2016-04-06 | 天津全华时代航天科技发展有限公司 | Vertical take-off and landing tandem wing unmanned aerial vehicle |
| CN105438461A (en) * | 2016-01-11 | 2016-03-30 | 成都学尚科技有限公司 | Power system for constructing aircraft and aircraft |
| CN105438461B (en) * | 2016-01-11 | 2018-06-29 | 成都学尚科技有限公司 | A kind of dynamical system and aircraft for constructing aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| A02 | Decision of refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A02 Effective date: 20040706 |