JP3200141U - Outer ring wing vehicle - Google Patents
Outer ring wing vehicle Download PDFInfo
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- JP3200141U JP3200141U JP2015001975U JP2015001975U JP3200141U JP 3200141 U JP3200141 U JP 3200141U JP 2015001975 U JP2015001975 U JP 2015001975U JP 2015001975 U JP2015001975 U JP 2015001975U JP 3200141 U JP3200141 U JP 3200141U
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- outer ring
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- 238000007664 blowing Methods 0.000 claims abstract description 4
- 230000001629 suppression Effects 0.000 abstract description 8
- 239000002828 fuel tank Substances 0.000 abstract description 7
- 238000001816 cooling Methods 0.000 abstract description 5
- 230000002401 inhibitory effect Effects 0.000 abstract 1
- 230000002093 peripheral Effects 0.000 description 3
- 238000004642 transportation engineering Methods 0.000 description 3
- 241000272184 Falconiformes Species 0.000 description 2
- 239000002965 rope Substances 0.000 description 2
- 230000000630 rising Effects 0.000 description 1
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Abstract
【課題】外周円輪翼に内側から風を吹き付けることで外周円輪翼に揚力を生じさせ、その風力により垂直に上昇、高度維持、降下ができる飛行体であって、更に外周円輪翼に風車の回転反動抑止渦翼、水平制御補助翼および方向舵の付属装備により直進、旋回航行が可能な飛行体を提供する。
【解決手段】筐体１０の上部には内側より風を受けて飛行体を浮上させるための外周輪翼１と中央にエンジン８を装着し、エンジンの上側に出た駆動軸７には外周輪翼に向けて風を吹き付ける遠心送風扇５とエンジンを冷却するためのエンジン冷却ファン６を装着した基本構成で、エンジンの下部の筐体内部に燃料タンク９を備え、更に外周輪翼には飛行体本体の筐体が遠心送風扇の回転反動による逆転つれ回りを抑制とする何枚かの渦状の自転抑止翼２と自転量微調、兼本体の向きを変える数枚の方向舵３と更に本体の傾きを変え進行方向を定める数枚のフラップ４により構成される。
【選択図】図１A flying body that generates lift by blowing wind from the inside to an outer ring wing, and that can vertically ascend, maintain altitude, and descend by the wind force. Provided with a windmill rotation recoil suppression vortex wing, a horizontal control auxiliary wing and a rudder attached to an aircraft capable of going straight and turning.
An outer ring 1 for receiving wind from the inside to float a flying object and an engine 8 at the center are mounted on an upper portion of a housing 10, and an outer ring is mounted on a drive shaft 7 that protrudes above the engine. The basic structure is equipped with a centrifugal fan 5 that blows wind toward the wings and an engine cooling fan 6 that cools the engine. A fuel tank 9 is provided inside the casing at the bottom of the engine. The body of the main body has several swirl rotation-inhibiting blades 2 and a number of rudders 3 that change the direction of the main body, and a number of rudder 3 that change the direction of the main body. It consists of several flaps 4 that change the inclination and determine the direction of travel.
[Selection] Figure 1
Description
本考案は外周円輪翼に内側から風を吹き付けることで外周円輪翼に揚力を生じさせ、その風力により垂直に上昇、高度維持、降下ができる飛行体であって、更に外周円輪翼に風車の回転反動抑止渦翼、水平制御補助翼および方向舵の付属装備により直進、旋回航行が可能な飛行体に関するものである。 The present invention is a flying object that can lift the outer ring wing by blowing wind from the inside to the outer ring wing, and can ascend, maintain altitude and descend vertically by the wind force. The present invention relates to a flying object capable of going straight and turning with the attached equipment of wind turbine rotation reaction restraint vortex wing, horizontal control auxiliary wing and rudder.
従来この種の機能をもつ飛行体はヘリコプターやドローそしてオスプレイなどがあるがプロペラを用いない飛行体はない。 Conventionally, there are helicopters, draws, and ospreys for aircrafts with this type of function, but there are no aircraft that do not use propellers.
従来の技術では上昇、下降するためにはプロペラの回転に依存していた。このことにより飛行体の全重量はプロペラを支える軸受けに架かり、これが軸受けの高負荷負担となり、その寿命かかわる問題となる。本案によれば、送風扇はあるもののプロペラではないことから送風羽扇の軸受けには飛行体の全重量は架からず、送風扇自身の自重のみで飛行体の全重量は外周輪翼が負担するので、軸受け高負荷負担による」軸受寿命の問題を全く排除したことにある。 In the prior art, the ascent and descent depended on the rotation of the propeller. As a result, the entire weight of the flying object is placed on the bearing that supports the propeller, which becomes a heavy load on the bearing and becomes a problem related to its life. According to the present plan, although there is a blower fan, it is not a propeller, so the entire weight of the flying object is not mounted on the bearing of the blower fan fan, and the entire weight of the flying object is borne by the outer ring blade only by its own weight. Therefore, the problem of bearing life due to bearing high load is completely eliminated.
一般に飛行機は前方に走行することにより向い風を翼に受け揚力を得るが、本案は飛行体の外周にドーナツ状の外周輪翼を設け、おの内側同心に装備する遠心送風扇より放射状に外周輪翼に向け吹き付けられる風により飛行機に翼に向い風を受けたのと同様の揚力を生じさせ飛行体を走行する必要もなく浮上させんとするものである。 In general, an airplane travels forward to receive wings from the wings to obtain lift, but in this proposal, a donut-shaped outer ring blade is provided on the outer periphery of the flying body, and the outer ring is radiated radially from a centrifugal fan installed concentrically on the inside. The wind blown toward the wing produces the same lift as an airplane receiving the wind toward the wing, so that the aircraft does not need to travel and rises.
本案では送風扇の回転反動による飛行体の自転、すなわち反対向きのつれ回りを抑止するため外周輪翼上面に幾つかの渦状の自転抑止翼を備えるが、自転を静止させる微調と向きの設定にはさらに外周輪翼の下面にある方向舵で行う。 In this proposal, to prevent the rotation of the flying body due to the rotation and reaction of the blower fan, that is, the rotation of the opposite direction, the upper surface of the outer ring blade is provided with several spiral rotation suppression blades. Is further done with a rudder on the underside of the outer ring blade.
飛行体の進路は飛行中、基本的には飛行体の水平に対する傾きによって決定され、その低い方向に進行する。傾きの調整は外周輪翼の外周辺部に設けられた幾つかのフラップを選択し上下に傾けることにより所望の方向の揚力変えて行う。 The flight path of the flying object is basically determined by the inclination of the flying object with respect to the horizontal during the flight, and travels in the lower direction. The inclination is adjusted by changing the lift in a desired direction by selecting several flaps provided on the outer peripheral part of the outer peripheral blade and tilting up and down.
飛行体は先述の様な機能を有することから、その場で浮上、上下動、ホバリング、そして向き変えはもとより向きを変えずに四方八方に自在に飛行することも可能である。普通ヘリコプターは横向きに飛行することはできないが本案は可能である。 Since the flying object has the functions described above, it is possible to fly freely in all directions without changing the direction as well as rising, moving up and down, hovering, and changing the direction. Ordinary helicopters cannot fly sideways, but this is possible.
本飛行体の筐体に操縦席を設ければ1人から数人を登場させたり荷物を載せたりして自家用移動手段、遊覧観光、小荷物移送、偵察、撮影などに供する。小型化して電動モータ駆動して無線操縦やコンピュータ操縦、衛星ＧＰＳナビとの併用により所定の場所にピンポイントで指定位置に到達でき用を果たせる。 If a cockpit is provided in the body of this aircraft, one to several people will appear or luggage will be used for private transportation, sightseeing tours, parcel transport, reconnaissance, photography, etc. It can be miniaturized and driven by an electric motor so that it can reach a specified position at a predetermined point by using radio control, computer control, and satellite GPS navigation.
観光、気象観測、自家用移動手段、偵察、撮影、荷物運搬、災害救助、高所ロープ張り、追跡など用途多数。 Many applications such as sightseeing, weather observation, personal transportation, reconnaissance, filming, luggage transport, disaster rescue, altitude rope tension, and tracking.
観光、気象観測、自家用移動手段、偵察、撮影、荷物運搬、災害救助、高所ロープ張り、追跡など用途多数。 Many applications such as sightseeing, weather observation, personal transportation, reconnaissance, filming, luggage transport, disaster rescue, altitude rope tension, and tracking.
1：外周輪翼、2：自転抑止翼、3：方向陀、4：フラップ、5：遠心送風扇、6：エンジン冷却ファン、7：駆動軸、8：エンジン、9：燃料タンク、10：筐体 1: outer ring blade, 2: rotation suppression blade, 3: directional rod, 4: flap, 5: centrifugal fan, 6: engine cooling fan, 7: drive shaft, 8: engine, 9: fuel tank, 10: housing body
本考案は外周輪翼に内側から風を吹き付けることで外周輪翼に揚力を生じさせ、その風力により垂直に上昇、高度維持、降下ができる飛行体であって、更に外周輪翼に風車の回転反動抑止渦翼、水平制御補助翼および方向舵の付属装備により直進、旋回航行が可能な飛行体に関するものである。 The present invention is a flying body that generates lift by blowing wind from the inside to the outer ring blades, and can vertically ascend, maintain altitude and descend by the wind force, and further rotate the wind turbine on the outer ring blades The present invention relates to an aircraft capable of going straight and turning with the attached equipment of recoil suppression vortex wing, horizontal control auxiliary wing and rudder.
従来この種の機能をもつ飛行体はヘリコプターやドローンそしてオスプレイなどがあるがプロペラを用いない飛行体はない。 Conventionally, there are helicopters, drones, and ospreys for aircrafts with this type of function, but there are no aircraft that do not use propellers.
従来の技術では上昇、下降するためにはプロペラの回転に依存していた。このことにより飛行体の全重量はプロペラを支える軸受けに架かり、これが軸受けの高負荷負担となり、その寿命かかわる問題となる。本案によれば、送風扇はあるもののプロペラではないことから送風扇の軸受けには飛行体の全重量は架からず、送風扇自身の自重のみで飛行体の全重量は外周輪翼が負担するので、軸受けの高負荷負担による軸受寿命の問題を全く排除したことにある。 In the prior art, the ascent and descent depended on the rotation of the propeller. As a result, the entire weight of the flying object is placed on the bearing that supports the propeller, which becomes a heavy load on the bearing and becomes a problem related to its life. According to the present plan, although there is a blower fan, it is not a propeller, so the entire weight of the flying object is not mounted on the bearing of the blower fan, and the entire weight of the flying object is borne by the outer ring wing only by its own weight. Therefore, the problem of the bearing life due to the high load of the bearing is completely eliminated.
一般に飛行機は前方に走行することにより向い風を翼に受け揚力を得るが、本案は飛行体の外周にドーナツ状の外周輪翼を設け、その内側同心に装備する遠心送風扇より放射状に外周輪翼に向け吹き付けられる風により飛行機の翼に向い風を受けたのと同様の揚力を生じさせ飛行体を走行する必要もなく浮上させんとするものである。 In general, an airplane travels forward to receive a wind from a wing and obtains lift.However, in this plan, a donut-shaped outer ring blade is provided on the outer periphery of the flying body, and the outer peripheral ring blade is radially radiated from a centrifugal fan installed concentrically on the inner side. The wind blown toward the aircraft produces lift similar to that received by the wind on the wings of the airplane, and is intended to surface without the need to travel the aircraft.
本案では送風扇の回転反動による飛行体の自転すなわち反対向きのつれ回り抑止するため外周輪翼上面に幾つか、渦状の自転抑止翼を備えるが微細な抑止調整と向き制御は外周輪翼の下面にある方向陀で行う。In this proposal, some of the upper surface of the outer ring blades are provided to prevent rotation of the flying body due to the rotational reaction of the blower fan, that is, rotating in the opposite direction. Follow direction 陀.
1：外周輪翼、2：自転抑止翼、3：方向舵、4：フラップ、5：遠心送風扇、6：エンジン冷却ファン、7：駆動軸、8：エンジン、9：燃料タンク、10：筐体1: outer ring blade, 2: rotation suppression blade, 3: rudder, 4: flap, 5: centrifugal fan, 6: engine cooling fan, 7: drive shaft, 8: engine, 9: fuel tank, 10: housing
Claims (1)
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JP3200141U true JP3200141U (en) | 2015-10-08 |
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