JP2019163017A - Flying object flying by electrically-driven air turbo fan engines - Google Patents
Flying object flying by electrically-driven air turbo fan engines Download PDFInfo
- Publication number
- JP2019163017A JP2019163017A JP2018074214A JP2018074214A JP2019163017A JP 2019163017 A JP2019163017 A JP 2019163017A JP 2018074214 A JP2018074214 A JP 2018074214A JP 2018074214 A JP2018074214 A JP 2018074214A JP 2019163017 A JP2019163017 A JP 2019163017A
- Authority
- JP
- Japan
- Prior art keywords
- flying object
- flight
- flying
- engine
- driven
- 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 claims abstract description 19
- 230000005611 electricity Effects 0.000 claims abstract description 10
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 19
- 239000001257 hydrogen Substances 0.000 claims description 18
- 229910052739 hydrogen Inorganic materials 0.000 claims description 18
- 239000001301 oxygen Substances 0.000 claims description 7
- 229910052760 oxygen Inorganic materials 0.000 claims description 7
- 239000007789 gas Substances 0.000 claims description 6
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 5
- 238000010248 power generation Methods 0.000 claims 1
- 239000007788 liquid Substances 0.000 description 8
- 239000011347 resin Substances 0.000 description 6
- 229920005989 resin Polymers 0.000 description 6
- 239000013065 commercial product Substances 0.000 description 4
- 239000003638 chemical reducing agent Substances 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 239000003365 glass fiber Substances 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 229910001220 stainless steel Inorganic materials 0.000 description 3
- 239000010935 stainless steel Substances 0.000 description 3
- 229920000049 Carbon (fiber) Polymers 0.000 description 2
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 2
- 229920006311 Urethane elastomer Polymers 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- 239000004917 carbon fiber Substances 0.000 description 2
- 150000002431 hydrogen Chemical class 0.000 description 2
- 229910052744 lithium Inorganic materials 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 229920000642 polymer Polymers 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 239000006200 vaporizer Substances 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 229910000737 Duralumin Inorganic materials 0.000 description 1
- 230000001174 ascending effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000000567 combustion gas Substances 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 238000003487 electrochemical reaction Methods 0.000 description 1
- 230000010006 flight Effects 0.000 description 1
- 239000002737 fuel gas Substances 0.000 description 1
- 239000002828 fuel tank Substances 0.000 description 1
- 239000011810 insulating material Substances 0.000 description 1
- 239000012212 insulator Substances 0.000 description 1
- 238000010792 warming Methods 0.000 description 1
Images
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/40—Application of hydrogen technology to transportation, e.g. using fuel cells
Landscapes
- Fuel Cell (AREA)
Abstract
Description
ヘリコプターに変わる飛行物体で垂直離着陸も可能で手軽に飛行が出来る。エネルギー源として水素と空気中の酸素を使用して燃料電池を使用し発電し動力として電動モーターでファンを高速で回し、従来のガスタービン不要となる。格段にエンジンが軽量になり、高価なガスタービンもなく信頼が強い電動モーターが原動力で飛行が可能になり、ファンを多段にすることで大きな風圧が出て飛行可能になる。また電気稼動なので火力を必要しないので有害の排気ガスも出ない次期世代の新しい乗り物を提供するものである。 A flying object that changes to a helicopter allows vertical take-off and landing, making it easy to fly. Electricity is generated by using a fuel cell using hydrogen and oxygen in the air as an energy source, and a fan is rotated at high speed with an electric motor as power, eliminating the need for a conventional gas turbine. The engine becomes much lighter, and there is no expensive gas turbine, and a highly reliable electric motor can fly with motive power. By using multiple fans, it is possible to fly with a large wind pressure. In addition, since it does not require thermal power because it is electrically operated, it will provide a new generation vehicle that does not generate harmful exhaust gas.
当発明は水素の燃料電池の電力で稼動する、近年水素自動車も市販され、水素での発電の大きさと発電量には問題はない。騒音が騒がしいヘリコプターの回転翼が一基では危険すぎるし高価すぎる。当発明は汎用品の電動モーターで駆動させ数基のエンジンで飛行させるので安全性が高まり操縦性も簡単にすることが可能で空気をたたく音も少なくなり次期のヘリコプターに変わる飛行物体が出来る。充電が十分であれば電気だけの短距離の飛行も可能であるが水素を高圧ガスや液体水素にすると長距離の飛行も可能になる。 In the present invention, hydrogen automobiles that are operated with the power of a hydrogen fuel cell are also commercially available in recent years. Noisy helicopter rotor blades are too dangerous and expensive. Since the present invention is driven by a general-purpose electric motor and is operated by several engines, the safety can be improved and the maneuverability can be simplified. If charging is sufficient, it is possible to fly over short distances using only electricity, but if hydrogen is used as high-pressure gas or liquid hydrogen, long-distance flights are also possible.
一般のヘリコブターのメインローターはファンジェットエンジンで駆動して大きな減速機で低速にして回転力を大きくしてローターを回転させている。重量も重く、燃料費も掛かっている。手軽に操縦が出来、安く製造が可能で軽く、もっと安全で操縦が簡単な飛行物体にする。場所を選べることなく離着出来て自動車ように簡単に操縦でき一般の人も手に入る飛行物体にする。 The main rotor of a general helicopter is driven by a fan jet engine and is rotated at a low speed by a large speed reducer to increase the rotational force. Heavy weight and fuel costs. A flying object that can be easily maneuvered, cheaply manufactured, light, safer and easier to maneuver. It is a flying object that can be taken off and on without choosing a place and can be easily operated like a car, and can be obtained by ordinary people.
水素によって燃料電池で発電することにより高い電力も可能であり長時間飛行にも可能になる。水素は元素が一番軽いので燃料の重さが軽い。減速の為の変速機も不要になりヘリコプターのように頭上にあるローターもないので静かになり、電動で今発明のターボファンエンジン(1)回して空気力で飛び何処でも離着陸が可能になる。図1のようにターボファンエンジンが4基或いは数基にすることで機体は更に安定を増し機体を少し前に倒して直進に進むことが出来るそしてエンジンの製作費がガスタービンを使用しないので非常に安くなり、燃料電池の使用し燃焼ガスの熱が出ないので地球温暖化にもよい。 By generating electricity with a fuel cell using hydrogen, high electric power is possible, and flight is possible for a long time. Hydrogen is the lightest element, so the weight of the fuel is light. The transmission for deceleration is not necessary, and there is no overhead rotor like a helicopter, so it becomes quiet, and the turbofan engine (1) of the present invention can be electrically driven to fly by aerodynamic force and take off and landing anywhere. As shown in Fig. 1, the number of turbofan engines can be increased to 4 or several so that the aircraft can be more stable, move forward and move straight ahead, and the production cost of the engine does not use a gas turbine. It is also cheaper and good for global warming because the fuel gas is used and the combustion gas does not generate heat.
電気的に飛行することにより構造が簡単で製造コストが安く提供が出来る。電気でターボファンを回転させるので新しいジェットエンジンになることによって電気的に出力のコントロールが簡単になり、また機体が軽く安価になる。この飛行物体は飛行機と違い滑走路が不要と道路がない所へも行けるので離島や山岳の人命救助に発揮出来る。機体が建物近くまで行けるのでビル火災には特に発揮出来る。新しい乗り物になり災害時にも活躍が期待出来る。 By flying electrically, the structure is simple and the manufacturing cost is low. Since the turbofan is rotated by electricity, it becomes easier to control the output electrically by using a new jet engine, and the aircraft is lighter and cheaper. Unlike a plane, this flying object can be used to save lives on isolated islands and mountains because it can be used where there is no runway and no road. Since the aircraft can go close to the building, it can be especially effective for building fires. It becomes a new vehicle and can be expected to play an active part in the event of a disaster.
図1飛行物体の透視図 座席は5席の場合でエアーのターボファンエンジン(1)上向きで4基によって飛行物体を浮上させ飛行する。燃料は球型高圧二重タンク(2)で高圧の水素ガスか液体を燃料として2基格納している。酸素は空気の中から使用する、水素と酸素の燃料電池(3)の固体高分子形の燃料電池の市販用を使用して飛行物体の電気エネルギーとして発電して使用する。
操縦席(9)で専属のパイロットが操縦する。ボディ(10)はガラス繊維樹脂かアルミ製で軽くする。機体のシャーシ(11)でジュラルミンなどの軽量の骨材である。Fig. 1 Perspective view of flying object When the number of seats is five, the flying object is levitated by four units with the turbofan engine (1) of the air facing upward. The fuel is stored in two spherical high-pressure double tanks (2) using high-pressure hydrogen gas or liquid as fuel. Oxygen is generated from the air and is used as electric energy of a flying object using a commercially available solid polymer fuel cell of hydrogen and oxygen fuel cell (3).
A dedicated pilot controls the cockpit (9). The body (10) is lightly made of glass fiber resin or aluminum. It is a lightweight aggregate such as duralumin in the chassis (11) of the fuselage.
図2 飛行物体で平面 立面そして側面方向から見た図面
シャーシ(11)の上にボディ(10)を乗せた形でアウトリガー(12)によって駐機時に機体を守る。燃料の水素用高圧二重タンク(2)は後部に2基乗せる。Fig. 2 Plane with flying object The aircraft is protected by the outrigger (12) while the body (10) is placed on the chassis (11) as seen from the elevation and side view. Two high-pressure double tanks (2) for hydrogen of fuel are mounted at the rear.
図3 飛行物体の系統図 水素は高圧に圧縮され球型の高圧二重タンク(2)から減圧弁(26)で減圧されてコントロール弁(27)で制御され水素酸素燃料電池(3)に入り電気化学反応によって発電する。空気用ブロア(28)で空気を加圧されコントール弁(27)定圧にされ空気中の酸素と水素の化合により電気が作られて燃料電池のセルの増減で電力を決める。リチウム電池(4)で電気を一時蓄電する。パワーユニット(5)で電圧上げる。200Vにモーターの入力にするために三相変換機(6)で交流に変換して三相交流にするコンロール制御盤(7)のコンピューターによって適切な飛行制御をする。操縦カン(8)で機体のコントロールをするレバー。球形高圧二重タンク(2)で水素ガスおよび液体を高圧で補充するので安全弁(29)は必要になる。燃料に液体水素を使用して長時間飛行する場合、気化器(33)よって電熱等で液体を気化させて使用する。 Fig. 3 System diagram of the flying object Hydrogen is compressed to high pressure, depressurized from the spherical high pressure double tank (2) by the pressure reducing valve (26), controlled by the control valve (27), and enters the hydrogen-oxygen fuel cell (3) Power is generated by electrochemical reaction. Air is pressurized by the air blower (28) to a constant pressure of the control valve (27), electricity is generated by the combination of oxygen and hydrogen in the air, and the electric power is determined by increasing or decreasing the number of cells of the fuel cell. The lithium battery (4) temporarily stores electricity. Increase the voltage with the power unit (5). Appropriate flight control is carried out by a computer of a control panel (7) which converts it into an alternating current by a three-phase converter (6) and converts it into a three-phase alternating current in order to make the motor input 200V. A lever that controls the aircraft with the control can (8). Since hydrogen gas and liquid are replenished at high pressure in the spherical high-pressure double tank (2), the safety valve (29) is necessary. When flying for a long time using liquid hydrogen as a fuel, the liquid is vaporized by an electric heat or the like by a vaporizer (33).
図4 電動のターボファンエンジン(1)の姿図と半分断面で内部の構造を示す。駆動は電動モーター(15)でファンを高速回転させる。ファン(17)は2段あり空気を送り込む圧力をさらに上げるためにファン(18)でもう一度あげて3段式で空気まわして圧力を上げる。エンジンの出口付近では面積を小さくして流速を上げる構造。モーターカバー(16)で電動モーター(15)を雨と埃から守る
ブレード(19)で鳥や異物からエンジン本体を守るためにあり。ボールベアリング(20)で高速軸受けであり無給か若しくは給油式になる。Fig. 4 The figure of the electric turbofan engine (1) and the internal structure in half section. The electric motor (15) drives the fan at high speed. The fan (17) has two stages. In order to further increase the pressure for sending air, the fan (18) is raised again by the fan (18) and the air is turned in a three-stage system to increase the pressure. A structure that reduces the area and increases the flow velocity near the exit of the engine. There is a blade (19) for protecting the electric motor (15) from rain and dust with the motor cover (16) to protect the engine body from birds and foreign objects. The ball bearing (20) is a high-speed bearing and can be unpaid or lubricated.
図5 電動のターボファンエンジン(1)の傾けた時の側面
構造上機体を前進や曲がるときに飛行するのは、機体を斜め前に傾ける必要があるので機体の傾ける角度を少なくする為の装置あり、上昇や下降はエンジンを垂直にする。Fig. 5 Side view when the electric turbofan engine (1) is tilted When flying forward or turning the aircraft, it is necessary to tilt the aircraft forward. Yes, ascending and descending makes the engine vertical.
図6 エアーのターボファンエンジン(1)とシャーシ(11)の周りの取り付け図減速機(13)と減速用モーター(14)がエンジンを傾ける装置の詳細Figure 6 Air turbofan engine (1) and installation diagram around the chassis (11) Details of the device where the reduction gear (13) and the reduction motor (14) tilt the engine
図7 水素の高圧二重タンク(2)の構造図 燃料を長距離飛行ために液体水素にするために二重構造にして、球形で一番内部を鏡面のステンレスタンク(32)でその外側は真空にして断熱する。ウレタンゴム緩衝材(31)でタンクとタンクが当たるため保護する。球形のステンレス製タンク(21)があり炭素繊維樹脂(22)で包み加工する。その外側にはガラス繊維樹脂(23)で外部衝撃のため更に補強する。球を包むように断熱材(24)で断熱する。外側と内側にも二重のタンクを備えた液体水素用タンクで真空地帯(30)がある。Fig. 7 Structure of the hydrogen high-pressure double tank (2) Double structure is used to make the fuel liquid hydrogen for long-distance flight. Insulate with vacuum. The urethane rubber cushioning material (31) protects the tank because it hits the tank. There is a spherical stainless steel tank (21) which is wrapped with carbon fiber resin (22). The outside is further reinforced with glass fiber resin (23) for external impact. Insulate with a heat insulator (24) so as to wrap the sphere. There is a vacuum zone (30) in the liquid hydrogen tank with double tanks on the outside and inside.
図8 水素の球形高圧二重タンク(2)を取り付けた拡大図面
機体にタンクを2基取り付けた時の拡大図面、機体が傾いて前に進むので機体にタンク取り付け座(25)によってボルト類で確実に固定する。Fig. 8 Enlarged drawing with the hydrogen spherical high-pressure double tank (2) attached. Enlarged drawing when the two tanks are attached. Securely fix.
図9 平面図 エンジンを多く取り付けた機種で多くの物資と人が乗せる。
図10 平面図 機体を浮かせて海難救助出来るフロート(34)取り付けた機体で軽量化した個人や海上救助用の機種。Fig. 9 Plan view This model is equipped with many engines and can carry many supplies and people.
Fig. 10 Plan view Personal and maritime rescue models that have been reduced in weight by the airframe attached with a float (34) that can rescue the sea by floating the aircraft.
新しい航空機の産業、操縦士の育成など新しい産業が出来る。
警察、消防、病院、救助隊など現在ヘリコブター使用しているとろは変えることが出来る。滑走路がない離島や山奥にも物資や人も行ける。空のタクシーとして利用でき、低価格も可能になり人命救助も活躍出来る。農業や漁業の観察調査も出来て物事を3次元で見ることが出来るので観光にも利用出来る。New industries such as new aircraft industry and pilot training.
Police, fire departments, hospitals, rescue teams, and other current helicopters can be changed. Goods and people can also go to remote islands and mountains that have no runway. It can be used as an empty taxi, and it can be used at low prices and can save lives. It can also be used for sightseeing because it can be used for observation in agriculture and fisheries to see things in three dimensions.
1 電動のターボファンエンジン
2 球形高圧二重タンク(市販品加工)
3 水素酸素燃料電池(固体高分子形)(市販品加工)
4 リチウム電池(市販品)
5 パワーユニット(市販品加工)
6 三相変換機(市販品加工)
7 コントロール制御盤
8 操縦カン
9 操縦席
10 ボデイー
11 シャーシ
12 アウトリガー
13 減速機(市販品)
14 減速機用モーター(市販品)
15 電動モーター(市販品)
16 モーターカバー
17 (強力樹脂)ファン
18 (アルミ)ファン
19 ブレード
20 ボールベアリング(市販品)
21 ステンレス製球形タンク
22 炭素繊維樹脂
23 ガラス繊維樹脂
24 断熱材
25 タンク取り付け座
26 減圧弁(市販品)
27 自動弁(市販品)
28 ブロア(市販品)
29 安全弁(市販品)
30 真空地帯
31 ウレタンゴム緩衝材
32 内側ステンレスタンク(球面仕上げ)
33 気化器
34 フロート1
3 Hydrogen-oxygen fuel cell (solid polymer type) (commercial product processing)
4 Lithium battery (commercially available)
5 Power unit (commercial product processing)
6 Three-phase conversion machine (commercial product processing)
7
14 Reducer motor (commercially available)
15 Electric motor (commercially available)
16 Motor cover 17 (Strong resin) Fan 18 (Aluminum)
21 Stainless steel spherical tank 22 Carbon fiber resin 23 Glass fiber resin 24
27 Automatic valve (commercially available)
28 Blower (commercially available)
29 Safety valve (commercially available)
30 Vacuum zone 31 Urethane rubber cushioning material 32 Inside stainless steel tank (spherical finish)
33
Claims (4)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2018074214A JP2019163017A (en) | 2018-03-20 | 2018-03-20 | Flying object flying by electrically-driven air turbo fan engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2018074214A JP2019163017A (en) | 2018-03-20 | 2018-03-20 | Flying object flying by electrically-driven air turbo fan engines |
Publications (1)
Publication Number | Publication Date |
---|---|
JP2019163017A true JP2019163017A (en) | 2019-09-26 |
Family
ID=68064535
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2018074214A Pending JP2019163017A (en) | 2018-03-20 | 2018-03-20 | Flying object flying by electrically-driven air turbo fan engines |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2019163017A (en) |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2003512215A (en) * | 1998-12-11 | 2003-04-02 | モラー・インターナショナル・インコーポレーテッド | Stability controller for robot controlled or remote controlled flight platforms |
JP2003170898A (en) * | 2001-12-07 | 2003-06-17 | Shin Kagaku Kaihatsu Kenkyusho:Kk | Air vehicle |
JP2006021733A (en) * | 2004-07-07 | 2006-01-26 | Kaido Ikeda | Vertical taking-off and landing machine installing rapid wind quantity generation wind direction changing device of double inversion two-axis tilt as device for lift and propulsion of machine body and using it as steering means |
JP2010132280A (en) * | 2008-12-08 | 2010-06-17 | Honeywell Internatl Inc | Vertical take off and landing unmanned aerial vehicle airframe structure |
JP2012132558A (en) * | 2010-12-18 | 2012-07-12 | Boeing Co:The | Continuous flow thermodynamic pump |
JP2017114186A (en) * | 2015-12-22 | 2017-06-29 | 株式会社プロドローン | Multi-copter |
-
2018
- 2018-03-20 JP JP2018074214A patent/JP2019163017A/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2003512215A (en) * | 1998-12-11 | 2003-04-02 | モラー・インターナショナル・インコーポレーテッド | Stability controller for robot controlled or remote controlled flight platforms |
JP2003170898A (en) * | 2001-12-07 | 2003-06-17 | Shin Kagaku Kaihatsu Kenkyusho:Kk | Air vehicle |
JP2006021733A (en) * | 2004-07-07 | 2006-01-26 | Kaido Ikeda | Vertical taking-off and landing machine installing rapid wind quantity generation wind direction changing device of double inversion two-axis tilt as device for lift and propulsion of machine body and using it as steering means |
JP2010132280A (en) * | 2008-12-08 | 2010-06-17 | Honeywell Internatl Inc | Vertical take off and landing unmanned aerial vehicle airframe structure |
JP2012132558A (en) * | 2010-12-18 | 2012-07-12 | Boeing Co:The | Continuous flow thermodynamic pump |
JP2017114186A (en) * | 2015-12-22 | 2017-06-29 | 株式会社プロドローン | Multi-copter |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US11912404B2 (en) | Vertical takeoff and landing aircraft | |
US9440736B2 (en) | Special personal electric helicopter device with integral wind turbine recharging capability | |
WO2019211875A1 (en) | Hybrid vertical takeoff and landing (vtol) aircraft with vehicle assist | |
US9096314B2 (en) | Electric VTOL aircraft | |
US6969027B2 (en) | Vertical takeoff and landing apparatus | |
JP6426165B2 (en) | Hybrid VTOL machine | |
US20190375495A1 (en) | Electrical vertical take-off and landing aircraft | |
US20180141652A1 (en) | Convertible airplane with exposable rotors | |
US20140103158A1 (en) | AirShip Endurance VTOL UAV and Solar Turbine Clean Tech Propulsion | |
US20200023970A1 (en) | Electric JetPack Device | |
WO2006006311A1 (en) | Rapid air quantity generating and wind direction changing device and aircraft having the device mounted on side face of airframe | |
JPH05501095A (en) | turbo craft | |
US20220355922A1 (en) | Vertical take-off and landing cocoon-type flying vehicle | |
US20230202652A1 (en) | Drone | |
US20020130220A1 (en) | Airships having simplied construction and improved maneuverability | |
US20180037319A1 (en) | Vertical take-off and landing aircraft (variants) | |
EP3746364A1 (en) | Vtol aircraft | |
CN104139858A (en) | Disc type aircraft | |
JP2020535051A (en) | Rotorcraft with propulsion on a rotating pole | |
JP2019163017A (en) | Flying object flying by electrically-driven air turbo fan engines | |
RU201900U1 (en) | Electric airship | |
US7997059B1 (en) | Propulsion system | |
RU2410284C1 (en) | Method of flight and aircraft to this end | |
US20200346630A1 (en) | Compact wind tunnel for flight and hover capabilities | |
CN220562969U (en) | Unmanned aerial vehicle of fire control that takes off and land perpendicularly of no oar formula |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
A977 | Report on retrieval |
Free format text: JAPANESE INTERMEDIATE CODE: A971007 Effective date: 20200923 |
|
A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20201006 |
|
A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20201124 |
|
A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20210518 |
|
A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20210713 |
|
A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20211116 |
|
A02 | Decision of refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A02 Effective date: 20220517 |