| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 61 | Transforming unmanned aerial / land vehicle | JP2010020310 | 2010-02-01 | JP5550930B2 | 2014-07-16 | エムレイ・アール・グーセン; ランドール・イー・ホーン |
| 62 | Freely wing of the hinge and truss retraction of the vehicle to fly | JP2013523150 | 2011-08-02 | JP2014503400A | 2014-02-13 | バウスフィールド、サミュエル、ホール; ロバーツ、ロバート、エヌ．; ブラウン、マシュー、エー．; アネマート、ウィレム、エー．ジェー． |
| 【解決手段】 飛行する乗り物用のトラスは一対の翼を支持し、これは展開形態と引き込み形態における前記翼の枢動を容易にする態様で行われる。 前記トラスは平行な上部および底部プレートを含み、その間には間隙がある。 前記翼にはウイングブラケットが固定され、当該ウイングブラケットは、ヒンジアセンブリにより前記トラスの前記上部プレートおよび底部プレートに枢動自在に支持される。 ラッチアセンブリを選択的に作動させて、前記ウイングブラケットと当該ブラケットに連結された翼を、前記展開形態または前記引き込み形態において、前記トラスに固定することにより、前記翼と前記トラスとの間の荷重が、前記ヒンジアセンブリを通じてではなく、主に前記ラッチアセンブリを通じて伝達されるようにすることが可能である。 前記トラス上および前記ウイングブラケット上のヒンジ位置は、翼端部から翼端部までの長さを最大限に伸ばすとともに、前記翼が完全に引き込まれたとき前記乗り物に必要な外形を最小限に抑えるように選択される。
【選択図】 図 |
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| 63 | Automobile | JP2012121017 | 2012-05-28 | JP2013244898A | 2013-12-09 | KOBAYASHI YOSHIYUKI |
| PROBLEM TO BE SOLVED: To provide an automobile including main wings which can be expanded to an expanded state for producing lift necessary for flying and can be contracted to a contracted state permitting retraction with respect to a side door.SOLUTION: An automobile 1 includes: a plurality of wheels 3a, 3b rotated by motive power output from a travel motive power source 24; a pair of right and left main wings 5 for producing lift necessary for flying, and a pair of right and left horizontal stabilizers 6; and a propulsion force generating unit 31 for producing propulsion force necessary for flying. The main wings 5 and the horizontal stabilizers 6 are configured to be freely expanded/contracted to a contracted state permitting retraction with respect to a wing retraction chamber 43 of side doors 4 mounted on both side parts of a vehicle body 2, or to an expanded state providing lift necessary for flying the automobile 1. | ||||||
| 64 | 空飛ぶ自動車 | JP2009545747 | 2008-12-02 | JPWO2010064326A1 | 2012-05-10 | 剛明 金森 |
| 本発明は、走行および飛行が可能な自動車に関する。従来の飛行機能を有する自動車は、自動車の幅や自動車の高さが大きく、道路での離着陸は困難であった。本発明は、飛行に必要な揚力を発生する配置した翼の集まりを用いて、自動車の幅や自動車の高さを小さくし、道路より離陸し、道路へ着陸することを可能にした。配置した翼の集まり158は、本体150に取り付けられており、翼の幅方向を、自動車の左右方向とし、自動車の上下方向と、自動車の前後方向とよりなる面内に翼を配置し、各翼がほぼ同じ揚力を発生する迎え角になるように、各翼の取付角を制御する翼の集まりである。本体150は、左操舵輪152a、左駆動輪153aを有し、これらの車輪を利用して走行する。推進部156はプロペラであり、飛行に必要な推力を発生する。昇降舵124、補助翼126および方向舵128は飛行時に姿勢制御する。 | ||||||
| 65 | Aircraft system capable of taxiing | JP2011532024 | 2009-10-19 | JP2012505792A | 2012-03-08 | ジョン，スチョル |
| Disclosed is a flying object system performing ground traveling, which travels on the ground and flies in the air. The flying object system travels with three or more wheels connected to a main body, generates flying force through wings symmetrically installed at both sides of the main body, and is provided with plural propellers, operated by a control lever and installed on the wings and at least a part of the main body, each of the wings being divided into a plurality of compartments to be folded or be changed in shape by pressure of gas or air. Therefore, the flying object system travels on a road on the ground and takes off and flies in the air in traffic congestion, and flies in the air and lands and travels on a road on the ground if necessary, thus rapidly moving to a destination without the effects of traffic congestion. | ||||||
| 66 | Multiple environmental agencies | JP2008516376 | 2006-06-14 | JP2008543647A | 2008-12-04 | アペロイグ，ジュリエン; グリツェル，トーマス; ティアルクス，セバスチャオ; ドゥミトル，アレクサンドリュ; プロポネット，ジーン−ギュイライン |
| 少なくとも１枚の翼が飛行用平衡維持第１態勢、水面移動飛行維持第２態勢と水没第３態勢間で折り曲げ可能である胴体２、翼４，５ならびに推進装置８が含まれる多重環境機関１
【選択図】図１ |
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| 67 | Improved vertical take-off and landing aircraft | JP2006532279 | 2004-02-02 | JP2006528583A | 2006-12-21 | モラー，ポール・エス |
| ２組の折曲げ可能な翼、その翼に取り付けられた２組の傾斜可能なナセル、垂直安定板、水平安定板、２組の補助推力装置をもつ胴体を含むＶＴＯＬ機である。 各ナセルは、その後部開口に配置されたベーンのシステムを含み、水平から所定の角度の範囲にわたって空気流を偏向させるために、そのベーンを延長し、後退させるためのアクチュエータが、ナセルを傾斜させる機構と共に設けられている。 各ナセルは、２組のエンジンも含み、その各々がファンを直接駆動する。 ファン同士は対向しており、反対の回転方向に同じ回転速度で動作する。 一代替実施形態では、補助推力装置を有する代わりに胴体に追加取り付けされたナセル２組を含む。 コンピュータ化された、冗長性をもつ飛行制御システムが、１つの飛行モードから他のモードに移行するとき機体の安定性を保つ。 | ||||||
| 68 | Flying motor vehicle | JP18717085 | 1985-08-26 | JPS6164505A | 1986-04-02 | DON AARU POORINGU |
| 69 | AERONAUTICAL CAR AND ASSOCIATED FEATURES | EP17744862.8 | 2017-01-26 | EP3408173A1 | 2018-12-05 | GOELET, John |
| An aeronautical car comprises a ground-travel system including at least one traction device, an air-travel system including at least one flight mechanism configured to be selectively moved between a first position when the aeronautical car is in a driving mode and a second position when the aeronautical car is in a flying mode, and a weather manipulation device. The weather manipulation device may be configured to manipulate at least one aspect of a weather condition while the aeronautical car is in the air. | ||||||
| 70 | FOLDING PROPELLER | EP16195552.1 | 2016-10-25 | EP3315400A1 | 2018-05-02 | Klein, Stefan; Macandrew, Doug; Rooms, Simon; Urik, Tomas; Daniel, Milos |
An aircraft, such as a flying car, comprising a body structure, lift structures (such as wings), control structures (such as fins, elevators, and ailerons), and a motor; a propeller connected to the motor and mounted for rotation about a drive axis to provide thrust; the propeller comprising a hub having a plurality of blades connected thereto; and a plurality of blade housings adjacent the propeller and extending substantially parallel to the drive axis; wherein the blades are mounted on the hub so as to be moveable between an expanded position in which the blades project radially from the hub, and a folded position in which each blade extends axially from the hub so as to lie in a respective blade housing.
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| 71 | A DIRECTIONAL CONTROL SYSTEM AND METHOD FOR A HYBRID AIR AND GROUND TRANSPORTATION VEHICLE | EP15801513.1 | 2015-10-08 | EP3204245A2 | 2017-08-16 | KLEIN, Stefan |
| A directional control system for a hybrid transportation vehicle for ground and air transportation. The vehicle has at least one steerable wheel for use in ground operation, the wheel being connected to a steering mechanism, wings having moveable control surfaces, and a tail having a moveable control surface. The system has a first shaft having a first control input at one end, wherein the first shaft is linked to the steering mechanism and a second shaft that extends through the first shaft and is independently rotatable and slidable with respect to the first shaft. The second shaft has a second control input at one end, a first linkage configured to transmit a rotational movement of the second shaft to control the moveable control surfaces on the wings, and a second linkage configured to transmit an axial movement of the second shaft to control the moveable control surface on the tail. | ||||||
| 72 | VEHICLE | EP12794527.7 | 2012-11-09 | EP2776259A1 | 2014-09-17 | STEKELENBURG, Michael Alwin William; KLOK, Christiaan Cornelis; VAN RIJN, Louis Petrus Valentijn Marie; SOETHOUDT, Wouter Adriaan; WEGERIF, Robert Christiaan |
| The present invention discloses a vehicle (1) capable of being converted between a flying condition and an automotive riding condition. The vehicle has a telescopically extendable tail (10) comprising a first tubular tail segment (11) and a second tail segment (12) disposed axially slideable within the first tubular tail segment. The tail is provided with at least two form-closing coupling members (21, 35; 31, 36) located at an axial distance (LI) from each other for providing a force-transferring coupling between the second tail segment (12) and the first tubular tail segment (11) in the extended state of the second tail segment (12), each of said form-closing coupling members (21, 35; 31, 36) capable of transferring torque and transverse forces, and each of said form-closing coupling members (21, 35; 31, 36) coming into engagement by axial displacement of the second tail segment (12) in the outward direction. | ||||||
| 73 | Mit einem einspurigen Straßenfahrzeug koppelbares Fluggerät | EP10014683.6 | 2010-11-17 | EP2327571B1 | 2014-05-28 | Farrag, Rainer |
| 74 | ROTORCRAFT WITH VARIABLE INCIDENT WING | EP09711303 | 2009-02-11 | EP2242684A4 | 2013-10-30 | SMITH DUDLEY E; JOINER WALTER C; ROBERTSON DANIEL B; LUDOLPH DAVID J; LANGSTON JENNIFER D |
| 75 | ROADABLE AIRCRAFT WITH FOLDING WINGS AND INTEGRATED BUMPERS AND LIGHTING | EP07748837.7 | 2007-01-05 | EP1973777A2 | 2008-10-01 | DIETRICH, Carl, Curtis; SCHWEIGHART, Samuel, Adam; MRACEK, Anna, Marie |
| A low-wing, low-span canard aircraft with a protected pusher-style propeller is designed to transition simply between use in the air and use on the ground, without any mechanical effort on the part of the pilot. The vehicle may include deformable aerodynamic bumpers, embedded road-safety vehicle lighting and license plates, a protected propeller, and an integrated RFID airport access system. The vehicle may be designed for potential certification by the Federal Aviation Administration as a Light Sport Aircraft. | ||||||
| 76 | Ultraleicht-Fluggerät mit der Möglichkeit der Fortbewegung in der Luft sowie auf der Strasse | EP03028070.5 | 2003-12-09 | EP1541465A1 | 2005-06-15 | Hegger, Christof |
Gegenstand der Erfindung ist ein Ultraleicht- Fluggerät, das eine Zulassung als Ultraleicht-Fluggerät, sowie eine Straßenzulassung erhält. Beide Zulassungen erfüllen die üblichen nationalen Bestimmungen des Landes, in dem das Ultraleicht-Fluggerät zugelassen wird. Erfindungsgemäß wird eine Ultraleicht-Fluggerät Gondel vorgestellt, die aus einen Rahmen (11), der einen Motor (12) mit einem Getriebe umschließt, vier Rädern und einer Sitzbank für zwei Personen besteht. |
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| 77 | IMPROVED VERTICAL TAKE-OFF AND LANDING VEHICLES | EP03709001.6 | 2003-02-06 | EP1478570A2 | 2004-11-24 | MOLLER, Paul, S. |
| A VTOL vehicle including a fuselage with two foldable wings, two tiltable nacelles attached to the wings, a vertical stabilizer, a horizontal stabilizer, and two auxiliary thrusters. Each nacelle contains a system of vanes located at the rear opening thereof, and actuators are provided for extending and retracting the vanes in conjunction with nacelle tilting mechanisms to deflect the airflow over a predetermined range of angles from the horizontal. Each nacelle also contains two rotary engines, each of which directly drives a fan. The fans face each other and operate in counter-rotating directions at the same rotational speed. An alternative embodiment includes two additional nacelles attached to the fuselage instead of having the auxiliary thrusters. A redundant computerized flight control system maintains stability of the vehicle as it transitions from one flight mode to another. | ||||||
| 78 | Amphibious aircraft | EP02021682.6 | 2002-09-27 | EP1298054A2 | 2003-04-02 | Tanaka, Akio |
A sea-land-sky craft capable of navigating on the water, running on the land and flying in the air (that is, climbing vertically, flying horizontally and hovering in the air) usable in a new transportation system. The sea-land-sky craft comprises counter-rotating rotors (14,15). Rotor shafts (12,13) are disposed at positions eccentric to the centers of the rotors and carry the rotors so that the orientation of the rotating wings can be turned. A cylindrical duct encloses the outer circumferences of the maximum diameters of the rotors rotations. A fuselage is located at a central portion of the craft. Movable struts are provided for connecting the cylindrical duct and the fuselage. In the sea-land-sky craft, the cylindrical duct is deformed into a fixed wing by the actions of the movable struts. |
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| 79 | Aircraft convertible into other aircrafts and into a trailer for motor vehicles | EP97830546.4 | 1997-10-27 | EP0839712A2 | 1998-05-06 | Perrotta, Pasquale Vittorio |
Aircraft with changeable geometry, height, weight (and also changeable carriage wheels' distance) on the ground or during flight, furnished with one or more engines mounted in the same frame and convertible into a trailer for motor vehicles. These characteristics are obtained thanks to: mechanical units mounted on the fuselage that allow fixed movements to some portions of the fuselage; adjustable front carriage's leg (4001), which can change its inclination, its length and its shape; carriage's rear portion (5000) formed by two half wings, whose roots are connected to the fuselage and their longitudinal ends to the wheels; engine casing (6001) of many shapes and sizes where various kinds of engines can be placed; fuselage's plate (6003) on which the engine casing can be placed in different positions; beams (7001 and 7004) that can be introduced in the fuselage to change the aircraft into a trailer for motor vehicles or into other types of aircrafts. |
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| 80 | 五栖运动魔方旅行箱 | CN200820091473.7 | 2008-01-11 | CN201164161Y | 2008-12-17 | 李卫红 |
| 本实用新型涉及一种五栖运动魔方旅行箱，包括皮划艇组件、滑翔机组件、滑行运动组件、野外生存用具。皮划艇组件包括气囊、固定框、连杆、伸缩式框架及气垫座椅；滑翔机组件包括伞翼、拉索及起落架；滑行运动组件包括至少一对滑板以及分别可装设于滑板底面的至少一对滑轮和至少一对冰刀；野外生存用具包括折叠式帐篷、吊挂式睡袋、折叠式桌子及煮锅等；上述各组件在收折时可进一步组合成一箱包结构。本实用新型针对陆、水、雪、冰、空等环境变换分别设计了符合其环境的娱乐运动组件，功能和组合形式变化多样、适应性强，可全面适应陆地、冰上、雪上、水上、空中五种不同的立体空间环境变换，且各组件适当折叠后可组成一个箱包从而便于携带。 | ||||||
