| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | 海空两栖飞行器 | CN201610327106.1 | 2016-05-17 | CN107379908A | 2017-11-24 | 张飞 |
| 一种海空两栖飞行器。机身1为梭形，竖直剖面形状近似为菱形。机身1中部为储水舱24，储水舱前舱壁14，储水舱后舱壁18，和机身中部形成储水舱24，同时机身中部设置有内置弹舱16。储水舱24前部设置有进水口15，后部设置有出水口17，顶部设置有出气口25。电动机11位于机身1尾部，电动机11上安装有螺旋桨12。右机翼2和左机翼3为可变后掠翼，分别位于机身1中部的右边和左边。右鸭翼4和左鸭翼5分别位于机身1前部的右边和左边。右机翼2上安装有右襟翼6和右副翼7。左机翼3上安装有左襟翼8和左副翼9。垂直尾翼10位于机身1的尾部上方。飞行器的起落架为前三点式分布。雷达和声呐13位于机身1的头部。 | ||||||
| 2 | 用于陆地和空中的混合式交通运输工具的转变方法以及该混合式交通运输工具 | CN201280047973.X | 2012-08-22 | CN103917388B | 2016-10-12 | S·克莱恩 |
| 用于陆地和空中的混合式交通运输工具的转变方法，所述方法包括下面的转变和互换步骤：倾转打开调整盖（7）。使两个整体机翼（1）从交通运输工具的纵向位置绕两个竖直轴（2）展开至飞行位置。通过绕水平轴线（3）倾转每个机翼（1）的后部，使机翼（1）的后部从机翼（1）的顶前部展开成张开的飞行位置。使机翼（1）以从0°至40°攻角alpha倾转地起飞和着陆。通过朝机身轴向移动前轮（5）而减小前轮轮距（5）。此外，描述了相应的用于陆地和空中的混合式交通运输工具，其包括用于从标准双辙或四辙汽车转变成用于在陆地或水上起飞和着陆的标准飞行器以及从用于在陆地或水上起飞和着陆的标准飞行器转变成标准双辙或四辙汽车的互换转变机构。 | ||||||
| 3 | 用于陆地和空中的混合式交通运输工具的转变方法以及该混合式交通运输工具 | CN201280047973.X | 2012-08-22 | CN103917388A | 2014-07-09 | S·克莱恩 |
| 用于陆地和空中的混合式交通运输工具的转变方法，所述方法包括下面的转变和互换步骤：倾转打开调整盖（7）。使两个整体机翼（1）从交通运输工具的纵向位置绕两个竖直轴（2）展开至飞行位置。通过绕水平轴线（3）倾转每个机翼（1）的后部，使机翼（1）的后部从机翼（1）的顶前部展开成张开的飞行位置。使机翼（1）以从0°至40°攻角alpha倾转地起飞和着陆。通过朝机身轴向移动前轮（5）而减小前轮轮距（5）。此外，描述了相应的用于陆地和空中的混合式交通运输工具，其包括用于从标准双辙或四辙汽车转变成用于在陆地或水上起飞和着陆的标准飞行器以及从用于在陆地或水上起飞和着陆的标准飞行器转变成标准双辙或四辙汽车的互换转变机构。 | ||||||
| 4 | 多功能汽车 | CN200510088924.2 | 2005-08-03 | CN1736743A | 2006-02-22 | 陈林 |
| 本发明涉及一种多功能汽车，其驾驶服务室包括有厨房和卫生间，车厢设置为工作区生活区或乘客区，并分别用隔板隔开，使用者在行车过程中根据需要休息、娱乐、工作或进行商务活动，多功能汽车装有可伸缩折叠的螺旋桨，使得多功能汽车具有飞行的功能；所述螺旋桨及车轮可收缩到车身内，整个汽车密封呈一体，可以像船一样在水中行驶；在螺旋桨没有伸展开前，多功能汽车保持了普通汽车的基本功能；不安装飞行设施的多功能汽车设置有厨房、卫生间、工作区、生活区或乘客区、可坐可躺可旋转的椅子、可折叠的桌板、电视、音响；多功能汽车的制作材料具有防爆防弹防撞击防火性能，车窗为防弹防辐射真空玻璃，既保暖防热隔音，又防恐安全。 | ||||||
| 5 | 陸上および空中用のハイブリッド運搬用ビークルの変形方法およびハイブリッド運搬用ビークル | JP2014528332 | 2012-08-22 | JP2014527495A | 2014-10-16 | シュテファン クレイン， |
| 陸上および空中用のハイブリッド運搬用ビークルの変形方法は、以下の変形および相互的ステップを含む:補強カバー(7)を傾けること。両方の翼(1)全体を2つの垂直軸(2)の周囲において、運搬用ビークルの長手方向位置から飛行位置まで拡張させること。水平軸(3)の周囲において、各翼(1)の後方を傾けることによって、翼(1)の後方部分を翼(1)の上部前方部分から、広げられた飛行位置まで拡張させること。翼の仰角α=0〜40?だけ翼(1)を離着陸のために傾けること。前輪(5)を胴体に向かって軸方向に移動させることによって、前輪輪距(5)が減少される。さらに、スターリング二輪または四輪自動車から、陸上または水上で離陸および着陸するためのスターリング航空機へ、およびその逆へ変形させるための相互的変形機構を含む、陸上および空中用の対応するハイブリッド運搬用ビークルも、説明される。 | ||||||
| 6 | Recovery and towing vehicle | EP85301104.7 | 1985-02-19 | EP0153187A2 | 1985-08-28 | Watson, Norman Frederick |
A recovery and towing vehicle which has been specifically designed for transport in a freighter aircraft and must necessarily therefore be of low profile to fit within the cargo space of an air-transport vehicle comprising a main chassis (1) on which is mounted a cab (3) with a removable upper part (5) and a slewing crane (7) having an extendable boom (11), a winch (10) and spades (23) mounted in slideways (29). The vehicle also is provided with a traditional supported lift towing boom (25) but instead of being mounted for pivoting movement on the ohassis (1), the boom (25) is mounted for generally vertical sliding movement. For this purpose, slideways (29) are provided on the inside of housing (31) for the spades and vertical movement of the boom (25) is under the control of the main crane boom (11) which can be connected to the boom (25) by means of a lift strop (41). By providing for the boom (25) to be movable vertically in slideways rather than being pivotally mounted on the chassis, a low profile chassis can be provided and the vertical dimensions of the vehicle can be kept compact. The slideways (29) may be straight or arcuate, arcuate slideways having the advantage of providing increased lift. Such increased lift can also be achieved by inserting a spacer wedge (61) between an anvil (55) at the base of the mast (27) and an abutment surface (59) on the folding boom (33). |
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| 7 | 陸上および空中用のハイブリッド運搬用ビークルの変形方法およびハイブリッド運搬用ビークル | JP2014528332 | 2012-08-22 | JP6034382B2 | 2016-11-30 | クレイン, シュテファン |
| 8 | Chassisscab car with double rearraxle | JP14715079 | 1979-11-15 | JPS55127214A | 1980-10-01 | POORU REGIYUU |
| 9 | 陸上および空中用のハイブリッド運搬用ビークルの変形方法およびハイブリッド運搬用ビークル | JP2016159844 | 2016-08-17 | JP6306106B2 | 2018-04-04 | シュテファン クレイン |
| 10 | 陸上および空中用のハイブリッド運搬用ビークルの変形方法およびハイブリッド運搬用ビークル | JP2016159844 | 2016-08-17 | JP2016190638A | 2016-11-10 | シュテファン クレイン |
| 【課題】陸上および空中用のハイブリッド運搬用ビークルの変形方法およびハイブリッド運搬用ビークルの提供。 【解決手段】陸上および空中用のハイブリッド運搬用ビークルの変形方法は、以下の変形および相互的ステップを含む:補強カバー(7)を傾けること。両方の翼(1)全体を2つの垂直軸(2)の周囲において、運搬用ビークルの長手方向位置から飛行位置まで拡張させること。水平軸(3)の周囲において、各翼(1)の後方を傾けることによって、翼(1)の後方部分を翼(1)の上部前方部分から、広げられた飛行位置まで拡張させること。翼の仰角α=0〜40°だけ翼(1)を離着陸のために傾けること。前輪(5)を胴体に向かって軸方向に移動させることによって、前輪輪距(5)が減少される。 【選択図】図2 |
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| 11 | HYBRID TRANSPORTATION VEHICLE FOR GROUND AND AIR, AND METHOD OF TRANSFORMING SUCH A VEHICLE | EP15184918.9 | 2012-08-22 | EP2977239A1 | 2016-01-27 | KLEIN, Stefan |
Hybrid transportation vehicle for ground and air consisting of a body (4), cabin (6), retractable wings (1), chassis and driving unit (8) with switching of the torque transfer between a propeller (9) situated at the rear of the vehicle and driven wheels (5), the vehicle containing reciprocal transformation mechanisms for transformation into an automobile or into an aircraft, where one or two first reciprocal transformation mechanisms for retraction and expansion of the wings (1) from or to a flying position are situated in the middle of the body (4); each first reciprocal transformation mechanism contains a first actuator and a vertical axis (2) for retraction and expansion of the wing (1) by tilting around the vertical axis between a flying position in which the axis of the wing is approximately perpendicular to the longitudinal axis of the vehicle, and a retracted position in which the wing axis is approximately parallel to the longitudinal axis of the vehicle; and two second reciprocal transformation mechanisms for changing the platform outline of the wings, each being situated separately in a wing body (1) and each containing a horizontal axis (3) of the wing and a second actuator, for tilting the rear part of each wing onto the top front part of the wing (1).
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| 12 | Hybrid transportation vehicle for ground and air, and method of transforming such a vehicle | EP12783374.7 | 2012-08-22 | EP2750905B1 | 2015-09-23 | KLEIN, Stefan |
| Hybrid transportation vehicle for ground and air consisting of a body (4), cabin (6), retractable wings (1), chassis and driving unit (8) with switching of the torque transfer between a propeller (9) situated at the rear of the vehicle and driven wheels (5), the vehicle containing reciprocal transformation mechanisms for transformation into an automobile or into an aircraft, where one or two first reciprocal transformation mechanisms for retraction and expansion of the wings (1) from or to a flying position are situated in the middle of the body (4); each first reciprocal transformation mechanism contains a first actuator and a vertical axis (2) for retraction and expansion of the wing (1) by tilting around the vertical axis between a flying position in which the axis of the wing is approximately perpendicular to the longitudinal axis of the vehicle, and a retracted position in which the wing axis is approximately parallel to the longitudinal axis of the vehicle; and two second reciprocal transformation mechanisms for changing the platform outline of the wings, each being situated separately in a wing body (1) and each containing a horizontal axis (3) of the wing and a second actuator, for tilting the rear part of each wing onto the top front part of the wing (1). | ||||||
| 13 | Recovery and towing vehicle | EP85301104 | 1985-02-19 | EP0153187A3 | 1985-09-25 | Watson, Norman Frederick |
A recovery and towing vehicle which has been specifically designed for transport in a freighter aircraft and must necessarily therefore be of low profile to fit within the cargo space of an air-transport vehicle comprising a main chassis (1) on which is mounted a cab (3) with a removable upper part (5) and a slewing crane (7) having an extendable boom (11), a winch (10) and spades (23) mounted in slideways (29). The vehicle also is provided with a traditional supported lift towing boom (25) but instead of being mounted for pivoting movement on the ohassis (1), the boom (25) is mounted for generally vertical sliding movement. For this purpose, slideways (29) are provided on the inside of housing (31) for the spades and vertical movement of the boom (25) is under the control of the main crane boom (11) which can be connected to the boom (25) by means of a lift strop (41). By providing for the boom (25) to be movable vertically in slideways rather than being pivotally mounted on the chassis, a low profile chassis can be provided and the vertical dimensions of the vehicle can be kept compact. The slideways (29) may be straight or arcuate, arcuate slideways having the advantage of providing increased lift. Such increased lift can also be achieved by inserting a spacer wedge (61) between an anvil (55) at the base of the mast (27) and an abutment surface (59) on the folding boom (33). |
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| 14 | HYBRID TRANSPORTATION VEHICLE FOR GROUND AND AIR, AND METHOD OF TRANSFORMING SUCH A VEHICLE | EP15184918.9 | 2012-08-22 | EP2977239B1 | 2017-04-12 | KLEIN, Stefan |
| Hybrid transportation vehicle for ground and air consisting of a body (4), cabin (6), retractable wings (1), chassis and driving unit (8) with switching of the torque transfer between a propeller (9) situated at the rear of the vehicle and driven wheels (5), the vehicle containing reciprocal transformation mechanisms for transformation into an automobile or into an aircraft, where one or two first reciprocal transformation mechanisms for retraction and expansion of the wings (1) from or to a flying position are situated in the middle of the body (4); each first reciprocal transformation mechanism contains a first actuator and a vertical axis (2) for retraction and expansion of the wing (1) by tilting around the vertical axis between a flying position in which the axis of the wing is approximately perpendicular to the longitudinal axis of the vehicle, and a retracted position in which the wing axis is approximately parallel to the longitudinal axis of the vehicle; and two second reciprocal transformation mechanisms for changing the platform outline of the wings, each being situated separately in a wing body (1) and each containing a horizontal axis (3) of the wing and a second actuator, for tilting the rear part of each wing onto the top front part of the wing (1). | ||||||
| 15 | TRANSFORMATION METHOD OF HYBRID TRANSPORTATION VEHICLE FOR GROUND AND AIR, AND HYBRID TRANSPORTATION VEHICLE ITSELF | EP12783374.7 | 2012-08-22 | EP2750905A1 | 2014-07-09 | KLEIN, Stefan |
| Hybrid transportation vehicle for ground and air consisting of a body (4), cabin (6), retractable wings (1), chassis and driving unit (8) with switching of the torque transfer between a propeller (9) situated at the rear of the vehicle and driven wheels (5), the vehicle containing reciprocal transformation mechanisms for transformation into an automobile or into an aircraft, where one or two first reciprocal transformation mechanisms for retraction and expansion of the wings (1) from or to a flying position are situated in the middle of the body (4); each first reciprocal transformation mechanism contains a first actuator and a vertical axis (2) for retraction and expansion of the wing (1) by tilting around the vertical axis between a flying position in which the axis of the wing is approximately perpendicular to the longitudinal axis of the vehicle, and a retracted position in which the wing axis is approximately parallel to the longitudinal axis of the vehicle; and two second reciprocal transformation mechanisms for changing the platform outline of the wings, each being situated separately in a wing body (1) and each containing a horizontal axis (3) of the wing and a second actuator, for tilting the rear part of each wing onto the top front part of the wing (1). | ||||||
| 16 | Recovery and towing vehicle | EP85301104.7 | 1985-02-19 | EP0153187B1 | 1988-08-10 | Watson, Norman Frederick |
| 17 | All-terrain vehicle | US15594977 | 2017-05-15 | US09944177B2 | 2018-04-17 | Burton D. Fischer; William B. Rodriguez |
| An all-terrain vehicle (“ATV”) a frame extending along a longitudinal centerline of the ATV. Additionally, the ATV includes a plurality of ground engaging members operably coupled to the frame which includes a first ground-engaging member and a second ground-engaging member positioned on a first side of the longitudinal centerline and a third ground-ground engaging member and a fourth ground-engaging member positioned on a second side of the longitudinal centerline. The ATV further includes a straddle seat supported by the frame and configured to support an operator, an engine supported by the frame, and an engine air inlet fluidly coupled to the engine and positioned forward of the straddle seat. | ||||||
| 18 | Transformation method of hybrid transportation vehicle for ground and air, and hybrid transportation vehicle itself | US15378121 | 2016-12-14 | US09815345B2 | 2017-11-14 | Stefan Klein |
| Transformation method of hybrid transportation vehicle for ground and air includes the following transformation and reciprocal steps: Tilting the compensation cover (7) on. Expansion of both whole wings (1) from the transportation vehicle longitudinal position around two vertical axes (2) into the flying position. Expansion of rear parts of wings (1) from the top front parts of wings (1) into the spread flying position by tilting the rear of each wing (1) around a horizontal axis (3). The take-off and landing tilting of wings (1) by an angle of attack alpha=0 to 40° of the wings onset. Front wheels track (5) is reduced by axially shifting the front wheels (5) towards the fuselage. Furthermore, a corresponding hybrid transportation vehicle for ground and air is described which contains reciprocal transformation mechanisms for transformation from a sterling double or four-track automobile into a sterling aircraft for take-off and landing on the ground or water, and vice versa. | ||||||
| 19 | TRANSFORMATION METHOD OF HYBRID TRANSPORTATION VEHICLE FOR GROUND AND AIR, AND HYBRID TRANSPORTATION VEHICLE ITSELF | US15378121 | 2016-12-14 | US20170297395A1 | 2017-10-19 | Stefan Klein |
| Transformation method of hybrid transportation vehicle for ground and air includes the following transformation and reciprocal steps: Tilting the compensation cover (7) on. Expansion of both whole wings (1) from the transportation vehicle longitudinal position around two vertical axes (2) into the flying position. Expansion of rear parts of wings (1) from the top front parts of wings (1) into the spread flying position by tilting the rear of each wing (1) around a horizontal axis (3). The take-off and landing tilting of wings (1) by an angle of attack alpha=0 to 40° of the wings onset. Front wheels track (5) is reduced by axially shifting the front wheels (5) towards the fuselage. Furthermore, a corresponding hybrid transportation vehicle for ground and air is described which contains reciprocal transformation mechanisms for transformation from a sterling double or four-track automobile into a sterling aircraft for take-off and landing on the ground or water, and vice versa. | ||||||
| 20 | Multi-stage tilting and multi-rotor flying car | US14647444 | 2013-02-25 | US09682772B2 | 2017-06-20 | Kwang Joon Yoon |
| The present invention provides a multi-stage tilting and multi-rotor flying car including: a main frame externally shaped like a rectangle and internally partitioned to have a grid structure; a body mounted at a center of the main frame in consideration of balance; a plurality of rotors mounted to the main frame to face upward; a plurality of wheels mounted to the main frame to face downward; body wings provided at opposite sides of the body; and an automatic driving controller provided in the body and controlling the rotors and the wheels, thereby having effects on spending only the minimum necessary flying time for taking off and landing in a narrow area, and improving flight performance three times higher in flight time and flight speed and five times higher in fight distance than a rotary-wing aircraft such as a helicopter while flying in the fixed-wing mode. | ||||||
