公开(公告)号：US20160122014A1

公开(公告)日：2016-05-05

申请号：US14897869

申请日：2014-06-03

Applicant: Soo-Young JANG

Inventor： Soo-Young JANG

IPC: B64C39/02 ,  G01C21/00 ,  B64F3/02 ,  B64B1/12 ,  B64D39/00

CPC classification number: B64C39/022 ,  B64B1/12 ,  B64B1/52 ,  B64D39/00 ,  B64F1/14 ,  B64F3/02 ,  F03D5/00 ,  F05B2240/922 ,  G01C21/005 ,  Y02E10/70 ,  Y02T50/82

Abstract: The present invention relates to a system for operating a flying object that is flown from the ground. The flying object operation system includes a flying object that is filled with a gas therein to stay in the sky, a ground unit installed on the ground, a wire unit connecting the flying object to the ground unit, and a buoyancy-generation unit disposed on a side of the flying object to obtain buoyancy through friction with air, thereby transferring the obtained buoyancy to the flying object. In the present invention, since additional wind-derived buoyancy obtained by the buoyancy-generation unit connected to the flying object is further generated, sufficient buoyancy may be supplied to the flying object in a high-altitude environment to stably operate the flying object. Also, since power generated by using the wind power generation unit is transmitted to the ground through the wire unit, the flying object operation system may be utilized as wind power generation equipment.

Abstract translation: 本发明涉及一种用于操作从地面飞行的飞行物体的系统。 飞行物体操作系统包括在其中填充有气体以留在天空中的飞行物体，安装在地面上的接地单元，将飞行物体连接到地面单元的线单元和布置在地面上的浮力发生单元 飞行物体的一侧通过与空气的摩擦获得浮力，从而将获得的浮力转移到飞行物体上。 在本发明中，由于与由飞行物体连接的浮力发生单元得到的额外的风力浮力进一步产生，所以可以在高空环境中向飞行物体供给足够的浮力，以稳定地操作飞行物体。 此外，由于通过使用风力发电单元产生的电力通过线单元传递到地面，所以飞行物体操作系统可以用作风力发电设备。

公开(公告)号：US20150217860A1

公开(公告)日：2015-08-06

申请号：US14415438

申请日：2012-07-17

Applicant: Donggyu Yang

Inventor： Donggyu Yang

IPC: B64C25/32 ,  B64C25/62 ,  B64C25/14

CPC classification number: B64C25/32 ,  B64C25/04 ,  B64C25/14 ,  B64C25/62 ,  B64F1/02 ,  B64F1/04 ,  Y02T50/82

Abstract: The aircraft capable of takeoff/landing via the fuselage thereof and the takeoff/landing system of the aircraft according to the present invention are configured such that multiple takeoff/landing rollers are arranged in a sliding direction such that the aircraft fuselage having a landing surface formed at the bottom thereof can safely land and slide in a sliding direction, thus enabling the aircraft fuselage to contact a running surface and takeoff/land without separate landing gear. Thus, not only can the weight of the aircraft be reduced, but the fuel consumption of the aircraft can be reduced as well, the useful space in the aircraft can be broadened, the length of the runway can be shortened due to the frictional force generated by the takeoff/landing device, and the safety during the takeoff/landing of the aircraft can be improved.

Abstract translation: 根据本发明的能够通过其机身起飞/着陆的飞行器和飞行器的起飞/着陆系统被构造成使得多个起飞/着陆滚轮沿滑动方向布置，使得具有着陆面的飞行器机身形​​成 在其底部可以安全地滑动并滑动方向，从而使飞机机身能够接触运行的表面，起飞/着陆，而无需单独的起落架。 因此，不仅可以减少飞机的重量，还可以减少飞机的燃料消耗，从而可以扩大飞机的有用空间，由于产生的摩擦力可以缩短跑道的长度 通过起飞/着陆装置，可以提高飞机起飞/着陆期间的安全性。

公开(公告)号：US09010969B2

公开(公告)日：2015-04-21

申请号：US13423483

申请日：2012-03-19

Applicant: Charles A. Roudeski ,  Eric W. Wise

Inventor： Charles A. Roudeski ,  Eric W. Wise

IPC: F21V7/00 ,  F21S8/00 ,  B64F1/20 ,  F21V7/04 ,  F21W111/06 ,  F21Y101/02 ,  F21V29/00 ,  F21V23/04

CPC classification number: F21V7/09 ,  B64D2203/00 ,  B64F1/20 ,  F21S8/032 ,  F21V5/048 ,  F21V7/0008 ,  F21V7/0058 ,  F21V7/041 ,  F21V7/048 ,  F21V23/009 ,  F21V23/0464 ,  F21V29/70 ,  F21V29/74 ,  F21V29/75 ,  F21W2111/06 ,  F21Y2107/00 ,  F21Y2115/10 ,  Y02T50/82 ,  Y10T29/49826

Abstract: A lighting system having a reflector with a plurality of reflecting surfaces. The plurality of reflecting surfaces have at least one optical axis, and the reflecting surfaces further include a linearly projected cross-section along a respective linear axis. A plurality of light emitting diodes (LEDs) are positioned in a line generally parallel to the linearly projected cross-section of the plurality of reflecting surfaces. The LEDs are oriented relative to an associated reflecting surface such that a central light-emitting axis of the plurality of LEDs is angled relative to the at least one optical axis of the associated reflecting surface at about 45°. The reflecting surfaces redirect and collimate a light output of the plurality of LEDs at an angle of about 45° with respect to the central light emitting axis of the plurality of LEDs.

Abstract translation: 一种具有具有多个反射面的反射体的照明系统。 多个反射表面具有至少一个光轴，并且反射表面还包括沿着相应直线轴线的直线投影的横截面。 多个发光二极管（LED）被定位在大致平行于多个反射表面的直线投影截面的线上。 LED相对于相关联的反射表面定向，使得多个LED的中心发光轴线相对于相关联的反射表面的至少一个光轴在大约45°处成角度。 反射表面相对于多个LED的中心发光轴线以大约45°的角度重定向和准直多个LED的光输出。

公开(公告)号：US08931290B2

公开(公告)日：2015-01-13

申请号：US13000524

申请日：2009-06-24

Applicant: Kenan Soenmez ,  Luc Leroy

Inventor： Kenan Soenmez ,  Luc Leroy

IPC: B60H1/32 ,  B64F1/36 ,  F25B7/00

CPC classification number: B64F1/364 ,  Y02T50/82

Abstract: An auxiliary cooling device is configured to be operated outside of an aircraft. The auxiliary cooling device is configured to be connected to an aircraft liquid cooling system which includes a refrigerating device, a coolant supply connection, a coolant discharge connection, and a control device. The auxiliary cooling device includes a cold source that is adapted to cool a coolant down to a desired low temperature, an auxiliary cooling device outlet which is connected to the cold source and connectable to the coolant supply connection. The auxiliary cooling device also includes an auxiliary cooling device inlet which is connected to the cold source and connectable to the coolant discharge connection of the aircraft liquid cooling system.

Abstract translation: 辅助冷却装置构造成在飞机外部操作。 辅助冷却装置被构造成连接到包括制冷装置，冷却剂供应连接，冷却剂排出连接和控制装置的飞机液体冷却系统。 辅助冷却装置包括适于将冷却剂冷却到期望的低温的冷源，连接到冷源并可连接到冷却剂供应连接的辅助冷却装置出口。 辅助冷却装置还包括辅助冷却装置入口，其连接到冷源并可连接到飞行器液体冷却系统的冷却剂排放连接。

公开(公告)号：US20120319871A1

公开(公告)日：2012-12-20

申请号：US13596203

申请日：2012-08-28

Applicant: Eric W. Wise

Inventor： Eric W. Wise

IPC: G08G5/04

CPC classification number: B64F1/20 ,  B64D2203/00 ,  F21S8/032 ,  F21V7/041 ,  F21V7/048 ,  F21W2111/06 ,  F21Y2115/10 ,  Y02T50/82

Abstract: A collision avoidance system includes a sensor adapted to detect at least one vehicle in the vicinity of a predetermined area and generate target data relating to the at least one vehicle. An awareness engine receives the target data and evaluates the target data for a threat of a collision. An alerting system is adapted to alert the at least one vehicle in the event of a threat of a collision, the alerting system being activated by the awareness engine.

Abstract translation: 碰撞避免系统包括适于检测预定区域附近的至少一辆车辆并产生与至少一辆车辆有关的目标数据的传感器。 感知引擎接收目标数据并评估目标数据以确定碰撞的威胁。 警报系统适于在发生碰撞的威胁的情况下警告该至少一辆车辆，该警报系统被该意识引擎激活。

公开(公告)号：US20120023985A1

公开(公告)日：2012-02-02

申请号：US13257669

申请日：2010-03-18

Applicant: Soren Risgaard Dahl ,  Bo Vork Nielsen ,  Henrik Olsson ,  Lars Schroder

Inventor： Soren Risgaard Dahl ,  Bo Vork Nielsen ,  Henrik Olsson ,  Lars Schroder

IPC: F25B49/02 ,  F25B49/00 ,  F25D17/06

CPC classification number: B64F1/362 ,  Y02T50/82

Abstract: A preconditioned air unit for supplying preconditioned air to an aircraft parked on the ground, the preconditioned air unit comprising a housing accommodating a flow duct with an air inlet for ambient air and an air outlet for connection to the parked aircraft, a blower connected with the flow duct for generation of an air flow from the air inlet toward the air outlet, at least one refrigeration system, each of which includes at least one compressor, at least one condenser, at least one expansion valve, and at least one evaporator connected in a flow circuit containing a refrigerant, and wherein the at least one evaporator interacts with the air flow in the flow duct, and at least one variable frequency driver for power supply of at least one of the at least one compressor of the at least one refrigeration system.

Abstract translation: 一种预处理空气单元，用于向驻留在地面上的飞机提供预调节的空气，所述预调节的空气单元包括容纳流动管道的壳体，所述流动管道具有用于环境空气的空气入口和用于连接到停放的飞行器的空气出口， 用于产生从空气入口朝向空气出口的空气流的流动管道，至少一个制冷系统，每个制冷系统包括至少一个压缩机，至少一个冷凝器，至少一个膨胀阀和至少一个蒸发器， 包含制冷剂的流动回路，并且其中所述至少一个蒸发器与所述流动管道中的空气流相互作用，以及用于至少一个所述至少一个制冷剂的至少一个压缩机中的至少一个的供电的可变频率驱动器 系统。

公开(公告)号：US20110253799A1

公开(公告)日：2011-10-20

申请号：US12681889

申请日：2010-03-19

Applicant: Choon San Kim

Inventor： Choon San Kim

IPC: A01G15/00

CPC classification number: E01H13/00 ,  B64F1/36 ,  G05D23/19 ,  Y02T50/82

Abstract: There is provided an apparatus for preventing and removing fog at an airport runway. The apparatus includes: a water tank 10 buried in a ground around a runway; a water tank temperature sensor 20 for sensing a water temperature in the water tank; a heater 30 provided inside the water tank, for heating water contained in the water tank; a cooling device 40 provided inside the water tank, for cooling water contained in the water tank; the sprinklers 50 installed at opposite sides along the runway and over the ground around the runway, and supplied with the water from the water tank to spray water towards the atmosphere over and around the runway; and a controller 60 controlling, on the basis of the water temperature of the water tank measured using the temperature sensor, operation of the sprinklers, the heater, and the cooling device, according to an externally inputted operational signal.

Abstract translation: 提供了一种在机场跑道上防止和除雾的装置。 该装置包括：埋设在跑道周围的地面中的水箱10; 用于感测水箱中的水温的水箱温度传感器20; 设置在水箱内部的加热器30，用于加热容纳在水箱中的水; 设置在水箱内部的用于冷却容纳在水箱中的水的冷却装置40; 喷洒器50安装在跑道的相对侧并且在跑道周围的地面上，并且从水箱中提供水以在跑道上和周围向大气喷射水; 以及根据外部输入的操作信号，根据使用温度传感器测量的水箱的水温控制喷洒器，加热器和冷却装置的操作的控制器60。

公开(公告)号：US08015925B2

公开(公告)日：2011-09-13

申请号：US12801660

申请日：2010-06-18

Applicant: Abner J. Simon

Inventor： Abner J. Simon

IPC: A63G1/00

CPC classification number: B60M7/00 ,  B61B5/02 ,  B64C37/00 ,  B64F1/10 ,  E01B25/00 ,  Y02T30/30 ,  Y02T50/82

Abstract: A transportation system includes a vehicle having wings, a propulsion system, a lifting gear coupling the vehicle to an undercarriage, and a guidance assembly movably connecting the undercarriage to guide rails. The wings generate aerodynamic lift when the vehicle exceeds a first speed. The lifting gear supports a load of the vehicle in a first position in relation to the undercarriage when the vehicle travels at less than the first speed, allows the vehicle to lift to a second position in relation to the undercarriage as the vehicle accelerates beyond the first speed, and maintains the vehicle in the second position when the vehicle exceeds the first speed. The guidance assembly shiftingly engages the guide rails through rollers that are in rolling contact with the guide rails when the vehicle is in the first position and are displaced from the guide rails when the vehicle is in the second position.

Abstract translation: 运输系统包括具有翼的车辆，推进系统，将车辆联接到起落架上的提升齿轮以及将起落架可移动地连接到导轨的引导组件。 当车辆超过第一速度时，机翼产生空气动力升力。 当车辆以小于第一速度行驶时，起重工具将车辆的负载相对于起落架支撑在第一位置，当车辆加速超过第一速度时，允许车辆相对于起落架升高到第二位置 并且当车辆超过第一速度时将车辆保持在第二位置。 引导组件通过在车辆处于第一位置时与导轨滚动接触的辊子转动地接合导轨，当车辆处于第二位置时，导向组件从导轨移位。

公开(公告)号：US07975959B2

公开(公告)日：2011-07-12

申请号：US11528647

申请日：2006-09-28

Applicant: Arie Perry ,  Ran Braier

Inventor： Arie Perry ,  Ran Braier

IPC: B64C25/50

CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/086 ,  B64C2201/187 ,  B64F1/00 ,  Y02T50/82

Abstract: A method for transferring airplanes and an unmanned airplane transfer system. The airplane transferring system includes: receiving a transfer signal responsive of a movement of an airplane control component; and transferring an airplane, by an unmanned airplane transfer system, in response to the transfer signal.

Abstract translation: 一种用于转移飞机和无人驾驶飞机转移系统的方法。 飞机传送系统包括：响应飞机控制部件的运动接收传送信号; 并且通过无人驾驶飞行器传送系统来响应于传送信号传送飞机。

公开(公告)号：US20100326311A1

公开(公告)日：2010-12-30

申请号：US12801660

申请日：2010-06-18

Applicant: Abner J. Simon

Inventor： Abner J. Simon

IPC: B61D15/00 ,  E01B25/00 ,  B60M1/02

CPC classification number: B60M7/00 ,  B61B5/02 ,  B64C37/00 ,  B64F1/10 ,  E01B25/00 ,  Y02T30/30 ,  Y02T50/82

Abstract: A transportation system includes a vehicle having wings, a propulsion system, a lifting gear coupling the vehicle to an undercarriage, and a guidance assembly movably connecting the undercarriage to guide rails. The wings generate aerodynamic lift when the vehicle exceeds a first speed. The lifting gear supports a load of the vehicle in a first position in relation to the undercarriage when the vehicle travels at less than the first speed, allows the vehicle to lift to a second position in relation to the undercarriage as the vehicle accelerates beyond the first speed, and maintains the vehicle in the second position when the vehicle exceeds the first speed. The guidance assembly shiftingly engages the guide rails through rollers that are in rolling contact with the guide rails when the vehicle is in the first position and are displaced from the guide rails when the vehicle is in the second position.

Abstract translation: 运输系统包括具有翼的车辆，推进系统，将车辆联接到起落架上的提升齿轮以及将起落架可移动地连接到导轨的引导组件。 当车辆超过第一速度时，机翼产生空气动力升力。 当车辆以小于第一速度行驶时，起重工具将车辆的负载相对于起落架支撑在第一位置，当车辆加速超过第一速度时，允许车辆相对于起落架升高到第二位置 并且当车辆超过第一速度时将车辆保持在第二位置。 引导组件通过在车辆处于第一位置时与导轨滚动接触的辊子转动地接合导轨，当车辆处于第二位置时，导向组件从导轨移位。