中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

62 records (took 0.015 seconds)

    ARTIFICIAL INTELLIGENCE-DRIVEN CARBON DIOXIDE SEQUESTRATION IN THE ATMOSPHERE
    1.
    发明公开
    ARTIFICIAL INTELLIGENCE-DRIVEN CARBON DIOXIDE SEQUESTRATION IN THE ATMOSPHERE 审中-公开

    公开(公告)号：US20230375746A1

    公开(公告)日：2023-11-23

    申请号：US17749400

    申请日：2022-05-20

    Applicant: Kyndryl, Inc.

    Inventor： Mauro Marzorati ,  Jeremy R. Fox ,  Sarbajit K. Rakshit ,  Ruben Luengas de la Fuente

    IPC: G01W1/18 ,  G08G5/00 ,  B64C39/02

    CPC classification number: G01W1/18 ,  G08G5/003 ,  B64C39/024 ,  B64C2201/125

    Abstract: Aspects of the present disclosure relate generally to reduction in environmental pollution and, more particularly, to systems and method of carbon dioxide (CO2) sequestration in the atmosphere. For example, a computer-implemented method includes receiving, by a computing device, locations of an atmospheric pollutant; determining, by a computing device, a location of a target area of the atmospheric pollutant for sequestration; determining, by the computing device, positioning and flight path data for airborne sequestration devices to sequester the atmospheric pollutant at the location of the target area of the atmospheric pollutant; and deploying, by the computing device, the airborne sequestration devices with reagent according to the positioning and the flight path data to sequester the atmospheric pollutant at the location of the target area of the atmospheric pollutant.

    Downrange wind profile measurement system and method of use
    5.
    发明授权
    Downrange wind profile measurement system and method of use 有权
    降风量测风系统及其使用方法

    公开(公告)号：US09506724B1

    公开(公告)日：2016-11-29

    申请号：US15161409

    申请日：2016-05-23

    Applicant: Lyman Robert Hazelton

    Inventor： Lyman Robert Hazelton

    IPC: G01W1/00 ,  G01S13/95 ,  F41G3/08 ,  F41G1/38 ,  B64D43/00 ,  G05D1/10

    CPC classification number: F41G3/08 ,  B64C39/024 ,  B64C2201/12 ,  B64C2201/125 ,  F41G1/38 ,  F41G1/545

    Abstract: A downrange wind measurement system includes an aerial vehicle with a global positioning system and a communication device; and a remote computer with a display for viewing access and a transceiver. A method to assist a shooter adjust for a wind speed and a wind angle of a wind prior to make a downrange shot includes creating a flight path for an aerial vehicle to fly alongside a projectile path; determining locations for a circular flight path via the flight path; measuring the wind speed and the wind angle along the circular flight path; transmitting the wind speed and the wind angle to a remote computer; and computing via the remote computer scope adjustments with the wind speed and wind angle.

    Abstract translation: 降序风测量系统包括具有全球定位系统和通信设备的飞行器; 以及具有用于观看访问的显示器和收发器的远程计算机。 一种在进行下一次射击之前辅助射手调整风速和风角度的方法包括创建用于飞行器飞行在飞行路径上的飞行路径; 确定通过飞行路径的圆形飞行路径的位置; 测量沿着圆形飞行路径的风速和风角; 将风速和风角传递到远程计算机; 并通过远程计算机进行范围调整与风速和风角度。

    APPARATUS AND SYSTEM FOR SMART SEEDING WITHIN CLOUD FORMATIONS
    6.
    发明申请
    APPARATUS AND SYSTEM FOR SMART SEEDING WITHIN CLOUD FORMATIONS 审中-公开
    用于在云计算中智能种子的装置和系统

    公开(公告)号：US20160299254A1

    公开(公告)日：2016-10-13

    申请号：US14685241

    申请日：2015-04-13

    Applicant: Lorenzo Martinez Martínez De La Escalera ,  Jorge Joaquin Canto Ibanez ,  Diego Martinez Martínez De La Escalera ,  Hernán Rivera Ramos ,  Lorenzo Martinez Gomez

    Inventor： Lorenzo Martinez Martínez De La Escalera ,  Jorge Joaquin Canto Ibanez ,  Diego Martinez Martínez De La Escalera ,  Hernán Rivera Ramos ,  Lorenzo Martinez Gomez

    IPC: G01W1/08 ,  B64C39/02 ,  A01G15/00

    CPC classification number: G01W1/08 ,  A01G15/00 ,  B64C39/024 ,  B64C2201/125

    Abstract: This invention consists of a unique apparatus and system consisting of devices, materials and methods specially engineered to perform high precision and smart cloud seeding by the dispersion of micro and nanoparticles of sodium chloride and similar chemistry compounds at specific locations with the purpose of rain induction and related applications. A safe and precise unmanned aerial vehicle UAV device instrumented with portable thermometer, hygrometer, barometer, anemometer and 3D visual register will scrutinize these internal cloud climate parameters. By means of these real time measurements and communications, a meteorological ground operating team is enabled to perform the data acquisition and processing from the clouds. This device and system be enabled to select the locations suitable for rain induction and perform on site accurate particulate seeding dispersion from a device mounted on the same UAV within the eligible clouds. Typical applications of this apparatus and system besides rain induction are fog condensation for airports, highways and other environments where visibility impairment may have critical consequences. This invention may also provide a valuable tool to provide solutions to control and mitigate snow, sleet and hail effects.

    Abstract translation: 本发明包括由特殊设计的设备，材料和方法组成的独特的装置和系统，该设备，材料和方法通过在特定位置处的微量和纳米颗粒和类似化学化合物的分散来实现高精度和智能云播种，其目的是降雨诱导和 相关应用。 一个安全，精确的无人驾驶飞行器无人机装备便携式温度计，湿度计，气压计，风速计和3D视觉记录仪将审查这些内部云气候参数。 通过这些实时测量和通信，气象地面操作团队能够从云层执行数据采集和处理。 该设备和系统能够选择适合雨水感应的位置，并从安装在合格云中的同一UAV上的设备进行现场准确的颗粒播种分散。 该设备和系统除了雨水诱导外，典型应用是机场，高速公路和其他视力障碍可能产生严重后果的环境的雾化。 本发明还可以提供一种有用的工具来提供控制和减轻雪，雨夹雪和冰雹效应的解决方案。

    AERIAL VEHICLE ACQUISITION OF SEISMIC DATA
    7.
    发明申请
    AERIAL VEHICLE ACQUISITION OF SEISMIC DATA 审中-公开
    空中数据采集车辆

    公开(公告)号：US20160003954A1

    公开(公告)日：2016-01-07

    申请号：US14793520

    申请日：2015-07-07

    Applicant: Schlumberger Technology Corporation

    Inventor： Floyd L. Broussard III ,  Hallgrim Ludvigsen ,  Chad Brockman ,  Stephen Whitley ,  Ross Graeber ,  Duo Chen ,  Andrew Richardson ,  Daniel Pupim Kano ,  Vijay Kumar

    IPC: G01V1/00 ,  G01V1/22 ,  B64C39/02

    CPC classification number: G01V1/003 ,  B64C2201/125 ,  G01V1/22

    Abstract: Methods and apparatus that facilitate acquisition of seismic data. A plurality of acquisition locations within an area of interest may be determined and provided to aerial vehicles. Seismic data may be received from the aerial vehicle. In another example, an aerial vehicle includes a positioning system that determines location of the apparatus; a seismic sensor that senses seismic data; a memory that stores seismic data; and a transceiver that provides telemetric data and the seismic data to a controller device. In at least one example, a method for acquiring seismic data is provided including receiving location information at an aerial vehicle. The aerial vehicle may navigate to a location based on the location information and a seismic sensor may acquire seismic data. The aerial vehicle may be navigated to a controller device and the acquired seismic data may be provided to the controller device.

    Abstract translation: 促进地震数据采集的方法和装置。 可以确定感兴趣区域内的多个采集位置并将其提供给飞行器。 可以从飞行器接收地震数据。 在另一个示例中，飞行器包括确定设备的位置的定位系统; 感测地震数据的地震传感器; 存储地震数据的记忆; 以及向控制器设备提供遥测数据和地震数据的收发器。 在至少一个示例中，提供了一种用于采集地震数据的方法，包括在飞行器处接收位置信息。 飞行器可以基于位置信息导航到位置，并且地震传感器可以获取地震数据。 飞行器可以导航到控制器设备，并且获取的地震数据可以被提供给控制器设备。

    System for Converting Propelling Thrust to Produce a Continuous Flow
    10.
    发明申请
    System for Converting Propelling Thrust to Produce a Continuous Flow 审中-公开

    公开(公告)号：US20190219488A1

    公开(公告)日：2019-07-18

    申请号：US16248580

    申请日：2019-01-15

    Applicant: Richard John McNamara

    Inventor： Richard John McNamara

    IPC: G01N1/22 ,  B64D47/00 ,  B64C39/02

    CPC classification number: G01N1/2247 ,  B64C39/024 ,  B64C2201/125 ,  B64D47/00 ,  G01N1/2273

    Abstract: A system for converting propelling thrust to produce a continuous flow is provided. The system can be integrated and/or retrofitted to the body of an aircraft. The system includes a pressure-lowering device and a sample chamber. The pressure-lowering device is used produce a low-pressure, continuous flow from a high-velocity propelling thrust source. Moreover, the pressure-lowering device is a passive flow generator that does not require a power source in order to produce a continuous flow from a propelling thrust. The design of the pressure-lowering device produces a flow rate that is independent of the aircraft motion. The sample chamber is used to measure and analyze ambient gases which are pulled through the sample chamber by the pressure-lowering device, as a result of the high-velocity air stream produced by the propelling thrust source.

Patent Agency Ranking