Integrated extracorporeal oxygenation and CO2 removal with ventilation system

    公开(公告)号:US11318237B2

    公开(公告)日:2022-05-03

    申请号:US17428654

    申请日:2020-02-06

    摘要: A transportable extracorporeal system includes a housing, a blood flow inlet, a blood flow outlet, a plurality of hollow gas permeable fibers, a gas inlet in fluid connection with inlets of the plurality of hollow gas permeable fibers, a gas outlet in fluid connection with outlets of the plurality of hollow gas permeable fibers, a first moving element, a concentrated oxygen generating device, a second moving element, a hollow transport conduit having a proximal opening and a distal opening and a power source configured to provide power to the first and second moving elements. The plurality of hollow gas permeable fibers comprising a gas transfer membrane. The concentrated oxygen generating device is configured to recycle waste oxygen from the gas transfer membrane to increase throughput and remove, by an adsorption/desorption process, unwanted gasses.

    Configurable oxygen concentrator and related method

    公开(公告)号:US10953187B2

    公开(公告)日:2021-03-23

    申请号:US16482427

    申请日:2018-06-01

    IPC分类号: A61M16/10 A61M16/00

    摘要: A configurable oxygen concentrator for providing various flow rates and volumes of concentrated oxygen to a patient includes an electro-mechanical assembly having a housing with a first face, a second face and an outer surface. The oxygen concentrator also includes a first battery, a second battery, a first adsorbent container and a second adsorbent container. The first and second batteries are removably mountable to the first face and the first and second adsorbent containers are removably mountable to the second face to permit modification of the concentrated oxygen capacity and operating life of the concentrator as the patient progresses through different stages of a breathing disease. The first battery has a first battery capacity that is less than a second battery capacity of the second battery. The first adsorbent container has a first adsorbent capacity that is less than a second adsorbent capacity of the second adsorbent container.

    Hybrid radiant energy aircraft engine
    8.
    发明授权
    Hybrid radiant energy aircraft engine 有权
    混合辐射能飞机发动机

    公开(公告)号:US09296288B2

    公开(公告)日:2016-03-29

    申请号:US13875449

    申请日:2013-05-02

    摘要: Hybrid aircraft propulsion systems are disclosed comprising an electrically driven ducted fan, a peripheral duct or enclosure, a combustion-produced source of radiant energy, radiant energy receivers or cold mirrors, and thermophotovoltaic or thermoelectric cell energy converters. An electric motor drives a partially or completely duct enclosed fan. Downstream and within the duct enclosure, radiant energy emitters irradiated receiver fins and thermophotovoltaic cells or thermoelectric cells. The receiver fins heat and expand the fan air, and the thermophotovoltaic cells or thermoelectric cells convert the radiant energy into electrical energy which is available to charge batteries and energize the fan motor. Thrust is provided via the acceleration of air by the fan and by the acceleration of air due to heat driven expansion.

    摘要翻译: 公开了混合式飞机推进系统,其包括电驱动管道风扇,外围管道或外壳,燃烧产生的辐射能源,辐射能量接收器或冷镜,以及热光伏或热电池能量转换器。 电动机驱动部分或完全封闭风扇。 下游和管道外壳内,辐射能发射器照射接收翅片和热光伏电池或热电池。 接收器翅片加热并膨胀风扇空气,并且热光伏电池或热电电池将辐射能转换成可用于对电池充电并为风扇电动机通电的电能。 通过风扇加速空气和由于热驱动膨胀而加速空气来提供推力。

    HYBRID RADIANT ENERGY AIRCRAFT ENGINE
    9.
    发明申请
    HYBRID RADIANT ENERGY AIRCRAFT ENGINE 有权
    混合放射能量飞机发动机

    公开(公告)号:US20140345281A1

    公开(公告)日:2014-11-27

    申请号:US13875449

    申请日:2013-05-02

    IPC分类号: B60K6/24 B60K6/28

    摘要: Hybrid aircraft propulsion systems are disclosed comprising an electrically driven ducted fan, a peripheral duct or enclosure, a combustion-produced source of radiant energy, radiant energy receivers or cold mirrors, and thermophotovoltaic or thermoelectric cell energy converters. An electric motor drives a partially or completely duct enclosed fan. Downstream and within the duct enclosure, radiant energy emitters irradiated receiver fins and thermophotovoltaic cells or thermoelectric cells. The receiver fins heat and expand the fan air, and the thermophotovoltaic cells or thermoelectric cells convert the radiant energy into electrical energy which is available to charge batteries and energize the fan motor. Thrust is provided via the acceleration of air by the fan and by the acceleration of air due to heat driven expansion.

    摘要翻译: 公开了混合式飞机推进系统,其包括电驱动管道风扇,外围管道或外壳,燃烧产生的辐射能源,辐射能量接收器或冷镜,以及热光伏或热电池能量转换器。 电动机驱动部分或完全封闭风扇。 下游和管道外壳内,辐射能发射器照射接收翅片和热光伏电池或热电池。 接收器翅片加热并膨胀风扇空气,并且热光伏电池或热电电池将辐射能转换成可用于对电池充电并为风扇电动机通电的电能。 通过风扇加速空气和由于热驱动膨胀而加速空气来提供推力。