Development of a Simple Air- and O2-Powered Ventilator for Care of COVID-19 Patients
开发用于护理 COVID-19 患者的简单空气和 O2 动力呼吸机
基本信息
- 批准号:555180-2020
- 负责人:
- 金额:$ 3.64万
- 依托单位:
- 依托单位国家:加拿大
- 项目类别:Alliance Grants
- 财政年份:2020
- 资助国家:加拿大
- 起止时间:2020-01-01 至 2021-12-31
- 项目状态:已结题
- 来源:
- 关键词:
项目摘要
This project aims to advance a novel, simple ventilator concept from an initial concept through development of a proof-of-concept prototype, to lab-based validation of the design. The main difference between this ventilator design and existing products in the market are that it is to be assembled mostly from off-the-shelf components, has almost no moving parts, and will be extremely low-cost (approximately ten times less expensive than most current ventilator models). The final design will be openly available to enable widespread adoption for manufacturing in case future waves of COVID-19 and/or other respiratory diseases require high levels of hospitalization in intensive care with ventilators.
The low cost of the proposed ventilator design should enable adoption of larger numbers of devices and may enable ventilation-supported care in developing nations where traditional ventilator costs are prohibitive. The outcome of the overall project will thus be highly significant for health outcomes in Canada and around the world for dealing with the current and future pandemics.
该项目旨在推进一种新颖、简单的通风机概念,从最初的概念,通过开发概念验证原型,到基于实验室的设计验证。这种通风机设计与市场上现有产品的主要区别在于,它主要是由现成的组件组装而成,几乎没有活动部件,并且成本极低(比目前大多数通风机型号便宜大约十倍)。最终设计将向公众开放,以便在未来的COVID-19和/或其他呼吸系统疾病浪潮中广泛采用,以备需要在重症监护病房中使用呼吸机进行高水平住院治疗。
项目成果
期刊论文数量(0)
专著数量(0)
科研奖励数量(0)
会议论文数量(0)
专利数量(0)
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Defoe, Jeffrey其他文献
Defoe, Jeffrey的其他文献
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{{ truncateString('Defoe, Jeffrey', 18)}}的其他基金
Rigorous Characterization, Modelling, and Mitigation of Aeroengine Response to Inlet Flow Distortion
航空发动机对进气流量畸变响应的严格表征、建模和缓解
- 批准号:
RGPIN-2015-06181 - 财政年份:2022
- 资助金额:
$ 3.64万 - 项目类别:
Discovery Grants Program - Individual
Rigorous Characterization, Modelling, and Mitigation of Aeroengine Response to Inlet Flow Distortion
航空发动机对进气流量畸变响应的严格表征、建模和缓解
- 批准号:
RGPIN-2015-06181 - 财政年份:2021
- 资助金额:
$ 3.64万 - 项目类别:
Discovery Grants Program - Individual
Rigorous Characterization, Modelling, and Mitigation of Aeroengine Response to Inlet Flow Distortion
航空发动机对进气流量畸变响应的严格表征、建模和缓解
- 批准号:
RGPIN-2015-06181 - 财政年份:2020
- 资助金额:
$ 3.64万 - 项目类别:
Discovery Grants Program - Individual
Numerical investigation of the behaviour of confined, impinging jets with assessment of advanced concepts to reduce unsteady pressure fluctuations in gas turbine testing facilities
对受限冲击射流行为进行数值研究,评估先进概念,以减少燃气轮机测试设施中的不稳定压力波动
- 批准号:
520185-2017 - 财政年份:2020
- 资助金额:
$ 3.64万 - 项目类别:
Collaborative Research and Development Grants
Numerical investigation of the behaviour of confined, impinging jets with assessment of advanced concepts to reduce unsteady pressure fluctuations in gas turbine testing facilities
对受限冲击射流行为进行数值研究,评估先进概念,以减少燃气轮机测试设施中的不稳定压力波动
- 批准号:
520185-2017 - 财政年份:2019
- 资助金额:
$ 3.64万 - 项目类别:
Collaborative Research and Development Grants
Rigorous Characterization, Modelling, and Mitigation of Aeroengine Response to Inlet Flow Distortion
航空发动机对进气流量畸变响应的严格表征、建模和缓解
- 批准号:
RGPIN-2015-06181 - 财政年份:2019
- 资助金额:
$ 3.64万 - 项目类别:
Discovery Grants Program - Individual
Rigorous Characterization, Modelling, and Mitigation of Aeroengine Response to Inlet Flow Distortion
航空发动机对进气流量畸变响应的严格表征、建模和缓解
- 批准号:
RGPIN-2015-06181 - 财政年份:2018
- 资助金额:
$ 3.64万 - 项目类别:
Discovery Grants Program - Individual
Numerical investigation of the behaviour of confined, impinging jets with assessment of advanced concepts to reduce unsteady pressure fluctuations in gas turbine testing facilities
对受限冲击射流行为进行数值研究,评估先进概念,以减少燃气轮机测试设施中的不稳定压力波动
- 批准号:
520185-2017 - 财政年份:2018
- 资助金额:
$ 3.64万 - 项目类别:
Collaborative Research and Development Grants
Rigorous Characterization, Modelling, and Mitigation of Aeroengine Response to Inlet Flow Distortion
航空发动机对进气流量畸变响应的严格表征、建模和缓解
- 批准号:
RGPIN-2015-06181 - 财政年份:2017
- 资助金额:
$ 3.64万 - 项目类别:
Discovery Grants Program - Individual
Rigorous Characterization, Modelling, and Mitigation of Aeroengine Response to Inlet Flow Distortion
航空发动机对进气流量畸变响应的严格表征、建模和缓解
- 批准号:
RGPIN-2015-06181 - 财政年份:2016
- 资助金额:
$ 3.64万 - 项目类别:
Discovery Grants Program - Individual
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