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
基本信息
- 批准号:RGPIN-2015-06181
- 负责人:
- 金额:$ 1.6万
- 依托单位:
- 依托单位国家:加拿大
- 项目类别:Discovery Grants Program - Individual
- 财政年份:2017
- 资助国家:加拿大
- 起止时间:2017-01-01 至 2018-12-31
- 项目状态:已结题
- 来源:
- 关键词:
项目摘要
This proposal aims to improve the sustainability of aviation by addressing challenges to realizing commercial aircraft with advanced, embedded propulsion systems. Embedded propulsion systems use jet engines integrated into the fuselage of the aircraft rather than hung from the wings. In such a configuration, fuel consumption could be reduced by up to 4%. This corresponds to a possible annual savings of up to $238 million for Canadian airlines alone. Worldwide, use of embedded propulsion systems could reduce carbon dioxide emissions by up to 28 million tonnes annually.
该提案旨在通过应对实现具有先进嵌入式推进系统的商用飞机的挑战来提高航空的可持续性。嵌入式推进系统使用集成在飞机机身中的喷气发动机,而不是悬挂在机翼上。在这样的配置中,燃料消耗可以减少高达4%。这相当于仅加拿大航空公司每年可能节省2.38亿加元。在全球范围内,使用嵌入式推进系统每年可以减少多达2800万吨的二氧化碳排放量。
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:
$ 1.6万 - 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:
$ 1.6万 - 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:
$ 1.6万 - 项目类别:
Discovery Grants Program - Individual
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
- 批准号:
555180-2020 - 财政年份:2020
- 资助金额:
$ 1.6万 - 项目类别:
Alliance 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:2020
- 资助金额:
$ 1.6万 - 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:
$ 1.6万 - 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:
$ 1.6万 - 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:
$ 1.6万 - 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:
$ 1.6万 - 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:2016
- 资助金额:
$ 1.6万 - 项目类别:
Discovery Grants Program - Individual
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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:
$ 1.6万 - 项目类别:
Discovery Grants Program - Individual