Supersonic jet-pump vacuum generators: combined experimental and numerical investigations for performance improvement
超音速喷射泵真空发生器:结合实验和数值研究以提高性能
基本信息
- 批准号:531476-2018
- 负责人:
- 金额:$ 5.05万
- 依托单位:
- 依托单位国家:加拿大
- 项目类别:Collaborative Research and Development Grants
- 财政年份:2018
- 资助国家:加拿大
- 起止时间:2018-01-01 至 2019-12-31
- 项目状态:已结题
- 来源:
- 关键词:
项目摘要
We aim to develop supersonic and large-scale jet-pumps in collaboration with our industrial Canadian partner, IVAC. This company utilizes jet-pumps for material transport related to a variety of industries, such as oil/gas, mining, and forestry. Currently, IVAC's jet-pumps face two primary issues. First, their suction mass flowrate is not optimized, which increases the pump operation cost. Second, the startup period of their operation is associated with unsteady large amplitude acoustic oscillations, which may potentially lead to fatigue and/or negatively influence the jet-pump performance.****The proposed project aims to address the above issues following both experimental and numerical investigations performed by two Master's students at the University of British Columbia (UBC). First, a one-dimensional gas-dynamics model will be developed. This model will serve as a guideline for the jet-pump design and allows for maximizing the suction flowrate. Then, following the predictions of the model, an experimental setup will be manufactured at UBC. The setup will be equipped with an array of pressure transducers and a Schlieren imaging system. A duplicate pressure measurement system will also be manufactured and integrated with the industrial IVAC system. The pressure data from both the UBC and IVAC setups will be measured, compared, and provided as input for Computational Fluid Dynamics simulations. Using these simulations and Schlieren images, unsteady dynamics of high-speed flows will be studied. Using the generated knowledge, the jet-pump design will be further modified to eliminate the negative impact of unsteady acoustics during the startup period. The newly-designed jet-pump will allow IVAC to increase the speed of material transport, which accelerates production in Canadian oil/gas, mining, and forestry industries that utilize IVAC jet-pumps.
我们的目标是与加拿大工业合作伙伴 IVAC 合作开发超音速和大型喷射泵。该公司利用喷射泵进行与石油/天然气、采矿和林业等多种行业相关的物料运输。目前,IVAC 的喷射泵面临两个主要问题。首先,它们的吸入质量流量没有得到优化,这增加了泵的运行成本。其次,其运行的启动期与不稳定的大幅声波振荡有关,这可能会导致疲劳和/或对喷射泵的性能产生负面影响。****拟议的项目旨在解决上述两个实验之后的问题以及由不列颠哥伦比亚大学 (UBC) 的两名硕士生进行的数值研究。首先,将开发一维气体动力学模型。该模型将作为喷射泵设计的指南,并允许最大化吸入流量。然后,根据模型的预测,UBC 将制造一个实验装置。该装置将配备一系列压力传感器和纹影成像系统。还将制造重复的压力测量系统并将其与工业 IVAC 系统集成。来自 UBC 和 IVAC 设置的压力数据将被测量、比较,并作为计算流体动力学模拟的输入。利用这些模拟和纹影图像,我们将研究高速流动的非定常动力学。利用生成的知识,将进一步修改喷射泵的设计,以消除启动期间不稳定声学的负面影响。新设计的喷射泵将使 IVAC 能够提高物料运输速度,从而加快使用 IVAC 喷射泵的加拿大石油/天然气、采矿和林业行业的生产。
项目成果
期刊论文数量(0)
专著数量(0)
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Kheirkhah, Sina其他文献
Contributions of flame thickening and extinctions to a heat release rate marker of intensely turbulent premixed hydrogen-enriched methane-air flames
- DOI:
10.1016/j.combustflame.2021.111481 - 发表时间:
2021-05-13 - 期刊:
- 影响因子:4.4
- 作者:
Mohammadnejad, Sajjad;An, Qiang;Kheirkhah, Sina - 通讯作者:
Kheirkhah, Sina
Kheirkhah, Sina的其他文献
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{{ truncateString('Kheirkhah, Sina', 18)}}的其他基金
Technology Development for Next Generation of Gas Turbine Engines: Turbulent Combustion Science and Thermoacoustics
下一代燃气轮机发动机技术开发:湍流燃烧科学和热声学
- 批准号:
RGPIN-2018-04554 - 财政年份:2022
- 资助金额:
$ 5.05万 - 项目类别:
Discovery Grants Program - Individual
Carbonaceous nanomaterials for improving combustion emissions of a gas turbine model combustor
用于改善燃气轮机模型燃烧室燃烧排放的碳质纳米材料
- 批准号:
567111-2021 - 财政年份:2021
- 资助金额:
$ 5.05万 - 项目类别:
Alliance Grants
Graphene-oxide doped jet-fuel combustion for aircraft propulsion: fuel burning rate estimation
用于飞机推进的氧化石墨烯掺杂喷气燃料燃烧:燃料燃烧率估算
- 批准号:
536828-2018 - 财政年份:2021
- 资助金额:
$ 5.05万 - 项目类别:
Collaborative Research and Development Grants
Technology Development for Next Generation of Gas Turbine Engines: Turbulent Combustion Science and Thermoacoustics
下一代燃气轮机发动机技术开发:湍流燃烧科学和热声学
- 批准号:
RGPIN-2018-04554 - 财政年份:2021
- 资助金额:
$ 5.05万 - 项目类别:
Discovery Grants Program - Individual
Graphene-oxide doped jet-fuel combustion for aircraft propulsion: fuel burning rate estimation
用于飞机推进的氧化石墨烯掺杂喷气燃料燃烧:燃料燃烧率估算
- 批准号:
536828-2018 - 财政年份:2020
- 资助金额:
$ 5.05万 - 项目类别:
Collaborative Research and Development Grants
Technology Development for Next Generation of Gas Turbine Engines: Turbulent Combustion Science and Thermoacoustics
下一代燃气轮机发动机技术开发:湍流燃烧科学和热声学
- 批准号:
RGPIN-2018-04554 - 财政年份:2020
- 资助金额:
$ 5.05万 - 项目类别:
Discovery Grants Program - Individual
Development of a thermally-efficient, durable, and low emission natural gas-fueled electric power generator
开发热效率高、耐用且低排放的天然气发电机
- 批准号:
525890-2018 - 财政年份:2019
- 资助金额:
$ 5.05万 - 项目类别:
Collaborative Research and Development Grants
Technology Development for Next Generation of Gas Turbine Engines: Turbulent Combustion Science and Thermoacoustics
下一代燃气轮机发动机技术开发:湍流燃烧科学和热声学
- 批准号:
RGPIN-2018-04554 - 财政年份:2019
- 资助金额:
$ 5.05万 - 项目类别:
Discovery Grants Program - Individual
Supersonic jet-pump vacuum generators: combined experimental and numerical investigations for performance improvement
超音速喷射泵真空发生器:结合实验和数值研究以提高性能
- 批准号:
531476-2018 - 财政年份:2019
- 资助金额:
$ 5.05万 - 项目类别:
Collaborative Research and Development Grants
Graphene-oxide doped jet-fuel combustion for aircraft propulsion: fuel burning rate estimation
用于飞机推进的氧化石墨烯掺杂喷气燃料燃烧:燃料燃烧率估算
- 批准号:
536828-2018 - 财政年份:2019
- 资助金额:
$ 5.05万 - 项目类别:
Collaborative Research and Development Grants
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