Minghua Wang , Liuyong Chang , Xuehuan Hu , Meiyin Zhu , Bin Zhang , Guangze Li , Zheng Xu
{"title":"颗粒损耗调查以及航空 nvPM 测量方法在宽粒度范围内的适用性","authors":"Minghua Wang , Liuyong Chang , Xuehuan Hu , Meiyin Zhu , Bin Zhang , Guangze Li , Zheng Xu","doi":"10.1016/j.partic.2024.09.012","DOIUrl":null,"url":null,"abstract":"<div><div>The precise measurement of non-volatile Particulate Matter (nvPM) is outlined in aviation engine emissions regulations by the International Civil Aviation Organization (ICAO). However, assessing particle losses in the sampling and transfer unit presents challenges, raising concerns about the system's reliability. Moreover, nvPM emissions from small and medium aircraft engines, with thrust not exceeding 26.7 kN, vary widely in size, adding complexity to the measurement process. To provide a comprehensive analysis of particle losses in the sampling and transfer subsystems, this study established a test bench equipped with a nanoparticle generator. The generator simulates nvPM emissions from medium and small aircraft engines and can consistently produce nvPMs with a wide range of concentrations (10³-10⁷/cm³) and size distributions (20–160 nm). Thermophoretic loss verification experiments were conducted within the sampling pipeline under significant temperature differences, investigating the effects of particle size, temperature gradient, and airflow rate on thermophoretic particle losses. The experimental results demonstrated good agreement with the predictions of the model proposed by United Technologies Research Centre (UTRC). After correcting for temperature, the experimental data showed a maximum disparity of 2% under typical engine exhaust conditions, validating the predictability of the thermophoretic loss model for various engine types. Furthermore, verification experiments for particle diffusion and bending losses were performed. Comparative analysis with the UTRC model revealed nvPM inertial deposition under laminar flow conditions with low Reynolds numbers (Re). As the Re increased, the measured data more closely aligned with the simulations. Bending losses due to secondary flow patterns ranged from 1% to 10%, depending on particle size and flow rate. This finding supports the applicability of aviation nvPM measurement methods across a wide particle size range. This research provides theoretical support for future nvPM measurements on various aircraft engines, laying the groundwork for improved accuracy and reliability in emissions monitoring.</div></div>","PeriodicalId":401,"journal":{"name":"Particuology","volume":"95 ","pages":"Pages 154-165"},"PeriodicalIF":4.1000,"publicationDate":"2024-09-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Investigation on the particle loss and applicability of aviation nvPM measurement methodology for wide particle size ranges\",\"authors\":\"Minghua Wang , Liuyong Chang , Xuehuan Hu , Meiyin Zhu , Bin Zhang , Guangze Li , Zheng Xu\",\"doi\":\"10.1016/j.partic.2024.09.012\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>The precise measurement of non-volatile Particulate Matter (nvPM) is outlined in aviation engine emissions regulations by the International Civil Aviation Organization (ICAO). However, assessing particle losses in the sampling and transfer unit presents challenges, raising concerns about the system's reliability. Moreover, nvPM emissions from small and medium aircraft engines, with thrust not exceeding 26.7 kN, vary widely in size, adding complexity to the measurement process. To provide a comprehensive analysis of particle losses in the sampling and transfer subsystems, this study established a test bench equipped with a nanoparticle generator. The generator simulates nvPM emissions from medium and small aircraft engines and can consistently produce nvPMs with a wide range of concentrations (10³-10⁷/cm³) and size distributions (20–160 nm). Thermophoretic loss verification experiments were conducted within the sampling pipeline under significant temperature differences, investigating the effects of particle size, temperature gradient, and airflow rate on thermophoretic particle losses. The experimental results demonstrated good agreement with the predictions of the model proposed by United Technologies Research Centre (UTRC). After correcting for temperature, the experimental data showed a maximum disparity of 2% under typical engine exhaust conditions, validating the predictability of the thermophoretic loss model for various engine types. Furthermore, verification experiments for particle diffusion and bending losses were performed. Comparative analysis with the UTRC model revealed nvPM inertial deposition under laminar flow conditions with low Reynolds numbers (Re). As the Re increased, the measured data more closely aligned with the simulations. Bending losses due to secondary flow patterns ranged from 1% to 10%, depending on particle size and flow rate. This finding supports the applicability of aviation nvPM measurement methods across a wide particle size range. This research provides theoretical support for future nvPM measurements on various aircraft engines, laying the groundwork for improved accuracy and reliability in emissions monitoring.</div></div>\",\"PeriodicalId\":401,\"journal\":{\"name\":\"Particuology\",\"volume\":\"95 \",\"pages\":\"Pages 154-165\"},\"PeriodicalIF\":4.1000,\"publicationDate\":\"2024-09-28\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Particuology\",\"FirstCategoryId\":\"88\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S167420012400186X\",\"RegionNum\":2,\"RegionCategory\":\"材料科学\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q2\",\"JCRName\":\"ENGINEERING, CHEMICAL\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Particuology","FirstCategoryId":"88","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S167420012400186X","RegionNum":2,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ENGINEERING, CHEMICAL","Score":null,"Total":0}
Investigation on the particle loss and applicability of aviation nvPM measurement methodology for wide particle size ranges
The precise measurement of non-volatile Particulate Matter (nvPM) is outlined in aviation engine emissions regulations by the International Civil Aviation Organization (ICAO). However, assessing particle losses in the sampling and transfer unit presents challenges, raising concerns about the system's reliability. Moreover, nvPM emissions from small and medium aircraft engines, with thrust not exceeding 26.7 kN, vary widely in size, adding complexity to the measurement process. To provide a comprehensive analysis of particle losses in the sampling and transfer subsystems, this study established a test bench equipped with a nanoparticle generator. The generator simulates nvPM emissions from medium and small aircraft engines and can consistently produce nvPMs with a wide range of concentrations (10³-10⁷/cm³) and size distributions (20–160 nm). Thermophoretic loss verification experiments were conducted within the sampling pipeline under significant temperature differences, investigating the effects of particle size, temperature gradient, and airflow rate on thermophoretic particle losses. The experimental results demonstrated good agreement with the predictions of the model proposed by United Technologies Research Centre (UTRC). After correcting for temperature, the experimental data showed a maximum disparity of 2% under typical engine exhaust conditions, validating the predictability of the thermophoretic loss model for various engine types. Furthermore, verification experiments for particle diffusion and bending losses were performed. Comparative analysis with the UTRC model revealed nvPM inertial deposition under laminar flow conditions with low Reynolds numbers (Re). As the Re increased, the measured data more closely aligned with the simulations. Bending losses due to secondary flow patterns ranged from 1% to 10%, depending on particle size and flow rate. This finding supports the applicability of aviation nvPM measurement methods across a wide particle size range. This research provides theoretical support for future nvPM measurements on various aircraft engines, laying the groundwork for improved accuracy and reliability in emissions monitoring.
期刊介绍:
The word ‘particuology’ was coined to parallel the discipline for the science and technology of particles.
Particuology is an interdisciplinary journal that publishes frontier research articles and critical reviews on the discovery, formulation and engineering of particulate materials, processes and systems. It especially welcomes contributions utilising advanced theoretical, modelling and measurement methods to enable the discovery and creation of new particulate materials, and the manufacturing of functional particulate-based products, such as sensors.
Papers are handled by Thematic Editors who oversee contributions from specific subject fields. These fields are classified into: Particle Synthesis and Modification; Particle Characterization and Measurement; Granular Systems and Bulk Solids Technology; Fluidization and Particle-Fluid Systems; Aerosols; and Applications of Particle Technology.
Key topics concerning the creation and processing of particulates include:
-Modelling and simulation of particle formation, collective behaviour of particles and systems for particle production over a broad spectrum of length scales
-Mining of experimental data for particle synthesis and surface properties to facilitate the creation of new materials and processes
-Particle design and preparation including controlled response and sensing functionalities in formation, delivery systems and biological systems, etc.
-Experimental and computational methods for visualization and analysis of particulate system.
These topics are broadly relevant to the production of materials, pharmaceuticals and food, and to the conversion of energy resources to fuels and protection of the environment.