مشخصات مقاله | |
ترجمه عنوان مقاله | ایجاد امکان توان خروجی فوق العاده بالا ژنراتورهای الکتریکی ترموآکوستیک هیبریدی با محل جک گازی |
عنوان انگلیسی مقاله | Post-positioned gas spring enables ultra-high output power of hybrid thermoacoustic electric generators |
نشریه | الزویر |
انتشار | مقاله سال 2024 |
تعداد صفحات مقاله انگلیسی | 9 صفحه |
هزینه | دانلود مقاله انگلیسی رایگان میباشد. |
نوع نگارش مقاله |
مقاله کوتاه (Short Communication) |
مقاله بیس | این مقاله بیس نمیباشد |
نمایه (index) | Scopus – Master Journal List – JCR – DOAJ |
نوع مقاله | ISI |
فرمت مقاله انگلیسی | |
ایمپکت فاکتور(IF) |
7.673 در سال 2022 |
شاخص H_index | 49 در سال 2024 |
شاخص SJR | 2.446 در سال 2022 |
شناسه ISSN | 2666-3864 |
شاخص Quartile (چارک) | Q1 در سال 2022 |
فرضیه | ندارد |
مدل مفهومی | ندارد |
پرسشنامه | ندارد |
متغیر | ندارد |
رفرنس | دارد |
رشته های مرتبط | برق |
گرایش های مرتبط | برق قدرت – ماشینهای الکتریکی |
نوع ارائه مقاله |
ژورنال |
مجله | Cell Reports Physical Science – گزارشات علوم فیزیکی مجله Cell |
دانشگاه | Chinese Academy of Sciences, China |
شناسه دیجیتال – doi |
https://doi.org/10.1016/j.xcrp.2024.101835 |
لینک سایت مرجع | https://www.sciencedirect.com/science/article/pii/S2666386424000602 |
کد محصول | e17712 |
وضعیت ترجمه مقاله | ترجمه آماده این مقاله موجود نمیباشد. میتوانید از طریق دکمه پایین سفارش دهید. |
دانلود رایگان مقاله | دانلود رایگان مقاله انگلیسی |
سفارش ترجمه این مقاله | سفارش ترجمه این مقاله |
فهرست مطالب مقاله: |
Summary Introduction Results and discussion Experimental procedures Acknowledgments Supplemental information References |
بخشی از متن مقاله: |
Summary High-capacity hybrid thermoacoustic electric generators (HTAEGs) are ideal in different small- and micro-scale energy systems, especially in space nuclear power systems. In this work, an HTAEG with a post-positioned gas spring is proposed. To demonstrate the superiority of the gas-spring-post-positioned design on high-capacity HTAEGs, an HTAEG prototype is modeled, built, and tested from the perspective of thermoacoustics accordingly. Experimental results demonstrate an output electric power of 15.0 kW. Furthermore, it could achieve the highest efficiency of 39.2% with an output electric power of 11.1 kW. Given that a 15-kW power output is an ultra-high level on a single-piston HTAEG of this type to date, and the achieved efficiency on the prototype is also encouraging, this work marks an important milestone in the development of high-capacity HTAEGs. It also demonstrates that the gas-spring-post-positioned design has significant advantages and enormous potential for application.
Introduction The thermoacoustic electric generator (TAEG) emerges as a promising dynamic conversion technology due to its exceptional reliability, extremely long lifespan, versatility in heat source utilization, and high intrinsic efficiency.1 These attributes render it particularly well suited for space and submarine thermoelectric applications.2,3 Within the TAEG family, a hybrid one (traditionally called the free-piston Stirling engine,4 currently recognized as a generalized thermoacoustic engine5) that incorporates a solid mass to tune the internal acoustic field transcends the conventional gas-tuning systems in the aspects of power density and thermal-to-electrical efficiency.6
Most recently, dramatic progress, e.g., 16-year non-stop operation and over 39% thermal-to-electrical efficiency,7 has stoked up the enthusiasm for the hybrid thermoacoustic electric generator (HTAEG) in space application. However, the current achievements are all confined in a rather small power level (i.e., around 100 W), not sufficient to cover various application scenarios. Scaling up to tens of kilowatt power while maintaining high reliability simultaneously is formidably challenging, and so far, there is no public literature reported on it. The main obstacle is the spring force mechanism that is imperative to tune the acoustic field. For low- and medium-power HTAEGs (ranging from tens of watts to kilowatts), planar springs are commonly employed as the spring force mechanism for their excellent compactness and radial rigidity.8 These planar springs can be positioned either at the bounce space or compression space, resulting in two distinct designs for HTAEG. Meanwhile, both designs have been extensively utilized in numerous HTAEG prototypes, with their reliability well demonstrated through ground tests.7
Results and discussion System configuration and numerical study |