{"id":57803,"date":"2026-05-26T08:35:08","date_gmt":"2026-05-26T06:35:08","guid":{"rendered":"https:\/\/www.nae.fr\/2026\/05\/26\/structural-parameter-optimization-and-performance-evaluation-of-hybrid-cooling-systems-for-electric-vertical-takeoff-and-landing-aircraft-battery-modules\/"},"modified":"2026-05-26T08:35:08","modified_gmt":"2026-05-26T06:35:08","slug":"structural-parameter-optimization-and-performance-evaluation-of-hybrid-cooling-systems-for-electric-vertical-takeoff-and-landing-aircraft-battery-modules","status":"publish","type":"post","link":"https:\/\/www.nae.fr\/en\/2026\/05\/26\/structural-parameter-optimization-and-performance-evaluation-of-hybrid-cooling-systems-for-electric-vertical-takeoff-and-landing-aircraft-battery-modules\/","title":{"rendered":"Structural Parameter Optimization and Performance Evaluation of Hybrid Cooling Systems for Electric Vertical Takeoff and Landing Aircraft Battery Modules"},"content":{"rendered":"<blockquote>\n<div class=\"summary\">\n<div class=\"crayon article-chapo-51727 article__chapo\">\n\nEfficient and reliable cooling is essential for ensuring the safety and performance of battery packs in electric vertical takeoff and landing (eVTOL) aircraft. To address the limitations of existing cooling methods in cooling capability and structural integration, this study proposes a hybrid cooling system combining air cooling, high-thermal-conductivity plates (HCPs), and phase-change material (PCM). The power demand in different eVTOL flight phases is first analyzed. A single-cell simulation model is then developed and validated through experiments. The effects of three key structural parameters on system performance are investigated, and their relative importance is quantified using sensitivity analysis. A multi-objective evaluation framework is further established to compare the proposed system with no cooling, passive cooling, and liquid cooling strategies.\n\n<\/div>\n<\/div><\/blockquote>\nPour en savoir plus :\u00a0<a href=\"https:\/\/www.mdpi.com\/2313-0105\/12\/5\/170\" target=\"_blank\" rel=\"noopener\">Structural Parameter Optimization and Performance Evaluation of Hybrid Cooling Systems for Electric Vertical Takeoff and Landing Aircraft Battery Modules<\/a>","protected":false},"excerpt":{"rendered":"<p>Efficient and reliable cooling is essential for ensuring the safety and performance of battery packs in electric vertical takeoff and landing (eVTOL) aircraft. To address the limitations of existing cooling methods in cooling capability and structural integration, this study proposes a hybrid cooling system combining air cooling, high-thermal-conductivity plates (HCPs), and phase-change material (PCM). The [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":55241,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"_acf_changed":false,"footnotes":""},"categories":[20,16],"tags":[35],"class_list":["post-57803","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-actualite-aeronautique","category-rti","tag-actualites"],"acf":[],"yoast_head":"<!-- This site is optimized with the Yoast SEO plugin v27.8 - https:\/\/yoast.com\/product\/yoast-seo-wordpress\/ -->\n<title>Structural Parameter Optimization and Performance Evaluation of Hybrid Cooling Systems for Electric Vertical Takeoff and Landing Aircraft Battery Modules - NAE<\/title>\n<meta name=\"robots\" content=\"index, follow, max-snippet:-1, max-image-preview:large, max-video-preview:-1\" \/>\n<link rel=\"canonical\" href=\"https:\/\/www.nae.fr\/en\/2026\/05\/26\/structural-parameter-optimization-and-performance-evaluation-of-hybrid-cooling-systems-for-electric-vertical-takeoff-and-landing-aircraft-battery-modules\/\" \/>\n<meta property=\"og:locale\" content=\"en_US\" \/>\n<meta property=\"og:type\" content=\"article\" \/>\n<meta property=\"og:title\" content=\"Structural Parameter Optimization and Performance Evaluation of Hybrid Cooling Systems for Electric Vertical Takeoff and Landing Aircraft Battery Modules - NAE\" \/>\n<meta property=\"og:description\" content=\"Efficient and reliable cooling is essential for ensuring the safety and performance of battery packs in electric vertical takeoff and landing (eVTOL) aircraft. To address the limitations of existing cooling methods in cooling capability and structural integration, this study proposes a hybrid cooling system combining air cooling, high-thermal-conductivity plates (HCPs), and phase-change material (PCM). The [&hellip;]\" \/>\n<meta property=\"og:url\" content=\"https:\/\/www.nae.fr\/en\/2026\/05\/26\/structural-parameter-optimization-and-performance-evaluation-of-hybrid-cooling-systems-for-electric-vertical-takeoff-and-landing-aircraft-battery-modules\/\" \/>\n<meta property=\"og:site_name\" content=\"NAE\" \/>\n<meta property=\"article:published_time\" content=\"2026-05-26T06:35:08+00:00\" \/>\n<meta property=\"og:image\" content=\"https:\/\/www.nae.fr\/wp-content\/uploads\/2026\/06\/logo-mdpi.png\" \/>\n\t<meta property=\"og:image:width\" content=\"276\" \/>\n\t<meta property=\"og:image:height\" content=\"182\" \/>\n\t<meta property=\"og:image:type\" content=\"image\/png\" \/>\n<meta name=\"author\" content=\"adminwa\" \/>\n<meta name=\"twitter:card\" content=\"summary_large_image\" \/>\n<meta name=\"twitter:label1\" content=\"Written by\" \/>\n\t<meta name=\"twitter:data1\" content=\"adminwa\" \/>\n\t<meta name=\"twitter:label2\" content=\"Est. reading time\" \/>\n\t<meta name=\"twitter:data2\" content=\"1 minute\" \/>\n<script type=\"application\/ld+json\" class=\"yoast-schema-graph\">{\"@context\":\"https:\\\/\\\/schema.org\",\"@graph\":[{\"@type\":\"Article\",\"@id\":\"https:\\\/\\\/www.nae.fr\\\/2026\\\/05\\\/26\\\/structural-parameter-optimization-and-performance-evaluation-of-hybrid-cooling-systems-for-electric-vertical-takeoff-and-landing-aircraft-battery-modules\\\/#article\",\"isPartOf\":{\"@id\":\"https:\\\/\\\/www.nae.fr\\\/2026\\\/05\\\/26\\\/structural-parameter-optimization-and-performance-evaluation-of-hybrid-cooling-systems-for-electric-vertical-takeoff-and-landing-aircraft-battery-modules\\\/\"},\"author\":{\"name\":\"adminwa\",\"@id\":\"https:\\\/\\\/www.nae.fr\\\/#\\\/schema\\\/person\\\/3d658e930f01449b7195ce4a78fcfc1e\"},\"headline\":\"Structural Parameter Optimization and Performance Evaluation of Hybrid Cooling Systems for Electric Vertical Takeoff and Landing Aircraft Battery Modules\",\"datePublished\":\"2026-05-26T06:35:08+00:00\",\"mainEntityOfPage\":{\"@id\":\"https:\\\/\\\/www.nae.fr\\\/2026\\\/05\\\/26\\\/structural-parameter-optimization-and-performance-evaluation-of-hybrid-cooling-systems-for-electric-vertical-takeoff-and-landing-aircraft-battery-modules\\\/\"},\"wordCount\":160,\"commentCount\":0,\"publisher\":{\"@id\":\"https:\\\/\\\/www.nae.fr\\\/#organization\"},\"image\":{\"@id\":\"https:\\\/\\\/www.nae.fr\\\/2026\\\/05\\\/26\\\/structural-parameter-optimization-and-performance-evaluation-of-hybrid-cooling-systems-for-electric-vertical-takeoff-and-landing-aircraft-battery-modules\\\/#primaryimage\"},\"thumbnailUrl\":\"https:\\\/\\\/www.nae.fr\\\/wp-content\\\/uploads\\\/2026\\\/06\\\/logo-mdpi.png\",\"keywords\":[\"Actualit\u00e9s\"],\"articleSection\":[\"Actualit\u00e9 A\u00e9ronautique\",\"RTI\"],\"inLanguage\":\"en-US\",\"potentialAction\":[{\"@type\":\"CommentAction\",\"name\":\"Comment\",\"target\":[\"https:\\\/\\\/www.nae.fr\\\/2026\\\/05\\\/26\\\/structural-parameter-optimization-and-performance-evaluation-of-hybrid-cooling-systems-for-electric-vertical-takeoff-and-landing-aircraft-battery-modules\\\/#respond\"]}]},{\"@type\":\"WebPage\",\"@id\":\"https:\\\/\\\/www.nae.fr\\\/2026\\\/05\\\/26\\\/structural-parameter-optimization-and-performance-evaluation-of-hybrid-cooling-systems-for-electric-vertical-takeoff-and-landing-aircraft-battery-modules\\\/\",\"url\":\"https:\\\/\\\/www.nae.fr\\\/2026\\\/05\\\/26\\\/structural-parameter-optimization-and-performance-evaluation-of-hybrid-cooling-systems-for-electric-vertical-takeoff-and-landing-aircraft-battery-modules\\\/\",\"name\":\"Structural Parameter Optimization and Performance Evaluation of Hybrid Cooling Systems for Electric Vertical Takeoff and Landing Aircraft Battery Modules - 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