{"id":582,"date":"2023-11-22T19:02:58","date_gmt":"2023-11-22T18:02:58","guid":{"rendered":"https:\/\/gearupmech.com\/efficiency-selflocking\/"},"modified":"2024-06-22T11:28:37","modified_gmt":"2024-06-22T10:28:37","slug":"efficiency-selflocking","status":"publish","type":"post","link":"https:\/\/gearupmech.com\/en\/efficiency-selflocking\/","title":{"rendered":"DIPROVEL: \u201cTechnology Demonstrator of an Aeronautical Hybrid Propulsion System for Light Aircraft Applications\u201d"},"content":{"rendered":"\t\t<div data-elementor-type=\"wp-post\" data-elementor-id=\"582\" class=\"elementor elementor-582 elementor-189\" data-elementor-post-type=\"post\">\n\t\t\t\t<div class=\"elementor-element elementor-element-3eb54eb e-flex e-con-boxed e-con e-parent\" data-id=\"3eb54eb\" data-element_type=\"container\">\n\t\t\t\t\t<div class=\"e-con-inner\">\n\t\t\t\t<div class=\"elementor-element elementor-element-057741e elementor-widget elementor-widget-text-editor\" data-id=\"057741e\" data-element_type=\"widget\" data-widget_type=\"text-editor.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t\t\t<p><strong>Partner<\/strong>: CMD, CIRA, UMBRA CUSCINETTI, VGA.<\/p>\n<p><strong>GearUp s.r.l. technical collaboration activities<\/strong><\/p>\n\t\t\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-68eb985 elementor-widget elementor-widget-text-editor\" data-id=\"68eb985\" data-element_type=\"widget\" data-widget_type=\"text-editor.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t\t\t<p>GearUp s.r.l. provided technical consultancy under the PON &#8211; DIPROVEL project &#8220;<em>Technology Demonstrator of an Aeronautical Hybrid Propulsion System for Light Aircraft Applications<\/em>&#8221; for the design of the parallel hybrid system for aeronautical applications (Cessna 337 aircraft) having a maximum power of 135 kW.<\/p>\n\t\t\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-e4b7d83 elementor-widget elementor-widget-image\" data-id=\"e4b7d83\" data-element_type=\"widget\" data-widget_type=\"image.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t<a href=\"https:\/\/gearupmech.com\/wp-content\/uploads\/2023\/11\/aereo.png\" data-elementor-open-lightbox=\"yes\" data-elementor-lightbox-title=\"aereo\" data-e-action-hash=\"#elementor-action%3Aaction%3Dlightbox%26settings%3DeyJpZCI6NzM1LCJ1cmwiOiJodHRwczpcL1wvZ2VhcnVwbWVjaC5jb21cL3dwLWNvbnRlbnRcL3VwbG9hZHNcLzIwMjNcLzExXC9hZXJlby5wbmcifQ%3D%3D\">\n\t\t\t\t\t\t\t<img fetchpriority=\"high\" decoding=\"async\" width=\"886\" height=\"498\" src=\"https:\/\/gearupmech.com\/wp-content\/uploads\/2023\/11\/aereo.png\" class=\"attachment-large size-large wp-image-735\" alt=\"\" srcset=\"https:\/\/gearupmech.com\/wp-content\/uploads\/2023\/11\/aereo.png 886w, https:\/\/gearupmech.com\/wp-content\/uploads\/2023\/11\/aereo-300x169.png 300w, https:\/\/gearupmech.com\/wp-content\/uploads\/2023\/11\/aereo-768x432.png 768w\" sizes=\"(max-width: 886px) 100vw, 886px\" \/>\t\t\t\t\t\t\t\t<\/a>\n\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-ff17a8d elementor-widget elementor-widget-text-editor\" data-id=\"ff17a8d\" data-element_type=\"widget\" data-widget_type=\"text-editor.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t\t\t<p>The hybrid powertrain consists of an SI internal combustion engine (CMD22), a permanent magnet synchronous electric machine (EMRAX 268 LV) controlled by a DC\/AC power converter (GVI Parker) and powered by a LiIon battery pack (composed of KOKAM cells).<\/p>\n<p>Specifically, it has been developed by GearUp Ltd:<\/p>\n<ul>\n<li>The mechanical coupling between heat engine and electric machine (by one-way bearing) <strong>Figure 1<\/strong>;<\/li>\n<li>The control strategies of the hybrid powertrain. This is based on the minimization theory of a Hemiltonian potential called &#8220;Equivalent Consumption and Minimization Strategy&#8221; (ECMS). The control strategy was implemented in a development control unit (FPGA) and tested in the laboratory in Real Time (RT) <strong>Figure 2<\/strong>.<\/li>\n<\/ul>\n\t\t\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-dd79b29 elementor-widget elementor-widget-image\" data-id=\"dd79b29\" data-element_type=\"widget\" data-widget_type=\"image.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t<a href=\"https:\/\/gearupmech.com\/wp-content\/uploads\/2023\/11\/propulsore-ibrido-aeronautico.png\" data-elementor-open-lightbox=\"yes\" data-elementor-lightbox-title=\"propulsore ibrido aeronautico\" data-e-action-hash=\"#elementor-action%3Aaction%3Dlightbox%26settings%3DeyJpZCI6NzM3LCJ1cmwiOiJodHRwczpcL1wvZ2VhcnVwbWVjaC5jb21cL3dwLWNvbnRlbnRcL3VwbG9hZHNcLzIwMjNcLzExXC9wcm9wdWxzb3JlLWlicmlkby1hZXJvbmF1dGljby5wbmcifQ%3D%3D\">\n\t\t\t\t\t\t\t<img decoding=\"async\" width=\"635\" height=\"467\" src=\"https:\/\/gearupmech.com\/wp-content\/uploads\/2023\/11\/propulsore-ibrido-aeronautico.png\" class=\"attachment-large size-large wp-image-737\" alt=\"\" srcset=\"https:\/\/gearupmech.com\/wp-content\/uploads\/2023\/11\/propulsore-ibrido-aeronautico.png 635w, https:\/\/gearupmech.com\/wp-content\/uploads\/2023\/11\/propulsore-ibrido-aeronautico-300x221.png 300w\" sizes=\"(max-width: 635px) 100vw, 635px\" \/>\t\t\t\t\t\t\t\t<\/a>\n\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-06d23ea elementor-widget elementor-widget-text-editor\" data-id=\"06d23ea\" data-element_type=\"widget\" data-widget_type=\"text-editor.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t\t\t<p><strong><em>Figure 1. CMD 22 and EMRAX 268 LV aeronautical hybrid engine.<\/em><\/strong><\/p>\n\t\t\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-332d5bd elementor-widget elementor-widget-text-editor\" data-id=\"332d5bd\" data-element_type=\"widget\" data-widget_type=\"text-editor.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t\t\t<p>The prototype has been made and tested in the laboratory at the University of Naples Federico II.<\/p>\n\t\t\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-64b69fa elementor-widget elementor-widget-image\" data-id=\"64b69fa\" data-element_type=\"widget\" data-widget_type=\"image.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t<a href=\"https:\/\/gearupmech.com\/wp-content\/uploads\/2023\/11\/modello-matematico-del-propulsore-ibrido-aeronautico-scaled-e1704340713125.jpg\" data-elementor-open-lightbox=\"yes\" data-elementor-lightbox-title=\"modello matematico del propulsore ibrido aeronautico\" data-e-action-hash=\"#elementor-action%3Aaction%3Dlightbox%26settings%3DeyJpZCI6NzQwLCJ1cmwiOiJodHRwczpcL1wvZ2VhcnVwbWVjaC5jb21cL3dwLWNvbnRlbnRcL3VwbG9hZHNcLzIwMjNcLzExXC9tb2RlbGxvLW1hdGVtYXRpY28tZGVsLXByb3B1bHNvcmUtaWJyaWRvLWFlcm9uYXV0aWNvLXNjYWxlZC1lMTcwNDM0MDcxMzEyNS5qcGcifQ%3D%3D\">\n\t\t\t\t\t\t\t<img decoding=\"async\" width=\"1024\" height=\"288\" src=\"https:\/\/gearupmech.com\/wp-content\/uploads\/2023\/11\/modello-matematico-del-propulsore-ibrido-aeronautico-1024x288.jpg\" class=\"attachment-large size-large wp-image-740\" alt=\"\" srcset=\"https:\/\/gearupmech.com\/wp-content\/uploads\/2023\/11\/modello-matematico-del-propulsore-ibrido-aeronautico-1024x288.jpg 1024w, https:\/\/gearupmech.com\/wp-content\/uploads\/2023\/11\/modello-matematico-del-propulsore-ibrido-aeronautico-300x84.jpg 300w, https:\/\/gearupmech.com\/wp-content\/uploads\/2023\/11\/modello-matematico-del-propulsore-ibrido-aeronautico-768x216.jpg 768w, https:\/\/gearupmech.com\/wp-content\/uploads\/2023\/11\/modello-matematico-del-propulsore-ibrido-aeronautico-1536x432.jpg 1536w, https:\/\/gearupmech.com\/wp-content\/uploads\/2023\/11\/modello-matematico-del-propulsore-ibrido-aeronautico-2048x576.jpg 2048w\" sizes=\"(max-width: 1024px) 100vw, 1024px\" \/>\t\t\t\t\t\t\t\t<\/a>\n\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-909720f elementor-widget elementor-widget-text-editor\" data-id=\"909720f\" data-element_type=\"widget\" data-widget_type=\"text-editor.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t\t\t<p><strong><em>Figure 2. Mathematical model of the Aeronautical hybrid engine created in Matlab\/Simulink.<\/em><\/strong><\/p>\n\t\t\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-6552190 elementor-widget elementor-widget-text-editor\" data-id=\"6552190\" data-element_type=\"widget\" data-widget_type=\"text-editor.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\t\t\t\t<p>Tests conducted in the laboratory confirm the numerical predictions simulated through a model built in Matlab\/Simulink in <strong>Figure 2<\/strong>. The results show that the hybrid propulsion system made for aviation applications can contribute in terms of reducing carbon dioxide <sub>CO2<\/sub> emissions and thus reducing overall fuel consumption in both &#8220;<em>plug-in<\/em>&#8221; configuration by about 30 percent and &#8220;<em>full-hybrid<\/em>&#8221; by 6 percent, while maintaining overall performance. The primary technological limitation of this aviation application is the high specific weight and volume of Li-ion batteries.<\/p>\n<p><strong>Publications<\/strong><\/p>\n<ul>\n<li>Fornaro, E. MANAGEMENT STRATEGIES FOR AIRCRAFT HYBRID PRUPULSION SYSTEM AND EXPERIMENTAL ASSESMENT. PhD Thesis, (2023) University of Naples Federico II. URL: <a href=\"http:\/\/www.fedoatd.unina.it\/id\/eprint\/1439\" target=\"_blank\" rel=\"noopener\">http:\/\/www.fedoatd.unina.it\/id\/eprint\/1439<\/a>.<\/li>\n<li>Fornaro, E., Cardone, M., &amp; Dannier, A. (2022). A Comparative Assessment of Hybrid Parallel, Series, and Full-Electric Propulsion Systems for Aircraft Application. <em>IEEE Access<\/em>, <em>10<\/em>, 28808-28820.<\/li>\n<li>Fornaro, E., Cardone, M., &amp; Dannier, A. (2022, June). Hybrid Electric Aircraft Model Based on ECMS Control. In <em>2022 International Symposium on Power Electronics, Electrical Drives, Automation and Motion (SPEEDAM)<\/em>(pp. 865-870).<\/li>\n<li>Fornaro, E., &amp; Tordela, C. (2023). <em>An Energy Management Strategy for Aeronautical Hybrid Propulsion Systems Based on an MPC Supervisor<\/em>(No. 2023-24-0026). SAE Technical Paper.<\/li>\n<\/ul>\n\t\t\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t","protected":false},"excerpt":{"rendered":"<p>Partner: CMD, CIRA, UMBRA CUSCINETTI, VGA. GearUp s.r.l. technical collaboration activities GearUp s.r.l. provided technical consultancy under the PON &#8211; DIPROVEL project &#8220;Technology Demonstrator of an Aeronautical Hybrid Propulsion System for Light Aircraft Applications&#8221; for the design of the parallel hybrid system for aeronautical applications (Cessna 337 aircraft) having a maximum power of 135 kW. [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":735,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"site-sidebar-layout":"default","site-content-layout":"","ast-site-content-layout":"default","site-content-style":"default","site-sidebar-style":"default","ast-global-header-display":"","ast-banner-title-visibility":"","ast-main-header-display":"","ast-hfb-above-header-display":"","ast-hfb-below-header-display":"","ast-hfb-mobile-header-display":"","site-post-title":"","ast-breadcrumbs-content":"","ast-featured-img":"","footer-sml-layout":"","theme-transparent-header-meta":"","adv-header-id-meta":"","stick-header-meta":"","header-above-stick-meta":"","header-main-stick-meta":"","header-below-stick-meta":"","astra-migrate-meta-layouts":"default","ast-page-background-enabled":"default","ast-page-background-meta":{"desktop":{"background-color":"var(--ast-global-color-4)","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-opacity":"","overlay-gradient":""},"tablet":{"background-color":"","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-opacity":"","overlay-gradient":""},"mobile":{"background-color":"","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-opacity":"","overlay-gradient":""}},"ast-content-background-meta":{"desktop":{"background-color":"var(--ast-global-color-5)","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-opacity":"","overlay-gradient":""},"tablet":{"background-color":"var(--ast-global-color-5)","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-opacity":"","overlay-gradient":""},"mobile":{"background-color":"var(--ast-global-color-5)","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-opacity":"","overlay-gradient":""}},"footnotes":""},"categories":[1],"tags":[],"class_list":["post-582","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-non-categorizzato"],"_links":{"self":[{"href":"https:\/\/gearupmech.com\/en\/wp-json\/wp\/v2\/posts\/582","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/gearupmech.com\/en\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/gearupmech.com\/en\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/gearupmech.com\/en\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/gearupmech.com\/en\/wp-json\/wp\/v2\/comments?post=582"}],"version-history":[{"count":16,"href":"https:\/\/gearupmech.com\/en\/wp-json\/wp\/v2\/posts\/582\/revisions"}],"predecessor-version":[{"id":1346,"href":"https:\/\/gearupmech.com\/en\/wp-json\/wp\/v2\/posts\/582\/revisions\/1346"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/gearupmech.com\/en\/wp-json\/wp\/v2\/media\/735"}],"wp:attachment":[{"href":"https:\/\/gearupmech.com\/en\/wp-json\/wp\/v2\/media?parent=582"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/gearupmech.com\/en\/wp-json\/wp\/v2\/categories?post=582"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/gearupmech.com\/en\/wp-json\/wp\/v2\/tags?post=582"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}