{"id":4843,"date":"2017-06-06T11:37:25","date_gmt":"2017-06-06T09:37:25","guid":{"rendered":"http:\/\/www.elleaing.com\/?page_id=4843"},"modified":"2020-09-25T15:21:53","modified_gmt":"2020-09-25T13:21:53","slug":"case-history-aerospace","status":"publish","type":"page","link":"https:\/\/www.elleaing.com\/en\/case-history-aerospace\/","title":{"rendered":"Case History Aerospace"},"content":{"rendered":"<p>[vc_row css_animation=&#8221;&#8221; row_type=&#8221;row&#8221; use_row_as_full_screen_section=&#8221;no&#8221; type=&#8221;full_width&#8221; angled_section=&#8221;no&#8221; text_align=&#8221;left&#8221; background_image_as_pattern=&#8221;without_pattern&#8221; css=&#8221;.vc_custom_1498142751590{margin-top: 50px !important;margin-bottom: 50px !important;}&#8221;][vc_column][vc_column_text]<\/p>\n<h5 style=\"text-align: center;\">The current ELLEA personnel took part in the following programs, preserving the related expertise and know how<\/h5>\n<p>[\/vc_column_text][\/vc_column][\/vc_row][vc_row css_animation=&#8221;&#8221; row_type=&#8221;row&#8221; use_row_as_full_screen_section=&#8221;no&#8221; type=&#8221;full_width&#8221; angled_section=&#8221;no&#8221; text_align=&#8221;left&#8221; background_image_as_pattern=&#8221;without_pattern&#8221; el_class=&#8221;casehistory-item&#8221;][vc_column width=&#8221;1\/2&#8243; el_class=&#8221;history-text&#8221;][vc_column_text]<\/p>\n<h3>EUROFIGHTER<\/h3>\n<h4>Design and Stress<\/h4>\n<p>Design and structural analysis of the Wing Pylons[\/vc_column_text][\/vc_column][vc_column width=&#8221;1\/2&#8243; css=&#8221;.vc_custom_1498487279282{background-image: url(https:\/\/www.elleaing.com\/wp-content\/uploads\/2017\/06\/eurofigther-typhoon-RAF.jpg?id=5175) !important;background-position: center !important;background-repeat: no-repeat !important;background-size: cover !important;}&#8221; el_id=&#8221;eurofighter&#8221; el_class=&#8221;history-image&#8221;][\/vc_column][\/vc_row][vc_row css_animation=&#8221;&#8221; row_type=&#8221;row&#8221; use_row_as_full_screen_section=&#8221;no&#8221; type=&#8221;full_width&#8221; angled_section=&#8221;no&#8221; text_align=&#8221;left&#8221; background_image_as_pattern=&#8221;without_pattern&#8221; el_class=&#8221;casehistory-item&#8221;][vc_column width=&#8221;1\/2&#8243; el_id=&#8221;aermacchi&#8221; css=&#8221;.vc_custom_1498487293294{background-image: url(https:\/\/www.elleaing.com\/wp-content\/uploads\/2017\/06\/aermacchi_m346.jpg?id=5178) !important;background-position: center !important;background-repeat: no-repeat !important;background-size: cover !important;}&#8221; el_class=&#8221;history-image&#8221;][\/vc_column][vc_column width=&#8221;1\/2&#8243; css=&#8221;.vc_custom_1498489377227{background-position: center !important;background-repeat: no-repeat !important;background-size: contain !important;}&#8221; el_class=&#8221;history-text&#8221;][vc_column_text]<\/p>\n<h3 class=\"normal flush\">AERMACCHI M346<\/h3>\n<h4 class=\"normal flush\">Design and Stress<\/h4>\n<p>FWD Fuselage: structural design, FEM development, check stress, hand calculation, reports on:<\/p>\n<ul>\n<li>Canopy<\/li>\n<li>Cabin Frames and Canted Frames<\/li>\n<li>Composite Lateral Panels<\/li>\n<li>Flight Control System<\/li>\n<li>Flight Deck Instrumentation Installation<\/li>\n<li>Radome<\/li>\n<li>Leading Edge<\/li>\n<\/ul>\n<p>&nbsp;<\/p>\n<p>Full Scale Static and Fatigue Test for flight certification<\/p>\n<p>Development of test intallations for:<\/p>\n<ul>\n<li>Leading Edge<\/li>\n<li>Flap<\/li>\n<li>Aileron<\/li>\n<li>Vertical Tail<\/li>\n<li>Fixed Leading Edge and Probe<\/li>\n<\/ul>\n<p>[\/vc_column_text][\/vc_column][\/vc_row][vc_row css_animation=&#8221;&#8221; row_type=&#8221;row&#8221; use_row_as_full_screen_section=&#8221;no&#8221; type=&#8221;full_width&#8221; angled_section=&#8221;no&#8221; text_align=&#8221;left&#8221; background_image_as_pattern=&#8221;without_pattern&#8221; el_class=&#8221;casehistory-item&#8221;][vc_column width=&#8221;1\/2&#8243; el_class=&#8221;history-text&#8221;][vc_column_text]<\/p>\n<h3 class=\"normal flush\">BOEING 787 Dreamliner<\/h3>\n<h4 class=\"normal flush\">Stress<\/h4>\n<p>Involved from PDR, CDR to flight test.<br \/>\nFE modelling and analysis of:<\/p>\n<ul>\n<li>Door Uplock Mechanism<\/li>\n<li>Landing Gear Uplock<\/li>\n<li>Section 44 and joints, realized in CFC and Titanium<\/li>\n<\/ul>\n<p>[\/vc_column_text][\/vc_column][vc_column width=&#8221;1\/2&#8243; css=&#8221;.vc_custom_1498487312161{background-image: url(https:\/\/www.elleaing.com\/wp-content\/uploads\/2017\/06\/boing-787.png?id=5180) !important;background-position: center !important;background-repeat: no-repeat !important;background-size: cover !important;}&#8221; el_id=&#8221;boeingdreamer&#8221; el_class=&#8221;history-image&#8221;][\/vc_column][\/vc_row][vc_row css_animation=&#8221;&#8221; row_type=&#8221;row&#8221; use_row_as_full_screen_section=&#8221;no&#8221; type=&#8221;full_width&#8221; angled_section=&#8221;no&#8221; text_align=&#8221;left&#8221; background_image_as_pattern=&#8221;without_pattern&#8221; el_class=&#8221;casehistory-item&#8221;][vc_column width=&#8221;1\/2&#8243; css=&#8221;.vc_custom_1498487322923{background-image: url(https:\/\/www.elleaing.com\/wp-content\/uploads\/2017\/06\/Bombardier-C-Series-100-300.jpg?id=5183) !important;background-position: center !important;background-repeat: no-repeat !important;background-size: cover !important;}&#8221; el_id=&#8221;borbandier&#8221; el_class=&#8221;history-image&#8221;][\/vc_column][vc_column width=&#8221;1\/2&#8243; css=&#8221;.vc_custom_1498489389618{background-position: center !important;background-repeat: no-repeat !important;background-size: contain !important;}&#8221; el_class=&#8221;history-text&#8221;][vc_column_text]<\/p>\n<h3 class=\"normal flush\">Bombardier C-Series 100 &amp; 300<\/h3>\n<h4 class=\"normal flush\">Stress<\/h4>\n<p>Involved in JDP and DDP.<br \/>\nFE modelling and analysis and hand calculation on:<\/p>\n<ul>\n<li>Wing to Body Fairing (metallic and composite)<\/li>\n<li>Mid Fuselage Circumferential Joints (Static &amp; Fatigue)<\/li>\n<li>Crease Beam (Static &amp; Fatigue)<\/li>\n<\/ul>\n<p>[\/vc_column_text][\/vc_column][\/vc_row][vc_row css_animation=&#8221;&#8221; row_type=&#8221;row&#8221; use_row_as_full_screen_section=&#8221;no&#8221; type=&#8221;full_width&#8221; angled_section=&#8221;no&#8221; text_align=&#8221;left&#8221; background_image_as_pattern=&#8221;without_pattern&#8221; el_class=&#8221;casehistory-item&#8221;][vc_column width=&#8221;1\/2&#8243; el_class=&#8221;history-text&#8221;][vc_column_text]<\/p>\n<h3 class=\"normal flush\">Airbus A380-800<\/h3>\n<h4>Stress<\/h4>\n<p>&nbsp;<\/p>\n<p style=\"text-align: justify;\"><strong>Pax Floor Main Deck (frames 38 to 50):<\/strong><\/p>\n<p style=\"text-align: justify;\">design, static and fatigue analysis, manufacturing drawings of floor beams, rails, crash links and trolley lift attachment, design of the support structures for aircraft equipments.<\/p>\n<p style=\"text-align: justify;\"><strong>Cargo Floor Main Deck (frames 38 to 45):<\/strong><\/p>\n<p style=\"text-align: justify;\">design, static and fatigue analysis, manufacturing drawings (cargo beam, main structures), design of the floor handling and transportation devices.<\/p>\n<p style=\"text-align: justify;\"><strong>Engine Nacelle (Rolls-Royce Trent 900 and General Electric GP7200 engines):<\/strong><\/p>\n<p style=\"text-align: justify;\">flight readiness and certification analysis (static, fatigue, optimizations) and reports.<\/p>\n<figure class=\"attachment attachment--image png attachment--preview\" data-attachment=\"\" data-caption=\"5.png\" data-preview-url=\"https:\/\/preview.3.basecamp.com\/3776662\/blobs\/95cec80a74131eeb68bdb1e4b9eee6ac0010\/previews\/full\/5.png\" data-download-url=\"https:\/\/3.basecamp.com\/3776662\/blobs\/95cec80a74131eeb68bdb1e4b9eee6ac0010\/download\/5.png?attachment=true\" data-size=\"180127\" data-content-type=\"image\/png\">\n<div class=\"attachment__frame attachment__hideable\"><\/div>\n<\/figure>\n<p>[\/vc_column_text][\/vc_column][vc_column width=&#8221;1\/2&#8243; css=&#8221;.vc_custom_1498487332447{background-image: url(https:\/\/www.elleaing.com\/wp-content\/uploads\/2017\/06\/Airbus-A380-800_1.jpg?id=5185) !important;background-position: center !important;background-repeat: no-repeat !important;background-size: cover !important;}&#8221; el_id=&#8221;airbus1&#8243; el_class=&#8221;history-image&#8221;][\/vc_column][\/vc_row][vc_row css_animation=&#8221;&#8221; row_type=&#8221;row&#8221; use_row_as_full_screen_section=&#8221;no&#8221; type=&#8221;full_width&#8221; angled_section=&#8221;no&#8221; text_align=&#8221;left&#8221; background_image_as_pattern=&#8221;without_pattern&#8221; el_class=&#8221;casehistory-item&#8221;][vc_column width=&#8221;1\/2&#8243; css=&#8221;.vc_custom_1501776209443{background-image: url(https:\/\/www.elleaing.com\/wp-content\/uploads\/2017\/06\/Airbus-A380-800-F.jpg?id=5965) !important;background-position: center !important;background-repeat: no-repeat !important;background-size: cover !important;}&#8221; el_id=&#8221;aiubus2&#8243; el_class=&#8221;history-image&#8221;][\/vc_column][vc_column width=&#8221;1\/2&#8243; css=&#8221;.vc_custom_1498489400680{background-position: center !important;background-repeat: no-repeat !important;background-size: contain !important;}&#8221; el_class=&#8221;history-text&#8221;][vc_column_text]<\/p>\n<h3 class=\"normal flush\">Airbus A380-800 F<\/h3>\n<h4 class=\"normal flush\">Design &amp; Stress<\/h4>\n<p>&nbsp;<\/p>\n<p style=\"text-align: justify;\">Design and stress analysis of the Upper and Main Deck Cargo Doors.<\/p>\n<ul>\n<li style=\"text-align: justify;\">Design (3d CAD, drawings, VPM integration), certification, reports, MRB and concessions.<\/li>\n<li style=\"text-align: justify;\">FEM modelling (GFEM and DFEM); FE structural analysis; detailed analysis of the door-fuselage interfaces; static, fatigue and damage tolerance reports.<\/li>\n<\/ul>\n<p>[\/vc_column_text][\/vc_column][\/vc_row][vc_row css_animation=&#8221;&#8221; row_type=&#8221;row&#8221; use_row_as_full_screen_section=&#8221;no&#8221; type=&#8221;full_width&#8221; angled_section=&#8221;no&#8221; text_align=&#8221;left&#8221; background_image_as_pattern=&#8221;without_pattern&#8221; el_class=&#8221;casehistory-item&#8221;][vc_column width=&#8221;1\/2&#8243; el_class=&#8221;history-text&#8221;][vc_column_text css=&#8221;.vc_custom_1601039751546{padding-top: 50px !important;padding-bottom: 50px !important;padding-left: 50px !important;}&#8221;]<\/p>\n<h3 class=\"normal flush\">Learjet 85<\/h3>\n<h4 class=\"normal flush\">Stress<\/h4>\n<p class=\"normal flush\">FE modelling and analysis on:<\/p>\n<ul>\n<li>Aft Pressure Bulkhead<\/li>\n<li>Avionic Pressure Floor<\/li>\n<li>Keel Beam<\/li>\n<li>Aft Frame<\/li>\n<li>Cabin Floor Frames<\/li>\n<li>EGRESS Provisions<\/li>\n<li>Fuselage Skin CFC Monolithic &amp; Core;<\/li>\n<\/ul>\n<p>[\/vc_column_text][\/vc_column][vc_column width=&#8221;1\/2&#8243; css=&#8221;.vc_custom_1498487356945{background-image: url(https:\/\/www.elleaing.com\/wp-content\/uploads\/2017\/06\/Learjet-85.jpg?id=5189) !important;background-position: center !important;background-repeat: no-repeat !important;background-size: cover !important;}&#8221; el_id=&#8221;learjet&#8221; el_class=&#8221;history-image&#8221;][\/vc_column][\/vc_row][vc_row css_animation=&#8221;&#8221; row_type=&#8221;row&#8221; use_row_as_full_screen_section=&#8221;no&#8221; type=&#8221;full_width&#8221; angled_section=&#8221;no&#8221; text_align=&#8221;left&#8221; background_image_as_pattern=&#8221;without_pattern&#8221; el_class=&#8221;casehistory-item&#8221;][vc_column width=&#8221;1\/2&#8243; css=&#8221;.vc_custom_1498487368369{background-image: url(https:\/\/www.elleaing.com\/wp-content\/uploads\/2017\/06\/Airbus-A350-XWB.jpg?id=5190) !important;background-position: center !important;background-repeat: no-repeat !important;background-size: cover !important;}&#8221; el_id=&#8221;aiubusa&#8221; el_class=&#8221;history-image&#8221;][\/vc_column][vc_column width=&#8221;1\/2&#8243; css=&#8221;.vc_custom_1498489411362{background-position: center !important;background-repeat: no-repeat !important;background-size: contain !important;}&#8221; el_class=&#8221;history-text&#8221;][vc_column_text css=&#8221;.vc_custom_1601039759337{padding-top: 0px !important;padding-bottom: 50px !important;padding-left: 50px !important;}&#8221;]<\/p>\n<h3 class=\"normal flush\">Airbus A350 XWB<\/h3>\n<h4 class=\"normal flush\">Stress<\/h4>\n<p>Airbus A350 XWB-900 (MSN001 to MSN005):<\/p>\n<ul>\n<li>Pylon Load Transfer Bracket: development of a software for stress check and weight reduction, residual strength analysis<\/li>\n<li>Track Cans and Funk Plates: DFEM, load definition, stress check and weight reduction<\/li>\n<li>Fixed leadin edge: residual strength analysis<\/li>\n<li>Fuselage (Section 15): FEM validation and check stress<\/li>\n<li>Wing: production support (concession)<\/li>\n<\/ul>\n<p>&nbsp;<\/p>\n<p>Airbus A350 XWB-1000:<\/p>\n<ul>\n<li>Fixed Leading edge: metallic ribs and composite panel sizing (B-Maturity)<\/li>\n<li>Rear Spar (Inboard &amp; Outboard Splice Joints, Fuel Quantity Indicator, Flap Tracks 3 &amp; 4)<\/li>\n<li>FE modelling (IFEM), validation, FE static analysis, hand calculation, reporting<\/li>\n<\/ul>\n<p>[\/vc_column_text][\/vc_column][\/vc_row][vc_row css_animation=&#8221;&#8221; row_type=&#8221;row&#8221; use_row_as_full_screen_section=&#8221;no&#8221; type=&#8221;full_width&#8221; angled_section=&#8221;no&#8221; text_align=&#8221;left&#8221; background_image_as_pattern=&#8221;without_pattern&#8221; el_class=&#8221;casehistory-item&#8221;][vc_column width=&#8221;1\/2&#8243; el_class=&#8221;history-text&#8221;][vc_column_text css=&#8221;.vc_custom_1601039769685{padding-top: 50px !important;padding-bottom: 50px !important;padding-left: 50px !important;}&#8221;]<\/p>\n<h3 class=\"normal flush\">MPCV Service Module<\/h3>\n<h4 class=\"normal flush\">Stress<\/h4>\n<ul>\n<li class=\"normal flush\">GFEM modification<\/li>\n<li class=\"normal flush\">Shear Panel FEM validation and test correlation<\/li>\n<li class=\"normal flush\">Mass saving study<\/li>\n<li class=\"normal flush\">FE analyses and feasibility studies on Auxiliary Thrust Support, Fuel Tank Support, Engine Support.<\/li>\n<\/ul>\n<p>[\/vc_column_text][\/vc_column][vc_column width=&#8221;1\/2&#8243; css=&#8221;.vc_custom_1498487378988{background-image: url(https:\/\/www.elleaing.com\/wp-content\/uploads\/2017\/06\/MPCV-Service-Module_2.jpg?id=5191) !important;background-position: center !important;background-repeat: no-repeat !important;background-size: cover !important;}&#8221; el_id=&#8221;mpcv&#8221; el_class=&#8221;history-image&#8221;][\/vc_column][\/vc_row][vc_row css_animation=&#8221;&#8221; row_type=&#8221;row&#8221; use_row_as_full_screen_section=&#8221;no&#8221; type=&#8221;full_width&#8221; angled_section=&#8221;no&#8221; text_align=&#8221;left&#8221; background_image_as_pattern=&#8221;without_pattern&#8221; el_class=&#8221;casehistory-item&#8221;][vc_column width=&#8221;1\/2&#8243; css=&#8221;.vc_custom_1536779084074{background-image: url(https:\/\/www.elleaing.com\/wp-content\/uploads\/2017\/06\/1_augusta_westland_aw169-1.jpg?id=6153) !important;background-position: center !important;background-repeat: no-repeat !important;background-size: cover !important;}&#8221; el_class=&#8221;history-image&#8221;][\/vc_column][vc_column width=&#8221;1\/2&#8243; el_class=&#8221;history-text&#8221;][vc_column_text css=&#8221;.vc_custom_1601039778195{padding-top: 50px !important;padding-bottom: 50px !important;padding-left: 50px !important;}&#8221;]<\/p>\n<h3 class=\"normal flush\">AGUSTA WESTLAND AW169<\/h3>\n<h4 class=\"normal flush\">Stress<\/h4>\n<p>Fixed Flight Controls \u2013 Certification of the improved collective design<\/p>\n<ul>\n<li>Multibody analysis; modelling, analyses set up and run, load extraction<\/li>\n<li>FE Analysis for static and fatigue evaluation: models preparation, analyses set up and run, post-processing<\/li>\n<li>Hand calculations for static and fatigue<\/li>\n<li>Certification analysis reports (static and fatigue)<\/li>\n<li>Full scale test for flight certification: preparation of test report for the static and operational tests<\/li>\n<\/ul>\n<p>[\/vc_column_text][\/vc_column][\/vc_row][vc_row css_animation=&#8221;&#8221; row_type=&#8221;row&#8221; use_row_as_full_screen_section=&#8221;no&#8221; type=&#8221;full_width&#8221; angled_section=&#8221;no&#8221; text_align=&#8221;left&#8221; background_image_as_pattern=&#8221;without_pattern&#8221; el_class=&#8221;casehistory-item&#8221;][vc_column width=&#8221;1\/2&#8243; el_class=&#8221;history-text&#8221;][vc_column_text css=&#8221;.vc_custom_1601039787935{padding-top: 50px !important;padding-bottom: 50px !important;padding-left: 50px !important;}&#8221;]<\/p>\n<h3 class=\"normal flush\">AGUSTA WESTLAND AW609<\/h3>\n<h4 class=\"normal flush\">Stress<\/h4>\n<p>Fixed Flight Controls<\/p>\n<ul>\n<li>Static analysis of the cyclic controls: FE models preparation, analyses set up and run, post-processing; hand calculations; certification report<\/li>\n<li>Full scale test for flight certification: preparation of test proposals for the static, operational and shear joints tests<\/li>\n<\/ul>\n<p>&nbsp;<\/p>\n<p>Cockpit &amp; Windshield \u2013 Bird Strike Simulation<\/p>\n<ul>\n<li>FE model check and modifications<\/li>\n<li>DFEM models preparation and integration into the GFEM<\/li>\n<li>Explicit analyses set-up and run<\/li>\n<li>Test\/Analysis correlation<\/li>\n<li>Analysis post-processing<\/li>\n<\/ul>\n<p>&nbsp;<\/p>\n<p>Fuel Tank \u2013 Drop Test<\/p>\n<ul>\n<li>FE model preparation<\/li>\n<li>Explicit analysis set-up and run<\/li>\n<li>Results post-processing<\/li>\n<\/ul>\n<p>[\/vc_column_text][\/vc_column][vc_column width=&#8221;1\/2&#8243; css=&#8221;.vc_custom_1536779105878{background-image: url(https:\/\/www.elleaing.com\/wp-content\/uploads\/2017\/06\/2_augusta_westland_aw609-1.jpg?id=6152) !important;background-position: center !important;background-repeat: no-repeat !important;background-size: cover !important;}&#8221; el_class=&#8221;history-image&#8221;][\/vc_column][\/vc_row][vc_row css_animation=&#8221;&#8221; row_type=&#8221;row&#8221; use_row_as_full_screen_section=&#8221;no&#8221; type=&#8221;full_width&#8221; angled_section=&#8221;no&#8221; text_align=&#8221;left&#8221; background_image_as_pattern=&#8221;without_pattern&#8221; el_class=&#8221;casehistory-item&#8221;][vc_column width=&#8221;1\/2&#8243; css=&#8221;.vc_custom_1536520181794{background-image: url(https:\/\/www.elleaing.com\/wp-content\/uploads\/2017\/06\/3_augusta_westland_aw249.jpg?id=6146) !important;background-position: center !important;background-repeat: no-repeat !important;background-size: cover !important;}&#8221; el_class=&#8221;history-image&#8221;][\/vc_column][vc_column width=&#8221;1\/2&#8243; el_class=&#8221;history-text&#8221;][vc_column_text css=&#8221;.vc_custom_1601039799570{padding-top: 50px !important;padding-bottom: 50px !important;padding-left: 50px !important;}&#8221;]<\/p>\n<h3 class=\"normal flush\">AGUSTA WESTLAND AW249<\/h3>\n<h4 class=\"normal flush\">Design &amp; Stress<\/h4>\n<p>Structural Design of the Forward Fuselage Primary Structure<\/p>\n<ul>\n<li>Nose Structure<\/li>\n<li>Under-Floor<\/li>\n<li>Upper Deck<\/li>\n<\/ul>\n<p>&nbsp;<\/p>\n<p>Multibody analysis of the Fixed Flight Controls: modelling, analyses set-up, post-processing<\/p>\n<p>&nbsp;<\/p>\n<p>Note: Work in progress at Ellea Ingegneria \u2013 Torino[\/vc_column_text][\/vc_column][\/vc_row][vc_row css_animation=&#8221;&#8221; row_type=&#8221;row&#8221; use_row_as_full_screen_section=&#8221;no&#8221; type=&#8221;full_width&#8221; angled_section=&#8221;no&#8221; text_align=&#8221;left&#8221; background_image_as_pattern=&#8221;without_pattern&#8221; el_class=&#8221;casehistory-item&#8221;][vc_column width=&#8221;1\/2&#8243; el_class=&#8221;history-text&#8221;][vc_column_text css=&#8221;.vc_custom_1601039807415{padding-top: 50px !important;padding-bottom: 50px !important;padding-left: 50px !important;}&#8221;]<\/p>\n<h3 class=\"normal flush\">AERMACCHI M345<\/h3>\n<h4 class=\"normal flush\">Design &amp; Stress<\/h4>\n<p>Forward Fuselage<\/p>\n<ul>\n<li>Structural Design<\/li>\n<li>FE analysis post-processing<\/li>\n<li>Hand calculations<\/li>\n<li>Report<\/li>\n<\/ul>\n<p>&nbsp;<\/p>\n<p>Note: Work in progress at Leonardo Velivoli \u2013 Venegono[\/vc_column_text][\/vc_column][vc_column width=&#8221;1\/2&#8243; css=&#8221;.vc_custom_1536520257945{background-image: url(https:\/\/www.elleaing.com\/wp-content\/uploads\/2017\/06\/4_aermacchi_m345.jpg?id=6147) !important;background-position: center !important;background-repeat: no-repeat !important;background-size: cover !important;}&#8221; el_class=&#8221;history-image&#8221;][\/vc_column][\/vc_row]<\/p>\n","protected":false},"excerpt":{"rendered":"<p>[vc_row css_animation=&#8221;&#8221; 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