{"id":270,"date":"2019-07-03T20:19:26","date_gmt":"2019-07-03T18:19:26","guid":{"rendered":"http:\/\/swift-online.de.via.a.srvmk.de\/en\/2019\/07\/03\/flugzeug\/"},"modified":"2019-08-29T10:57:11","modified_gmt":"2019-08-29T08:57:11","slug":"aircraft","status":"publish","type":"post","link":"https:\/\/swift-online.de\/en\/aircraft\/","title":{"rendered":"Aircraft"},"content":{"rendered":"\n<h3 class=\"wp-block-heading\">Typical Applications<\/h3>\n\n\n\n<ul class=\"wp-block-list\"><li>Check load assumptions for front and main landing gear<\/li><li>Check of load assumption for wings and structure of aircraft in special missions (display of target)<\/li><li>Check of strain and moment<\/li><li>Life time monitoring power plant and structure to adapt inspection intervals, to increase system safety and to extend lifetime<\/li><li>Check load assumptions for front and main landing gear, taileron loads at particular load cases<\/li><li>Bending and torsion moments, oil temperature<\/li><li>Analysis of increased propeller vibration loads at cross wind<\/li><li>Load assumption checks for aircrafts on special missions (instruction) <\/li><\/ul>\n\n\n\n<p>Over a period of approximately 6 months, between scheduled air services, the loads in the aircraft body and front and main landing gear were continuously monitored. Of particular interest were the loads at take-off and landing for subsequent comparison with specific fracture tests. The SQTMS evaluation method is ideal for such a monitoring, allowing a Rainflow to be created off-line. Further examples of suitable items to be subjected to monitoring are the wings, tail, internal cabin pressure and miscellaneous displays. With propeller-driven aircraft increased propeller loads due to crosswinds can be analysed \u2013 both on the ground and in the air. <\/p>\n","protected":false},"excerpt":{"rendered":"<p>Typical Applications Check load assumptions for front and main landing gear Check of load assumption for wings and structure of aircraft in special missions (display of target) Check of strain and moment Life time monitoring power plant and structure to adapt inspection intervals, to increase system &hellip; <\/p>\n<p><a href=\"https:\/\/swift-online.de\/en\/aircraft\/\" class=\"more-link\"><span class=\"morelink-icon\">Read more<\/span><\/a><\/p>\n","protected":false},"author":2,"featured_media":145,"comment_status":"closed","ping_status":"closed","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[10],"tags":[],"class_list":["post-270","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-micro-ii"],"aioseo_notices":[],"_links":{"self":[{"href":"https:\/\/swift-online.de\/en\/wp-json\/wp\/v2\/posts\/270","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/swift-online.de\/en\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/swift-online.de\/en\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/swift-online.de\/en\/wp-json\/wp\/v2\/users\/2"}],"replies":[{"embeddable":true,"href":"https:\/\/swift-online.de\/en\/wp-json\/wp\/v2\/comments?post=270"}],"version-history":[{"count":2,"href":"https:\/\/swift-online.de\/en\/wp-json\/wp\/v2\/posts\/270\/revisions"}],"predecessor-version":[{"id":406,"href":"https:\/\/swift-online.de\/en\/wp-json\/wp\/v2\/posts\/270\/revisions\/406"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/swift-online.de\/en\/wp-json\/wp\/v2\/media\/145"}],"wp:attachment":[{"href":"https:\/\/swift-online.de\/en\/wp-json\/wp\/v2\/media?parent=270"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/swift-online.de\/en\/wp-json\/wp\/v2\/categories?post=270"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/swift-online.de\/en\/wp-json\/wp\/v2\/tags?post=270"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}