{"id":118,"date":"2026-03-19T10:54:22","date_gmt":"2026-03-19T02:54:22","guid":{"rendered":"http:\/\/www.envsin-testchamber.com\/?p=118"},"modified":"2026-05-24T09:22:28","modified_gmt":"2026-05-24T01:22:28","slug":"aerospace-avionics","status":"publish","type":"post","link":"https:\/\/www.envsin-testchamber.com\/pl\/aerospace-avionics\/","title":{"rendered":"Lotnictwo i kosmonautyka"},"content":{"rendered":"<p><span style=\"font-family: arial, helvetica, sans-serif;\">Produkty lotnicze maj\u0105 ekstremalne wymagania dotycz\u0105ce niezawodno\u015bci. Od \u015brodowisk o wysokiej temperaturze i wilgotno\u015bci na ziemi do \u015brodowisk o niskiej temperaturze i niskim ci\u015bnieniu na du\u017cych wysoko\u015bciach, od intensywnych wibracji podczas startu i l\u0105dowania do ekstremalnych r\u00f3\u017cnic temperatur w przestrzeni kosmicznej, lotniczy sprz\u0119t elektroniczny musi utrzymywa\u0107 precyzyjne dzia\u0142anie w r\u00f3\u017cnych trudnych warunkach.<\/span><\/p>\n<p><span style=\"font-family: arial, helvetica, sans-serif;\">Ten plan testowania zosta\u0142 zaprojektowany w celu spe\u0142nienia specjalnych wymaga\u0144 produkt\u00f3w lotniczych i zapewnia us\u0142ugi testowania niezawodno\u015bci, kt\u00f3re s\u0105 zgodne z normami wojskowymi i lotniczymi. System testowy ma szeroki zakres temperatur, mo\u017cliwo\u015b\u0107 szybkiej zmiany temperatury i funkcj\u0119 symulacji niskiego ci\u015bnienia, co mo\u017ce spe\u0142ni\u0107 wymagania testowe r\u00f3\u017cnych lotniczych urz\u0105dze\u0144 elektronicznych, system\u00f3w pok\u0142adowych i materia\u0142\u00f3w lotniczych.<\/span><\/p>\n<p>&nbsp;<\/p>\n<p><span style=\"font-family: arial, helvetica, sans-serif;\">Obowi\u0105zuj\u0105ce normy:<\/span><br \/>\n<span style=\"font-family: arial, helvetica, sans-serif;\">MIL-STD-810<\/span><br \/>\n<span style=\"font-family: arial, helvetica, sans-serif;\">GJB 150<\/span><br \/>\n<span style=\"font-family: arial, helvetica, sans-serif;\">DO-160<\/span><br \/>\n<span style=\"font-family: arial, helvetica, sans-serif;\">RTCA\/DO-160<\/span><\/p>\n<p>&nbsp;<\/p>\n<p><span style=\"font-family: arial, helvetica, sans-serif;\">Projekt testowy:<\/span><br \/>\n<span style=\"font-family: arial, helvetica, sans-serif;\">1. Testy dzia\u0142ania i przechowywania w wysokich i niskich temperaturach 2. Gwa\u0142towna zmiana temperatury i testy szoku termicznego 3. Testy symulacyjne niskiego ci\u015bnienia i wysoko\u015bci 4. Testy korozyjne w wilgotnym cieple i mgle solnej 5. Kompleksowe testy wibracji i wstrz\u0105s\u00f3w<\/span><\/p>\n<p>&nbsp;<\/p>\n<p><span style=\"font-family: arial, helvetica, sans-serif;\">Typowe zastosowania:<\/span><br \/>\n<span style=\"font-family: arial, helvetica, sans-serif;\">1. Lotniczy sprz\u0119t elektroniczny i instrumenty 2. Lotnicze systemy radarowe i komunikacyjne 3. Materia\u0142y lotnicze i elementy konstrukcyjne 4. Systemy i komponenty bezza\u0142ogowych statk\u00f3w powietrznych<\/span><\/p>","protected":false},"excerpt":{"rendered":"<p>Aerospace products have extreme requirements for reliability. From high temperature and high humidity environments on the ground to low temperature and low pressure environments at high altitudes, from intense vibrations during takeoff and landing to extreme temperature differences in space, aviation electronic equipment needs to maintain precise operation under various harsh conditions. This testing plan [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":119,"comment_status":"closed","ping_status":"closed","sticky":false,"template":"","format":"standard","meta":{"_acf_changed":false,"footnotes":""},"categories":[13],"tags":[],"class_list":["post-118","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-application"],"acf":[],"_links":{"self":[{"href":"https:\/\/www.envsin-testchamber.com\/pl\/wp-json\/wp\/v2\/posts\/118","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/www.envsin-testchamber.com\/pl\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/www.envsin-testchamber.com\/pl\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/www.envsin-testchamber.com\/pl\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/www.envsin-testchamber.com\/pl\/wp-json\/wp\/v2\/comments?post=118"}],"version-history":[{"count":2,"href":"https:\/\/www.envsin-testchamber.com\/pl\/wp-json\/wp\/v2\/posts\/118\/revisions"}],"predecessor-version":[{"id":1039,"href":"https:\/\/www.envsin-testchamber.com\/pl\/wp-json\/wp\/v2\/posts\/118\/revisions\/1039"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/www.envsin-testchamber.com\/pl\/wp-json\/wp\/v2\/media\/119"}],"wp:attachment":[{"href":"https:\/\/www.envsin-testchamber.com\/pl\/wp-json\/wp\/v2\/media?parent=118"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/www.envsin-testchamber.com\/pl\/wp-json\/wp\/v2\/categories?post=118"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/www.envsin-testchamber.com\/pl\/wp-json\/wp\/v2\/tags?post=118"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}