{"id":6058,"date":"2023-11-21T11:13:05","date_gmt":"2023-11-21T11:13:05","guid":{"rendered":"https:\/\/www.sabaerospace.com\/subsystemy-konstrukce-satelitu\/"},"modified":"2024-02-23T17:28:22","modified_gmt":"2024-02-23T17:28:22","slug":"subsystemy-konstrukce-satelitu","status":"publish","type":"page","link":"https:\/\/www.sabaerospace.com\/cs\/subsystemy-konstrukce-satelitu\/","title":{"rendered":"Subsyst\u00e9my konstrukce satelitu"},"content":{"rendered":"

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<\/div><\/div>[vc_column_text]Stabilita konstrukce kosmick\u00e9 lodi z\u00e1vis\u00ed na subsyst\u00e9mech<\/strong> navr\u017een\u00fdch tak, aby odol\u00e1valy nam\u00e1h\u00e1n\u00ed, zat\u00ed\u017een\u00ed p\u0159i vyn\u00e1\u0161en\u00ed, letu voln\u00fdm p\u00e1dem a pohonn\u00fdm sil\u00e1m. Kosmi\u010dt\u00ed in\u017een\u00fd\u0159i se neust\u00e1le pot\u00fdkaj\u00ed s probl\u00e9mem minimalizace hmotnosti p\u0159i zachov\u00e1n\u00ed stability a zv\u00fd\u0161en\u00ed pevnosti.<\/p>\n

Spole\u010dnost SAB rovn\u011b\u017e z\u00edskala zna\u010dn\u00e9 zku\u0161enosti s \u0159e\u0161en\u00edmi pro um\u00edst\u011bn\u00ed optick\u00e9ho u\u017eite\u010dn\u00e9ho n\u00e1kladu<\/strong>. Spole\u010dnost SAB Aerospace \u0159\u00edd\u00ed cel\u00fd proces od n\u00e1vrhu mechanick\u00fdch a d\u00edl\u010d\u00edch sestav, p\u0159es v\u00fdrobu a testov\u00e1n\u00ed a\u017e po dod\u00e1n\u00ed fin\u00e1ln\u00edho kosmick\u00e9ho komponentu p\u0159ipraven\u00e9ho k integraci a vyn\u00e1\u0161en\u00ed.[\/vc_column_text]

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P\u0159esn\u00e9 obr\u00e1b\u011bn\u00ed<\/h2><\/div>
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<\/div><\/div>[vc_column_text]SAB Aerospace nab\u00edz\u00ed kapacity p\u0159esn\u00e9ho obr\u00e1b\u011bn\u00ed<\/strong> a odstra\u0148ov\u00e1n\u00ed t\u0159\u00edsek<\/strong>. Jakmile konstruk\u010dn\u00ed odd\u011blen\u00ed vytvo\u0159\u00ed n\u00e1vrhy, ode\u0161lou se do odd\u011blen\u00ed t\u0159\u00edskov\u00e9ho obr\u00e1b\u011bn\u00ed, kter\u00e9 pou\u017e\u00edv\u00e1 CAM<\/strong> software k v\u00fdvoji procesu a simulaci n\u00e1stroj\u016f a zm\u011bn n\u00e1stroj\u016f.<\/p>\n

Dokon\u010den\u00e9 n\u00e1vrhy d\u00edl\u016f jsou p\u0159evedeny do strojov\u00e9ho jazyka a hlin\u00edkov\u00fd blok je p\u0159esn\u011b obroben. Simulovan\u00e9 operace se opakuj\u00ed, aby se odstranil materi\u00e1l a vyrobil hotov\u00fd v\u00fdrobek podle v\u00fdkres\u016f.[\/vc_column_text]

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<\/div><\/div>[vc_column_text]Mezi vlastn\u00edm vybaven\u00edm a vybaven\u00edm um\u00edst\u011bn\u00fdm v partnersk\u00fdch testovac\u00edch centrech
\nspole\u010dnost SAB Aerospace m\u016f\u017ee prov\u00e1d\u011bt:[\/vc_column_text]
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    \n
  • Mechanick\u00e9 testy<\/li>\n
  • Struktur\u00e1ln\u00ed anal\u00fdza<\/li>\n
  • Tepeln\u00e1 anal\u00fdza<\/li>\n
  • Kosmick\u00e9 simula\u010dn\u00ed testy<\/li>\n
  • V\u00fdpo\u010detn\u00ed simulace<\/li>\n
  • Vibra\u010dn\u00ed a r\u00e1zov\u00e9 zkou\u0161ky<\/li>\n
  • Tepeln\u00e9 testy ve vakuu<\/li>\n
  • Zkou\u0161ky statick\u00e9 pevnosti a tuhosti<\/li>\n<\/ul>\n

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    Aditivn\u00ed v\u00fdroba<\/h2><\/div>
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    <\/div><\/div>[vc_column_text]Dal\u0161\u00ed kl\u00ed\u010dovou v\u00fdrobn\u00ed technologi\u00ed, kterou spole\u010dnost SAB Aerospace vyu\u017e\u00edv\u00e1, je aditivn\u00ed v\u00fdroba<\/strong>. Jedn\u00e1 se o technologii, kter\u00e1 zp\u016fsobila revoluci ve vysoce p\u0159esn\u00e9 v\u00fdrob\u011b.<\/p>\n

    Integrace aditivn\u00ed v\u00fdroby do na\u0161ich konstruk\u010dn\u00edch a v\u00fdrobn\u00edch proces\u016f zvy\u0161uje p\u0159esnost a efektivitu.<\/p>\n

    Aditivn\u00ed v\u00fdroba je vhodn\u00e1 zejm\u00e9na pro v\u00fdrobu p\u0159esn\u00fdch kosmick\u00fdch<\/strong> komponent\u016f<\/strong> na m\u00edru a umo\u017e\u0148uje konstruovat lehk\u00e9 a robustn\u00ed v\u00fdrobky.[\/vc_column_text]

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    Inovativn\u00ed materi\u00e1ly<\/h2><\/div>
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    <\/div><\/div>[vc_column_text]\u0158e\u0161en\u00ed jedine\u010dn\u011b slo\u017eit\u00fdch technick\u00fdch probl\u00e9m\u016f, kter\u00e9 p\u0159in\u00e1\u0161\u00ed provoz ve vesm\u00edru, vy\u017eaduje vynal\u00e9zav\u00e9 pou\u017eit\u00ed materi\u00e1l\u016f, strategick\u00e9ho designu a pokro\u010dil\u00fdch v\u00fdrobn\u00edch technik. In\u017een\u00fd\u0159i spole\u010dnosti SAB Aerospace pou\u017e\u00edvaj\u00ed lehk\u00e9 materi\u00e1ly a\u00a0pokro\u010dil\u00e9 konstruk\u010dn\u00ed techniky k optimalizaci pom\u011bru hmotnosti a pevnosti sv\u00fdch kosmick\u00fdch komponent.<\/p>\n

    n\u017een\u00fd\u0159i spole\u010dnosti SAB Aerospace z\u00edskali hlubok\u00e9 zku\u0161enosti s materi\u00e1ly, jako jsou\u00a0hlin\u00edk<\/strong>\u00a0a\u00a0plasty vyztu\u017een\u00e9 uhl\u00edkov\u00fdmi vl\u00e1kny<\/strong>. Tyto zku\u0161enosti byly p\u0159\u00ednosem pro programy optick\u00e9ho u\u017eite\u010dn\u00e9ho n\u00e1kladu, na kter\u00fdch se spole\u010dnost pod\u00edlela, jako je\u00a0OPSIS<\/strong>\u00a0(Optick\u00fd syst\u00e9m pro sn\u00edmkov\u00e1n\u00ed a sledov\u00e1n\u00ed),\u00a0METIS<\/strong>\u00a0(Solar Orbiter Instrument) a\u00a0EUCLID<\/strong>\u00a0v r\u00e1mci ESA.[\/vc_column_text][\/vc_column_inner][\/vc_row_inner]

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    N\u00e1vrh a modelov\u00e1n\u00ed<\/h2><\/div>
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    <\/div><\/div>[vc_column_text]Simulovan\u00e9 modely se pou\u017e\u00edvaj\u00ed k anal\u00fdze mechanick\u00fdch deformac\u00ed v d\u016fsledku teplotn\u00edch zm\u011bn na ob\u011b\u017en\u00e9 dr\u00e1ze. Proces modelov\u00e1n\u00ed umo\u017e\u0148uje spole\u010dnosti definovat limity a zahrnout do sv\u00fdch n\u00e1vrh\u016f odpov\u00eddaj\u00edc\u00ed tolerance. In\u017een\u00fd\u0159i spole\u010dnosti SAB Aerospace pou\u017e\u00edvaj\u00ed softwarov\u00e9 programy ke kontrole tuhosti, pevnosti a dodr\u017eov\u00e1n\u00ed po\u017eadavk\u016f na stabilitu.<\/p>\n

    Spole\u010dnost pou\u017e\u00edv\u00e1 MsC<\/strong>, NASTRAN<\/strong> (CAE n\u00e1stroj\/\u0159e\u0161i\u010d), HyperMesh<\/strong> (CAE\/FEM pre- a post-processing) a Optistruct<\/strong> (struktur\u00e1ln\u00ed optimalizace a anal\u00fdza). Ve\u0161ker\u00e9 konstruk\u010dn\u00ed \u010dinnosti spole\u010dnosti jsou zalo\u017eeny na 3D po\u010d\u00edta\u010dov\u011b podporovan\u00e9m konstruk\u010dn\u00edm softwaru, jako je Unigraphics NX<\/strong>.<\/p>\n

    Proces modelov\u00e1n\u00ed umo\u017e\u0148uje spole\u010dnosti SAB Aerospace plnit nejn\u00e1ro\u010dn\u011bj\u0161\u00ed po\u017eadavky vesm\u00edrn\u00fdch program\u016f. K n\u011bkter\u00fdm in\u017een\u00fdrsk\u00fdm \u00fasp\u011bch\u016fm spole\u010dnosti pat\u0159\u00ed \u00fa\u010dast na v\u00fdvoji mechanick\u00e9 konstrukce\u00a0Galileo FOC<\/strong>,\u00a0ExoMars 2015\u00a0<\/strong>a\u00a0EDRS-C<\/strong>\u00a0ve spolupr\u00e1ci s OHB System AG.[\/vc_column_text][\/vc_column_inner][\/vc_row_inner]

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    [vc_row full_width=“stretch_row“ css_animation=“zoomIn“][vc_column][vc_column_text]Stabilita konstrukce kosmick\u00e9 lodi z\u00e1vis\u00ed na subsyst\u00e9mech navr\u017een\u00fdch tak, aby odol\u00e1valy nam\u00e1h\u00e1n\u00ed, zat\u00ed\u017een\u00ed p\u0159i vyn\u00e1\u0161en\u00ed, letu voln\u00fdm p\u00e1dem a pohonn\u00fdm sil\u00e1m. Kosmi\u010dt\u00ed in\u017een\u00fd\u0159i se neust\u00e1le pot\u00fdkaj\u00ed s probl\u00e9mem minimalizace hmotnosti p\u0159i zachov\u00e1n\u00ed stability a zv\u00fd\u0161en\u00ed pevnosti. Spole\u010dnost SAB rovn\u011b\u017e z\u00edskala zna\u010dn\u00e9 zku\u0161enosti s \u0159e\u0161en\u00edmi pro um\u00edst\u011bn\u00ed optick\u00e9ho u\u017eite\u010dn\u00e9ho n\u00e1kladu. Spole\u010dnost SAB Aerospace \u0159\u00edd\u00ed […]<\/p>\n","protected":false},"author":1,"featured_media":0,"parent":0,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":{"footnotes":""},"class_list":["post-6058","page","type-page","status-publish","hentry","no-thumb"],"yoast_head":"\nSubsyst\u00e9my konstrukce satelitu - Sab Aerospace<\/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.sabaerospace.com\/cs\/subsystemy-konstrukce-satelitu\/\" \/>\n<meta property=\"og:locale\" content=\"cs_CZ\" \/>\n<meta property=\"og:type\" content=\"article\" \/>\n<meta property=\"og:title\" content=\"Subsyst\u00e9my konstrukce satelitu - Sab Aerospace\" \/>\n<meta property=\"og:description\" content=\"[vc_row full_width=“stretch_row“ css_animation=“zoomIn“][vc_column][vc_column_text]Stabilita konstrukce kosmick\u00e9 lodi z\u00e1vis\u00ed na subsyst\u00e9mech navr\u017een\u00fdch tak, aby odol\u00e1valy nam\u00e1h\u00e1n\u00ed, zat\u00ed\u017een\u00ed p\u0159i vyn\u00e1\u0161en\u00ed, letu voln\u00fdm p\u00e1dem a pohonn\u00fdm sil\u00e1m. 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