Aircraft seat arrangement, aircraft seat, method for manufacturing aircraft seat arrangement and modular system

The invention relates to an aircraft seat arrangement (46a-c) having a multi-part backrest frame unit (10a-c), comprising at least one first side frame element (12a-c), at least one second side frame element (14a; 14b) arranged on a side of the backrest frame unit (10a-c) opposite the first side fra...

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Bibliographische Detailangaben
Hauptverfasser: JASLI, ZOLTAN, SCHREIER TIM, DRENCZAK, THOMAS
Format: Patent
Sprache:chi ; eng
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Zusammenfassung:The invention relates to an aircraft seat arrangement (46a-c) having a multi-part backrest frame unit (10a-c), comprising at least one first side frame element (12a-c), at least one second side frame element (14a; 14b) arranged on a side of the backrest frame unit (10a-c) opposite the first side frame element (12a-c); 14b), and at least one transverse frame element (16a; 16b), which is designed to be separated from the side frame elements (12a-c, 14a-c) and to connect the side frame elements (12a-c, 14a-c). 16'a; 16b, 16b; 16c) for a motor vehicle. According to the invention, the transverse frame element (16a; 16'a; 16b, 16b; 16c) is designed to be at least substantially plate-shaped. 本发明涉及一种具有多件式靠背框架单元(10a-c)的飞机座椅装置(46a-c),包括:至少一个第一侧框架元件(12a-c),至少一个布置在靠背框架单元(10a-c)的与第一侧框架元件(12a-c)相对的一侧上的第二侧框架元件(14a;14b),以及至少一个构成为与侧框架元件(12a-c,14a-c)分离并将侧框架元件(12a-c,14a-c)连接的横向框架元件(16a;16'a;16b;16c)。提出的是,横向框架元件(16a;16'a;16b;16c)构成为至少基本上板状。