Aircraft seat power switching over unit mount frame

The utility model provides an aircraft seat power switching over unit mount frame, including the seat power, two stringers that are parallel to each other and be fixed in every stringer on the fixed band of two stringers, still include the mounting bracket, four edges of mounting bracket are provide...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: WANG GUOFA, YANG FENG
Format: Patent
Sprache:eng
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:The utility model provides an aircraft seat power switching over unit mount frame, including the seat power, two stringers that are parallel to each other and be fixed in every stringer on the fixed band of two stringers, still include the mounting bracket, four edges of mounting bracket are provided with mounting hole I, its through the screw pass mounting hole I close soon with the fixed band of stringer on the nut in, the mounting bracket middle part is provided with the recess that matches with the seat source phase, both ends are provided with mounting hole II respectively about the recess, in the seat power bottom entry recess, and through fixed to the mounting bracket with the seat source phase in the plastics snap -fastener insert the installation hole II. Because be provided with the recess on the mounting bracket, the seat power is fixed in inserting the recess, therefore the seat power laminates with the mounting bracket more, and fixed firmness can improve, effective simple fixing the seat power on the aircraft stringer. This aircraft seat power switching over unit mount frame is practical, high -efficient, need not not change original aircraft structure, can make things convenient for safely install the aircraft with the seat power on.