| 
                 | 
        |||||||
SPATIAL SLIDING-LINK MECHANISM OF RETRACTABLE AIRCRAFT LANDING GEAR | 
        |||||||
|---|---|---|---|---|---|---|---|
                
                
                     
                
                 Ansicht vergrößern
             | 
            
                Beschreibung
                 
                    Link 3 with wheel d turns about fixed axis 0-0 of a frame member of the aircraft. Link 1 is connected by spherical pair A to link 3 and by a sliding pair to link 2 which, in turn, is connected by spherical pair B to the frame member. When piston 1 moves into cylinder 2, link 3 is turned about axis 0-0 to retract the landing gear.  | 
        ||||||
| Verknüpfte Datensätze | |||||||
  | 
        |||||||
| Permanentlinks | |||||||
| 
                 | 
        |||||||
| Datenbereitsteller | |||||||
| 
                 | 
        |||||||
    





                