ADJUSTABLE IRON FITTING FOR THE INSTALLATION AND FITTING OF AIRCRAFT FAIRING
It is intended for installing and fitting, in conjunction with other iron fittings, a fairing on an aircraft in correspondence with a housing located at the junction of a stabiliser and a fuselage of an aircraft structure. Wherein each iron fitting comprises: a base plate (5) joined integrally to a...
Gespeichert in:
Hauptverfasser: | , |
---|---|
Format: | Patent |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
Zusammenfassung: | It is intended for installing and fitting, in conjunction with other iron fittings, a fairing on an aircraft in correspondence with a housing located at the junction of a stabiliser and a fuselage of an aircraft structure. Wherein each iron fitting comprises: a base plate (5) joined integrally to a torsion box (6) of the stabiliser (3); a mobile support (7) joined integrally to the fairing (1) and which is guided, over a linear movement, over the base plate (5); an adjustment screw (8) that is coupled into a threaded opening (15) of the base plate (5), which screw joins this base plate (5) to the mobile support (7), with the rotation of said adjustment screw (8) in combination with a retaining plate (23) dragging the respective mobile support (7) that is integral to the fairing (1). |
---|