A mounting system for an aircraft fuselage (10) includes one or more fixed anchors (20) attached to the fuselage (10). A plurality of vertically adjustable anchors (30) are likewise attached to the fuselage (10), wherein each vertically adjustable anchor (30) includes a spinwheel (50) on a threaded shaft (60). An adapter plate (40) is attached to the fixed anchors (20) and the adjustable anchors (30), wherein a contact surface of the spinwheel (50) directly engages with the adapter plate (40).
RADOME MOUNTING SYSTEM
RADOMMONTAGESYSTEM
SYSTÈME DE MONTAGE DE RADÔME
2025-02-05
Patent
Electronic Resource
English
BEHIND THE RADOME MOUNTING SYSTEM FOR AIRCRAFT AVIONICS EQUIPMENT
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