Vibration Isolation System

An aircraft, comprising:

• a fuselage comprising an inner wall and an outer wall;
• an interior cabin defined by an interior wall comprising an inner surface facing the cabin and an outer surface facing the inner wall of the fuselage;
• a cavity between the inner wall of the fuselage and the outer surface of the interior wall of the cabin;
• and
• a plurality of vibration isolators disposed in the cavity, each of the vibration isolators being attached between the inner wall of the fuselage and the outer surface of the interior wall of the cabin, and each of the vibration isolators comprising:
• a first isolator attached to the inner wall of the fuselage;
• a second isolator attached to the outer surface of the interior wall of the cabin;
• and
• an intermediate mass attached between the first isolator and the second isolator.

An aircraft, comprising:

• a fuselage comprising an inner wall and an outer wall;
• an interior cabin defined by a cabin wall comprising an inner surface facing the cabin and an outer surface facing the inner wall of the fuselage;
• a cavity between the inner wall of the fuselage and the outer surface of the cabin wall;
• an cable holder comprising at least one cable holder section disposed in the cavity for holding one or more cables;
• and
• a plurality of vibration isolators disposed in the cavity, each of the vibration isolators comprising:
• a first isolator attached between the inner wall of the fuselage and the cable holder;
• and
• a second isolator attached between the outer surface of the cabin wall and the cable holder.

An aircraft, comprising:

• a fuselage;
• an interior structure disposed within the fuselage;
• a plurality of vibration isolators disposed between the fuselage and the interior structure, each of the vibration isolators comprising:
• a first isolator;
• a second isolator;
• and
• an intermediate mass disposed between the first isolator and the second isolator.