Systems and methods for insulation of aircraft cooling systems

An system comprising:

• a first tube and a second tube, wherein the first tube and the second tube are configured to transport a heat transfer fluid;
• a drainage container;
• and
• an insulating apparatus surrounding the first tube and the second tube, the insulating apparatus comprising:
• an elongated strip including a first end and a second end;
• a medial portion running along a length of the elongated strip from the first end to the second end;
• a first edge from the first end to the second end,
• wherein the first edge curls around a first longitudinal axis toward the medial portion to form a first wrap portion with a first cavity defined by an interior surface of the first wrap portion;
• wherein the first tube is located within the first cavity;
• a second edge from the first end to the second end,
• wherein the second edge curls around a second longitudinal axis toward the medial portion to form a second wrap portion with a second cavity defined by an interior surface of the second wrap portion;
• wherein the second tube is located within the second cavity;
• and
• a channel above the medial portion, the channel defined by an exterior surface of each of the first wrap portion and the second wrap portion;
• wherein the first cavity and the second cavity are interconnected with the channel through a first gap and a second gap, respectively;
• and
• wherein liquid produced by the first tube and the second tube flows through the first gap and the second gap, respectively, and is collected at the channel to be transported to the drainage container.