Hot air duct

Claim 1

A hot air duct for use in aircraft comprising a thin walled tube, a plurality of linearly spaced reinforcing rings secured to the external surface of the tube to prevent the tube from collapsing if the internal pressure of the tube drops substantially, each of said reinforcing rings formed from sheet material and comprising a channel-shaped portion with oppositely extending flange mounting portions attached to the channel shaped portion, said reinforcing rings mounted on the external surface of the tube so the channel shaped portions project radially outwardly providing a heat radiating and a spacing surface around the tube with the channel shaped portion opening inwardly and facing and completely closed off by the external surface of the tube to reinforce the tube, defining thereby a ring shaped chamber around the tube, said oppositely extending flange mounting portions rigidly fastened to the external surface of the tube, an aligned opening formed in each side of each of the channel shaped portions providing thereby communication between the interior and exterior of the channel-shaped portion, said reinforcing rings mounted on the thin walled tube so that the aligned openings in each channel shaped portion of the reinforcing ring are all in linear alignment with each other to define continuous air channels running parallel to the axis of the tube along the length of the tube whereby the external surface of the tube can be cooled readily if a flow of cold air is directed through the said aligned openings in the ring shaped chambers of the reinforcing rings, when said rings engage and serve as a spacer between said duct and a surrounding surface said channel shaped portions extending radially outwardly far enough so if said hot air duct is mounted closely adjacent a surface in the aircraft said channel shaped portions serve as spacers to keep the surface of the tube from rubbing against the surface of the aircraft.