Double wall ducting

Claim 2

For use in jet aircraft, a lightweight, high-strength duct comprising: two thin annular sheet metal tubes, the tube metals being equivalents, one of said tubes being snugly fitted within the other, said tubes having substantially continuous cylindrical wall surfaces, the inner surface of the outer tube being in substantially coextensive contact with the outer surface of the inner tube, longitudinally spaced stiffening members on the outer tube, said stiffening members being spaced by relatively long expanses of cylindrical wall surface, and venting means in one of the tubes to prevent pressure differentials between the two tubes at various altitudes and temperatures, said duct having approximately the same strength as a single wall tube of an equivalent metal weighing twice as much.

Claim 3

The invention according to claim 1 in which: said stiffening members are annular stiff, self-supporting beads, V-shaped in cross section, extending radially outwardly from the outer tube.

Claim 4

The invention according to claim 2 in which: said venting means is a vent hole in one or more of said beads.

Claim 5

The invention according to claim 2 in which: said venting means is one or more holes through the wall of the inner tube.

Claim 6

The invention according to claim 1 in which: said tubes are sealed together at spaced longitudinal intervals.

Claim 7

The invention according to claim 1 in which: the inner surface of the inner tube is smooth for uninterrupted flow therethrough.

Claim 8

The invention according to claim 6 in which: each tube is butt welded along its longitudinal edges.

Claim 9

The invention according to claim 1 in which: the ratio of longitudinal cylindrical wall surface length between stiffening members to the longitudinal length of the stiffening members is of the order of approximately 11 to 1.

Claim 10

The invention according to claim 1 in which: the ratio of longitudinal cylindrical wall surface length between stiffening members to the longitudinal length of the stiffening members is at least 11 to 1.

Claim 11

The invention according to claim 1 in which: the sheet metal tubes each have a wall thickness of approximately 0.006 inch, and the sheet metal is one selected from the group consisting of titanium, aluminum, Inconel 625 alloy, and Cres 321 alloy.

Claim 12

The invention according to claim 1 in which: the sheet metal tubes each have a wall thickness of approximately 0.006 inch, and the sheet metal is titanium.

Claim 13

In a jet engine powered aircraft, a jet engine having an air compressor, and air bleed line extending from said engine aft of said compressor to bleed off compressed air, a compressed air cooler for receiving and cooling said bleed air, a discharge air line from said cooler receiving said cooled air and being connected to an air service duct of the aircraft; the improvement in said air service duct comprising: two thin annular sheet metal tubes, the tube metals being equivalents, one of said tubes being snugly fitted within the other, said tubes having substantially continuous cylindrical wall surfaces, the inner surface of the outer tube being in substantially coextensive contact with the outer surface of the inner tube, longitudinally spaced stiffening members on the outer tube, said stiffening members being spaced by relatively long expanses of cylindrical wall surface, and venting means in one of the tubes to prevent pressure differentials between the two tubes at various altitudes and temperatures, said duct having approximately the same strength as a single wall tube of an equivalent metal weighing twice as much.

Claim 14

In a jet engine powered aircraft, a jet engine having an air compressor, and air bleed line extending from said engine aft of said compressor to bleed off compressed air, a compressed air cooler for receiving and cooling said bleed air, a discharge air line from said cooler receiving said cooled air and being connected to an air service duct of the aircraft; the improvement in said air service duct comprising: two thin annular sheet metal tubes, the tube metals being equivalents, one of said tubes being snugly fitted within the other, said tubes having substantially continuous cylindrical wall surfaces, the inner surface of the outer tube being in substantially coextensive contact with the outer surface of the inner tube, longitudinally spaced stiffening members on the outer tube, said stiffening members being spaced by relatively long expanses of cylindrical wall surface, and venting means in one of the tubes to prevent pressure differentials between the two tubes at various altitudes and temperatures, said duct having approximately the same strength as a single wall tube of an equivalent metal weighing twice as much.

Claim 15

The invention according to claim 12 in which: said tubes are sealed together at spaced longitudinal intervals.

Claim 16

The invention according to claim 12 in which: the ratio of longitudinal cylindrical wall surface length between stiffening members to the longitudinal length of the stiffening members is of the order of approximately 11 to 1.

Claim 17

The invention according to claim 12 in which: the ratio of longitudinal cylindrical wall surface length between stiffening members to the longitudinal length of the stiffening members is at least 11 to 1.

Claim 18

The invention according to claim 12 in which: said stiffening members are annular stiff, self-supporting beads, V-shaped in cross section, extending radially outwardly from the outer tube.

Claim 19

The invention according to claim 16 in which: said venting means is a vent hole in at least one of said beads.

Claim 20

The invention according to claim 16 in which: said venting means are comprised of a plurality of longitudinally spaced vent holes, each of said vent holes being positioned to vent adjacent a respective bead.