Gas turbine engine case counterflow thermal control

Claim 2

A thermal control apparatus for a gas turbine engine casing, said thermal control apparatus comprising; at least two axially spaced apart circumferentially disposed continuous flowpaths in heat transfer communication with an axially extending section of the casing, a means of counterflowing a heat transfer fluid through said flowpaths such that said fluid in one flowpath flows in a clockwise direction and said fluid in the other of said flowpaths flows in a counterclockwise direction, and a means for effecting heat transfer between said fluid and said casing section.

Claim 3

A thermal control apparatus as claimed in claim 1 wherein said flowpaths are in parallel fluid flow communication.

Claim 4

A thermal control apparatus as claimed in claim 2 wherein said counterflowing means comprises an axially extending manifold having clockwise and counterclockwise facing inlets in fluid supply communication with corresponding ones of said clockwise and counterclockwise flowing flow paths.

Claim 5

A thermal control apparatus as claimed in claim 3 further comprising two manifolds supplying two corresponding sets of said counterflowing flowpaths.

Claim 6

A thermal control apparatus as claimed in claim 4 further comprising two sectors about the engine casing wherein each of said manifolds supplies said fluid to flowpaths in each of said sectors such that one of said manifolds supplies said clockwise flowing flowpaths and the other of said manifolds supplies said counterclockwise flowing flowpaths extending through each one of said sectors.

Claim 7

A thermal control apparatus as claimed in claim 5 further comprising at least one annular thermal control ring associated with said section of the engine casing axially disposed between said set of said counterflowing flowpaths and a support means tying an annular stator assembly to said thermal control ring such that expansion and contraction of said thermal control ring will cause a corresponding expansion and contraction of said stator assembly.

Claim 8

A thermal control apparatus as claimed in claim 6 wherein said stator assembly comprises a segmented annular stator shroud.

Claim 9

A thermal control apparatus as claimed in claim 7 wherein said means for effecting heat transfer between said heat transfer fluid and said casing is by impingement and comprises circumferentially disposed spray tubes containing said flowpaths and impingement apertures in said spray tubes arranged to impinge said fluid onto said thermal control ring to effect thermal control of said thermal control ring.

Claim 10

A thermal control apparatus as claimed in claim 5 further comprising: forward and aft axially spaced apart thermal control rings associated with said section of the engine casing, a first set and second set of two axially spaced apart circumferentially disposed counterflowing continuous heat transfer flowpaths in heat transfer communication with an axially extending section of the casing, said first and second sets of counterflowing continuous heat transfer flowpaths comprise three axially spaced apart circumferentially disposed counterflowing continuous heat transfer flowpaths interdigitated with said thermal control rings, a support means tying forward and aft ends of an annular stator assembly to corresponding ones of said forward and aft thermal control rings such that expansion and contraction of said thermal control rings will cause a corresponding expansion and contraction of said stator assembly, said means of counterflowing comprises a means to flow heat transfer fluid through said first and third heat transfer flowpaths in a first circumferential direction and through said second heat transfer flowpath in a second counterflowing direction, and said first and second heat transfer flowpaths are arranged to effect heat transfer between heat transfer fluid and said first thermal control ring and said third and second flowpaths are arranged to effect heat transfer between heat transfer fluid and said second thermal control ring.

Claim 11

A thermal control apparatus as claimed in claim 9 wherein said stator assembly comprises a segmented annular stator shroud.

Claim 12

A thermal control apparatus as claimed in claim 10 wherein said means for effecting heat transfer between said heat transfer fluid and said rings comprises circumferentially disposed spray tubes containing said flowpaths and impingement apertures in said spray tubes arranged to spray said fluid onto said thermal control rings to effect thermal control of said thermal control rings.

Claim 13

A gas turbine engine comprising; an annular engine casing surrounding a portion of the engine's rotor, at least two axially spaced apart circumferentially disposed flowpaths in heat transfer communication with an axially extending section of the casing, a means of counterflowing air through said flowpaths such that the air in one flowpath flows in a clockwise direction and the air in the other of said flowpaths flows in a counterclockwise direction, a compressor means and a means for supplying air from said compressor to said means of counterflowing air, and a means for effecting heat transfer between air and said casing section.

Claim 14

A gas turbine engine comprising; an annular engine casing surrounding a portion of the engine's rotor, at least two axially spaced apart circumferentially disposed flowpaths in heat transfer communication with an axially extending section of the casing, a means of counterflowing air through said flowpaths such that the air in one flowpath flows in a clockwise direction and the air in the other of said flowpaths flows in a counterclockwise direction, a compressor means and a means for supplying air from said compressor to said means of counterflowing air, and a means for effecting heat transfer between air and said casing section.