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US3916990A Expired / Lapsed US ⏱️ 0.0 years remaining

Gas turbine regenerator

Assignee: Foster Wheeler Inc
•
Filing: 1974-07-03
•
Granted: 1975-11-04
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Expires: 1994-07-03
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Abstract

Abstract A heat exchanger in which a plurality of tubes are supported in a spaced parallel relationship between two tube sheets. A conduit is provided in a parallel relation to the tubes for supplying a fluid to the tubes, and the arrangement is such that one of the tube sheets is fixed relative to the conduit and the other tube sheet moves relative to the conduit to accommodate thermal expansion and contraction of the tubes. A support unit is provided for supporting the tubes in a spaced parallel relationship while allowing an additional fluid to pass between the tubes in a heat exchange relation to the first fluid. A cooling liquid may be mixed with the first fluid prior to the heat exchange with the additional fluid.

Inventors

  • 👤 Anthony Ruhe
  • 👤 Robert R Steel
  • 👤 John W Varney

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-08 20:28
CPC Classifications
F; F28; F28F; F28F9/00; F28F9/007; F28F9/013; F28F9/0135; F28D; F28D7/00; F28D7/16; F28D7/163; F28D7/1669; F28F9/02; F28F9/0236; F28F9/0239; F28F2265/00; F28F2265/26

Claims Analysis

Total Claims: 12
Claim 1
Independent Claim 459 words
A gas turbine regenerator through which the exhaust gasses of a gas turbine are adapted to pass in heat exchange relation with combustion air of the gas turbine for injecting cooling fluid into; and heating, the combustion air enteringing said gas turbine comprising: a conduit having an inlet for receiving the combustion air and an outlet for discharging same, a tube sheet connected to and supported by said conduit, a header connected to said tube sheet, a plurality of tubes extending parallel to said conduit, one end of each of said tubes being supported by said tube sheet in communication with said header, whereby said header reverses the fluid flow from said conduit and passes said combustion air into said tubes, an additional tube sheet supporting the other ends of said tubes, a sleeve connected at one end to the conduit close to the inlet thereof and to said additional tube sheet at a free end thereof spaced from said conduit inlet and surrounding a portion of said conduit with the inner wall of said sleeve extending in a spaced relation to the outer surface of said conduit to permit relative movement therebetween, an additional header connected to said additional tube sheet and to said sleeve at the end thereof close to the conduit inlet, said additional header adapted to receive said combustion air from said other ends of said tubes and discharge same from the outlet formed therethrough, and a housing having a circular cross-section located coaxially with respect to said conduit the tubes enclosed in an annular space defined between said housing and conduit having an inlet for receiving the exhaust gases of said gas turbine and an inlet for discharging said same in a counterflow relation to said combustion air in said tubes, said exhaust gases being at a relatively high temperature than said combustion air with the resultant thermal expansion of said tubes being accommodated by movement of said sleeve and therefore said additional tube sheet and additional header relative to said conduit; at least one support unit for supporting tubes in a spaced relation within the housing, said unit comprising a plurality of interconnected strips formed into a grid pattern defining a first series of openings for respectively receiving said tubes said openings spaced uniformly about the exterior surface of the tubes forming a spaced sleeve thereabout, and a second series of openings for permitting the passage of the combustion air therethrough, said strips being interlaced with at least one side being slotted to facilitate said interconnection, and a fluid injection means for injecting of cooling fluid into the conduit near the inlet for mixing with said combustion air, the heat exchange between the combustion air gases being sufficient to vaporize the cooling fluid.
Claim 2
Dependent Claim 459 words
A gas turbine regenerator through which the exhaust gasses of a gas turbine are adapted to pass in heat exchange relation with combustion air of the gas turbine for injecting cooling fluid into; and heating, the combustion air enteringing said gas turbine comprising: a conduit having an inlet for receiving the combustion air and an outlet for discharging same, a tube sheet connected to and supported by said conduit, a header connected to said tube sheet, a plurality of tubes extending parallel to said conduit, one end of each of said tubes being supported by said tube sheet in communication with said header, whereby said header reverses the fluid flow from said conduit and passes said combustion air into said tubes, an additional tube sheet supporting the other ends of said tubes, a sleeve connected at one end to the conduit close to the inlet thereof and to said additional tube sheet at a free end thereof spaced from said conduit inlet and surrounding a portion of said conduit with the inner wall of said sleeve extending in a spaced relation to the outer surface of said conduit to permit relative movement therebetween, an additional header connected to said additional tube sheet and to said sleeve at the end thereof close to the conduit inlet, said additional header adapted to receive said combustion air from said other ends of said tubes and discharge same from the outlet formed therethrough, and a housing having a circular cross-section located coaxially with respect to said conduit the tubes enclosed in an annular space defined between said housing and conduit having an inlet for receiving the exhaust gases of said gas turbine and an inlet for discharging said same in a counterflow relation to said combustion air in said tubes, said exhaust gases being at a relatively high temperature than said combustion air with the resultant thermal expansion of said tubes being accommodated by movement of said sleeve and therefore said additional tube sheet and additional header relative to said conduit; at least one support unit for supporting tubes in a spaced relation within the housing, said unit comprising a plurality of interconnected strips formed into a grid pattern defining a first series of openings for respectively receiving said tubes said openings spaced uniformly about the exterior surface of the tubes forming a spaced sleeve thereabout, and a second series of openings for permitting the passage of the combustion air therethrough, said strips being interlaced with at least one side being slotted to facilitate said interconnection, and a fluid injection means for injecting of cooling fluid into the conduit near the inlet for mixing with said combustion air, the heat exchange between the combustion air gases being sufficient to vaporize the cooling fluid.
Claim 3
Dependent Claim 78 words
The gas turbine regenerator of claim 1 wherein said conduit, said tubes and said housing extend primarily vertically, with said tube sheet and said header being disposed at the upper portion thereof, and with said sleeve, said additional tube sheet and said additional header being disposed at the lowEr portion thereof, said combustion air passing from the lower portion of said conduit upwardly and then downwardly through said tubes, and said exhaust gases passing upwardly through said housing.
Claim 4
Dependent Claim 78 words
The gase turbine regenerator of claim 1 wherein said conduit, said tubes and said housing extend primarily horizontally, with said tube sheet and said header being disposed at the upper portion thereof, and with said sleeve, said additional tube sheet and said additional header being disposed at the lower portion thereof, said combustion air passing from the lower portion of said conduit upwardly and then downwardly through said tubes, and said exhaust gases passing upwardly through said housing.
Claim 5
Dependent Claim 41 words
The heat exchanger of claim 1 wherein said first fluid is air at a relatively low temperature from an air compressor and wherein said second fluid is a gas at a relatively high temperature from the exhaust of a gas turbine.
Claim 6
Dependent Claim 42 words
The gas turbine regenerator of claim 1 wherein said cooling fluid is water in liquid form when injected and wherein the heat exchange between said combustion air and exhaust gases is sufficient to heat said combustion air and vaporize said cooling water.
Claim 7
Dependent Claim 36 words
The gas turbine regenerator of claim 5 wherein said water injection means comprises a toroidal spray nozzle having a plurality of holes and an inlet for communicating a water supply thereto for injection into said conduit.
Claim 8
Dependent Claim 20 words
The gas turbine regenerator of claim 6 further comprising bracket means for supporting said toroidal spray nozzle within said conduit.
Claim 9
Dependent Claim 22 words
The gas turbine regenerator of claim 1 wherein said cooling fluid is a liquid, at least a portion of which is combustible.
Claim 10
Dependent Claim 39 words
The gas turbine regenerator of claim 1 wherein said combustion air is at a relatively low temperature from an air compressor and wherein said exhaust gas is at a relatively high temperature from the exhaust of the gas turbine.
Claim 11
Dependent Claim 85 words
The gas turbine regenerator system of claim 1 comprising a plurality of heat exchangers, a supply conduit for the combustion air, means connecting said supply conduit to each of said heat exchangers, an outlet conduit for said combustion air means connecting said outlet conduit to each of said heat exchangers, a supply manifold connected to each of said heat exchangers for supplying the exhaust gases to said heat exchangers, and an exhaust manifold connected to each of said heat exchangers for receiving said exhaust gases.
Claim 12
Dependent Claim 37 words
The gas turbine regenerator system of claim 10 wherein; said supply conduit is connected to an air compressor, said outlet conduit is connected to a combustion chamber, and said supply manifold is connected to the gas turbine.

References Cited (Backward Citations)

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US3589438A Cited
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USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1978-11-03 1979-05-05 1979-11-04 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1982-11-03 1983-05-05 1983-11-04 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1986-11-03 1987-05-05 1987-11-04 $7700.00 Window Closed / Lapsed

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