US4424667A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Apparatus for increasing the efficiency of a gas turbine engine
Assignee: Individual
•
Filing: 1982-06-07
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Granted: 1984-01-10
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Expires: 2002-06-07
Abstract
Abstract Apparatus for improving the operating efficiency of a gas turbine engine includes a heat pump and a pair of heat exchangers for use in conjunction with the engine. The first heat exchanger is disposed in the flow path of the engine upstream of its compressor section, while the second heat exchanger is disposed in the engine flow path downstream of the compressor section and upstream of the combustor section of the engine. A portion of the work output of the engine is used to operate the heat pump so as to cause cooling of air in the flow path at the first heat exchanger and heating of air in the flow path at the second heat exchanger.
Inventors
- 👤 Arthur E. Fanning
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-01 22:13
CPC Classifications
F; F02; F02C; F02C7/00; F02C7/08; F02C7/12; F02C7/14; F02C7/141; F02C7/143; F25; F25B; F25B11/00; F25B29/00; F25B29/003; Y; Y02; Y02T; Y02T50/00; Y02T50/60
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
166 words
In a gas turbine engine including, in serial relationship, a compressor section, a combustor section and a turbine section, with said turbine section having an output shaft and all of said sections together defining a flow path, initially, for air and, later, for products of combustion through said engine, apparatus for improving the operating efficiency of said engine, comprising: (a) a first heat exchanger disposed within said flow path of said engine upstream of said compressor section; (b) a second heat exchanger disposed within said flow path of said engine upstream of said combustor section and downstream of said compressor section; (c) pumping means interconnecting said first and second heat exchangers so as to cause cooling of air in said flow path at said first heat exchanger and heating of air in said flow path at said second heat exchanger; and (d) means for coupling said output shaft of said turbine section with said pumping means so as to drive the latter with said output shaft.
Claim 2
Dependent Claim
166 words
In a gas turbine engine including, in serial relationship, a compressor section, a combustor section and a turbine section, with said turbine section having an output shaft and all of said sections together defining a flow path, initially, for air and, later, for products of combustion through said engine, apparatus for improving the operating efficiency of said engine, comprising: (a) a first heat exchanger disposed within said flow path of said engine upstream of said compressor section; (b) a second heat exchanger disposed within said flow path of said engine upstream of said combustor section and downstream of said compressor section; (c) pumping means interconnecting said first and second heat exchangers so as to cause cooling of air in said flow path at said first heat exchanger and heating of air in said flow path at said second heat exchanger; and (d) means for coupling said output shaft of said turbine section with said pumping means so as to drive the latter with said output shaft.
Claim 3
Dependent Claim
52 words
Apparatus for improving operating efficiency of a gas turbine engine as recited in claim 1, wherein said pumping means includes: a working fluid; a heat pump; and conduit means interconnecting said pump and said first and second heat exchanger so as to form an endless closed circulation path for said working fluid.
Claim 4
Dependent Claim
60 words
Apparatus for improving operating efficiency of a gas turbine engine as recited in claim 2, wherein: said heat pump has a compressor portion, a turbine portion and an input shaft interconnecting said portions; and said coupling means includes a drive train connecting said input shaft of said heat pump to said output shaft of said turbine section of said engine.
Claim 5
Dependent Claim
169 words
Apparatus for improving operating efficiency of a gas turbine engine as recited in claim 3, further comprising: valve means incorporated in said conduit means and actuatable between open and closed conditions for respectively allowing and obstructing the flow of working fluid through said conduit means; clutch means operatively connected with said drive train and selectively actuatable for coupling and uncoupling said heat pump to and from said engine; and means for actuating said valve means and said clutch means so as to respectively close said valve means and uncouple said heat pump from said engine for rendering said heat pump inoperative, or to respectively open said valve means and couple said heat pump to said engine for rendering said heat pump operative, said heat pump when operative causing circulation of working fluid about said endless closed path and cooling of air in said flow path of said engine at said first heat exchanger and heating of air in said flow path of said engine at said second heat exchanger.
Claim 6
Dependent Claim
524 words
In a gas turbine engine including, in serial relationship, a compressor section, a combustor section and a turbine section, with said turbine section having an output shaft and all of said sections together defining a flow path, initially, for air and, later, for products of combustion through said engine, apparatus for improving the operating efficiency of said engine, comprising: (a) a first heat exchanger disposed within said flow path of said engine upstream of said compressor section and having opposite inlet and outlet ends, (b) a second heat exchanger disposed within said flow path of said engine upstream of said combustor section and downstream of said compressor section and having opposite inlet and outlet ends; (c) a heat pump having a compressor portion, a turbine portion and an input shaft interconnecting said portions, said compressor and turbine portions each having input and output ends; (d) a working fluid; (e) a first conduit interconnecting said output end of said turbine portion of said heat pump with said inlet end of said first heat exchanger for providing flow of working fluid from said heat pump to said first heat exchanger; (f) a second conduit interconnecting said outlet end of said first heat exchanger with said input end of said compressor portion of said heat pump for providing return flow of working fluid from said first heat exchanger to said heat pump; (g) a third conduit interconnecting said output end of said compressor portion of said heat pump with said inlet end of said second heat exchanger for providing flow of working fluid from said heat pump to said second heat exchanger; (h) a fourth conduit interconnecting said outlet end of said second heat exchanger with said input end of said turbine portion of said heat pump for providing return flow of working fluid from said second heat exchanger to said heat pump; (i) a drive train interconnecting said output shaft of said turbine section of said engine with said input shaft of said heat pump for utilizing a portion of the work output of said engine to drive said heat pump; (j) a clutch operatively connected with said drive train and selectively actuatable for coupling and uncoupling said heat pump to and from said engine; (k) a first valve incorporated in said second conduit and actuatable between open and closed conditions for respectively allowing and obstructing the flow of working fluid through said second conduit; (l) a second valve incorporated in said fourth conduit and actuatable between open and closed conditions for respectively allowing and obstructing the flow of working fluid through said fourth conduit; and (m) means for actuating said first and second valves and said clutch so as to respectively close said valves and uncouple said heat pump from said engine for rendering said heat pump inoperative, or to respectively open said valves and couple said heat pump to said engine for rendering said heat pump operative, said heat pump when operative causing cooling of air in said flow path of said engine at said first heat exchanger and heating of air in said flow path of said engine at said second heat exchanger.
Claim 7
Dependent Claim
524 words
In a gas turbine engine including, in serial relationship, a compressor section, a combustor section and a turbine section, with said turbine section having an output shaft and all of said sections together defining a flow path, initially, for air and, later, for products of combustion through said engine, apparatus for improving the operating efficiency of said engine, comprising: (a) a first heat exchanger disposed within said flow path of said engine upstream of said compressor section and having opposite inlet and outlet ends, (b) a second heat exchanger disposed within said flow path of said engine upstream of said combustor section and downstream of said compressor section and having opposite inlet and outlet ends; (c) a heat pump having a compressor portion, a turbine portion and an input shaft interconnecting said portions, said compressor and turbine portions each having input and output ends; (d) a working fluid; (e) a first conduit interconnecting said output end of said turbine portion of said heat pump with said inlet end of said first heat exchanger for providing flow of working fluid from said heat pump to said first heat exchanger; (f) a second conduit interconnecting said outlet end of said first heat exchanger with said input end of said compressor portion of said heat pump for providing return flow of working fluid from said first heat exchanger to said heat pump; (g) a third conduit interconnecting said output end of said compressor portion of said heat pump with said inlet end of said second heat exchanger for providing flow of working fluid from said heat pump to said second heat exchanger; (h) a fourth conduit interconnecting said outlet end of said second heat exchanger with said input end of said turbine portion of said heat pump for providing return flow of working fluid from said second heat exchanger to said heat pump; (i) a drive train interconnecting said output shaft of said turbine section of said engine with said input shaft of said heat pump for utilizing a portion of the work output of said engine to drive said heat pump; (j) a clutch operatively connected with said drive train and selectively actuatable for coupling and uncoupling said heat pump to and from said engine; (k) a first valve incorporated in said second conduit and actuatable between open and closed conditions for respectively allowing and obstructing the flow of working fluid through said second conduit; (l) a second valve incorporated in said fourth conduit and actuatable between open and closed conditions for respectively allowing and obstructing the flow of working fluid through said fourth conduit; and (m) means for actuating said first and second valves and said clutch so as to respectively close said valves and uncouple said heat pump from said engine for rendering said heat pump inoperative, or to respectively open said valves and couple said heat pump to said engine for rendering said heat pump operative, said heat pump when operative causing cooling of air in said flow path of said engine at said first heat exchanger and heating of air in said flow path of said engine at said second heat exchanger.
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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) | 1987-01-09 | 1987-07-11 | 1988-01-10 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1991-01-09 | 1991-07-11 | 1992-01-10 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1995-01-09 | 1995-07-11 | 1996-01-10 | $7700.00 | Window Closed / Lapsed |