US2568787A - Steam power plant using exhaust from auxiliary gas turbine for condensing steam - Google Patents

Steam power plant using exhaust from auxiliary gas turbine for condensing steam Download PDF

Info

Publication number
US2568787A
US2568787A US528756A US52875644A US2568787A US 2568787 A US2568787 A US 2568787A US 528756 A US528756 A US 528756A US 52875644 A US52875644 A US 52875644A US 2568787 A US2568787 A US 2568787A
Authority
US
United States
Prior art keywords
steam
combustion
boiler
pressure
gases
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US528756A
Inventor
Bosch Herbert Alvin
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US528756A priority Critical patent/US2568787A/en
Application granted granted Critical
Publication of US2568787A publication Critical patent/US2568787A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01KSTEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
    • F01K23/00Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids
    • F01K23/02Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled
    • F01K23/06Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle

Definitions

  • This invention relates to apparatus for converting the heat energy of fuels into work, particularly wherein the products of combustion are maintained under compression within a steam generator.
  • the invention is adaptable for use as a stationary installation or a power plant in a land, water or air vehicle.
  • An object of the invention is to provide an apparatus whose construction is relatively low per horse power and to convert into work as much of the heat energy as possible from the fuel.
  • the method includes burning the fuel and air under a much higher degree of pressure than usual and cooling the gases of combustion by having them pass through or over boiler tubes under pressure in the generation of steam. In so doing the pressure of the steam in the boiler and that of the products of combustion is the same.
  • This condition of equal pressure is maintained by connecting the chamber confining the gases of combustion with the steam chamber in the proper locations and manner hereinafter explained. There is also maintained a counterflow of the gases of combustion or the water and other liquid in the boiler to permit the greatest cooling of the gases of combustion and heating of the boiler liquid in a minimum boiler space.
  • the steam after expanding and doing work is passed through the condenser and condensate returned to the boiler and the heat given off by the steam is recovered. This heat recovered is used to assist combustion.
  • the gases of combustion because of their relatively high compression are expanded in two or more stages. Since a large range of expansion is provided the products of combustion can be cooled to a considerable extent and still be maintained under relatively high pressure. While in this relatively cool condition the gases are passed through a condenser with a counterflow of exhaust steam wherein the products of combustion are warmed and the steam is condensed.
  • the products of combustion can be expanded to atmospheric pressure at a temperature of appressor is connected by belts 6 and 6 which connect the turbine shafts 6 and I respectively to a countershaft 8.
  • a crank 6 formed in the countershaft 6 is drivingly connected to the compressor piston Ill.
  • the compressor has a cylinder II surrounded by a spaced water jacket I2 whichis connected to a boiler I3 by pipes I4 and I5.
  • Circulation of water through the jacket I2 is induced by a water pump I6 which pumps water from the relatively cool right hand end section of the boiler I3 into the compressor water jacket I2, and returns it somewhat warmer through the pipe I5 to the left hand end of the boiler which is the high temperature end thereof.
  • the compressor intake and outlet check valves I1 and I6 are operated in a conventional manner.
  • the valve I8 opens on the compression stroke of the piston I0 and permits air to enter the boiler combustion chamber I31; and the valve I1 opens on the intake stroke of the piston III to allow a fresh change of air to enter the compressor cylinder II through the pipe I9 which is fed by an air fan 20 which is used to pull air through the pipe 2I and a section 22a of a steam condenser indicated generally at 22, the pressure being approximately 15 pounds per square inch gauge pressure.
  • the fan 26 is mounted on the main shaft 6 of the gas turbine 2.
  • a fuel pump 23 is mounted at the left hand end of the boiler I3 and has a fuel injection nozzle 24 which extends to the boiler combustion chamber I3a. Interposed in the injection nozzle 24 is a control valve 26 through which extends a shaft 26 having a flyball governor 21 on its upper end. The lower end of the shaft 26 is geared to the main countershaft 8 which drives the compressor I and is in turn driven by the gas turbines 2 and 3. The speed of rotation of the turbines 2 and 3 naturally determines the speed of the shafts I and 26? and the governor 21 regulates the flow of fuel to the combustion chamber I3a in response to such speeds.
  • a spark plug 26 is provided for ignition of the fuel pumped to the combustion chamber I3a.
  • Air under pressure is supplied from the compressor I through a pipe 26 which enters the combustion chamber I3a adjacent the end of the fuel nozzle 24 and the spark plug 26.
  • a shield 30 in the combustion chamber I 3a diffuses the burning fuel mixture through the combustion chamber I3a to secure complete combustion before entering the tubes of the boiler I3.
  • the gases of combustion pass through the boiler I3 through tubes 3I to a header 32 at the right hand end of the boiler.
  • a pipe 33 leads from the header 32 to conduct the gases of com- 3 bustion to the intake of the turbine 2.
  • a suitable hand valve 34 is interposed in the gas line 33 to assist in maintaining the proper pressure of the combustion gases and regulate their flow.
  • the combustion gases are partially expanded as they pass through'the turbine 2 and are then conducted through a pipe 35 to the section 22b of the condenser 22.
  • the combustion gases pass around the tubes 36 and thence into a pipe 3'1 which constitutes the intake for the second gas turbine 3.
  • a flow and pressure control valve 31a is interposed in the pipe 3'5.
  • Turbines 2 and 3 are for the purpose of driving the compressor and the fan 20 respectively and are not for external work.
  • a steam dome or collector 38 Mounted on the upper side of the steam boiler H is a steam dome or collector 38, and a pipe 39 extends from said dome to the intake of a steam turbine 40.
  • is adapted to permit regulation of steam pressure in the line 39.
  • the steam passing through the turbine is expanded and it passes through the steam outlet pipe 42 and through the tubes 36 of the condenser sections 22a and 22b.
  • the steam is condensed by air entering the inlet 43 of the condenser section 2211 under the influence of the pump 20 which is connected to the lower side of the condenser section 22a by the pipe 2
  • the steam is also condensed by the combustion gases traveling through the condenser section 2217 by means of the inlet pipe 35jand outlet pipe 31.
  • a partition 44 separates the condenser sections 22a and 22b to prevent mixture of the air entering the inlet 43 and the combustion gases passing through the condenser sections 22b.
  • the condensed steam leaves the condenser 22 through a pipe 45 which is connected to a header 46- at theright hand side of the condenser 22.
  • the pipe 45 is connected to a pump 41 and the outlet of the pump is connected by a pipe 48 to the boiler water spaces 49 about the tubes 3
  • the pump 41 is preferably connected to the shaft of the steam turbine 40.
  • the steam condenser 22 mentioned above maintains as, near as possible a counterfiow of the steam fluid and the cooling fluid to permit the greatest efficiencyv of operation.
  • a pressure equalizing pipe 52 connects the steam dome 38 with the header 32 which is a portion of the combustion gas chamber in the boiler .13 and said pressure equalizer pipe 52 maintains an equality of pressure on both sides of the tubes. 3
  • the fan 20 causes a flow of air through the condenser section 22a where the air is warmed somewhat and is preferably at a pressure of 15 pounds per square inch.
  • This air passes from the pump 20 to the compressor and is then pumped from the compressor to the boiler combustion chamber
  • the check valve ll admits air from the pump pipe
  • are cooled faster by reason of their thinness and as a result a more rapid return of travel through the tubes is possible whereby their capacity is accordingly increased.
  • the pressure of the combustion gases after passing through the tubes is still.600 pounds less of course the small amount necessary to force them to travel through the tubes.
  • combustion gases are cooled and afford such a large range of expansion they can be expanded to about pounds per square inch and cooled in the processto about 35 to 40 F.
  • the gases passingthrough the turbine 2 from the boiler 13 are expanded to about 100 pounds per square inch pressure and the valve 34 can be regulated to maintain this pressure.
  • the combustion gases are cooled to about 35 to 40 F. and then passed to the condenser section 22b where by reason of a counterfiow of condensing steam the combustion gases are considerablywarmed.
  • the gases then are conducted to the second gas turbine 3 and areexhausted to atmospheric pressure through the outlet 3a.
  • the valve 31a controls the flow from the condenser section 22b and maintains the proper pressure therein.
  • the steam generated in the boiler I3 is maintained at about 600 pounds per square inch by a proper setting of the 'valve 4
  • This steam pressure of 600 pounds neutralizes the combustion gas pressure of 600 pounds and relieves the boiler tubes of the necessity of withstanding any pressure.
  • any difierences in pressure are equalized by the pressure equalizing pipe 52.
  • the steam generated in the boiler i3 travels to the steam turbine 40 where it is permitted to expand in operating the turbine.
  • the expanded steam travels through the pipe 42 and through the con"- denser tubes 36 of the condenser sections 22a and 22b. In passing through those portions of the tubes 36 in the condenser section 22a the steam is cooled by the counterfiow of air induced by the fan 20.
  • the steam then passes through those portions of the tubes 36 in the condenser section 22b where it is condensed by a counterflow of the gases of combustion which at that point are relatively cool.
  • the condensed steam is returned to the boiler through the pipes 45 and 48 by the action of the pump 41.
  • the compressor I might be initially started by any suitable means such as an electric motor 53 which also might be used by reason of connection with the main countershaft 8 to start the fan 20 and the fuel pump 23.
  • the fuel mixture is ignited by the spark plug 28 and after ignition electrical energy to said plug is cut off.
  • and combustion gas valve 34 would each be closed until the compressor has increased the pressure to approximately 20 pounds per inch.
  • the pressure equalizing pipe 52 will maintain the pressure equal on both sides of the boiler tubes.
  • the valve 34 can be opened whereupon the combustion gases leaving the boiler will operate the turbine 2.
  • the turbine 2 can then be utilized to drive the fan 20, the compressor l, and the fuel pump 23. As soon as the boiler reaches the'correct temperature and pressure the valve 4
  • An apparatus of the character described including a combustion chamber having fuel and air inlets, means for delivering fuel and air under pressure to said inlets and burning said fuel under pressure in said combustion chamber, a steam chamber having an inlet for liquid to be vaporized and a steam outlet, said chamber being in heat exchange relationship with said combustion chamber and having conduits therethrough in communication with the combustion chamber for the passage of the products of combustion so that they give of!
  • a header communicating with the conduits for receiving air utilized for combustion, reheat the partially cooled products of combustion and condense the steam to liquid, a conduit extending between and in communication with the outlet header of the heat exchanger and the steam chamber to return the condensedsteam and a third power unit connected with the outlet of the second section of the heat exchanger for operation by the reheated products of combustion, said products of combustion being expanded to below atmospheric temperature, said combustion chamber and said conduits being constructed to produce a pressure in said conduit above 600 p. s. i. and said conduits having enough heat transfer surface to produce a low enough temperature in said header to permit said expansion to below atmospheric temperature.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Description

p 25, 1951 H. A. BOSCH STEAM POWER PLANT USING EXHAUST FROM AUXILIARY GAS TURBINE FOR CONDENSING STEAM Filed March 30, 1944 jhvervfior 24M MWYMO A fiornggs Patented Sat. 251951 STEAM POWER PLANT USING EXHAUST FROM AUXILIARY GAS TURBINE FOR CONDENSING STEAM Herbert Alvin Bosch, Lake Elizabeth Township, Kandiyohi County, Minn.
Application March 30, 1944, Serial No. 528,756
. 2 Claims. (Cl. ISO-39.17)
This invention relates to apparatus for converting the heat energy of fuels into work, particularly wherein the products of combustion are maintained under compression within a steam generator. The invention is adaptable for use as a stationary installation or a power plant in a land, water or air vehicle.
An object of the invention is to provide an apparatus whose construction is relatively low per horse power and to convert into work as much of the heat energy as possible from the fuel.
Generally the method includes burning the fuel and air under a much higher degree of pressure than usual and cooling the gases of combustion by having them pass through or over boiler tubes under pressure in the generation of steam. In so doing the pressure of the steam in the boiler and that of the products of combustion is the same. This permits the use of much thinner and cheaper boiler tubes than used heretofore wherein the tubes have been subjected to a higher pressure only on one side thereof. This condition of equal pressure is maintained by connecting the chamber confining the gases of combustion with the steam chamber in the proper locations and manner hereinafter explained. There is also maintained a counterflow of the gases of combustion or the water and other liquid in the boiler to permit the greatest cooling of the gases of combustion and heating of the boiler liquid in a minimum boiler space. The steam after expanding and doing work is passed through the condenser and condensate returned to the boiler and the heat given off by the steam is recovered. This heat recovered is used to assist combustion.
The gases of combustion because of their relatively high compression are expanded in two or more stages. Since a large range of expansion is provided the products of combustion can be cooled to a considerable extent and still be maintained under relatively high pressure. While in this relatively cool condition the gases are passed through a condenser with a counterflow of exhaust steam wherein the products of combustion are warmed and the steam is condensed. The products of combustion can be expanded to atmospheric pressure at a temperature of appressor is connected by belts 6 and 6 which connect the turbine shafts 6 and I respectively to a countershaft 8. A crank 6 formed in the countershaft 6 is drivingly connected to the compressor piston Ill. The compressor has a cylinder II surrounded by a spaced water jacket I2 whichis connected to a boiler I3 by pipes I4 and I5. Circulation of water through the jacket I2 is induced by a water pump I6 which pumps water from the relatively cool right hand end section of the boiler I3 into the compressor water jacket I2, and returns it somewhat warmer through the pipe I5 to the left hand end of the boiler which is the high temperature end thereof. The compressor intake and outlet check valves I1 and I6 are operated in a conventional manner.
The valve I8 opens on the compression stroke of the piston I0 and permits air to enter the boiler combustion chamber I31; and the valve I1 opens on the intake stroke of the piston III to allow a fresh change of air to enter the compressor cylinder II through the pipe I9 which is fed by an air fan 20 which is used to pull air through the pipe 2I and a section 22a of a steam condenser indicated generally at 22, the pressure being approximately 15 pounds per square inch gauge pressure. The fan 26 is mounted on the main shaft 6 of the gas turbine 2.
A fuel pump 23 is mounted at the left hand end of the boiler I3 and has a fuel injection nozzle 24 which extends to the boiler combustion chamber I3a. Interposed in the injection nozzle 24 is a control valve 26 through which extends a shaft 26 having a flyball governor 21 on its upper end. The lower end of the shaft 26 is geared to the main countershaft 8 which drives the compressor I and is in turn driven by the gas turbines 2 and 3. The speed of rotation of the turbines 2 and 3 naturally determines the speed of the shafts I and 26? and the governor 21 regulates the flow of fuel to the combustion chamber I3a in response to such speeds. A spark plug 26 is provided for ignition of the fuel pumped to the combustion chamber I3a. Air under pressure is supplied from the compressor I through a pipe 26 which enters the combustion chamber I3a adjacent the end of the fuel nozzle 24 and the spark plug 26. A shield 30 in the combustion chamber I 3a diffuses the burning fuel mixture through the combustion chamber I3a to secure complete combustion before entering the tubes of the boiler I3. The gases of combustion pass through the boiler I3 through tubes 3I to a header 32 at the right hand end of the boiler. A pipe 33 leads from the header 32 to conduct the gases of com- 3 bustion to the intake of the turbine 2. A suitable hand valve 34 is interposed in the gas line 33 to assist in maintaining the proper pressure of the combustion gases and regulate their flow.
The combustion gases are partially expanded as they pass through'the turbine 2 and are then conducted through a pipe 35 to the section 22b of the condenser 22. The combustion gases pass around the tubes 36 and thence into a pipe 3'1 which constitutes the intake for the second gas turbine 3. A flow and pressure control valve 31a is interposed in the pipe 3'5. Turbines 2 and 3 are for the purpose of driving the compressor and the fan 20 respectively and are not for external work.
Mounted on the upper side of the steam boiler H is a steam dome or collector 38, and a pipe 39 extends from said dome to the intake of a steam turbine 40. A valve 4| is adapted to permit regulation of steam pressure in the line 39. The steam passing through the turbine is expanded and it passes through the steam outlet pipe 42 and through the tubes 36 of the condenser sections 22a and 22b. The steam is condensed by air entering the inlet 43 of the condenser section 2211 under the influence of the pump 20 which is connected to the lower side of the condenser section 22a by the pipe 2|. The steam is also condensed by the combustion gases traveling through the condenser section 2217 by means of the inlet pipe 35jand outlet pipe 31. A partition 44 separates the condenser sections 22a and 22b to prevent mixture of the air entering the inlet 43 and the combustion gases passing through the condenser sections 22b.
The condensed steam leaves the condenser 22 through a pipe 45 which is connected to a header 46- at theright hand side of the condenser 22. The pipe 45 is connected to a pump 41 and the outlet of the pump is connected by a pipe 48 to the boiler water spaces 49 about the tubes 3| in the boiler. prevents back flow of liquid through said pipe 48. The pump 41 is preferably connected to the shaft of the steam turbine 40.
The steam condenser 22 mentioned above maintains as, near as possible a counterfiow of the steam fluid and the cooling fluid to permit the greatest efficiencyv of operation.
A pressure equalizing pipe 52 connects the steam dome 38 with the header 32 which is a portion of the combustion gas chamber in the boiler .13 and said pressure equalizer pipe 52 maintains an equality of pressure on both sides of the tubes. 3| in the boiler i3. Consequently, the tubes are not subjected to any unenua pres'ure and. can thereby be made of much lighter material than it has been possible to use heretofore.
A summary of the principal'features -01 the invention is as follows:
A higher compression of the gases of combustion in theboiler tubes to a pressure of 600 pounds per square inch, for example, such pressure being the same on the opposite sides of the boiler tubes; thepressure equalizing conduit connecting the area of the combustion gases with that of the generated steam to secure this equality of pres- 'sure; thinner boiler tubes and greater economy of construction as well as greater capacity to exchange heat between the combustion gases and the boiler water: the recovery of the latent heat of vaporization from the condenser 22 for work in a new and simple manner; cooling of the gases of combustion in the first stage of expansion to a point where they can act as a cooling agent in the condenser 22; the conversion of the heat ab- A check valve 50 in the pipe 48 sorbed by the combustion gases into work in the second stage of expansion of such gases; and the preheating of air to be used for combustion, said preheating being accomplished in one portion of the condenser 22.
In operation the fan 20 causes a flow of air through the condenser section 22a where the air is warmed somewhat and is preferably at a pressure of 15 pounds per square inch. This air passes from the pump 20 to the compressor and is then pumped from the compressor to the boiler combustion chamber |3a through the pipe 29. Of course. it is understood that the check valve ll admits air from the pump pipe |3 to the com" pressor cylinder H on the downward stroke of the piston l0, while on the upward stroke of the piston the check valve closes and the valve l8 permits the piston to force air into and through the pipe 29.
At the same time that air is being fed under pressure to the boiler combustion chamber |3a fuel is introduced through the nozzle 24 and is burned with said air under pressure. In normal operation the pressure in the combustion chamber and boiler tubes is approximately 600 pounds per square inch. Because of the high compression the gases of combustionhave a higher temperature than would result from combustion without such compression.
Because of the balance of pressures on the inner and outer sides of the boiler tubes 3| they can be made much thinner and need only be constructed to prevent the leakage of liquids and withstand a fairly high temperature. The thick ness of the tubes while considerably less than those of a conventional type would necessarily depend upon the material from which they are made and size or diameter, and whether the tubes are to be used in a stationary power plant or built to withstand vibration as in a rapidly moving power plant. The heat exchange capacity of the boiler due to the extreme relative thin ness of theboiler tubes is greatly increased be yond the heat exchange capacity of present boilers. The entire boiler could therefore be made smaller and at less expense.
The gases of combustion passing through the tubes 3| are cooled faster by reason of their thinness and as a result a more rapid return of travel through the tubes is possible whereby their capacity is accordingly increased. The pressure of the combustion gases after passing through the tubes is still.600 pounds less of course the small amount necessary to force them to travel through the tubes.
Because the combustion gases are cooled and afford such a large range of expansion they can be expanded to about pounds per square inch and cooled in the processto about 35 to 40 F. The gases passingthrough the turbine 2 from the boiler 13 are expanded to about 100 pounds per square inch pressure and the valve 34 can be regulated to maintain this pressure. After this expansion the combustion gases are cooled to about 35 to 40 F. and then passed to the condenser section 22b where by reason of a counterfiow of condensing steam the combustion gases are considerablywarmed. The gases then are conducted to the second gas turbine 3 and areexhausted to atmospheric pressure through the outlet 3a. The valve 31a controls the flow from the condenser section 22b and maintains the proper pressure therein.
The steam generated in the boiler I3 is maintained at about 600 pounds per square inch by a proper setting of the 'valve 4| which controls the rate of flow through the pipe 39. This steam pressure of 600 pounds neutralizes the combustion gas pressure of 600 pounds and relieves the boiler tubes of the necessity of withstanding any pressure. Of course, any difierences in pressure are equalized by the pressure equalizing pipe 52. The steam generated in the boiler i3 travels to the steam turbine 40 where it is permitted to expand in operating the turbine. The expanded steam travels through the pipe 42 and through the con"- denser tubes 36 of the condenser sections 22a and 22b. In passing through those portions of the tubes 36 in the condenser section 22a the steam is cooled by the counterfiow of air induced by the fan 20. The steam then passes through those portions of the tubes 36 in the condenser section 22b where it is condensed by a counterflow of the gases of combustion which at that point are relatively cool. The condensed steam is returned to the boiler through the pipes 45 and 48 by the action of the pump 41.
The following might be one method of starting the apparatus. The compressor I might be initially started by any suitable means such as an electric motor 53 which also might be used by reason of connection with the main countershaft 8 to start the fan 20 and the fuel pump 23. The fuel mixture is ignited by the spark plug 28 and after ignition electrical energy to said plug is cut off. The steam valve 4| and combustion gas valve 34 would each be closed until the compressor has increased the pressure to approximately 20 pounds per inch. The pressure equalizing pipe 52 will maintain the pressure equal on both sides of the boiler tubes. When the pressure has reached about 20 pounds per inch the valve 34 can be opened whereupon the combustion gases leaving the boiler will operate the turbine 2. The turbine 2 can then be utilized to drive the fan 20, the compressor l, and the fuel pump 23. As soon as the boiler reaches the'correct temperature and pressure the valve 4| can be opened to start the steam turbine 40.
It is evident from the foregoing explanation of the operation of this invention that the entire heat energy of the fuel is converted into work except for unavoidable losses such as radiation. friction, etc. This is evident from the fact that the latent heat of vaporization is recovered from the condenser and converted into work and from the fact that the gases of combustion are released 6 the products of combustion, said header havi an outlet for said products, a power unit connected with the steam outlet of the steam chamher for operation by the steam and in which the steam is expanded, a second power unit connected with the outlet of the header for operation by the products of combustion and in which the products are expanded, a heat exchanger including a first section having an air inlet and an air outlet, means affording communication between said outlet and the air inlet of the combustion chamber, a separate, closed heat exchanger section having an inlet and an outlet, through which the partially cooled products of combustion pass, said last mentioned inlet being in communication with said second power unit, conduits passing through both sections of said heat exchanger, inlet and outlet headers in communication with the respective ends of said last mentioned conduits, a, conduit extending between said first mentioned power unit and said inlet header for the passage of steam, the steam passing through the conduits in the heat exchanger into the outlet header in successive heat exchange relation with the air flowing through the first section of the heat exchanger and the partially cooled products of combustion flowing through the second section of the heat exchanger so as to preheat the at atmospheric pressure and relatively low temperatures.
It will, of course, be understood that various changes may be made in the form, details, arrangement and proportions of the various parts without departing from the scope of my invention.
I claim:
1. An apparatus of the character described including a combustion chamber having fuel and air inlets, means for delivering fuel and air under pressure to said inlets and burning said fuel under pressure in said combustion chamber, a steam chamber having an inlet for liquid to be vaporized and a steam outlet, said chamber being in heat exchange relationship with said combustion chamber and having conduits therethrough in communication with the combustion chamber for the passage of the products of combustion so that they give of! heat to produce steam, a header communicating with the conduits for receiving air utilized for combustion, reheat the partially cooled products of combustion and condense the steam to liquid, a conduit extending between and in communication with the outlet header of the heat exchanger and the steam chamber to return the condensedsteam and a third power unit connected with the outlet of the second section of the heat exchanger for operation by the reheated products of combustion, said products of combustion being expanded to below atmospheric temperature, said combustion chamber and said conduits being constructed to produce a pressure in said conduit above 600 p. s. i. and said conduits having enough heat transfer surface to produce a low enough temperature in said header to permit said expansion to below atmospheric temperature.
2. An apparatus as defined in and by claim 1 wherein a conduit is provided in communication between the steam chamber and the header that receives the products of combustion for balancing the pressures between the steam chamber and the conduits passing therethrough.
HERBERT ALVIN BOSCH.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 13,209 Blanchard July 10, 1855 ,669 Fell Feb. 17, 1880 6 ,640 Dunklee Sept. 19, 1882 0 ,205 Hogan July 14, 1914 1,769,743 IeBlanc July 1, 1930 ,97 ,83 Forsling Oct. 30, 1934 ,095,984 Holzwarth Oct. 19, 1937 ,221,185 Farlow Nov. 12, 1940 2,268,357 Turner Dec. 30, 1941 2,294,700 Stroehlen Sept. 1, 1942 FOREIGN PATENTS Number Country Date 21 Great Britain Jan. 5, 1858
US528756A 1944-03-30 1944-03-30 Steam power plant using exhaust from auxiliary gas turbine for condensing steam Expired - Lifetime US2568787A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US528756A US2568787A (en) 1944-03-30 1944-03-30 Steam power plant using exhaust from auxiliary gas turbine for condensing steam

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US528756A US2568787A (en) 1944-03-30 1944-03-30 Steam power plant using exhaust from auxiliary gas turbine for condensing steam

Publications (1)

Publication Number Publication Date
US2568787A true US2568787A (en) 1951-09-25

Family

ID=24107047

Family Applications (1)

Application Number Title Priority Date Filing Date
US528756A Expired - Lifetime US2568787A (en) 1944-03-30 1944-03-30 Steam power plant using exhaust from auxiliary gas turbine for condensing steam

Country Status (1)

Country Link
US (1) US2568787A (en)

Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2613495A (en) * 1945-02-16 1952-10-14 Moore Inc Vapor and gas power plant utilizing equipressure vapor generator
US2702453A (en) * 1949-07-09 1955-02-22 Mercier Dev Corp Equipressure power generating plant and method of operating same
US2787121A (en) * 1946-01-28 1957-04-02 Bouffart Maurice Arrangement for cooling combustion chambers and compressors of a stationary power plant with water or steam from a boiler
US2955429A (en) * 1957-07-16 1960-10-11 Gen Electric Double reheat compound turbine powerplant
US2982266A (en) * 1955-03-10 1961-05-02 Babcock & Wilcox Co Binary fluid power plant and method of operating the same
US3007306A (en) * 1958-06-17 1961-11-07 Thompson Ramo Wooldridge Inc Vapor cycle engine
US3087304A (en) * 1958-12-22 1963-04-30 Walter Hellmuth Method and device for propelling submarine vehicles
US3164958A (en) * 1960-04-23 1965-01-12 Babcock & Wilcox Ltd Combined gas-steam turbine cycle power plant
US3172258A (en) * 1956-09-21 1965-03-09 Babcock & Wilcox Ltd Nuclear power plant
US3242345A (en) * 1961-11-09 1966-03-22 Trw Inc Lightweight electrical generator set employing a mercury power cycle and nitrogen cover gas
US3266246A (en) * 1963-02-01 1966-08-16 Licencia Talalmanyokat Binary vapor generating systems for electric power generation
US3538709A (en) * 1968-08-12 1970-11-10 Donald G Pensel Vapor driven engine
US5622043A (en) * 1993-04-20 1997-04-22 Humphries, Jr.; James J. Gas and steam electrical power generating system
US6389814B2 (en) 1995-06-07 2002-05-21 Clean Energy Systems, Inc. Hydrocarbon combustion power generation system with CO2 sequestration
US6523349B2 (en) 2000-03-22 2003-02-25 Clean Energy Systems, Inc. Clean air engines for transportation and other power applications
US6622470B2 (en) 2000-05-12 2003-09-23 Clean Energy Systems, Inc. Semi-closed brayton cycle gas turbine power systems
US6868677B2 (en) 2001-05-24 2005-03-22 Clean Energy Systems, Inc. Combined fuel cell and fuel combustion power generation systems
US6945029B2 (en) 2002-11-15 2005-09-20 Clean Energy Systems, Inc. Low pollution power generation system with ion transfer membrane air separation
US7021063B2 (en) 2003-03-10 2006-04-04 Clean Energy Systems, Inc. Reheat heat exchanger power generation systems
US20070101718A1 (en) * 2005-11-07 2007-05-10 Veritask Energy Systems, Inc. Method of efficiency and emissions performance improvement for the simple steam cycle
US7882692B2 (en) 2004-04-16 2011-02-08 Clean Energy Systems, Inc. Zero emissions closed rankine cycle power system
US20160040558A1 (en) * 2014-08-07 2016-02-11 Siemens Aktiengesellschaft Thermal power plant with a steam turbine

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US13209A (en) * 1855-07-10 Air and steam eng-ine
US224669A (en) * 1880-02-17 Production of motive power
US264640A (en) * 1882-09-19 Gas-refining and steam-power apparatus
US1103205A (en) * 1912-03-19 1914-07-14 Daniel Hogan Steam-generating apparatus.
US1769743A (en) * 1923-03-22 1930-07-01 Leblanc Vickers Maurice Sa Auxiliary condenser for two-stage air ejectors
US1978837A (en) * 1933-01-18 1934-10-30 Gen Electric Gas turbine power plant
US2095984A (en) * 1927-11-17 1937-10-19 Holzwarth Gas Turbine Co Explosion turbine plant
US2221185A (en) * 1938-05-12 1940-11-12 Farlow Thomas Marshall Power generating unit
US2268357A (en) * 1939-03-06 1941-12-30 Edward T Turner Method and apparatus for producing power
US2294700A (en) * 1939-10-13 1942-09-01 Gen Electric Elastic fluid power plant

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US13209A (en) * 1855-07-10 Air and steam eng-ine
US224669A (en) * 1880-02-17 Production of motive power
US264640A (en) * 1882-09-19 Gas-refining and steam-power apparatus
US1103205A (en) * 1912-03-19 1914-07-14 Daniel Hogan Steam-generating apparatus.
US1769743A (en) * 1923-03-22 1930-07-01 Leblanc Vickers Maurice Sa Auxiliary condenser for two-stage air ejectors
US2095984A (en) * 1927-11-17 1937-10-19 Holzwarth Gas Turbine Co Explosion turbine plant
US1978837A (en) * 1933-01-18 1934-10-30 Gen Electric Gas turbine power plant
US2221185A (en) * 1938-05-12 1940-11-12 Farlow Thomas Marshall Power generating unit
US2268357A (en) * 1939-03-06 1941-12-30 Edward T Turner Method and apparatus for producing power
US2294700A (en) * 1939-10-13 1942-09-01 Gen Electric Elastic fluid power plant

Cited By (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2613495A (en) * 1945-02-16 1952-10-14 Moore Inc Vapor and gas power plant utilizing equipressure vapor generator
US2787121A (en) * 1946-01-28 1957-04-02 Bouffart Maurice Arrangement for cooling combustion chambers and compressors of a stationary power plant with water or steam from a boiler
US2702453A (en) * 1949-07-09 1955-02-22 Mercier Dev Corp Equipressure power generating plant and method of operating same
US2982266A (en) * 1955-03-10 1961-05-02 Babcock & Wilcox Co Binary fluid power plant and method of operating the same
US3172258A (en) * 1956-09-21 1965-03-09 Babcock & Wilcox Ltd Nuclear power plant
US2955429A (en) * 1957-07-16 1960-10-11 Gen Electric Double reheat compound turbine powerplant
US3007306A (en) * 1958-06-17 1961-11-07 Thompson Ramo Wooldridge Inc Vapor cycle engine
US3087304A (en) * 1958-12-22 1963-04-30 Walter Hellmuth Method and device for propelling submarine vehicles
US3164958A (en) * 1960-04-23 1965-01-12 Babcock & Wilcox Ltd Combined gas-steam turbine cycle power plant
US3242345A (en) * 1961-11-09 1966-03-22 Trw Inc Lightweight electrical generator set employing a mercury power cycle and nitrogen cover gas
US3266246A (en) * 1963-02-01 1966-08-16 Licencia Talalmanyokat Binary vapor generating systems for electric power generation
US3538709A (en) * 1968-08-12 1970-11-10 Donald G Pensel Vapor driven engine
US5622043A (en) * 1993-04-20 1997-04-22 Humphries, Jr.; James J. Gas and steam electrical power generating system
US7043920B2 (en) 1995-06-07 2006-05-16 Clean Energy Systems, Inc. Hydrocarbon combustion power generation system with CO2 sequestration
US6389814B2 (en) 1995-06-07 2002-05-21 Clean Energy Systems, Inc. Hydrocarbon combustion power generation system with CO2 sequestration
US6598398B2 (en) 1995-06-07 2003-07-29 Clean Energy Systems, Inc. Hydrocarbon combustion power generation system with CO2 sequestration
US6523349B2 (en) 2000-03-22 2003-02-25 Clean Energy Systems, Inc. Clean air engines for transportation and other power applications
US6622470B2 (en) 2000-05-12 2003-09-23 Clean Energy Systems, Inc. Semi-closed brayton cycle gas turbine power systems
US6824710B2 (en) 2000-05-12 2004-11-30 Clean Energy Systems, Inc. Working fluid compositions for use in semi-closed brayton cycle gas turbine power systems
US6910335B2 (en) 2000-05-12 2005-06-28 Clean Energy Systems, Inc. Semi-closed Brayton cycle gas turbine power systems
US6637183B2 (en) 2000-05-12 2003-10-28 Clean Energy Systems, Inc. Semi-closed brayton cycle gas turbine power systems
US6868677B2 (en) 2001-05-24 2005-03-22 Clean Energy Systems, Inc. Combined fuel cell and fuel combustion power generation systems
US6945029B2 (en) 2002-11-15 2005-09-20 Clean Energy Systems, Inc. Low pollution power generation system with ion transfer membrane air separation
US7021063B2 (en) 2003-03-10 2006-04-04 Clean Energy Systems, Inc. Reheat heat exchanger power generation systems
US7882692B2 (en) 2004-04-16 2011-02-08 Clean Energy Systems, Inc. Zero emissions closed rankine cycle power system
US20070101718A1 (en) * 2005-11-07 2007-05-10 Veritask Energy Systems, Inc. Method of efficiency and emissions performance improvement for the simple steam cycle
US7690201B2 (en) * 2005-11-07 2010-04-06 Veritask Energy Systems, Inc. Method of efficiency and emissions performance improvement for the simple steam cycle
US20100139276A1 (en) * 2005-11-07 2010-06-10 Veritask Energy Systems, Inc. Method of Efficiency and Emissions Performance Improvement for the Simple Steam Cycle
US8453452B2 (en) 2005-11-07 2013-06-04 Veritask Energy Systems, Inc. Method of efficiency and emissions performance improvement for the simple steam cycle
US20160040558A1 (en) * 2014-08-07 2016-02-11 Siemens Aktiengesellschaft Thermal power plant with a steam turbine

Similar Documents

Publication Publication Date Title
US2568787A (en) Steam power plant using exhaust from auxiliary gas turbine for condensing steam
US2115338A (en) Gas turbine system
US2280765A (en) Gas turbine thermic engine
US4841722A (en) Dual fuel, pressure combined cycle
US2078956A (en) Gas turbine system
US2653447A (en) Combined condensing vapor and gas turbine power plant
US2717491A (en) Heat and power supply system with integrated steam boiler and gas turbine plant
US3177659A (en) Heat exchange apparatus
US2633707A (en) Compound plant for producing mechanical power and heating steam with gas and steam turbines
US3835650A (en) Steam air preheater for a steam boiler system
US2469679A (en) Gas turbine
US2428136A (en) Combustion gas and waste heat steam turbine
US2298663A (en) Gas turbine plant
JPS6388227A (en) Method of operating gas turbine unit
US3006146A (en) Closed-cycle power plant
US2421387A (en) Hot air turbine power plant with automatic air supply control
US3461667A (en) Method and apparatus for mixing gas and steam in a gas turbine plant
US2109237A (en) Power plant
US3374621A (en) Gas turbine auxiliary for steam power plants
US2374510A (en) Gas turbine plant
US2095984A (en) Explosion turbine plant
US1702264A (en) Gas turbine
US2478851A (en) Gas turbine plant
US2543677A (en) Gas turbine plant
US3264826A (en) Method of peaking a power plant system