(12) United States Patent (10) Patent No.: US 6,644,011 B2 Cheng (45) Date of Patent: Nov
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USOO6644O11B2 (12) United States Patent (10) Patent No.: US 6,644,011 B2 Cheng (45) Date of Patent: Nov. 11, 2003 (54) ADVANCED CHENG COMBINED CYCLE 5,370,772 A * 12/1994 Arpalahti et al. ........ 60/39.182 5,613,356 A * 3/1997 Frutschi................... 60/39.182 (75) Inventor: Dah Yu Cheng, Los Altos Hills, CA 6.256,978 B1 7/2001 Gericke et al. .......... 60/39.182 (US) * cited by examiner (73) ASSignee: She's yet Systems, Inc., Mountain Primary Examiner Michael Koczo 1eW, (US) (74) Attorney, Agent, or Firm-Cooper & Dunham LLP (*) Notice: Subject to any disclaimer, the term of this (57) ABSTRACT patent is extended or adjusted under 35 U.S.C. 154(b) by 0 days. An Advanced Cheng Combined Cycle engine is a combi nation of the Cheng Cycle or the Advanced Cheng Cycle and (21) Appl. No.: 09/816,588 a combined cycle, and Serves to further enhance the power 9 generation capability of either the Cheng Cycle, the (22) Filed: Mar 23, 2001 Advanced Cheng Cycle, or the combined cycle alone. Agas O O turbine is provided, having a turbine generating power, a (65) Prior Publication Data compressor receiving power from the turbine, and a com US 2001/0039797 A1 Nov. 15, 2001 bustion chamber to which is input compressed air from the compressor along with fuel and combustion products for Related U.S. Application Data producing energy to drive the turbine, the gas turbine (60) Provisional application No. 60/191,599, filed on Mar. 24, producing a hot stream gas. Aheat recovery Steam generator 2000. receives hot Stream gas produced by the gas turbine and (51) Int. Cl. .................................................. FO2C 6/18 generates high-pressure Steam therefrom. A Steam turbine (52) U.S. CI. 60/39.182; 60/39.55; 60/806 receives and is driven by high-pressure Steam generated by (58) Field of search - - - - - - - - - - - s 60/39 1s2 39.55 the heat recovery Steam generator. The Steam turbine bleeds - - - - - - - - - - - - - - -60's06 39.5 775.29052 intermediate-pressure Steam for cooling the turbine and for 9 - 1 - as s injection back into the combustion chamber of the gas (56) References Cited turbine. A control valve throttles down high-pressure Steam generated by the heat recovery Steam generator to a low U.S. PATENT DOCUMENTS pressure steam for injection back into the combustion cham 4,069,424 A 1/1978 Burkett ........................ 290/52 ber of the gas turbine. 4,519,207 A * 5/1985 Okabe et al. ............ 60/39.182 4,907.406 A * 3/1990 Kirikami et al. ......... 60/39.182 1 Claim, 4 Drawing Sheets St. Fuel (Duct Burner) Supplimental Air CCC COatrols U.S. Patent Nov. 11, 2003 Sheet 2 of 4 US 6,644,011 B2 Fuel (Duct Burner) Supplimental Air 62 CCC Controls 90 Cooling 85 to FIG. 4 U.S. Patent Nov. 11, 2003 Sheet 3 of 4 US 6,644,011 B2 Fue XNXX7 f22 Nie 23 Steam f00 ff AA Supplemental-/ E. DUCTBURNER OWNOX BURNERSYSTEM FIG. 5 U.S. Patent Nov. 11, 2003 Sheet 4 of 4 US 6,644,011 B2 !! US 6,644,011 B2 1 2 ADVANCED CHENG COMBINED CYCLE psia) at a temperature greater than 750 degrees Fahrenheit (F), which is used to drive the steam turbine. The steam is REFERENCE TO RELATED APPLICATION then condensed by a condenser and recycled back into the This present application claims the benefit of provisional boiler. Heat is rejected from the condenser by means of a Application Serial No. 60/191,599 filed on Mar. 24, 2000, cooling mechanism, usually a cooling tower. which is hereby incorporated by reference. Both the Cheng Cycle and the Advanced Cheng Cycle were conceived by the Applicant of the present invention in FIELD the 1970s, and one or both have been the subject of a number of prior art patents, including U.S. Pat. Nos. 3,978,661, This patent specification relates to the field of heat 4,128,994, 4,248,039, 4,297.841, 4,417,438, and 5,233,826, engines, and more particularly, to an Advanced Cheng which are hereby incorporated by reference. Combined Cycle engine that combines features of the com bined cycle and the Cheng Cycle or the Advanced Cheng The Cheng Cycle engine is a dual-fluid engine which Cycle. makes use of two Separate working fluids. Each fluid is compressed Separately, but they are combined in a Single 15 BACKGROUND mixture for expansion and heat regeneration. This cycle essentially combines a Brayton cycle and regenerative Aheat engine is a device that converts heat to work for the Rankine cycle System in parallel Such that operational purpose of Supplying power. There are many different appli limitations of compression ratio in the Brayton cycle, upper cations of heat engines, ranging from Small transportable temperature in the Rankine cycle, and waste heat rejection engines to very large Stationary engines. Typical applica in both cycles are removed or reduced. An important feature tions include engines for automobiles, Ships, aircrafts, and of this cycle is regeneration using the Rankine cycle work power plants. In Steam, gas, or hydroelectric power plants, ing fluid. the device that drives the electric generator is the turbine. AS FIG. 2 is a block diagram of the Cheng Cycle, which, like the fluid passes through the turbine, work is done against the the combined cycle, comprises a gas turbine. A heat recov blades which are attached to the shaft. As a result, the shaft 25 ery Steam generator (HRSG) also recovers the Cheng rotates, and the turbine produces work. Cycle's exhaust waste heat, but usually at a lower pressure A gas turbine engine is a heat engine that is operated by (under 1000 psia) and at a much higher Steam temperature. a gas or liquid fuel rather than being operated, for example, The generated Steam is then injected back into the gas by Steam or water. The two major application areas of gas turbine through a combustion chamber, which has down turbine engines are aircraft propulsion and electric power Stream turbine Stages that include both power augmentation generation. When used for aircraft propulsion, the gas tur for the turbine and cooling for the high temperature com bine produces just enough power to drive the compressor ponents. After undergoing these processes, the gas turbine and to drive a Small generator to power the auxiliary exhaust comprises both air and Steam. This additional Steam equipment. The high-velocity exhaust gases are responsible will allow the Heat Recovery Steam Generator (HRSG) to for producing the necessary thrust to propel the aircraft. 35 generate more Steam than normal gas turbine waste heat can In the application area of electric power generators, gas produce alone. turbines are used as Stationary power plants to generate FIG. 6 illustrates the components associated with an electricity. Gas turbine power plants are mostly utilized in embodiment of the Cheng Cycle. The gas turbine has a the power generation industry to cover emergencies and 40 compressor 10 linked to a turbine 13 by shaft and output to peak periods, because of their relatively low cost and quick a load. The air intake through compressed air port 1 is response time. With the deregulation of public utilities, compressed and then discharged at 2. The compressed air Systems must attain peaking power during working hours to enters a combustion chamber 12. Fuel enters the combustion follow the load profile of electrical consumption. chamber through port 11, and Steam comes from the heat Three well-known cycles for heat engines relating to gas 45 recovery steam generator (HRSG) to port 3. The mixing of turbines are the combined cycle, the Cheng cycle, and the the combusted air and Steam reaches a predetermined tur Advanced Cheng cycle. FIG. 1 is a block diagram of a bine inlet temperature, then discharges from outlet 4 through typical combined cycle. The combined cycle is a combina turbine 13, exiting the turbine at outlet 5. Exhaust gas then tion of a gas turbine cycle (known in the art as a “Brayton” passes through the heat recovery Steam generator, which is cycle) and a steam turbine cycle (known in the art as a 50 divided into two parts: a Superheater 14, and a water-to “Rankine” cycle) in series. Steam generator 15. The hot exhaust gas enters the Super The waste heat from the gas turbine cycle is used to boil heater 14, gives up the heat to Superheat the Steam entering the water in the Separate Steam cycle. A working fluid is a at 8 and exiting at 3. A duct burning capability is not fluid to and from which beat is transferred while undergoing depicted here, but would normally be located at 6. The a cycle. The combined cycle has separate loops for two 55 remainder of the heat is recovered by the unit evaporator 15 working fluids with two Separate and distinct power tur and exits at valve 17. The exhaust gas at 7 has the option of bines. The two working fluids are not mixed, unlike in the going through a cleanup or condensing unit 20, then to the Cheng cycle as will be explained below. Although Steam atmosphere. Water can be recovered through 20 or can be generated from the exhaust waste heat of a gas turbine totally used as a makeup entering or mixing with 19. Water powers the combined cycle, very high preSSure at a low 60 is compressed to a high pressure through a pump 18. The temperature is used to economically drive a conventional pump exit goes into the Steam generator at 9, and the Steam turbine and its associated accessories.