[특허]Method and apparatus for cooling the inlet air of gas turbine and internal combustion engine prime movers

Method and apparatus for cooling the inlet air of gas turbine and internal combustion engine prime movers 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F02C-001/00
출원번호	US-0054869 (1993-04-28)
발명자 / 주소	Holenberger Charles R. (611 S. Euclid St Fullerton CA 92635)
인용정보	피인용 횟수 : 97 인용 특허 : 0

초록 ▼

A multi-stage method and apparatus for cooling the inlet air of internal combustion engine and gas turbine prime movers with various load applications comprising: generating and providing a multi-stage refrigerated cooling system associated with the air inlet of internal combustion engine and gas turbine prime movers which provides thermodynamic efficiencies in accordance with a divided psychrometric inlet air cooling path enthalpy curve; cascading the cooled refrigerant from a first cooling stage as the liquid feed into a subsequent lower temperature cooling stage for cooling to the desired temperature; energizing power means to drive the prime mover and refrigerant cooling system; and adjusting the power means based on current energy costs to optimize net revenues to produce electricity or useful work from the prime mover application.

대표청구항 ▼

A method for optimizing the power output and performance of combustion prime movers such as gas turbines and internal combustion engines having air inlets taking in inlet air at the minimum acceptable inlet air temperature to prevent damage to the prime mover and its auxiliary components for admixture with fuel for combustion, and associated with a prime mover load application to increase power output and reduce fuel consumption, comprising: a. inputting into a computer processor a data base containing the prime mover\s performance output, fuel consumption, heat rate, the load application power, output power, parasitic load consumption, and other related performance system information, b. computer generating optimal thermodynamic cooling efficiencies corresponding to a sectionalized, sequentially divided psychrometric turbine inlet air cooling path enthalpy curve of the average ambient air temperature prime mover performance and the optimum air inlet temperature for maximum prime mover performance, c. Structuring and providing a stage refrigerant cooling system having separate refrigerant cooling components mounted within and associated with the air inlet to provide incremental sequential staged cooling of the inlet air by circulating refrigerant to absorb heat from the inlet air and deliver the absorbed heat to a heat sink to increase the cycle efficiency of the refrigeration system by using cooled condensate to subcool the liquid refrigerant before expansion; d. Cascading from stage to stage cooled refrigerant from a first cooling stage as feed into a successive subsequent cooling stage to sequentially cool the inlet air to a desired temperature for optimum prime mover performance, e. Inputting into the computer processor current operating costs associated with fuel consumption, maintenance, and other related operating costs of the prime mover, and current revenues from energy generation by the prime mover load application, f. Generating the optimal net revenue performance curve for the prime mover and prime mover load application, and g. Powering and adjusting power means to drive the prime mover and multi-stage refrigerant cooling system in accordance with the optimal net revenue performance curve.

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IPC	Description
A	생활필수품
A62	인명구조; 소방(사다리 E06C)
A62B	인명구조용의 기구, 장치 또는 방법(특히 의료용에 사용되는 밸브 A61M 39/00; 특히 물에서 쓰이는 인명구조 장치 또는 방법 B63C 9/00; 잠수장비 B63C 11/00; 특히 항공기에 쓰는 것, 예. 낙하산, 투출좌석 B64D; 특히 광산에서 쓰이는 구조장치 E21F 11/00)
A62B-1/08	.. 윈치 또는 풀리에 제동기구가 있는 것

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Method and apparatus for cooling the inlet air of gas turbine and internal combustion engine prime movers 원문보기

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Method and apparatus for cooling the inlet air of gas turbine and internal combustion engine prime movers 원문보기

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