Hybrid turboshaft power system and method based on supercritical carbon dioxide

A carbon dioxide and power system technology, applied in the direction of machines/engines, steam engine devices, mechanical equipment, etc., can solve problems such as high-temperature gas ejection

Pending Publication Date: 2019-08-09
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] Another problem with the traditional turboshaft power system is that about 5% of the high-temperature gas is sprayed out

Method used

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  • Hybrid turboshaft power system and method based on supercritical carbon dioxide
  • Hybrid turboshaft power system and method based on supercritical carbon dioxide
  • Hybrid turboshaft power system and method based on supercritical carbon dioxide

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Embodiment Construction

[0030] figure 1 It is a hybrid turboshaft power system based on supercritical carbon dioxide proposed by the present invention. Refer to figure 1 with figure 2 Explain the working process of the system when the helicopter working environment is good.

[0031] When the working environment is good, the traditional gas turbine is working, close the S-CO2 gas supply section electric switch valve A9, S-CO2 gas supply section electric switch valve B11, S-CO2 gas supply section electric switch valve C19, and supplement gas section electric switch valve 27. The electric switch valve 30 of the chemical reaction gas supply section, the electric switch valve 24 of the chemical reaction feed section, and the electric switch valve 17 of the carbon dioxide discharge section, open the electric switch valve 5 of the gas discharge section. The outside air enters the compressor 1, compressed and enters the combustion chamber 2 at a constant pressure, and then flows through the check valve 3 of the...

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Abstract

The invention discloses a hybrid turboshaft power system and method based on supercritical carbon dioxide, and belongs to the field of new energy and high efficiency power. The system mainly includesa compressor, a combustion chamber, a turbine, a heat storage tank, an S-CO2 gas storage tank, a solid fuel storage tank, a chemical reactor, a heat exchanger, a carbon dioxide buffer tank, a carbon dioxide exhaust storage tank, a cyclone separator and a solid powder recovery tank. The hybrid turboshaft power system and method are characterized in that with the help of the supercritical property and high energy storage density of the carbon dioxide, the strong power capability can be generated after heating; the S-CO2 needs to be properly heated before work doing, and one heat source can be selected from heat of tail gas of a conventional gas turbine; and the heat storage tank is used for realizing storage and release of energy, and the temperature of the exhausted tail gas can be reduced;as for preparation of the S-CO2, the S-CO2 can be produced in advance at the grid load low ebb period, and therefore an auxiliary power system can work without the aid of the compressor. The system can reduce infrared radiation, can reduce use of traditional fossil energy, and has high environmental protection.

Description

Technical field [0001] The invention discloses a hybrid turboshaft power system and method based on supercritical carbon dioxide, and belongs to the field of new energy and high-efficiency power. Background technique [0002] The traditional turboshaft power system is an open power output system, so the design of the intake duct is complicated and difficult. In the event of sand, dust or hail and other weather, the particles in the airflow must be gathered together and separated from the air and discharged outside the machine. Create a good air intake environment for the compressor to work stably. [0003] Another problem with traditional turboshaft power systems is that about 5% of high-temperature gas is ejected outward. The heat flow discharged from the system will produce strong infrared radiation; the common solution is to suck in the outside air, mix it with the high-temperature gas and cool it out. [0004] Carbon dioxide is non-toxic, has good physical and chemical properti...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F01K7/32F01K11/02F01K13/02F01K25/10
CPCF01K7/32F01K11/02F01K13/02F01K25/103
Inventor 陈恺祺蒲文灏张豪宋张扬岳晨何纬峰韩东
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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