Combined system of gas turbine
A gas turbine and combined system technology, which is applied in gas turbine installations, charging systems, turbine/propulsion fuel delivery systems, etc., can solve the problem that the latent heat of gasification is not effectively recovered or utilized.
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0026] Please check figure 1 , a gas turbine combined system, including a gas turbine fueled by ammonia, a low-temperature recovery device 5 and a waste heat recovery device 7 . The gas turbine includes a liquid ammonia supply device 4 , a compressor 2 , a combustor 1 and a turbine 3 . The low temperature recovery device 5 is connected between the liquid ammonia supply device 4 and the combustion chamber 1, the liquid ammonia is changed into gaseous ammonia by the low temperature recovery device 5, and the gaseous ammonia is supplied into the combustion chamber 1, and the low temperature recovery device 5 recovers The cooling capacity of liquid ammonia gasification. The compressor 2 is connected to the combustor 1 to compress gas including air and supply it to the combustor 1 . The combustor 1 contains the mixed combustion of gaseous ammonia and air. The exhaust gas from the combustor 1 drives the turbine 3 to run and is discharged from the exhaust passage 6. The turbine 3 a...
Embodiment 2
[0030] Please check figure 2 , it differs from Embodiment 1 in that: the low-temperature recovery device 5 includes a heat exchange path through which the liquid ammonia changes from liquid ammonia to gaseous ammonia, and the heat exchange path recovers the cooling capacity of the vaporization of liquid ammonia . The heat exchange channel cooperates with the compressor 2 to cool the air through the heat exchange channel, and the cooled air enters the compressor 2 . Due to the high latent heat of vaporization of liquid ammonia (at -33.41°C and 101.325kPa, the latent heat of vaporization reaches 1371.18kJ / kg), the air temperature is lowered, a higher air compression ratio is obtained, and the air intake volume is increased. At the same time, the liquid ammonia vaporizes to absorb the heat generated by the blades of the compressor 2, thereby reducing the temperature of the blades.
[0031] The waste heat recovery device 7 includes a heat exchanger, which can be at least one of...
Embodiment 3
[0034] Please check image 3 , a gas turbine combined system, including a gas turbine fueled by ammonia, a low-temperature recovery device 5 and a waste heat recovery device 7 . The gas turbine includes a combustor 1 , a compressor 2 , a turbine 3 and a liquid ammonia supply device 4 . The low-temperature recovery device 5 includes a heat exchange passage through which liquid ammonia changes from liquid ammonia to gaseous ammonia. image 3 A partial side sectional view diagrammatically showing a specific application example of the gas turbine integrated system of the present invention. refer to image 3 An output shaft 11 is rotatably supported in a casing 10 of the gas turbine, and the output shaft 11 is connected to the generator 7 via a speed reducer. The compressor 2 is constituted by a multistage compressor having a plurality of stationary blades 12 supported by a housing 10 and a plurality of moving blades 13 formed on an output shaft 11, and suction air entering from...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More 


