摘要:
A turboexpander-compressor system (200) includes an expander (210) configured to expand an incoming gas (214), a first set of moveable inlet guide vanes (218) configured to control a pressure of the incoming gas, a compressor (224) configured to compress a gas received from the expander (210), a shaft (230) configured to support and rotate an expander impeller (212) and a compressor impeller (226), a second set of moveable inlet guide vanes (232) attached to the compressor (224) and configured to control a pressure of the gas input into the compressor (224), and a controller (240) configured to acquire information about a rotating speed of the shaft (230), a pressure and a temperature of the incoming gas, a pressure and a temperature of the gas output from the expander (210), and to control the second set of moveable inlet guide vanes (232) to maximize a ratio between the rotating speed of the shaft (230) and a drop of an enthalpy across the expander (210), in off-design conditions.
摘要:
Method and nozzle adjustment mechanism (50) for adjusting a flow of a fluid. The nozzle adjustment mechanism (50) includes a fixed ring (52); at least a vane (56) connected to the fixed ring (52) by a pivot pin (70) and configured to rotate with the pivot pin (70); an adjusting ring (54) rotatably connected to the fixed ring (52) and configured to rotate around a longitudinal axis (Z) of the nozzle adjustment mechanism (50); and a connection mechanism (58, 60) connecting the at least a vane (56) to the adjusting ring (54) and configured to move the at least a vane (56) when the adjusting ring is (54) rotated, the connection mechanism (58, 60) including a lever component (58) and a link component (60) connected to each other. The lever component (58) is connected to the at least a vane (56) and the link component (60) is connected to the adjusting ring (54).
摘要:
Method and nozzle adjustment mechanism (50) for adjusting a flow of a fluid. The nozzle adjustment mechanism (50) includes a fixed ring (52); at least a vane (56) connected to the fixed ring (52) by a pivot pin (70) and configured to rotate with the pivot pin (70); an adjusting ring (54) rotatably connected to the fixed ring (52) and configured to rotate around a longitudinal axis (Z) of the nozzle adjustment mechanism (50); and a connection mechanism (58, 60) connecting the at least a vane (56) to the adjusting ring (54) and configured to move the at least a vane (56) when the adjusting ring is (54) rotated, the connection mechanism (58, 60) including a lever component (58) and a link component (60) connected to each other. The lever component (58) is connected to the at least a vane (56) and the link component (60) is connected to the adjusting ring (54).
摘要:
A turboexpander-compressor system (200) includes an expander (210) configured to expand an incoming gas (214), a first set of moveable inlet guide vanes (218) configured to control a pressure of the incoming gas, a compressor (224) configured to compress a gas received from the expander (210), a shaft (230) configured to support and rotate an expander impeller (212) and a compressor impeller (226), a second set of moveable inlet guide vanes (232) attached to the compressor (224) and configured to control a pressure of the gas input into the compressor (224), and a controller (240) configured to acquire information about a rotating speed of the shaft (230), a pressure and a temperature of the incoming gas, a pressure and a temperature of the gas output from the expander (210), and to control the second set of moveable inlet guide vanes (232) to maximize a ratio between the rotating speed of the shaft (230) and a drop of an enthalpy across the expander (210), in off-design conditions.
摘要:
Method and nozzle adjustment mechanism (50) for adjusting a flow of a fluid. The nozzle adjustment mechanism (50) includes a fixed ring (52); at least a vane (56) connected to the fixed ring (52) by a pivot pin (70) and configured to rotate with the pivot pin (70); an adjusting ring (54) rotatably connected to the fixed ring (52) and configured to rotate around a longitudinal axis (Z) of the nozzle adjustment mechanism (50); and a connection mechanism (58, 60) connecting the at least a vane (56) to the adjusting ring (54) and configured to move the at least a vane (56) when the adjusting ring is (54) rotated, the connection mechanism (58, 60) including a lever component (58) and a link component (60) connected to each other. The lever component (58) is connected to the at least a vane (56) and the link component (60) is connected to the adjusting ring (54).