摘要:
An inner bleed structure of the 2-shaft gas turbine includes a slit 51 for leading part of compressed air to a cavity is formed between a wall surface of a rotor wheel 25 of the compressor 2 equipped with a last stage rotor of the compressor 2 which is connected to a first rotating shaft 6 and end of an inner casing 27, and a bleed hole 52 for leading part of compressed air after flowing down the last stage of the compressor 2 to a cavity formed in the inner side of the inner casing 27 at the downstream side of the last stage of the compressor 2.
摘要:
A transonic blade is provided that operates in a flow field where flow has a transonic speed or higher in an axial-flow rotating machine and that concurrently achieves a reduction in shock loss and in the local stress of the blade. The transonic blade includes a hub cross-sectional surface joined to a rotating shaft or an outer circumferential side casing of a rotating machine; a tip cross-sectional surface located furthest from the hub cross-sectional surface in a spanwise direction which is a vertical direction of the rotating shaft; a leading edge located on an upstream side; and a trailing edge located on a downstream side. At least a part of a passing working fluid flow has a transonic speed or higher. A portion of a stacking line which is a line connecting together respective gravity centers of cross-sectional surfaces located from the hub cross-sectional surface to the tip cross-sectional surface is located on a downstream side of a stacking center in a flow direction of a working fluid main flow.
摘要:
Provided is a two-shaft gas turbine with improved reliability that improves output power and efficiency and is stably operated by establishing a balance between the driving force of a compressor 1 and the output power of a high-pressure turbine 3H in the case where the two-shaft gas turbine is applied to a system in which the flow rate of fluid flowing into a combustor 2 is increased compared with a simple cycle gas turbine. A portion of working fluid 37 driving the high-pressure turbine 3H is allowed to flow not into the high-pressure turbine 3H but into a low-pressure turbine 3L.
摘要:
in a screw rotor including a female rotor member (1) and a male rotor member (2) rotatable about parallel shafts (3) and (4) respectively while meshing with each other, the forward face flank of the female rotor member (1) is composed of a first flank (7) of the forward face formed by a parabolic curve, and a second flank (8) of the forward face formed by a circular arc of a radius R 2 , and the backward face flank of the female rotor member (1) is composed of a first flank (9) of the backward face generated by the backward face tooth top flank of the male rotor member (2) having a radius R., and a second flank (10) of the backward face formed by a circular arc of a radius R 3 which is smaller than the radius R 2 of the second flank (7) of the forward face flank. The tooth profile of the male rotor member (2) is essentially formed by the forward face flank and the backward face flank of the male rotor member (2).
摘要:
A heat pump includes an evaporator 10 evaporating water; a steam compressor 1 compressing the vapor generated by the evaporator 10; a vapor supply duct 31 adapted to supply the vapor 30 compressed by the compressor 1 to steam-utilizing facility 2; a measuring device 91 for measuring a state of vapor between the evaporator 10 and the compressor 1; and a valve 81 adjusting an amount of vapor flowing in the compressor 1 based on information from the measuring device 91.
摘要:
A method of controlling an operation of a 2-shaft gas turbine comprises, when an operation of a 2-shaft gas turbine is changed to reduce a load from a predetermined load, a first step of reducing a rotating speed of a compressor (1) and a second step of reducing a working airflow in the compressor (1). With the method, a reduction in compressor (1) efficiency during partial load operation of the gas turbine can be suppressed, and a surge margin of the compressor can be ensured.
摘要:
in a screw rotor including a female rotor member (1) and a male rotor member (2) rotatable about parallel shafts (3) and (4) respectively while meshing with each other, the forward face flank of the female rotor member (1) is composed of a first flank (7) of the forward face formed by a parabolic curve, and a second flank (8) of the forward face formed by a circular arc of a radius R 2 , and the backward face flank of the female rotor member (1) is composed of a first flank (9) of the backward face generated by the backward face tooth top flank of the male rotor member (2) having a radius R., and a second flank (10) of the backward face formed by a circular arc of a radius R 3 which is smaller than the radius R 2 of the second flank (7) of the forward face flank. The tooth profile of the male rotor member (2) is essentially formed by the forward face flank and the backward face flank of the male rotor member (2).
摘要:
A gas turbine having a compressor for compressing air, a combustor (2) for taking in compressed air discharged from the compressor (1), mixing it with fuel, and burning them, and a turbine (3) driven by combustion gas generated in the combustor (2), comprising: inlet guide vanes (6) installed at a stage near an inlet of the compressor (1) for adjusting a compressor flow rate by changing an attaching angle thereof, a steam injection mechanism (7) for injecting steam to the combustor (2), a steam adjustment valve for adjusting the steam injection rate, and a steam rate control mechanism for adjusting an opening of the steam adjustment valve, a steam monitoring mechanism (23) for monitoring the steam rate injected to the combustor (2), an air temperature monitoring mechanism (24) for monitoring an atmospheric temperature, and a control unit (46) for determining whether a restriction value of the steam injection rate using a temperature, an opening of the inlet guide vanes (6), and the steam injection rate as indexes is satisfied, and controlling at least one of a temperature of air flowing into the compressor (1), the steam injection rate, and the inlet guide vane opening.