Independently-controlled gas turbine inlet guide vanes and variable stator vanes
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F01D-017/26
F01D-017/16
F02C-007/057
출원번호
US-0091540
(2011-04-21)
등록번호
US-9068470
(2015-06-30)
발명자
/ 주소
Mills, Jeffrey Patrick
Ruddy, Jeffrey Mark
출원인 / 주소
GENERAL ELECTRIC COMPANY
대리인 / 주소
Nixon & Vanderhye P.C.
인용정보
피인용 횟수 :
3인용 특허 :
20
초록▼
A system adjusts positions of gas turbine inlet guide vanes (IGVs) and variable stator vanes (VSVs). The system includes a hydraulic power unit providing a supply of hydraulic fluid, an IGV servo in fluid communication with the hydraulic power unit, and a VSV servo in fluid communication with the hy
A system adjusts positions of gas turbine inlet guide vanes (IGVs) and variable stator vanes (VSVs). The system includes a hydraulic power unit providing a supply of hydraulic fluid, an IGV servo in fluid communication with the hydraulic power unit, and a VSV servo in fluid communication with the hydraulic power unit. An IGV cylinder set is provided in fluid communication with the hydraulic power unit via the IGV servo and is connected to the IGVs. The IGV cylinder set effects displacement of the IGVs between a closed position and a fully open position. A VSV cylinder set is provided in fluid communication with the hydraulic power unit via the VSV servo. The VSVs include multiple stages linked together with a torque shaft. The VSV cylinder set is connected to the torque shaft, and the VSV cylinder set effects simultaneous displacement of the stages of the VSVs between a closed position and a fully open position. The IGV servo and the VSV servo respectively control delivery of hydraulic fluid from the hydraulic power unit to the IGV cylinder set and the VSV cylinder set, and the IGV servo and the VSV servo are independently controllable.
대표청구항▼
1. A system for adjusting positions of gas turbine inlet guide vanes (IGVs) including a first set of vanes and variable stator vanes (VSVs) including a second set of vanes, the system comprising: a hydraulic power unit providing a supply of hydraulic fluid;an IGV servo in fluid communication with th
1. A system for adjusting positions of gas turbine inlet guide vanes (IGVs) including a first set of vanes and variable stator vanes (VSVs) including a second set of vanes, the system comprising: a hydraulic power unit providing a supply of hydraulic fluid;an IGV servo in fluid communication with the hydraulic power unit;a VSV servo in fluid communication with the hydraulic power unit;an IGV cylinder set in fluid communication with the hydraulic power unit via the IGV servo and connected to the IGVs, the IGV cylinder set effecting tandem displacement of the first set of vanes between a closed position and a fully open position;a VSV cylinder set in fluid communication with the hydraulic power unit via the VSV servo, the VSV cylinder set being separate and independent from the IGV cylinder set, the VSVs including the second set of vanes across multiple stages linked together with a torque shaft, wherein VSV cylinder set is connected to the torque shaft, and wherein the VSV cylinder set effects simultaneous displacement of the stages of the VSVs between a closed position and a fully open position,wherein the IGV servo and the VSV servo respectively control delivery of hydraulic fluid from the hydraulic power unit to the IGV cylinder set and the VSV cylinder set, and wherein the IGV servo and the VSV servo are independently controllable; andtrip valves cooperable with each of the IGV servo and the VSV servo, each of the trip valves being activated to bypass the IGV and VSV servos, respectively, and close the IGVs and the VSVs. 2. A system according to claim 1, wherein the IGV cylinder set comprises a first IGV cylinder for one side of the IGVs and a second IGV cylinder for an opposite side of the IGVs, and wherein the VSV cylinder set comprises a first VSV cylinder for one side of the VSVs and a second VSV cylinder for an opposite side of the VSVs, the hydraulic fluid being equally delivered to the first and second IGV cylinders, and equally to the first and second VSV cylinders. 3. A system according to claim 1, further comprising a position detecting assembly producing a signal representative of a position of the IGVs and the VSVs. 4. A system according to claim 3, wherein the position detecting assembly comprises a linear variable differential transformer (LVDT) internally positioned in each of the IGV cylinder set and the VSV cylinder set, the LVDTs measuring a length of the respective cylinder sets. 5. A system according to claim 1, further comprising a manifold interposed between the hydraulic power unit and the IGV and VSV servos, the manifold distributing hydraulic fluid to the IGV and VSV servos. 6. A system according to claim 1, further comprising a temperature sensor measuring an exhaust temperature of the gas turbine, wherein the positions of the IGVs and the VSVs are adjusted according to the exhaust temperature. 7. A system according to claim 1, further comprising filters positioned between the IGV servo and the IGV cylinder set and between the VSV servo and the VSV cylinder set. 8. A system according to claim 1, further comprising a filter positioned between the hydraulic power unit and the IGV and VSV servos. 9. A system according to claim 1, wherein the IGV cylinder set and the VSV cylinder set are biased toward an extended position corresponding to the closed position of the IGVs and the VSVs, and wherein the trip valves are configured such that activation of the trip valves drains the hydraulic fluid from the IGV cylinder set and the VSV cylinder set, thereby closing the IGVs and the VSVs. 10. A gas turbine comprising: a compressor receiving inlet air and mixing the inlet air with fuel;a combustor that receives the inlet air and fuel mixture and that combusts the mixture to produce hot products of combustion; anda turbine receiving the hot products of combustion and converting the hot products of combustion into work,the compressor including a set of inlet guide vanes (IGVs) and a set of variable stator vanes (VSVs), wherein respective positions of the IGVs and the VSVs affect a performance efficiency of the gas turbine, and the compressor including a system for adjusting the positions of the set of IGVs and the set of VSVs, the system includes: a hydraulic power unit providing a supply of hydraulic fluid,an IGV servo in fluid communication with the hydraulic power unit,a VSV servo in fluid communication with the hydraulic power unit,an IGV cylinder set in fluid communication with the hydraulic power unit via the IGV servo and connected to the IGVs, the IGV cylinder set effecting tandem displacement of the IGVs between a closed position and a fully open position,a VSV cylinder set in fluid communication with the hydraulic power unit via the VSV servo, the VSV cylinder set being separate and independent from the IGV cylinder set, the VSVs including the second set of vanes across multiple stages linked together with a torque shaft, wherein VSV cylinder set is connected to the torque shaft, and wherein the VSV cylinder set effects simultaneous displacement of the stages of the VSVs between a closed position and a fully open position,wherein the IGV servo and the VSV servo respectively control delivery of hydraulic fluid from the hydraulic power unit to the IGV cylinder set and the VSV cylinder set, and wherein the IGV servo and the VSV servo are independently controllable, andtrip valves cooperable with each of the IGV servo and the VSV servo, each of the trip valves being activated to bypass the IGV and VSV servos, respectively, and close the IGVs and the VSVs. 11. A gas turbine according to claim 10, wherein the IGV cylinder set comprises a first IGV cylinder for one side of the IGVs and a second IGV cylinder for an opposite side of the IGVs, and wherein the VSV cylinder set comprises a first VSV cylinder for one side of the VSVs and a second VSV cylinder for an opposite side of the VSVs, the hydraulic fluid being equally delivered to the first and second IGV cylinders, and equally to the first and second VSV cylinders. 12. A gas turbine according to claim 10, further comprising a position detecting assembly producing a signal representative of a position of the IGVs and the VSVs. 13. A gas turbine according to claim 12, wherein the position detecting assembly comprises a linear variable differential transformer (LVDT) internally positioned in each of the IGV cylinder set and the VSV cylinder set, the LVDTs measuring a length of the respective cylinder sets. 14. A gas turbine according to claim 10, further comprising a temperature sensor measuring an exhaust temperature of the gas turbine, wherein the positions of the IGVs and the VSVs are adjusted according to the exhaust temperature. 15. A gas turbine according to claim 10, wherein the IGV cylinder set and the VSV cylinder set are biased toward an extended position corresponding to the closed position of the IGVs and the VSVs, and wherein the trip valves are configured such that activation of the trip valves drains the hydraulic fluid from the IGV cylinder set and the VSV cylinder set, thereby closing the IGVs and the VSVs.
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이 특허에 인용된 특허 (20)
Reed Terry J. (North Huntingdon PA) Smith Jack R. (Pittsburgh PA), Control apparatus for modulating the inlet guide vanes of a gas turbine employed in a combined cycle electric power gene.
Wickert, Thomas Edward; Sweet, Bryan Edward, Method and operational strategy for controlling variable stator vanes of a gas turbine power generator compressor component during under-frequency events.
Andrew Philip Lynn ; Marks Paul Thomas ; Dwyer Daniel Robert ; Stampfli John David ; Cotroneo Joseph Anthony ; Miller Harold Edward ; Wesorick Ronald Richard, Method of operation of industrial gas turbine for optimal performance.
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