US2963032A - Hydraulic system for steam turbine - Google Patents

Hydraulic system for steam turbine Download PDF

Info

Publication number
US2963032A
US2963032A US837009A US83700959A US2963032A US 2963032 A US2963032 A US 2963032A US 837009 A US837009 A US 837009A US 83700959 A US83700959 A US 83700959A US 2963032 A US2963032 A US 2963032A
Authority
US
United States
Prior art keywords
pump
liquid
oil
turbine
pressure
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US837009A
Inventor
Clarence E Kenney
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Allis Chalmers Corp
Original Assignee
Allis Chalmers Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US390472A external-priority patent/US2949122A/en
Application filed by Allis Chalmers Corp filed Critical Allis Chalmers Corp
Priority to US837009A priority Critical patent/US2963032A/en
Application granted granted Critical
Publication of US2963032A publication Critical patent/US2963032A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/20Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted
    • F01D17/22Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted the operation or power assistance being predominantly non-mechanical
    • F01D17/26Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted the operation or power assistance being predominantly non-mechanical fluid, e.g. hydraulic

Definitions

  • This invention relates generally to a hydraulic system for supplying liquid under pressure to a machine and more specifically to an improved system in a steam turbine for supplying high pressure oil for operating auxiliary hydraulic systems such as a governing system, and low pressure oil for lubrication.
  • auxiliary hydraulic systems such as a governing system, and low pressure oil for lubrication.
  • the nature of the present invention resides in the provision of an improved hydraulic system for steam turbines whereby none of the high pressure fluid supplied by the main pump to the hydraulic turbine, bypasses the hydraulic turbine to pass through pressure reducing means for low pressure bearing lubrication. Instead, the discharge of the low pressure pump is utilized for bearing lubrication with the hydraulic turbine discharging to the intake of the main pump. Therefore, more of the energy derived from the drop in pressure from the high pressure produced by the main pump to the low pressure required for lubrication, is utilized to operate the hydraulic turbine and low pressure pump, .and none of this energy is wastefully dissipated by bypassing the hydraulic turbine and throttling for lubrication purposes as has heretofore been done.
  • Another object of the invention is to provide a systern for supplying liquid to a machine at two different pressures that are more economical than prior known systems.
  • this invention is illustrated as applied to a machine such as a steam turbine indicated generally at 1 and having a shaft 2, a lubrication system including a bearing 3 to which oil is supplied under pressure, and a servomotor indicated generally at 4 in the governing system to which oil is supplied under pressure through a conduit 5.
  • the governor is arranged to control a servomotor which may be in the form of a piston 6 slidably arranged in a cylinder 7, for positioning a turbine inlet control valve 8.
  • Motive fluid is supplied to the turbine 1 through an inlet conduit and the speed and output of the turbine are controlled by regulation of the valve 8 through the sermomotor 4.
  • Any other suitable known type of governing system for turbines may be substituted for the governor and servomotor 4. i
  • a liquid which may be oil for lubricating the turbine and a second liquid which may be water or another noninflammable liquid for actuating the governing system, is supplied from a reservoir 12, which is customarily located at a level below the turbine 1 so that the oil supplied to the bearings and other components may conveniently be drained back to the reservoir 12 by gravity.
  • the oil for lubricating the turbine may be a petroleum product or any other suitable known liquid having lubricating properties. In the drawing the turbine lubrication system is drained by means of a conduit 13.
  • the reservoir 12 is divided by means of a plate 10 into two hydraulically independent reservoirs or compart-ments, one 12a for the high pressure system utilizing a noninflammable liquid, and another 12b for the low pressure system that utilizes oil.
  • a main pump may be driven by any suitable prime mover but is preferably directly coupled to an extension 16 of the turbine shaft 2.
  • This main pump-1 4 has an impeller, not shown, mounted directly on the turbine shaft extension 16.
  • the pump is enclosed by a casing 17 which defines an annular pump inlet 18 and a discharge scroll 21. Any suitable type of pump other than a centrifugal pump may also be employed.
  • the discharge scroll 21 of the pump 14 communicates with a discharge pipe 22, to which is connected the servomotor supply conduit 5.
  • a suitable pressure regulating valve 23 may be incorporated in the conduit 5 to maintain the pressure of the liquid supplied to the servomotor 4 constant at a preselected value.
  • Spent liquid from the servomotor 4 returns through conduit 24 to the inlet 18 of pump 14, as noted hereinafter.
  • a suitable check valve 25 is provided in conduit 22 to prevent flow of liquid in a reverse direction through pump 14.
  • a hydraulic turbine 26 Arranged, in the liquid reservoir 12a or in any other suitable location is a hydraulic turbine 26 consisting of a housing 27, an impeller, not shown, and an inlet scroll 31.
  • a conduit 32 supplies liquid under pressure from the discharge scroll 21 of pump 14 to the inlet scroll 31 of turbine 26. Liquid discharge from the turbine 26 is led by a conduit 33 to the inlet 18 of the main pump 14.
  • the shaft 34 of the hydraulic turbine 26 is a common or connected shaft to a hydraulic pump 36.
  • the hydraulic pump 36 is located below the level of the oil in reservoir 12b and may be placed within the reservoir as shown. It defines an inlet opening 37 for admitting oil from the reservoir 12b to the pump impeller, not shown, and to a pump discharge scroll 38.
  • a conduit 41 containing a check valve 42 delivers low pressure oil from the discharge scroll 38 to the inlet of a suitable oil cooler 43 through which cooling water is circulated.
  • lubricating oil is supplied to a hydraulic seal of a hydrogen cooled electric generator, not shown, driven by steam turbine 1 and through a reducer 44 and conduit 45 to the lubrication system and bearing 3 of the steam turbine.
  • an auxiliary starting pump 65 driven by a motor 64 is used to provide low pressure oil to the lubrication system and bearing 3.
  • an auxiliary source of liquid under pressure is required to actuate the servomotor 4 and to prime the governing system.
  • This source may comprise a second auxiliary pump group indicated generally at 48 and consisting of a motor 51 driving a centrifugal pump 52 similar to pump 36 located below the liquid level in reservoir 12a.
  • An inlet opening 53 is arranged to admit liquid from reservoir 12a to the pump 52.
  • a conduit 54 supplies liquid under pressure from the pump 52 through a suitable check valve 55 to the conduit where the liquid is supplied to the servomotor 4.
  • the low pressure oil discharge from the pump 65 is led by a conduit 68 to the conduit 41 leading into the oil cooler 43. From the oil cooler 43, the low pressure oil is supplied through reducer 44 and through conduit 45 to the lubrication system of the turbine.
  • the motors 51 and 64 are energized and liquid is supplied by the starting pump 52 to servomotor 4 and lubricating oil is supplied by pump 65 to bearing 3.
  • Check valve 25 in conduit 22 prevents this priming liquid from flowing backwards through the main pump 14.
  • Check valve 42 in conduit 41 prevents oil from flowing backwards through pump 36.
  • Suitable control means both indicated generally as 71 may be provided for the starting motor 51 and motor 64, and so arranged that the motors are automatically deenergized when the pressure in conduits 32 and 41, respectively, rises to a value in excess of the preselected value determined by a spring 72 in each control system 71.
  • the control systems 71 each comprise a toggle switch 73 which is well known in the art coupled to a piston 75, so that the switch 73 breaks the circuit to the motors when liquid pressure in conduits 32 and 41, respectively, exceeds the preselected value determined by the spring 72 forcing the piston 75 inward.
  • the spring 72 biases the piston 75 so that the switch 73 is in a closed position so that motor 51 and motor 64 will be energized whenever the pressure in conduit 32 and/or 41 falls below the preselected value of a spring 72.
  • the hydraulic system for the steam turbine 1 in eflect comprises a high pressure circuit and a low pressure circuit with the shaft 34 connecting theturbine 26 of the high pressure circuit to the pump 36 of the low pressure circuit.
  • the high pressure circuit comprises the main pump 14 in series with the parallel connected servomotor 4 of the steam turbine 1, and the hydraulic turbine 26.
  • the low pressure circuit comprises the pump 36, the oil cooler 43 and the lubrication system of the steam turbine connected in series.
  • liquid is delivered by the main pump 14 to the conduit 22 at a pressure suitable for operation of the servomotor 4.
  • This pressure may be of the order of 200 pounds per square inch, which is considerably higher than is ordinarily used for lubrication purposes.
  • the turbine lubrication system may be of the order of only 15 pounds per square inch.
  • An important feature of the invention is that the reduction of the liquid, pressure from the value required for operation of the servomotor 4 to that required for maintaining the prime of the pump 14 is accomplished in a manner which makes use of the energy represented by this pressure drop. This is efifected by causing the pressure drop to occur across the hydraulic turbine 26 which serves to drive the hydraulic pump 36. This method of conserving the energy in the system is found to make an important contribution to the overall efiiciency of the prime mover by reducing the power needed to drive the pump 14.
  • This improved liquid supply system provides a liquid, which may be noninflammable, at a comparatively high pressure for operating hydraulic devices such as a servomotor 4, and also supplies oil at a much lower pressure for lubrication.
  • This is accomplished by the high speed pump 14 coupled directly to the shaft 2 of the prime mover 1 without intermediate gearing and having the hydraulic turbine 26 arranged to positively prime the main pump 14 when the steam turbine 1 is at its operating speed.
  • the hydraulic turbine 26 is driven by energy derived from the drop in pressure from the high value required for the servomotor 4' to the lower value required to maintain the prime of pump 14.
  • the high pressure liquid system may utilize water or any other noninflammable liquid that is completely separate from the low pressure liquid system utilizing lubricating oil whereas in the parent application a common liquid is used for both the governing and lubrication systems.
  • a hydraulic system including a machine requiring a primary supply of noninflammable liquid at a comparative high pressure and a secondary supply of lubricating oil at a lower pressure, the combination of a first pump arranged to be driven by the machine; a hydraulic turbine; a servomotor requiring a supply of noninflammable liquid at a high pressure; said first pump, said hydraulic turbine, and saidservomotor forming a closed high pressure circuit with the discharge of said first pump supplied to the intake of said hydraulic turbine and said servomotor, and the discharge of said hydraulic turbine and said servomotor supplied to the intake of said first pump; a first reservoir; a second pump arranged to receive liquid from said first reservoir, the discharge of said second pump supplied to said servomotor to start the machine, and the discharge from said servomotor supplied to the intake of said first pump to prime said first pump; a first control means for automatically interrupting the flow of liquid from said second pump into said high pressure circuit when the pressure of the liquid delivered by said first pump exceeds the liquid pressure developed by
  • a first pump arranged to be driven by the steam turbine; a hydraulic turbine; a first conduit connecting the output of said first pump to the input of said hydraulic turbine; a second conduit connecting the output of said hydraulic turbine to the input of said first pump whereby it is positively primed during normal operation; a servomotor requiring a supply of liquid at a high pressure; a third conduit connecting the output of said first pump to the input of said servomotor; a fourth conduit connecting the output of said servomotor to the input of said first pump; a first liquid resrvoir; means for starting the steam turbine and priming said first pump including a second pump arranged to receive liquid from said first reservoir and to supply high pressure liquid through a fifth conduit to the inlet of said servomotor to actuate said servomotor to cause steam to be admitted to the steam turbine to start the steam turbine and the output

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Description

Dec. 6, 1960 c. E. KENNEY I 2,963,032 HYDRAULIC SYSTEM FOR STEAM TURBINE Original Filed Nov. e, 1953 2,963,032 HYDRAULIC SYSTEM FOR STEAM TURBINE Clarence E. Kenney, Waukesha, Wis., assignor to Allis- Chalmers Manufacturing Company, Milwaukee, Wis.
Original application Nov. 6, 1953, Scr. No. 390,472. and this application Aug. 31, 1959, Ser. No.
2 Claims. (Cl. 137-17) This invention relates generally to a hydraulic system for supplying liquid under pressure to a machine and more specifically to an improved system in a steam turbine for supplying high pressure oil for operating auxiliary hydraulic systems such as a governing system, and low pressure oil for lubrication. This is a division of my copending application entitled Hydraulic System for Steam Turbine, Serial Number 390,472, filed November 6, 1953.
It has heretofore been proposed to supply high and low pressure oil to a prime mover such as a steam tur bine by providing a main centrifugal pump directly coupled to the prime mover shaft. A portion of the discharge from the main pump which is at a high pressure is supplied to the governing system of the turbine and to a hydraulic turbine; the remainder of the discharge of the main pump is bypassed around the hydraulic turbine and passes through pressure reducing means to an oil cooler and then supplied to bearings of the prime mover. The hydraulic turbine derives its energy from the pressure differential between the high pressureintake from the main pump and low pressure discharge of oil from the hydraulic turbine. A low pressure pump is directly connected to and driven by the hydraulic turbine. The low pressure pump takes suction from a reservoir and discharges to the intake of the main pump. The nature of the present invention resides in the provision of an improved hydraulic system for steam turbines whereby none of the high pressure fluid supplied by the main pump to the hydraulic turbine, bypasses the hydraulic turbine to pass through pressure reducing means for low pressure bearing lubrication. Instead, the discharge of the low pressure pump is utilized for bearing lubrication with the hydraulic turbine discharging to the intake of the main pump. Therefore, more of the energy derived from the drop in pressure from the high pressure produced by the main pump to the low pressure required for lubrication, is utilized to operate the hydraulic turbine and low pressure pump, .and none of this energy is wastefully dissipated by bypassing the hydraulic turbine and throttling for lubrication purposes as has heretofore been done.
It is therefore an object of the present invention to more efiiciently utilize the available energy represented by the pressure drop between the high value required for the governing system and hydraulic turbine and the low value required for lubrication.
Another object of the invention is to provide a systern for supplying liquid to a machine at two different pressures that are more economical than prior known systems.
nited. States Patent 0 e.
Patented Dec. 6, 1960 Another object of the invention is to require smaller above will be apparent from the following description when read in connection with the accompanying drawing, in which a diagrammatic view is shown, partly in section, of a system embodying the invention.
Referring to the drawing, this invention is illustrated as applied to a machine such as a steam turbine indicated generally at 1 and having a shaft 2, a lubrication system including a bearing 3 to which oil is supplied under pressure, and a servomotor indicated generally at 4 in the governing system to which oil is supplied under pressure through a conduit 5. As is well known, the governor is arranged to control a servomotor which may be in the form of a piston 6 slidably arranged in a cylinder 7, for positioning a turbine inlet control valve 8. Motive fluid is supplied to the turbine 1 through an inlet conduit and the speed and output of the turbine are controlled by regulation of the valve 8 through the sermomotor 4. Any other suitable known type of governing system for turbines may be substituted for the governor and servomotor 4. i
A liquid, which may be oil for lubricating the turbine and a second liquid which may be water or another noninflammable liquid for actuating the governing system, is supplied from a reservoir 12, which is customarily located at a level below the turbine 1 so that the oil supplied to the bearings and other components may conveniently be drained back to the reservoir 12 by gravity. The oil for lubricating the turbine may be a petroleum product or any other suitable known liquid having lubricating properties. In the drawing the turbine lubrication system is drained by means of a conduit 13.
The reservoir 12 is divided by means of a plate 10 into two hydraulically independent reservoirs or compart-ments, one 12a for the high pressure system utilizing a noninflammable liquid, and another 12b for the low pressure system that utilizes oil.
,In accordancewith the invention, a main pump, indicated generally at 14, may be driven by any suitable prime mover but is preferably directly coupled to an extension 16 of the turbine shaft 2. This main pump-1 4 has an impeller, not shown, mounted directly on the turbine shaft extension 16. The pump is enclosed by a casing 17 which defines an annular pump inlet 18 and a discharge scroll 21. Any suitable type of pump other than a centrifugal pump may also be employed.
The discharge scroll 21 of the pump 14 communicates with a discharge pipe 22, to which is connected the servomotor supply conduit 5. A suitable pressure regulating valve 23 may be incorporated in the conduit 5 to maintain the pressure of the liquid supplied to the servomotor 4 constant at a preselected value. Spent liquid from the servomotor 4 returns through conduit 24 to the inlet 18 of pump 14, as noted hereinafter. A suitable check valve 25 is provided in conduit 22 to prevent flow of liquid in a reverse direction through pump 14.
Arranged, in the liquid reservoir 12a or in any other suitable location is a hydraulic turbine 26 consisting of a housing 27, an impeller, not shown, and an inlet scroll 31. A conduit 32 supplies liquid under pressure from the discharge scroll 21 of pump 14 to the inlet scroll 31 of turbine 26. Liquid discharge from the turbine 26 is led by a conduit 33 to the inlet 18 of the main pump 14. The shaft 34 of the hydraulic turbine 26 is a common or connected shaft to a hydraulic pump 36. The hydraulic pump 36 is located below the level of the oil in reservoir 12b and may be placed within the reservoir as shown. It defines an inlet opening 37 for admitting oil from the reservoir 12b to the pump impeller, not shown, and to a pump discharge scroll 38. A conduit 41 containing a check valve 42 delivers low pressure oil from the discharge scroll 38 to the inlet of a suitable oil cooler 43 through which cooling water is circulated.
From the oil cooler 43,. lubricating oil is supplied to a hydraulic seal of a hydrogen cooled electric generator, not shown, driven by steam turbine 1 and through a reducer 44 and conduit 45 to the lubrication system and bearing 3 of the steam turbine.
In starting the turbine 1 an auxiliary starting pump 65 driven by a motor 64 is used to provide low pressure oil to the lubrication system and bearing 3. Also, an auxiliary source of liquid under pressure is required to actuate the servomotor 4 and to prime the governing system. This source may comprise a second auxiliary pump group indicated generally at 48 and consisting of a motor 51 driving a centrifugal pump 52 similar to pump 36 located below the liquid level in reservoir 12a. An inlet opening 53 is arranged to admit liquid from reservoir 12a to the pump 52. A conduit 54 supplies liquid under pressure from the pump 52 through a suitable check valve 55 to the conduit where the liquid is supplied to the servomotor 4. The low pressure oil discharge from the pump 65 is led by a conduit 68 to the conduit 41 leading into the oil cooler 43. From the oil cooler 43, the low pressure oil is supplied through reducer 44 and through conduit 45 to the lubrication system of the turbine.
To start the system, the motors 51 and 64 are energized and liquid is supplied by the starting pump 52 to servomotor 4 and lubricating oil is supplied by pump 65 to bearing 3. Check valve 25 in conduit 22 prevents this priming liquid from flowing backwards through the main pump 14. Check valve 42 in conduit 41 prevents oil from flowing backwards through pump 36. When the liquid pressure in the governing portion of the system rises to the proper value for actuating the servomotor 4, turbine 1 may be started and brought up to speed, during which the discharge pressure of the main pump 14 will increase to its normal operating value so that check valve 25 is caused to open. When the pressure in conduits 22, 32, produced by the operation of the main pump 14, rises above that produced in conduit 54 by the starting pump 52, the check valve 55 will act to prevent any leakage of oil from conduit 22 backwards through conduit'54.
Suitable control means both indicated generally as 71 may be provided for the starting motor 51 and motor 64, and so arranged that the motors are automatically deenergized when the pressure in conduits 32 and 41, respectively, rises to a value in excess of the preselected value determined by a spring 72 in each control system 71. The control systems 71 each comprise a toggle switch 73 which is well known in the art coupled to a piston 75, so that the switch 73 breaks the circuit to the motors when liquid pressure in conduits 32 and 41, respectively, exceeds the preselected value determined by the spring 72 forcing the piston 75 inward. The spring 72 biases the piston 75 so that the switch 73 is in a closed position so that motor 51 and motor 64 will be energized whenever the pressure in conduit 32 and/or 41 falls below the preselected value of a spring 72.
From the above description of the apparatus, the hydraulic system for the steam turbine 1 in eflect comprises a high pressure circuit and a low pressure circuit with the shaft 34 connecting theturbine 26 of the high pressure circuit to the pump 36 of the low pressure circuit. The high pressure circuit comprises the main pump 14 in series with the parallel connected servomotor 4 of the steam turbine 1, and the hydraulic turbine 26. The low pressure circuit comprises the pump 36, the oil cooler 43 and the lubrication system of the steam turbine connected in series.
During normal operation of the steam turbine 1, liquid is delivered by the main pump 14 to the conduit 22 at a pressure suitable for operation of the servomotor 4. This pressure may be of the order of 200 pounds per square inch, which is considerably higher than is ordinarily used for lubrication purposes. The turbine lubrication system may be of the order of only 15 pounds per square inch.
An important feature of the invention is that the reduction of the liquid, pressure from the value required for operation of the servomotor 4 to that required for maintaining the prime of the pump 14 is accomplished in a manner which makes use of the energy represented by this pressure drop. This is efifected by causing the pressure drop to occur across the hydraulic turbine 26 which serves to drive the hydraulic pump 36. This method of conserving the energy in the system is found to make an important contribution to the overall efiiciency of the prime mover by reducing the power needed to drive the pump 14.
This improved liquid supply system provides a liquid, which may be noninflammable, at a comparatively high pressure for operating hydraulic devices such as a servomotor 4, and also supplies oil at a much lower pressure for lubrication. This is accomplished by the high speed pump 14 coupled directly to the shaft 2 of the prime mover 1 without intermediate gearing and having the hydraulic turbine 26 arranged to positively prime the main pump 14 when the steam turbine 1 is at its operating speed. The hydraulic turbine 26 is driven by energy derived from the drop in pressure from the high value required for the servomotor 4' to the lower value required to maintain the prime of pump 14. With this improved arrangement, a minimum quantity of liquid need be handled by the main oil pump 14, so that the power required for operating the system is kept to a minimum. By using the pressure drop inherent in the system to furnish energy for driving the hydraulic pump 36, a further important improvement in the power consumption of the system is obtained. With this invention, a very much smaller quantity of liquid need be pumped, than in other previously suggested systems. By thus reducing the volume flow in the system, the piping to and from the main oil pump may be smaller than in other systems. The main pump 14, the hydraulic turbine 26 and the pump 36 are designed for maximum efficiency with the main pump 14 delivering just enough pressure to operate the turbine 26 (which in turn operates pump 36) and to provide the required quantity of oil back to the main pump 14. There is no wastage of the energy available from the aforementioned pressure drop since all of the liquid from the main pump 14 passes through the hydraulic turbine 26.
The difference between the hydraulic systems shown in the accompanying drawing and the referred to parent application is that in the accompanying drawing the high pressure liquid system may utilize water or any other noninflammable liquid that is completely separate from the low pressure liquid system utilizing lubricating oil whereas in the parent application a common liquid is used for both the governing and lubrication systems.
Although but one embodiment of a dual fluid system has been illustrated and described, it will be apparent to those skilled in the art that various changes and modifications may be made therein without departing from the spirit of the invention or from the scope of the appended claims.
What is claimed is:
1. In a hydraulic system including a machine requiring a primary supply of noninflammable liquid at a comparative high pressure and a secondary supply of lubricating oil at a lower pressure, the combination of a first pump arranged to be driven by the machine; a hydraulic turbine; a servomotor requiring a supply of noninflammable liquid at a high pressure; said first pump, said hydraulic turbine, and saidservomotor forming a closed high pressure circuit with the discharge of said first pump supplied to the intake of said hydraulic turbine and said servomotor, and the discharge of said hydraulic turbine and said servomotor supplied to the intake of said first pump; a first reservoir; a second pump arranged to receive liquid from said first reservoir, the discharge of said second pump supplied to said servomotor to start the machine, and the discharge from said servomotor supplied to the intake of said first pump to prime said first pump; a first control means for automatically interrupting the flow of liquid from said second pump into said high pressure circuit when the pressure of the liquid delivered by said first pump exceeds the liquid pressure developed by said second pump; a second reservoir; a third pump arranged to receive oil from said second reservoir, said third pump arranged to be driven by said hydraulic turbine of said high pressure circuit; a low pressure lubrication system for the machine, said third pump and said lubrication system forming a low pressure circuit with the discharge from said third pump supplied to said lubrication system and the discharge from said lubrication system returned to said second reservoir; and means for supplying oil to said lubrication system when the machine is being started, said means comprising a fourth pump arranged to receive oil from said second reservoir, said fourth pump and said lubrication system forming a low pressure circuit with the discharge from said fourth pump supplied to said lubrication system and the discharge from said lubrication system returned to said second reservoir; and second control means for automatically interrupting the flow of low pressure oil from said fourth pump to said lubrication system when the pressure of oil delivered by said third pump exceeds the oil pressure developed by said fourth pump.
2. In a hydraulic system including a steam turbine requiring a primary supply of liquid at a comparative high pressure and a secondary supply of oil at a lower pressure, the combination of: a first pump arranged to be driven by the steam turbine; a hydraulic turbine; a first conduit connecting the output of said first pump to the input of said hydraulic turbine; a second conduit connecting the output of said hydraulic turbine to the input of said first pump whereby it is positively primed during normal operation; a servomotor requiring a supply of liquid at a high pressure; a third conduit connecting the output of said first pump to the input of said servomotor; a fourth conduit connecting the output of said servomotor to the input of said first pump; a first liquid resrvoir; means for starting the steam turbine and priming said first pump including a second pump arranged to receive liquid from said first reservoir and to supply high pressure liquid through a fifth conduit to the inlet of said servomotor to actuate said servomotor to cause steam to be admitted to the steam turbine to start the steam turbine and the output of said servomotor supplied to said first pump to prime said first pump; first control means for automatically deenergizing said second pump when the pressure of the liquid delivered by said first pump exceeds the high pressure liquid delivered by said second pump; a second oil reservoir; a third pump arranged to receive oil from said second reservoir, said third pump arranged to be driven by said hydraulic turbine; a lubrication system for the steam turbine requiring a supply of oil at a low pressure; a sixth conduit connecting the output of said third pump to the input of said lubrication system; a seventh conduit connecting the output of said lubrication system to said reservoir; means for supplying low pressure oil to said lubrication system when the steam turbine is being started including a fourth pump arranged to receive oil from said second reservoir and to supply low pressure oil through an eighth conduit to said lubrication system; second control means for automatically deenergizing said fourth vpump when the pressure of the oil delivered by said third pump exceeds the low pressure oil delivered by said fourth pump, and check valve means in said third, said fifth, said sixth and said eighth conduits for preventing reverse flow through said first pump, said second pump, said third pump and said fourth pump, respectively.
No references cited.
US837009A 1953-11-06 1959-08-31 Hydraulic system for steam turbine Expired - Lifetime US2963032A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US837009A US2963032A (en) 1953-11-06 1959-08-31 Hydraulic system for steam turbine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US390472A US2949122A (en) 1953-11-06 1953-11-06 Hydraulic system for steam turbine
US837009A US2963032A (en) 1953-11-06 1959-08-31 Hydraulic system for steam turbine

Publications (1)

Publication Number Publication Date
US2963032A true US2963032A (en) 1960-12-06

Family

ID=27013160

Family Applications (1)

Application Number Title Priority Date Filing Date
US837009A Expired - Lifetime US2963032A (en) 1953-11-06 1959-08-31 Hydraulic system for steam turbine

Country Status (1)

Country Link
US (1) US2963032A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4191356A (en) * 1978-06-08 1980-03-04 Caterpillar Tractor Co. Engine mounting base
US10604003B2 (en) * 2016-09-26 2020-03-31 Hyundai Motor Company Hydraulic pressure supply system of automatic transmission for hybrid vehicle and cooling the jacket of a motor with low pressure supply to low pressure part

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4191356A (en) * 1978-06-08 1980-03-04 Caterpillar Tractor Co. Engine mounting base
US10604003B2 (en) * 2016-09-26 2020-03-31 Hyundai Motor Company Hydraulic pressure supply system of automatic transmission for hybrid vehicle and cooling the jacket of a motor with low pressure supply to low pressure part

Similar Documents

Publication Publication Date Title
US2711071A (en) Arrangement for starting a prime mover by independently driven lubricating pump
US3658153A (en) Lubricating oil system for a prime mover
US4629033A (en) Positive displacement pump utilized in lube oil system for turbomachinery
US4362020A (en) Hermetic turbine generator
US4899850A (en) Lubricating device for a turbomachine
US4446377A (en) Low collapse speed lube oil pumping system for turbomachinery
US3486582A (en) Lubrication system for a gas turbine engine
US2440980A (en) Turbine oil system with pump priming arrangement
US4105093A (en) Control system for pressurized lubricating system
GB1497784A (en) Turbine lubrication system
US3472024A (en) Starting system for a gas turbine plant
US4243892A (en) Energy-efficient fluid medium pumping system
US2963032A (en) Hydraulic system for steam turbine
US3998052A (en) Hydraulic turning arrangement for a turbine rotor
US2949122A (en) Hydraulic system for steam turbine
JP5473713B2 (en) Turbine lubricating oil supply method and apparatus
US1284662A (en) Centrifugal pump and compressor.
US3991564A (en) Dual pressure level oil supply system
US2735367A (en) kenney
SU694943A1 (en) Arrangement for oil supply of shaft seals in a turbogenerator with hydrogen cooling
US3068653A (en) Unitized arrangement of auxiliaries in power system generation
SU375443A1 (en) LUBRICATION SYSTEM
CN112943717B (en) Hydraulic starting system for aeroderivative gas turbine generator set
CN214617096U (en) Shielding pump annotates liquid cleaning system
RU2691230C1 (en) Gas compressor unit