CN216157720U - Small radial flow turbine expander starting system - Google Patents

Small radial flow turbine expander starting system Download PDF

Info

Publication number
CN216157720U
CN216157720U CN202121419910.5U CN202121419910U CN216157720U CN 216157720 U CN216157720 U CN 216157720U CN 202121419910 U CN202121419910 U CN 202121419910U CN 216157720 U CN216157720 U CN 216157720U
Authority
CN
China
Prior art keywords
small
radial flow
air inlet
turboexpander
pipeline
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.)
Active
Application number
CN202121419910.5U
Other languages
Chinese (zh)
Inventor
袁龙健
刁安娜
孙远
杨小强
李佳骏
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.)
711th Research Institute of CSIC
Original Assignee
Shanghai Marine Diesel Engine Research Institute
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
Application filed by Shanghai Marine Diesel Engine Research Institute filed Critical Shanghai Marine Diesel Engine Research Institute
Priority to CN202121419910.5U priority Critical patent/CN216157720U/en
Application granted granted Critical
Publication of CN216157720U publication Critical patent/CN216157720U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Control Of Turbines (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)

Abstract

A starting system of a small radial flow turboexpander comprises an air inlet main pipe, a main pipeline, a bypass pipeline, a detection device and a control device. One end of the air inlet main pipe is a medium gas inlet, the other end of the air inlet main pipe is communicated with one end of the main pipeline and one end of the bypass pipeline respectively, and the other end of the main pipeline and the other end of the bypass pipeline are communicated with an inlet and an outlet of the small-sized runoff turboexpander respectively. The main pipeline and the bypass pipeline are respectively provided with a regulating quick-closing valve and a bypass regulating valve. The detection device is used for detecting the air inlet pressure of the air inlet main pipe and the rotating speed of the small radial flow turboexpander in real time. The control device is used for receiving the setting of the air inlet pressure of the air inlet main pipe and the rotating speed of the expansion machine from the outside, receiving the valve state signal and the detection result of the detection device, and controlling and adjusting the opening of the quick closing valve and the bypass adjusting valve. The utility model can realize the quick start of the small-sized radial flow turboexpander and ensure the safe and reliable start process.

Description

Small radial flow turbine expander starting system
Technical Field
The utility model relates to an expander technology, in particular to a starting technology of a radial flow turboexpander.
Background
As a novel small-sized runoff turboexpander, the centrifugal turboexpander is rarely applied to domestic engineering, and the introduction of a starting system and a starting method of the centrifugal turboexpander is also very little. If a startup system and method similar to a large axial flow turbine is adopted, problems exist because: the centrifugal turbo expander is characterized in that the blades are short and small, the rotor mass is small, and under the condition of higher medium parameters, the rotating speed is easy to excessively fly up at the moment of starting, so that the starting stability of a unit is influenced; 2, a main steam valve and a regulating valve are arranged on an air inlet pipeline of a general steam turbine, and a long time of warming pipes and warming valves exists during startup, which is opposite to the concept that a centrifugal turbo expander needs to be started quickly; 3 when an emergency working condition such as overspeed occurs, the main steam valve and the regulating valve are quickly closed, but the main steam valve and the regulating valve are limited by the quick closing time and the leakage grade of the regulating valve, and a part of media between the main steam valve and the regulating valve still enters the steam turbine. Therefore, it is important to design a special starting system and method to ensure safe, reliable and fast starting of the centrifugal turboexpander.
Disclosure of Invention
The utility model aims to provide a starting system of a small-sized runoff turboexpander, which can realize the quick starting of the small-sized runoff turboexpander and ensure the safety and reliability of the starting process.
The starting system of the small radial flow turboexpander comprises an air inlet main pipe, a main pipeline, a bypass pipeline, a detection device and a control device; one end of the air inlet main pipe is a medium gas inlet, the other end of the air inlet main pipe is respectively communicated with one end of the main path pipeline and one end of the bypass pipeline, the other end of the main path pipeline is communicated with an inlet of the small-sized runoff turbo expander, and the other end of the bypass pipeline is communicated with an outlet of the small-sized runoff turbo expander; a main pipeline is provided with a regulating quick-closing valve, and a bypass pipeline is provided with a bypass regulating valve; the detection device is used for detecting the air inlet pressure of the air inlet main pipe and the rotating speed of the small radial flow turboexpander in real time; the control device is used for receiving the external air inlet pressure of an air inlet main pipe and setting the rotating speed of the small-sized radial flow turboexpander, receiving and adjusting valve state signals fed back by the quick-closing valve and the bypass adjusting valve and detection results sent by the detection device, and controlling and adjusting the opening degree of the quick-closing valve and the opening degree of the bypass adjusting valve so that the small-sized radial flow turboexpander can operate at the set air inlet pressure and the set rotating speed.
The utility model has at least the following advantages:
1. in the embodiment, a main pipeline adopts a regulating quick-closing valve to replace a main steam valve and a regulating valve arranged on an air inlet pipeline in the prior art, so that the number of valves and a pipeline connected between the regulating valve and the main steam valve in the prior art are reduced, the arrangement of the air inlet pipeline is simpler, the size of the whole machine is reduced, the time for warming the pipe and the valve can be shortened, and the starting speed of the small radial flow turboexpander is accelerated;
2. after the quick closing valve is adjusted to be quickly cut off, the gas quantity of the residual pipeline entering the small radial flow turboexpander is obviously reduced, the rotating speed can be ensured to be quickly reduced, and the safety of the starting process is improved;
3. compared with the starting mode of warming the valve and then warming the pipe in the prior art, the embodiment of the utility model can finish the operations of warming the pipe, warming the valve and warming the pipe at one time during starting, thereby shortening the starting time;
4. the opening degrees of the regulating quick closing valve and the bypass regulating valve are controlled by the control device in the process from the start of the small radial flow turboexpander to the rising to the warming rotating speed, so that the stable rising speed can be ensured, and the rotating speed is not excessively raised;
5. the opening degree of adjusting the quick closing valve and the bypass regulating valve is controlled by the control device in the process that the small-size runoff turboexpander rises from the warm-up rotating speed to the rated rotating speed, the small-size runoff turboexpander can be guaranteed to rapidly and safely pass through a critical rotating speed area, and after the rated rotating speed is reached, the rotating speed overshoot is small and the fluctuation is small.
Drawings
Fig. 1 is a schematic diagram showing the construction of one embodiment of the start-up system of the small-sized radial flow turboexpander of the present invention.
Fig. 2 is a schematic diagram illustrating the control principle of an embodiment of the start-up system of the small-sized radial flow turboexpander according to the present invention.
Detailed Description
The present invention is described in further detail below with reference to the attached drawing figures.
Please refer to fig. 1 and fig. 2. The starting system of the small radial flow turboexpander according to one embodiment of the utility model comprises an air inlet manifold 11, a main pipeline 12, a bypass pipeline 13, a detection device and a control device.
One end of the air inlet main pipe 11 is a medium gas inlet, the other end of the air inlet main pipe 11 is communicated with one end of the main pipeline 12 and one end of the bypass pipeline 13 respectively, the other end of the main pipeline 12 is communicated with an inlet of the small-sized runoff turbo expander 7, and the other end of the bypass pipeline 13 is communicated with an outlet of the small-sized runoff turbo expander 7.
In the present embodiment, the small-sized radial flow turboexpander 7 is a centrifugal turboexpander. By "compact" is meant a radial flow turboexpander with a power output of 4Mw or less.
In the present embodiment, the centrifugal turboexpander 7 is connected to the generator 9 through the gear box 8. Wherein, the centrifugal turbo expander adopts a cantilever type structure to be installed on the gear box 8, and has compact integral structure and convenient arrangement.
The main pipeline 12 is provided with a regulating quick-closing valve 41, and the bypass pipeline is provided with a bypass regulating valve 42. The regulating quick-closing valve 41 is arranged close to the inlet of the small-sized radial flow turboexpander 7. The function of adjusting the quick-closing valve 41 to integrate the adjusting valve and the quick-closing valve into a whole simplifies the arrangement of the valve on the air inlet pipeline, and is closer to the inlet of the small-sized radial flow turboexpander 7, so that the cutting-off effect is more obvious. The quick closing time of the adjusting quick closing valve 41 is less than 0.5s, and the high-precision hydraulic design is adopted, so that the adjusting precision is high, and the response speed is high. The bypass regulating valve 42 is used for controlling the inlet pressure of the inlet manifold, and the regulating quick-closing valve 41 is used for controlling the rotating speed of the small-sized radial flow turboexpander 7.
Further, a filter 51 and a flow transmitter 52 are arranged on the main pipeline 12, and the filter 51 is used for filtering impurities in the medium.
The detection device is used for detecting the air inlet pressure of the air inlet manifold 11 and the rotating speed of the small-sized radial flow turboexpander 7 in real time. In the present embodiment, the detection means includes a pressure transmitter 21 for detecting the intake pressure of the intake manifold 11 and a rotation speed transmitter 22 for detecting the rotation speed of the compact radial flow turboexpander 7. Optionally, a rotational speed transmitter 22 is mounted on the output shaft of the gearbox 8.
The control device is used for receiving the external air inlet pressure of the air inlet manifold 11 and the set rotating speed of the small-sized radial flow turboexpander, receiving and adjusting valve state signals fed back by the quick-closing valve 41 and the bypass adjusting valve 42 and detection results sent by the detection device, and controlling and adjusting the opening degrees of the quick-closing valve 41 and the bypass adjusting valve 42, so that the small-sized radial flow turboexpander 7 can operate at the set air inlet pressure and the set rotating speed.
In the embodiment, the control device comprises a human-computer interaction part 31 and a controller 32, and the human-computer interaction part 31 is connected with the controller 32. Optionally, the human-computer interaction part 31 is a touch screen, and the controller 32 is a PLC controller.
The starting process of the starting system of the small radial flow turboexpander according to the embodiment of the utility model is as follows:
a. starting the small-sized radial flow turboexpander 7, setting the air inlet pressure of the air inlet manifold 11 to be P1 through a control device, wherein P1= P0+ A, P0 is the air inlet pressure required by starting the preset small-sized radial flow turboexpander (from a static state to the time of realizing rotation), A is a constant value, and is more than or equal to 0 and less than or equal to 0.1MPa, and in the embodiment, P1= P0+0.1 MPa;
b. the control device controls the opening degree of the bypass regulating valve 42 according to the set value P1 of the intake pressure and the measured value of the intake pressure, so that the intake pressure of the intake manifold reaches P1; since the initial measured value of the intake pressure of the intake manifold 11 is less than P1, in step b, the control means generally gradually decreases the opening degree of the bypass regulator valve 42 to increase the intake pressure of the intake manifold, and optionally PID-controls the opening degree of the bypass regulator valve according to the deviation between the intake pressure set value P1 and the measured value of the intake pressure so that the intake pressure of the intake manifold reaches P1;
c. after the inlet pressure of the inlet manifold reaches P1, setting the rotation speed of the small-sized radial flow turboexpander to be V0 through the control device, wherein V0 is the preset warming-up rotation speed of the small-sized radial flow turboexpander;
d. the control device controls the opening of the quick-closing valve according to the set rotating speed value V0 and the rotating speed measurement value of the small-sized radial flow turboexpander so that the rotating speed of the small-sized radial flow turboexpander reaches V0; since the small-scale radial flow turboexpander 7 is in a static state before, in step d, the control device generally gradually increases the opening degree of the regulating fast-closing integrated valve 41 to increase the rotation speed of the small-scale radial flow turboexpander 7, and optionally, the control device performs PID control on the opening degree of the regulating fast-closing valve 41 according to the deviation between the rotation speed set value V0 and the rotation speed measured value of the small-scale radial flow turboexpander to make the rotation speed of the small-scale radial flow turboexpander 7 reach V0;
e. after the small-sized radial flow turboexpander runs at the rotating speed V0 for a preset time t (at the moment, the quick-closing integral valve 41 is adjusted to be in a large opening degree), the air inlet pressure of the air inlet main pipe is set to be P through the control deviceForehead (forehead),PForehead (forehead)The rated air inlet pressure of the small radial flow turbine expansion machine 7; alternatively, 3 minutes ≦ t ≦ 5 minutes, t being 5 minutes in this embodiment, so the state of operation at speed V0 is maintained for 5 minutes for valve warming and warm-up purposes;
f. the control device sets a value P according to the intake pressureForehead (forehead)And the measured value of the intake pressure controls the opening of the bypass regulating valve so that the intake pressure of the intake manifold 11 reaches PForehead (forehead)(ii) a During this process, the control unit generally maintains the rotational speed set point at a gradually decreasing opening of the bypass regulator valve 42, but as the intake manifold pressure increasesHigh, the control means will gradually decrease the opening of the regulating quick-closing valve 41. Alternatively, the control means is responsive to the inlet pressure setpoint PForehead (forehead)Deviation from the measured value of the intake pressure PID controls the opening of the bypass regulator valve 42 so that the intake pressure of the intake manifold 11 reaches PForehead (forehead)
g. The intake pressure of the intake manifold 11 reaches PForehead (forehead)Then, the rotating speed of the small radial flow turboexpander is set to be V through the control deviceForehead (forehead),VForehead (forehead)The rated rotating speed of the small radial flow turbine expansion machine 7;
h. the control device is based on the set value V of the rotating speedForehead (forehead)And the rotating speed measurement value of the small-sized radial flow turboexpander controls the opening of the regulating quick-closing valve 41 so as to ensure that the rotating speed of the small-sized radial flow turboexpander reaches VForehead (forehead). Alternatively, the control device sets the value V according to the rotating speedForehead (forehead)The deviation between the measured value of the rotating speed of the small-sized radial flow turboexpander carries out PID control on the opening degree of the regulating quick-closing valve 41 so as to ensure that the rotating speed of the small-sized radial flow turboexpander reaches VForehead (forehead)
In this embodiment, the regulating quick-closing valve 41 is kept fully closed and the bypass regulating valve 42 is kept fully open before starting the small-sized radial flow turboexpander 7 so that the medium passes entirely through the bypass line 13 without entering the main line 12.
The intake pressure P0 required for the start-up of the small-scale radial flow turboexpander 7 and the warm-up rotation speed V0 of the small-scale radial flow turboexpander were obtained by a test comprising the steps of:
the regulating quick-closing valve 41 is kept fully closed, the bypass regulating valve 42 is kept fully open, and all media pass through the bypass pipeline 13 and do not enter the main pipeline 12;
fully opening the regulating quick-closing valve 41;
the opening degree of the bypass regulating valve 42 is gradually reduced, so that the intake pressure of the intake manifold 11 is increased until the opening degree of the regulating quick-closing valve 41 is kept unchanged after the small-sized radial flow turboexpander 7 starts to rotate, the intake pressure value at the moment is recorded as the intake pressure P0 required by the start of the small-sized radial flow turboexpander, and the highest rotation speed which the small-sized radial flow turboexpander 7 can reach is recorded as the warming-up rotation speed V0 (namely, the rotation speed value which the small-sized radial flow turboexpander 7 finally reaches under the condition that the intake pressure is equal to P0).
In any step from the step a to the step h, if the rotating speed measured value of the small-sized radial flow turboexpander 7 exceeds the preset upper rotating speed limit, the control device 7 controls and adjusts the quick closing valve 41 to be fully closed, and the air source is cut off, so that the safety of the unit is ensured.
Further, in step h, the rotating speed of the small-sized radial flow turboexpander 7 reaches VForehead (forehead)In the process, the control device controls the opening of the regulating quick-closing valve 41, so that the rotating speed increasing rate of the small-sized runoff turboexpander 7 is gradually reduced (namely the speed increasing process is fast first and slow later), the small-sized runoff turboexpander 7 can be further ensured to rapidly and safely pass through a critical rotating speed area, and after the rated rotating speed is reached, the rotating speed overshoot is small and the fluctuation is small.

Claims (7)

1. The starting system of the small radial flow turboexpander is characterized by comprising an air inlet main pipe, a main pipeline, a bypass pipeline, a detection device and a control device;
one end of the air inlet main pipe is a medium gas inlet, the other end of the air inlet main pipe is respectively communicated with one end of the main path pipeline and one end of the bypass pipeline, the other end of the main path pipeline is communicated with an inlet of the small-sized runoff turbo expander, and the other end of the bypass pipeline is communicated with an outlet of the small-sized runoff turbo expander;
the main pipeline is provided with a regulating quick-closing valve, and the bypass pipeline is provided with a bypass regulating valve;
the detection device is used for detecting the air inlet pressure of the air inlet main pipe and the rotating speed of the small radial flow turboexpander in real time;
the control device is used for receiving the external air inlet pressure of the air inlet main pipe and setting the rotating speed of the small-sized radial flow turboexpander, receiving valve state signals fed back by the adjusting quick-closing valve and the bypass adjusting valve and detection results sent by the detection device, and controlling the opening degree of the adjusting quick-closing valve and the opening degree of the bypass adjusting valve so that the small-sized radial flow turboexpander can operate at the set air inlet pressure and the set rotating speed.
2. The startup system of a compact radial flow turboexpander according to claim 1, wherein said detecting means includes a pressure transmitter for detecting an intake pressure of said intake manifold and a rotational speed transmitter for detecting a rotational speed of the compact radial flow turboexpander.
3. The startup system of a small radial flow turboexpander according to claim 1, wherein the control means includes a human machine interface component and a controller, the human machine interface component being connected to the controller.
4. The startup system of a small radial flow turboexpander according to claim 3, wherein said human-machine interface component is a touch screen.
5. The startup system of a small radial flow turboexpander according to claim 3 or 4, wherein the controller is a PLC controller.
6. The startup system of a small-scale radial flow turboexpander according to claim 1, wherein the small-scale radial flow turboexpander is a centrifugal turboexpander.
7. The startup system of a small radial flow turboexpander according to claim 6, wherein said centrifugal turboexpander is connected to an electric generator through a gearbox.
CN202121419910.5U 2021-06-25 2021-06-25 Small radial flow turbine expander starting system Active CN216157720U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202121419910.5U CN216157720U (en) 2021-06-25 2021-06-25 Small radial flow turbine expander starting system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202121419910.5U CN216157720U (en) 2021-06-25 2021-06-25 Small radial flow turbine expander starting system

Publications (1)

Publication Number Publication Date
CN216157720U true CN216157720U (en) 2022-04-01

Family

ID=80835972

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202121419910.5U Active CN216157720U (en) 2021-06-25 2021-06-25 Small radial flow turbine expander starting system

Country Status (1)

Country Link
CN (1) CN216157720U (en)

Similar Documents

Publication Publication Date Title
CN113404554A (en) Small radial flow turboexpander starting system and starting method thereof
EP0083109B1 (en) Combined plant having steam turbine and gas turbine connected by single shaft
US9567906B2 (en) Systems and methods for controlling aircraft main engine speeds by adjusting compressed air flow from an APU
US9303565B2 (en) Method and system for operating a turbine engine
EP2339128A2 (en) Method for starting a turbomachine
US10526923B2 (en) Combined cycle plant, control method of same, and control device of same
CN112502796B (en) Operation control system and operation control method of SCO2 expander
JP6222993B2 (en) 2-shaft gas turbine
JPS62251409A (en) Method and device for cooling steam turbine in single-shaft combined plant
US20110238358A1 (en) Method for determining when to perform a test of an overspeed protection system of a powerplant machine
CN102878100A (en) Control method for preventing surging generated during normal halting of single-shaft purified terephthalic acid (PTA) compressor unit
CN108956183A (en) Expanding machine experimental rig and its test method
WO2012076726A1 (en) Multiple turbocharger control
CN216157720U (en) Small radial flow turbine expander starting system
EP2339127A2 (en) Method for starting a turbomachine
JPH11229898A (en) Start-up control device of gas turbine
JP2954754B2 (en) Operation control device for gas turbine system and pressurized fluidized bed boiler power plant
Rowen Operating characteristics of heavy-duty gas turbines in utility service
CN105424392A (en) Supercharged boiler test stand
CN213116405U (en) Detection apparatus for high cycle fatigue test of booster impeller and turbine
JP2015212540A (en) System and method for controlling turbine speed using torque converter
CN205192774U (en) Supercharged boiler test bench
JP3703872B2 (en) gas turbine
CN214468852U (en) Control system of catalytic device smoke exhaust ventilator
CN112902023A (en) Steam pipeline pressurization system and full-automatic control method thereof

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
CP01 Change in the name or title of a patent holder

Address after: 201108 Shanghai city Minhang District Huaning Road No. 3111

Patentee after: The 711 Research Institute of China Shipbuilding Corp.

Address before: 201108 Shanghai city Minhang District Huaning Road No. 3111

Patentee before: Shanghai Marine Diesel Engine Research Institute

CP01 Change in the name or title of a patent holder