Semi-physical simulation test bench and test method for multi-machine parallel operation device of gas turbines

Patent metadata

Field	Value
Publication number	US-12130202-B2
Application number	US-202217801178-A
Country	US
Kind code	B2
Filing date	Jun 28, 2022
Priority date	Jun 28, 2021
Publication date	Oct 29, 2024
Grant date	Oct 29, 2024

Abstract

The present disclosure provides a semi-physical simulation test bench and test method for a multi-machine parallel operation device of gas turbines. The gas turbines are all connected with gearbox shafts through SSS clutches, torque meters and couplers, and then a hydraulic dynamometer, an electric turbine dynamometer and a generator are independently or jointly driven through couplers and torque meters so as to charge a storage battery. Multi-shaft gearboxes comprise parallel operation gearboxes, and are connected with a bridging gearbox through couplers, electromagnetic clutches, supports, torque meters and couplers. The gas turbines can drive an electric dynamometer and the electric turbine dynamometer independently or cooperatively, so that the system has good operation characteristics under different working conditions. Meanwhile, the storage battery is additionally arranged, the flexibility of the test bench is improved, and the energy utilization rate is increased.

First claim

What is claimed is:

1. A semi-physical simulation test bench for a multi-machine parallel operation device of gas turbines, comprising a first simulation gas turbine, a second simulation gas turbine, a third simulation gas turbine, a storage battery, an electric turbine dynamometer, a hydraulic dynamometer, a generator, a first parallel operation gearbox, a second parallel operation gearbox and a bridging gearbox;
wherein the electric turbine dynamometer is connected with a first torque meter and the first parallel operation gearbox; the first simulation gas turbine, a first SSS clutch and a second torque meter are connected in sequence and connected with the first parallel operation gearbox; the hydraulic dynamometer is connected with a third torque meter and the second parallel operation gearbox; the storage battery, the generator and a first electromagnetic clutch are connected in sequence and connected with the second parallel operation gearbox;
the second simulation gas turbine, a third SSS clutch and a fifth torque meter are connected in sequence and connected with the second parallel operation gearbox; the third simulation gas turbine, a second SSS clutch and a fourth torque meter are connected in sequence and connected with the first parallel operation gearbox; after a sixth torque meter, a first support and a second electromagnetic clutch are connected in sequence, the sixth torque meter is connected with the bridging gearbox, and the second electromagnetic clutch is connected with the first parallel operation gearbox; and after a seventh torque meter, a second support and a third electromagnetic clutch are connected in sequence, the seventh torque meter is connected with the bridging gearbox, and the third electromagnetic clutch is connected with the second parallel operation gearbox.

2. A semi-physical simulation test method for a multi-machine parallel operation device of gas turbines, wherein the working modes of the gas turbines comprise electric propelling modes, and the electric propelling modes comprise a storage battery power supply propelling mode and a laboratory power supply propelling mode;
firstly, in a storage battery power supply propelling mode, the storage battery drives simulation gas turbines to be in a running state, three simulation gas turbines such as a first simulation gas turbine, a second simulation gas turbine and a third simulation gas turbine are all in a running state; a first SSS clutch and a third SSS clutch are both closed, and the first simulation gas turbine is connected with a first parallel operation gearbox through a second torque meter and then drives an electric turbine dynamometer through a first torque meter; the second simulation gas turbine is connected with a second parallel operation gearbox through a fifth torque meter and then drives a hydraulic dynamometer through a third torque meter; and
the third simulation gas turbine is connected with the first parallel operation gearbox through a fourth torque meter, power is separated into two paths, the third simulation gas turbine drives the electric turbine dynamometer through the first torque meter in a first path of power; and reaches a bridging gearbox through a second electromagnetic clutch, a first support and a sixth torque meter in a second path of power; then is connected with the second parallel operation gearbox through a seventh torque meter, a second support and a third electromagnetic clutch, and then drives the hydraulic dynamometer through the third torque meter; and
secondly, in the laboratory power supply propelling mode, a laboratory power supply drives motors to be in a running state, the three simulation gas turbines such as the first simulation gas turbine, the second simulation gas turbine and the third simulation gas turbine are all in a running state; a first SSS clutch and a third SSS clutch are both closed, and the first simulation gas turbine is connected with the first parallel operation gearbox through the second torque meter and then drives the electric turbine dynamometer through the first torque meter; the second simulation gas turbine is connected with the second parallel operation gearbox through the fifth torque meter and then drives the hydraulic dynamometer through the third torque meter; and the third simulation gas turbine is connected with the first parallel operation gearbox through the fourth torque meter, power is separated into two paths, the third simulation gas turbine drives the electric turbine dynamometer through the first torque meter in the first path of power; and reaches the bridging gearbox through the second electromagnetic clutch, the first support and the sixth torque meter in the second path of power; then is connected with the second parallel operation gearbox through the seventh torque meter, the second support and the third electromagnetic clutch, and then drives the hydraulic dynamometer through the third torque meter.

3. A semi-physical simulation test bench for a multi-machine parallel operation device of gas turbines, comprising:
a test system, the test system comprising a first simulation gas turbine, a storage battery, an electric turbine dynamometer, a first SSS clutch, a second SSS clutch, a third SSS clutch, a hydraulic dynamometer and a generator, a first torque meter, a second torque meter, a third torque meter, a fourth torque meter, a fifth torque meter, a sixth torque meter, a seventh torque meter, a first electromagnetic clutch, a second electromagnetic clutch, a third electromagnetic clutch, a first support, a second support, a second simulation gas turbine, a third simulation gas turbine, couplers, a first parallel operation gearbox, a second parallel operation gearbox and a bridging gearbox;
wherein the first simulation gas turbine is connected with the first parallel operation gearbox through the first SSS clutch, the second torque meter and a second coupler; and the first parallel operation gearbox is connected with the electric turbine dynamometer through a first coupler and the first torque meter in sequence; the second simulation gas turbine is connected with the second parallel operation gearbox through the third SSS clutch, the fifth torque meter and an eighth coupler in sequence; and the second parallel operation gearbox is connected with the hydraulic dynamometer through a third coupler and the third torque meter in sequence; and the third simulation gas turbine is connected with the first parallel operation gearbox through the second SSS clutch, the fourth torque meter and a fifth coupler in sequence; power is separated into two paths, the first parallel operation gearbox drives the electric turbine dynamometer through the first coupler and the first torque meter in the first path of power; and reaches the bridging gearbox through a sixth coupler, the second electromagnetic clutch, the first support, the sixth torque meter and a tenth coupler in the second path of power; the bridging gearbox is connected with the second parallel operation gearbox through a ninth coupler, the seventh torque meter, the second support, the third electromagnetic clutch and a seventh coupler; and the second parallel operation gearbox drives the hydraulic dynamometer through the third coupler and the third torque meter; and
a monitoring control system, the monitoring control system comprising a data processing simulation machine, an execution mechanism control system, an upper computer and a security and protection detector;
wherein the data processing simulation machine can perform real-time solution calculation from a controller model to a prime mover model, and performs data acquisition and data output; the execution mechanism control system comprises a first motor, a second motor, a third motor, a first motor frequency converter, a second motor frequency converter, a third motor frequency converter, a gener

Assignees

• Univ Harbin Eng

Inventors

• Wang Zhitao
• Li Jian
• Ming Liang
• Li Shuying
• Ma Jiayi
• Guan Tianhao
• Luo Jiafan

Classifications

• G01M15/02 Primary

  Details or accessories of testing apparatus · CPC title

• G01M15/14 Primary

  Testing gas-turbine engines or jet-propulsion engines · CPC title

• Y02T90/00

  Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation · CPC title

• G01D21/02

  Measuring two or more variables by means not covered by a single other subclass · CPC title