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CN115492690A - A light multi-shaft gas turbine starting structure and starting method - Google Patents

A light multi-shaft gas turbine starting structure and starting method Download PDF

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Publication number
CN115492690A
CN115492690A CN202211178574.9A CN202211178574A CN115492690A CN 115492690 A CN115492690 A CN 115492690A CN 202211178574 A CN202211178574 A CN 202211178574A CN 115492690 A CN115492690 A CN 115492690A
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Prior art keywords
clutch
generator
shaft
gas
starting
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Chinese (zh)
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李明
孟晓波
韩哲
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China Hangfa Gas Turbine Co ltd
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China Hangfa Gas Turbine Co ltd
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26Starting; Ignition
    • F02C7/268Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/275Mechanical drives

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Eletrric Generators (AREA)

Abstract

一种轻型多轴燃气轮机起动结构及起动方法,起动结构包括燃气发生器、动力涡轮轴、离合器、联轴器及发电机;燃气发生器与动力涡轮轴通过离合器连接配合;发电机通过联轴器与动力涡轮轴相连;离合器主动组件连接在动力涡轮轴上,离合器从动组件连接在燃气发生器上。起动方法为:当燃气轮机需要起动时,首先控制离合器处于接合状态,然后将发电机作为电动机,通过发电机带动动力涡轮轴转动,进而通过处于接合状态的离合器带得燃气发生器同步升转,且在升转期间完成供油和点火步骤,当燃气发生器的转动达到脱开转速时,切断离合器的主动组件与从动组件之间的连接,使燃气发生器在起动程序控制下继续升转至慢车转速,直至完成燃气轮机的起动过程。

Figure 202211178574

A light-duty multi-shaft gas turbine starting structure and starting method, the starting structure includes a gas generator, a power turbine shaft, a clutch, a coupling and a generator; the gas generator and the power turbine shaft are connected through a clutch; the generator is connected through a coupling It is connected with the power turbine shaft; the clutch active component is connected with the power turbine shaft, and the clutch driven component is connected with the gas generator. The starting method is as follows: when the gas turbine needs to be started, first control the clutch to be in the engaged state, then use the generator as a motor to drive the power turbine shaft to rotate through the generator, and then drive the gas generator to rotate synchronously through the engaged clutch, and The oil supply and ignition steps are completed during the up-rotation period. When the rotation of the gas generator reaches the disengagement speed, the connection between the driving component and the driven component of the clutch is cut off, so that the gas generator continues to up-rotate under the control of the starting program. Idle speed until the start-up process of the gas turbine is completed.

Figure 202211178574

Description

一种轻型多轴燃气轮机起动结构及起动方法A light multi-shaft gas turbine starting structure and starting method

技术领域technical field

本发明属于燃气轮机技术领域,特别是涉及一种轻型多轴燃气轮机起动结构及起动方法。The invention belongs to the technical field of gas turbines, and in particular relates to a starting structure and a starting method of a light multi-shaft gas turbine.

背景技术Background technique

对于某些轻型多轴燃气轮机来说,由于结构的特殊性,其动力涡轮轴穿过燃气发生器内部,导致燃气发生器两端无法直接连接外部动力装置(起动电机)。For some light multi-shaft gas turbines, due to the special structure, the power turbine shaft passes through the inside of the gas generator, so that the two ends of the gas generator cannot be directly connected to the external power device (starter motor).

目前,传统的解决方法是在燃气发生器上增加锥齿轮,通过一副锥齿轮将起动电机的动力传递给燃气发生器。但是,由于整个传动系统需设置锥齿轮、传动轴、减速齿轮、离合器以及联轴器等,导致传动系统结构复杂,导致该起动方法会显著增加燃气轮机的整机产品成本,从而降低了产品竞争力。At present, the traditional solution is to add a bevel gear to the gas generator, and transmit the power of the starter motor to the gas generator through a pair of bevel gears. However, since the entire transmission system needs to be equipped with bevel gears, transmission shafts, reduction gears, clutches, and couplings, etc., resulting in a complex structure of the transmission system, this starting method will significantly increase the overall product cost of the gas turbine, thereby reducing product competitiveness. .

发明内容Contents of the invention

针对现有技术存在的问题,本发明提供一种轻型多轴燃气轮机起动结构及起动方法,通过在动力涡轮轴和燃气发生器之间安装自动控制或手动控制的离合器,将发电机作为电动机使用来带动动力涡轮轴,再通过离合器将起动力矩传递给燃气发生器,以实现燃气轮机的起动,不但简化了传动系统结构,而且有效降低了燃气轮机的整机产品成本,有利于产品竞争力的提升。Aiming at the problems existing in the prior art, the present invention provides a light-duty multi-shaft gas turbine starting structure and starting method. By installing an automatic or manual control clutch between the power turbine shaft and the gas generator, the generator is used as a motor to Drive the power turbine shaft, and then transmit the starting torque to the gas generator through the clutch to realize the start of the gas turbine, which not only simplifies the structure of the transmission system, but also effectively reduces the cost of the complete product of the gas turbine, which is conducive to the improvement of product competitiveness.

为了实现上述目的,本发明采用如下技术方案:一种轻型多轴燃气轮机起动结构,包括燃气发生器、动力涡轮轴、离合器、联轴器及发电机;所述燃气发生器与动力涡轮轴之间通过离合器连接配合;所述发电机通过联轴器与动力涡轮轴相连接;所述离合器的主动组件连接在动力涡轮轴上,离合器的从动组件连接在燃气发生器上。In order to achieve the above object, the present invention adopts the following technical solutions: a light multi-shaft gas turbine starting structure, including a gas generator, a power turbine shaft, a clutch, a shaft coupling and a generator; The clutch is connected and matched; the generator is connected with the power turbine shaft through a shaft coupling; the active assembly of the clutch is connected with the power turbine shaft, and the driven assembly of the clutch is connected with the gas generator.

所述离合器采用自动控制的离合器或手动控制的离合器。Described clutch adopts the clutch of automatic control or the clutch of manual control.

一种轻型多轴燃气轮机起动方法,采用了所述的轻型多轴燃气轮机起动结构,具体为:当燃气轮机需要起动时,首先控制离合器的主动组件与从动组件处于接合状态,然后将发电机作为电动机,通过发电机带动动力涡轮轴转动,进而通过处于接合状态的离合器带得燃气发生器同步升转,且在升转期间完成供油和点火步骤,当燃气发生器的转动达到脱开转速时,切断离合器的主动组件与从动组件之间的连接,使燃气发生器在起动程序控制下继续升转至慢车转速,直至完成燃气轮机的起动过程。A method for starting a light multi-shaft gas turbine, which adopts the starting structure of a light multi-shaft gas turbine, specifically: when the gas turbine needs to be started, firstly control the active assembly and the driven assembly of the clutch to be in the engaged state, and then use the generator as a motor , through the generator to drive the power turbine shaft to rotate, and then through the clutch in the engaged state to drive the gas generator to rotate up synchronously, and complete the oil supply and ignition steps during the up-rotation period, when the rotation of the gas generator reaches the disengagement speed, Cut off the connection between the active component and the driven component of the clutch, so that the gas generator continues to rise to the idle speed under the control of the starting program until the starting process of the gas turbine is completed.

本发明的有益效果:Beneficial effects of the present invention:

本发明的轻型多轴燃气轮机起动结构及起动方法,通过在动力涡轮轴和燃气发生器之间安装自动控制或手动控制的离合器,将发电机作为电动机使用来带动动力涡轮轴,再通过离合器将起动力矩传递给燃气发生器,以实现燃气轮机的起动,不但简化了传动系统结构,而且有效降低了燃气轮机的整机产品成本,有利于产品竞争力的提升。In the starting structure and starting method of the light multi-shaft gas turbine of the present invention, an automatic control or manual control clutch is installed between the power turbine shaft and the gas generator, and the generator is used as a motor to drive the power turbine shaft, and then the starting The torque is transmitted to the gas generator to realize the start of the gas turbine, which not only simplifies the structure of the transmission system, but also effectively reduces the cost of the whole product of the gas turbine, which is conducive to the improvement of product competitiveness.

附图说明Description of drawings

图1为本发明的一种轻型多轴燃气轮机起动结构的结构原理图;Fig. 1 is a structural principle diagram of a light-duty multi-shaft gas turbine starting structure of the present invention;

图中,1—燃气发生器,2—动力涡轮轴,3—离合器,3.1—主动组件,3.2—从动组件,4—联轴器,5—发电机。In the figure, 1—gas generator, 2—power turbine shaft, 3—clutch, 3.1—driving component, 3.2—driven component, 4—coupling, 5—generator.

具体实施方式detailed description

下面结合附图和具体实施例对本发明做进一步的详细说明。The present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.

如图1所示,一种轻型多轴燃气轮机起动结构,包括燃气发生器1、动力涡轮轴2、离合器3、联轴器4及发电机5;所述燃气发生器1与动力涡轮轴2之间通过离合器3连接配合;所述发电机5通过联轴器4与动力涡轮轴2相连接;所述离合器3的主动组件3.1连接在动力涡轮轴2上,离合器3的从动组件3.2连接在燃气发生器1上。As shown in Figure 1, a kind of light multi-shaft gas turbine starting structure comprises gas generator 1, power turbine shaft 2, clutch 3, shaft coupling 4 and generator 5; The generator 5 is connected with the power turbine shaft 2 through the shaft coupling 4; the active assembly 3.1 of the clutch 3 is connected to the power turbine shaft 2, and the driven assembly 3.2 of the clutch 3 is connected to the Gas generator 1 on.

所述离合器3采用自动控制的离合器或手动控制的离合器。Described clutch 3 adopts the clutch of automatic control or the clutch of manual control.

一种轻型多轴燃气轮机起动方法,采用了所述的轻型多轴燃气轮机起动结构,具体为:当燃气轮机需要起动时,首先控制离合器3的主动组件3.1与从动组件3.2处于接合状态,然后将发电机5作为电动机,通过发电机5带动动力涡轮轴2转动,进而通过处于接合状态的离合器3带得燃气发生器1同步升转,且在升转期间完成供油和点火步骤,当燃气发生器1的转动达到脱开转速时,切断离合器3的主动组件3.1与从动组件3.2之间的连接,使燃气发生器1在起动程序控制下继续升转至慢车转速,直至完成燃气轮机的起动过程。A method for starting a light multi-shaft gas turbine, which adopts the starting structure of a light multi-shaft gas turbine, specifically: when the gas turbine needs to be started, firstly control the active component 3.1 of the clutch 3 and the driven component 3.2 to be in the engaged state, and then generate electricity Engine 5 acts as an electric motor, drives the power turbine shaft 2 to rotate through the generator 5, and then drives the gas generator 1 to rotate synchronously through the clutch 3 in the engaged state, and completes the steps of oil supply and ignition during the upgrade period, when the gas generator When the rotation of 1 reaches the disengagement speed, the connection between the active component 3.1 and the driven component 3.2 of the clutch 3 is cut off, so that the gas generator 1 continues to rise to the idle speed under the control of the starting program until the starting process of the gas turbine is completed.

实施例中的方案并非用以限制本发明的专利保护范围,凡未脱离本发明所为的等效实施或变更,均包含于本案的专利范围中。The solutions in the embodiments are not intended to limit the scope of patent protection of the present invention, and all equivalent implementations or changes that do not deviate from the present invention are included in the patent scope of this case.

Claims (3)

1. A light-duty multiaxis gas turbine starts structure which characterized in that: the device comprises a fuel gas generator, a power turbine shaft, a clutch, a coupler and a generator; the fuel gas generator is connected and matched with the power turbine shaft through a clutch; the generator is connected with the power turbine shaft through a coupler; the driving assembly of the clutch is connected to the power turbine shaft, and the driven assembly of the clutch is connected to the gas generator.
2. A light-weight multi-shaft gas turbine starting structure according to claim 1, wherein: the clutch adopts an automatically controlled clutch or a manually controlled clutch.
3. A light-weight multi-shaft gas turbine starting method using the light-weight multi-shaft gas turbine starting structure of claim 1, characterized by comprising: when the gas turbine needs to be started, firstly, a driving component and a driven component of the clutch are controlled to be in a joint state, then the generator is used as a motor, the power turbine shaft is driven to rotate by the generator, the gas generator is driven to synchronously rotate through the clutch in the joint state, the oil supply and ignition steps are completed during the rotation, when the rotation of the gas generator reaches the disengaging rotation speed, the connection between the driving component and the driven component of the clutch is cut off, and the gas generator continues to rotate to the slow vehicle rotation speed under the control of a starting program until the starting process of the gas turbine is completed.
CN202211178574.9A 2022-09-27 2022-09-27 A light multi-shaft gas turbine starting structure and starting method Pending CN115492690A (en)

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Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2001193476A (en) * 2000-01-14 2001-07-17 Ishikawajima Harima Heavy Ind Co Ltd Multi-shaft gas turbine starting apparatus and starting method
CN101628627A (en) * 2008-07-18 2010-01-20 尤洛考普特公司 Hybrid power plant and method of controlling such a power plant
CN104956036A (en) * 2012-11-08 2015-09-30 诺沃皮尼奥内股份有限公司 Gas turbine in mechanical drive applications and operating methods
CN105579690A (en) * 2013-05-31 2016-05-11 诺沃皮尼奥内股份有限公司 Gas turbines in mechanical drive applications and operating methods
CN205578118U (en) * 2016-04-26 2016-09-14 中科合肥微小型燃气轮机研究院有限责任公司 High -speed small -size gas turbine generating system that declines that directly drives
CN108180045A (en) * 2018-02-07 2018-06-19 上海电气电站设备有限公司 Gas-steam Combined Cycle peak regulation phase modulation shaft system of unit support construction
CN108204279A (en) * 2016-12-16 2018-06-26 通用电气公司 Double-fed type induction generator system and the method for operating multiaxis gas-turbine unit
CN111441867A (en) * 2020-03-20 2020-07-24 中国科学院工程热物理研究所 A compressed air energy storage system for gas turbine combined cycle generator set
CN213016561U (en) * 2020-09-08 2021-04-20 贵州黎阳天翔科技有限公司 Cantilever motor transmission structure of micro gas turbine
CN114030622A (en) * 2021-11-29 2022-02-11 上海尚实能源科技有限公司 Aviation auxiliary power device and aircraft

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2001193476A (en) * 2000-01-14 2001-07-17 Ishikawajima Harima Heavy Ind Co Ltd Multi-shaft gas turbine starting apparatus and starting method
CN101628627A (en) * 2008-07-18 2010-01-20 尤洛考普特公司 Hybrid power plant and method of controlling such a power plant
CN104956036A (en) * 2012-11-08 2015-09-30 诺沃皮尼奥内股份有限公司 Gas turbine in mechanical drive applications and operating methods
CN105579690A (en) * 2013-05-31 2016-05-11 诺沃皮尼奥内股份有限公司 Gas turbines in mechanical drive applications and operating methods
CN205578118U (en) * 2016-04-26 2016-09-14 中科合肥微小型燃气轮机研究院有限责任公司 High -speed small -size gas turbine generating system that declines that directly drives
CN108204279A (en) * 2016-12-16 2018-06-26 通用电气公司 Double-fed type induction generator system and the method for operating multiaxis gas-turbine unit
CN108180045A (en) * 2018-02-07 2018-06-19 上海电气电站设备有限公司 Gas-steam Combined Cycle peak regulation phase modulation shaft system of unit support construction
CN111441867A (en) * 2020-03-20 2020-07-24 中国科学院工程热物理研究所 A compressed air energy storage system for gas turbine combined cycle generator set
CN213016561U (en) * 2020-09-08 2021-04-20 贵州黎阳天翔科技有限公司 Cantilever motor transmission structure of micro gas turbine
CN114030622A (en) * 2021-11-29 2022-02-11 上海尚实能源科技有限公司 Aviation auxiliary power device and aircraft

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