CN115683030A - Gas turbine engagement angle measuring device and method - Google Patents
Gas turbine engagement angle measuring device and method Download PDFInfo
- Publication number
- CN115683030A CN115683030A CN202211498209.6A CN202211498209A CN115683030A CN 115683030 A CN115683030 A CN 115683030A CN 202211498209 A CN202211498209 A CN 202211498209A CN 115683030 A CN115683030 A CN 115683030A
- Authority
- CN
- China
- Prior art keywords
- measuring device
- clutch
- angle
- connecting shaft
- gas turbine
- 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.)
- Pending
Links
Images
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E20/00—Combustion technologies with mitigation potential
- Y02E20/16—Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]
Landscapes
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
Abstract
Description
技术领域technical field
本发明涉及燃气发电技术,尤其是一种燃气轮机啮合角测量装置及方法。The invention relates to gas power generation technology, in particular to a gas turbine meshing angle measuring device and method.
背景技术Background technique
燃气轮机联合循环(Combined-Cycle Gas Turbine,CCGT),又称燃气—蒸汽联合循环,是指将燃气轮机和蒸汽轮机组合起来的一种发电方式,主要由燃气轮机(压气机、燃烧室、透平、控制系统和辅助系统)、余热锅炉、蒸汽轮机三部分构成。燃气轮机的压气机吸入空气压缩后送入燃烧室内,使燃料(油或天然气)燃烧产生高温高压燃气,进入燃气轮机膨胀做功发电,再将燃气轮机排出的气体引入锅炉(余热锅炉),作为锅炉的热源,利用锅炉产生的蒸汽进入蒸汽轮机再发电;这样就形成了燃气轮机和蒸汽轮机共同作为原动机的联合循环发电系统;余热利用式的系统简单,燃气轮机出力占总出力的比例大,蒸汽轮机不能单独运行。Combined-Cycle Gas Turbine (CCGT), also known as gas-steam combined cycle, refers to a power generation method that combines a gas turbine and a steam turbine, and is mainly composed of a gas turbine (compressor, combustion chamber, turbine, control system and auxiliary system), waste heat boiler and steam turbine are composed of three parts. The compressor of the gas turbine inhales and compresses the air and sends it into the combustion chamber, so that the fuel (oil or natural gas) is burned to produce high-temperature and high-pressure gas, which enters the gas turbine to expand and generate power, and then the gas discharged from the gas turbine is introduced into the boiler (waste heat boiler) as the heat source of the boiler. The steam generated by the boiler is used to enter the steam turbine to generate electricity; thus, a combined cycle power generation system is formed in which the gas turbine and the steam turbine act as the prime mover; the waste heat utilization system is simple, and the output of the gas turbine accounts for a large proportion of the total output, and the steam turbine cannot be operated alone .
如授权公告号为CN206753668U的中国专利文件公开的“一种燃气蒸汽联合循环机组的单轴布置结构”,第一机组、第二机组均包括轴系轴向上依次设置的燃气轮机、发电机、3S离合器、蒸汽轮机和凝汽器 。如公布号为CN110284930A的中国专利文件公开的“一种西门子9F燃机联合循环机组恒排汽缸温度离合器啮合控制方法”,机组发电机与汽轮机之间采用SSS离合器啮合;通过在机组启动期间适当破坏真空,增加安装与凝汽器内的轴承膨胀量,可有效降低机组启动期间振动。For example, the Chinese patent document with the authorized announcement number CN206753668U discloses "a single-shaft arrangement structure of a gas-steam combined cycle unit", the first unit and the second unit include gas turbines, generators, 3S Clutches, steam turbines and condensers. For example, the Chinese patent document with the publication number CN110284930A discloses "a Siemens 9F gas turbine combined cycle unit constant exhaust cylinder temperature clutch engagement control method", the SSS clutch is used between the unit generator and the steam turbine; Vacuum increases the installation and bearing expansion in the condenser, which can effectively reduce the vibration during unit startup.
上述燃气轮机联合循环机组中,缺少3S离合器工作时轴系对中的检测,在啮合过程中,由于3S离合器齿轮传动及其结构设计,导致其两侧转子的啮合间隙存在随机性,会导致轴瓦振动敏感性增强、引起振动偏大,普遍存在3S离合器振动大的问题 。In the gas turbine combined cycle unit mentioned above, there is a lack of detection of shafting alignment when the 3S clutch is working. During the meshing process, due to the gear transmission and structural design of the 3S clutch, the meshing gap between the rotors on both sides is random, which will cause vibration of the bearing bush. Sensitivity increases, resulting in large vibrations, and the problem of large vibrations in 3S clutches is common.
发明内容Contents of the invention
本发明的目的在于提供一种燃气轮机啮合角测量装置及方法,用于解决现有燃气轮机联合循环机组中3S离合器振动大的问题。The object of the present invention is to provide a gas turbine meshing angle measurement device and method, which are used to solve the problem of large vibration of the 3S clutch in the existing gas turbine combined cycle unit.
为了解决上述问题,本发明提供一种燃气轮机啮合角测量装置,包括依次连接的燃气轮机、发电机、3S离合器和汽轮机,发电机与所述3S离合器之间的第一连接轴上安装有第一轴瓦、第二轴瓦,所述3S离合器与所述汽轮机之间的第二连接轴上安装有第三轴瓦、第四轴瓦;所述第一连接轴上设有用于检测所述第一连接轴的旋转位置角度的第一键相测量装置,所述第二连接轴上设有用于检测所述第二连接轴的旋转位置角度的第二键相测量装置,所述3S离合器与所述第一连接轴相连的转盘外侧上设有第三键相测量装置,所述3S离合器与所述第二连接轴相连的转盘外侧上设有第四键相测量装置。In order to solve the above problems, the present invention provides a gas turbine meshing angle measurement device, which includes a gas turbine, a generator, a 3S clutch and a steam turbine connected in sequence, and a first bearing bush is installed on the first connecting shaft between the generator and the 3S clutch , the second bearing bush, the third bearing bush and the fourth bearing bush are installed on the second connecting shaft between the 3S clutch and the steam turbine; The first key-phase measuring device for the position angle, the second connecting shaft is provided with a second key-phase measuring device for detecting the rotational position angle of the second connecting shaft, the 3S clutch and the first connecting shaft A third key phase measurement device is provided on the outside of the connected turntable, and a fourth key phase measurement device is provided on the outside of the turntable where the 3S clutch is connected to the second connecting shaft.
本发明提供的燃气轮机啮合角测量装置还具有以下技术特征:The gas turbine meshing angle measuring device provided by the present invention also has the following technical features:
进一步地,所述第二轴瓦、所述第三轴瓦还连接有振动测量装置 。Further, the second bearing bush and the third bearing bush are also connected with a vibration measuring device.
进一步地,所述第一轴瓦、所述第四轴瓦还连接振动测量装置 。Further, the first bearing bush and the fourth bearing bush are also connected to a vibration measuring device.
进一步地,所述第一键相测量装置、所述第一键相测量装置布置于所述第一连接轴、所述第二连接轴的同侧 。Further, the first key phase measuring device and the first key phase measuring device are arranged on the same side of the first connecting shaft and the second connecting shaft.
进一步地,所述第三键相测量装置、所述第四键相测量装置布置于所述第一连接轴、所述第二连接轴的另一侧。Further, the third key phase measurement device and the fourth key phase measurement device are arranged on the other side of the first connection shaft and the second connection shaft.
本发明还提供一种燃气轮机啮合角测量方法,包括上述燃气轮机啮合角测量装置,所述发电机与所述汽轮机之间的所述3S离合器的啮合角度等于所述第一连接轴的旋转位置角度与所述第二连接轴的旋转位置角度的差值。The present invention also provides a method for measuring the meshing angle of a gas turbine, which includes the above gas turbine meshing angle measuring device, and the meshing angle of the 3S clutch between the generator and the steam turbine is equal to the rotation position angle of the first connecting shaft and The difference between the rotation position angles of the second connection shaft.
进一步地,所述3S离合器的啮合角度α=1/2(α1 + α3 - α2 -α4),其中α1为所述第一连接轴的旋转位置角度,α2为所述第二连接轴的旋转位置角度,α3为所述3S离合器与所述第一连接轴相连的转盘的旋转位置角度,α4为所述3S离合器与所述第二连接轴相连的转盘的旋转位置角度。Further, the engagement angle of the 3S clutch is α=1/2 (α1 + α3 - α2 - α4), where α1 is the rotation position angle of the first connection shaft, and α2 is the rotation position of the second connection shaft Angle, α3 is the rotation position angle of the turntable connected with the first connection shaft of the 3S clutch, and α4 is the rotation position angle of the turntable connected with the second connection shaft of the 3S clutch.
本发明具有如下有益效果:通过设置检测第一连接轴的旋转位置角度的第一键相测量装置,设置检测第二连接轴的旋转位置角度的第二键相测量装置,可根据第一连接轴的旋转位置角度、第二连接轴的旋转位置角度计算第一连接轴、第二转轴的相对转角,由此获得3S离合器啮合时的啮合角,能够为分析振动原因提供准确的3S离合器啮合角度,可减少机组振动轴系稳定性问题处理时间,综合轴瓦的振动测量数据可用以指导3S离合器啮合前后轴系稳定的治理 。The present invention has the following beneficial effects: by setting the first key-phase measuring device for detecting the rotation position angle of the first connecting shaft, and setting the second key-phase measuring device for detecting the rotational position angle of the second connecting shaft, the Calculate the relative rotation angle of the first connecting shaft and the second rotating shaft based on the rotation position angle of the rotation position angle of the second connecting shaft, and thus obtain the meshing angle of the 3S clutch, which can provide an accurate 3S clutch meshing angle for analyzing the cause of vibration. It can reduce the time to deal with the stability of the vibration shaft system of the unit, and the vibration measurement data of the comprehensive bearing bush can be used to guide the treatment of the shaft system stability before and after the 3S clutch is engaged.
附图说明Description of drawings
图1为本发明实施例的燃气轮机啮合角测量装置的结构示意图 。Fig. 1 is a schematic structural diagram of a gas turbine meshing angle measurement device according to an embodiment of the present invention.
具体实施方式Detailed ways
下文中将参考附图并结合实施例来详细说明本发明。需要说明的是,在不冲突的情况下,本发明中的实施例及实施例中的特征可以相互组合。Hereinafter, the present invention will be described in detail with reference to the drawings and examples. It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other.
如图1所示的本发明的燃气轮机啮合角测量装置的实施例中,该燃气轮机啮合角测量装置及方法置包括依次连接的燃气轮机10、发电机20、3S离合器30和汽轮机40,发电机20与所述3S离合器30之间的第一连接轴11上安装有第一轴瓦21、第二轴瓦21,所述3S离合器30与汽轮机40之间的第二连接轴12上安装有第三轴瓦23、第四轴瓦24;第一连接轴11上设有用于检测第一连接轴11的旋转位置角度α1的第一键相测量装置41,第二连接轴12上设有用于检测第二连接轴12的旋转位置角度α2的第二键相测量装置42,所述3S离合器30与第一连接轴11相连的转盘31外侧上设有第三键相测量装置43,所述3S离合器30与第二连接轴12相连的转盘32外侧上设有第四键相测量装置44。In the embodiment of the gas turbine meshing angle measuring device of the present invention as shown in Figure 1, this gas turbine meshing angle measuring device and method set include
本申请通过设置检测第一连接轴的旋转位置角度的第一键相测量装置,设置检测第二连接轴的旋转位置角度的第二键相测量装置,可根据第一连接轴的旋转位置角度、第二连接轴的旋转位置角度计算第一连接轴、第二转轴的相对转角,由此获得3S离合器啮合时的啮合角,能够为分析振动原因提供准确的3S离合器啮合角度,可减少机组振动轴系稳定性问题处理时间,综合轴瓦的振动测量数据可用以指导3S离合器啮合前后轴系稳定的治理 。In the present application, by setting the first key-phase measuring device for detecting the rotational position angle of the first connecting shaft, and setting the second key-phase measuring device for detecting the rotational position angle of the second connecting shaft, according to the rotational position angle of the first connecting shaft, Calculate the relative rotation angle of the first connecting shaft and the second rotating shaft from the rotation position angle of the second connecting shaft, thereby obtaining the meshing angle when the 3S clutch is engaged, which can provide an accurate 3S clutch meshing angle for analyzing the cause of vibration, and can reduce the vibration axis of the unit The time to deal with the system stability problem, the vibration measurement data of the comprehensive bearing bush can be used to guide the treatment of the shaft system stability before and after the 3S clutch is engaged.
在本申请的一个实施例中,优选地,第二轴瓦22、第三轴瓦23还连接有振动测量装置,由此根据3S离合器啮合时不同的3S离合器啮合角度对应的第二轴瓦22、第三轴瓦23的振动情况,可建立振动分析模型。 优选地, 第一轴瓦21、第四轴瓦24还连接振动测量装置,由此可根据3S离合器啮合时不同的3S离合器啮合角度对应的第一轴瓦21、第二轴瓦22、第三轴瓦23、第四轴瓦24的振动情况,可建立振动分析模型,用以分析机组振动的原因。In one embodiment of the present application, preferably, the second bearing
在本申请的一个实施例中,优选地,如图1所示,第一键相测量装置41、第一键相测量装置42布置于第一连接轴11、第二连接轴12的同侧,具体而言,第一键相测量装置41、第二键相测量装置42共用同一个轴系坐标,可简化3S离合器啮合角度的计算过程;优选地,第三键相测量装置43、第四键相测量装置44布置于第一连接轴11、第二连接轴12的另一侧,由此可提高3S离合器啮合角度检测的可靠性。In one embodiment of the present application, preferably, as shown in FIG. 1 , the first key
本发明的另一个实施例还提供一种燃气轮机啮合角测量装置方法,该燃气轮机啮合角测量装置方法包括上述燃气轮机啮合角测量装置,发电机20与汽轮机40之间的3S离合器30的啮合角度α=α1 - α2 ,α1为第一连接轴11的旋转位置角度,α2为第二连接轴12的旋转位置角度。本申请通过设置第一键相测量装置、第二键相测量装置测量第一连接轴、第二连接轴的旋转位置角度,由此可计算获得3S离合器啮合时的啮合角度,能够为分析振动原因提供准确的3S离合器啮合角度,可减少机组振动轴系稳定性问题处理时间。Another embodiment of the present invention also provides a gas turbine meshing angle measuring device method, the gas turbine meshing angle measuring device method includes the above-mentioned gas turbine meshing angle measuring device, the meshing angle α of the
在本申请的一个实施例中,优选地,3S离合器的啮合角度α=1/2(α1 + α3 - α2 -α4),其中α1为所述第一连接轴的旋转位置角度,α2为所述第二连接轴的旋转位置角度,α3为所述3S离合器与所述第一连接轴相连的转盘的旋转位置角度,α4为所述3S离合器与所述第二连接轴相连的转盘的旋转位置角度,由此可提高3S离合器啮合角度检测的可靠性。In one embodiment of the present application, preferably, the engagement angle of the 3S clutch α=1/2 (α1 + α3 - α2 - α4), where α1 is the rotation position angle of the first connecting shaft, and α2 is the The rotation position angle of the second connection shaft, α3 is the rotation position angle of the turntable that the 3S clutch is connected to the first connection shaft, and α4 is the rotation position angle of the turntable that the 3S clutch is connected to the second connection shaft , thereby improving the reliability of 3S clutch engagement angle detection.
最后应说明的是:以上实施例仅用以说明本发明的技术方案,而非对其限制;尽管参照前述实施例对本发明进行了详细的说明,本领域的普通技术人员应当理解:其依然可以对前述各实施例所记载的技术方案进行修改,或者对其中部分技术特征进行等同替换;而这些修改或者替换,并不使相应技术方案的本质脱离本发明各实施例技术方案的精神和范围。Finally, it should be noted that: the above embodiments are only used to illustrate the technical solutions of the present invention, rather than to limit them; although the present invention has been described in detail with reference to the foregoing embodiments, those of ordinary skill in the art should understand that: it can still be Modifications are made to the technical solutions described in the foregoing embodiments, or equivalent replacements are made to some of the technical features; and these modifications or replacements do not make the essence of the corresponding technical solutions deviate from the spirit and scope of the technical solutions of the various embodiments of the present invention.
Claims (7)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211498209.6A CN115683030A (en) | 2022-11-28 | 2022-11-28 | Gas turbine engagement angle measuring device and method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211498209.6A CN115683030A (en) | 2022-11-28 | 2022-11-28 | Gas turbine engagement angle measuring device and method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN115683030A true CN115683030A (en) | 2023-02-03 |
Family
ID=85056170
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202211498209.6A Pending CN115683030A (en) | 2022-11-28 | 2022-11-28 | Gas turbine engagement angle measuring device and method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN115683030A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009244050A (en) * | 2008-03-31 | 2009-10-22 | Mitsubishi Heavy Ind Ltd | Shaft misalignment amount detection method in drive power transmission mechanism using self aligning engagement clutch |
| CN106017903A (en) * | 2016-07-14 | 2016-10-12 | 贵州电网有限责任公司电力科学研究院 | Steam turbine generator unit shafting eccentricity and phase measuring device and steam turbine generator unit shafting eccentricity and phase measuring method |
| CN206753668U (en) * | 2017-03-14 | 2017-12-15 | 珠海市钰海电力有限公司 | A kind of single shaft arrangement of Combined cycle gas-steam turbine unit |
| CN110017805A (en) * | 2019-03-20 | 2019-07-16 | 中国大唐集团科学技术研究院有限公司火力发电技术研究院 | A kind of NCB residual heat utilization-type turbine shafting centering on-Line Monitor Device and method |
| CN114486240A (en) * | 2021-12-23 | 2022-05-13 | 华北电力科学研究院有限责任公司 | Engagement method and device for steam turbine clutch |
-
2022
- 2022-11-28 CN CN202211498209.6A patent/CN115683030A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009244050A (en) * | 2008-03-31 | 2009-10-22 | Mitsubishi Heavy Ind Ltd | Shaft misalignment amount detection method in drive power transmission mechanism using self aligning engagement clutch |
| CN106017903A (en) * | 2016-07-14 | 2016-10-12 | 贵州电网有限责任公司电力科学研究院 | Steam turbine generator unit shafting eccentricity and phase measuring device and steam turbine generator unit shafting eccentricity and phase measuring method |
| CN206753668U (en) * | 2017-03-14 | 2017-12-15 | 珠海市钰海电力有限公司 | A kind of single shaft arrangement of Combined cycle gas-steam turbine unit |
| CN110017805A (en) * | 2019-03-20 | 2019-07-16 | 中国大唐集团科学技术研究院有限公司火力发电技术研究院 | A kind of NCB residual heat utilization-type turbine shafting centering on-Line Monitor Device and method |
| CN114486240A (en) * | 2021-12-23 | 2022-05-13 | 华北电力科学研究院有限责任公司 | Engagement method and device for steam turbine clutch |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Fahmi et al. | A comprehensive review on mechanical failures cause vibration in the gas turbine of combined cycle power plants | |
| Hada et al. | Test results of the world’s first 1,600 C J-series gas turbine | |
| CN105841966B (en) | A kind of suitable for turbogenerator vibration multi based on forward reasoning | |
| CN101699046A (en) | Method for partitioning total output of single shaft gas-steam combined cycle generating set | |
| US11041782B2 (en) | Secure systems and methods for machine monitoring | |
| CN101403648A (en) | Steam flow excitation fault real-time diagnosis method for large steam turbine-generator | |
| Kim et al. | Performance analysis of bladeless jet propulsion micro-steam turbine for micro-CHP (combined heat and power) systems utilizing low-grade heat sources | |
| JP2011102581A (en) | Method and system for increasing efficiency of pressurized machine | |
| CN110017805A (en) | A kind of NCB residual heat utilization-type turbine shafting centering on-Line Monitor Device and method | |
| Vanieiev et al. | Investigation of a turbogenerator based on the vortex expansion machine with a peripheral side channel | |
| CN115683030A (en) | Gas turbine engagement angle measuring device and method | |
| CN102087140B (en) | Method for analyzing stability of low-frequency vibration main peak frequency of turbo generator set | |
| Huang et al. | Angle misalignment detection and its suppression algorithm in rotor system based on speed signal | |
| CN102103037B (en) | Method for analyzing correlation between low-frequency vibration and power increase of turbine generator set | |
| CN104344956A (en) | Bearing fault simulation method for wind power generation gearbox | |
| JP2006207558A (en) | Extracted back-pressure steam turbine equipment and operation method thereof | |
| Dong et al. | Working process of steam turbine and establishment of start-up model | |
| CN115758040B (en) | Method for distinguishing the power of steam turbine and gas turbine in single-shaft combined cycle generator set | |
| Mohanty et al. | Enhancement of Turbine Performance Using Root Cause Failure Analysis and LPDE Correction | |
| Kasilov et al. | Cogeneration steam turbines from Siemens: New solutions | |
| CN110284930A (en) | A kind of Siemens 9F combustion engine combined cycle unit perseverance exhaust casing temperature clutch engagement control method | |
| Wang et al. | Fault Diagnosis for Motor Based on EMD Algorithm | |
| Xie et al. | Modeling and Power-Hardware-in-the-Loop Validation of Synchronous Machine Governor | |
| CN110554318B (en) | High-speed alternating-current generator test bed considering speed regulation interval | |
| CN119803986A (en) | Fault information generation method, device, storage medium and computing device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |