[go: up one dir, main page]

CN111486476A - A New Intelligent Suppressor of Combustion Instability - Google Patents

A New Intelligent Suppressor of Combustion Instability Download PDF

Info

Publication number
CN111486476A
CN111486476A CN202010272310.4A CN202010272310A CN111486476A CN 111486476 A CN111486476 A CN 111486476A CN 202010272310 A CN202010272310 A CN 202010272310A CN 111486476 A CN111486476 A CN 111486476A
Authority
CN
China
Prior art keywords
combustion
sound absorption
suppressor
absorption pipeline
sealing piston
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
Application number
CN202010272310.4A
Other languages
Chinese (zh)
Inventor
刘云鹏
颜应文
李伟
田泽民
李井华
刘勇
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.)
Nanjing University of Aeronautics and Astronautics
Original Assignee
Nanjing University of Aeronautics and Astronautics
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 Nanjing University of Aeronautics and Astronautics filed Critical Nanjing University of Aeronautics and Astronautics
Priority to CN202010272310.4A priority Critical patent/CN111486476A/en
Publication of CN111486476A publication Critical patent/CN111486476A/en
Pending legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/26Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid with provision for a retention flame
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details

Landscapes

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

Abstract

The invention discloses a novel intelligent suppressor for unstable combustion, which belongs to the field of combustion.A control system is used for sampling oscillation pressure generated by unstable combustion in real time, analyzing oscillation dominant frequency of the oscillation pressure in real time and rapidly, and then outputting an adjusting signal through a stepping motor; the sealing piston in the sound absorption pipeline is connected with the precise screw rod, the rotary lifting component is utilized to adjust the up-and-down movement of the sealing piston through rotation, and a gear arranged outside the rotary lifting component and the stepping motor form a gear transmission mechanism, so that the position of the sealing piston in the sound absorption pipeline can be adjusted through the stepping motor, and the working frequency of the sound absorption pipeline is adjusted; the invention ensures that the suppressor has a larger working frequency range, can ensure the optimal suppression effect and solves the problems of single control frequency and narrower working frequency band of the traditional combustion unstable passive controller.

Description

一种新型燃烧不稳定智能抑制器A New Intelligent Suppressor of Combustion Instability

技术领域technical field

本发明属于燃烧领域,涉及一种燃烧不稳定抑制器,具体是一种新型燃烧不稳定智能抑制器。The invention belongs to the field of combustion, and relates to a combustion instability suppressor, in particular to a novel combustion instability intelligent suppressor.

背景技术Background technique

近年来人们逐渐关注燃烧低污染排放问题,而贫燃料燃烧技术在降低排放方面具有较大的发展潜力,但这使得燃料燃烧对于声波扰动变得更加敏感,容易发生燃烧不稳定现象。燃烧不稳定现象广泛存在于燃气轮机燃烧室、火箭发动机以及锅炉等燃烧系统中。燃烧火焰等产生的声波扰动经过系统边界反射到达火焰位置后进一步对火焰进行干扰,当火焰热释放脉动与声波同相位(相位差小于90°)时两者相互耦合、相互驱动,产生幅值较大的振荡声波,其不仅增加了燃烧熄火的风险,还会对燃烧系统造成严重的结构破坏。In recent years, people have gradually paid attention to the issue of low-pollution emissions from combustion, and lean-fuel combustion technology has great development potential in reducing emissions, but this makes fuel combustion more sensitive to acoustic disturbances and prone to combustion instability. Combustion instability occurs widely in combustion systems such as gas turbine combustors, rocket engines, and boilers. The sound wave disturbance generated by the combustion flame, etc., is reflected by the system boundary and reaches the flame position to further interfere with the flame. When the flame heat release pulsation and the sound wave are in the same phase (the phase difference is less than 90°), the two are coupled and driven each other, resulting in a relatively high amplitude. Large oscillating sound waves, which not only increase the risk of flameout, but also cause severe structural damage to the combustion system.

综上所述,燃烧不稳定是声波脉动与火焰脉动之间的相互耦合引起的,因此不同学者研究了不同种控制方法以降低热释放脉动,同时通过吸收声波能量来降低燃烧不稳定的发生风险或者降低振荡压力的脉动幅值。对于燃烧不稳定的控制方法主要分为主动控制和被动控制。在燃烧不稳定主动控制中控制系统根据采样的振荡压力信号通过动作器(高频电磁阀或者扬声器等)向燃烧系统内输入控制能量对声波或者火焰进行干扰;而在燃烧不稳定被动控制中则不需要额外向被控系统中输入能量,往往会由于被动控制器的加入改变了原始系统的特性,使得原始系统的燃烧不稳定现象得到消除或者减弱。To sum up, the combustion instability is caused by the mutual coupling between the sonic pulsation and the flame pulsation. Therefore, different scholars have studied different control methods to reduce the heat release pulsation, and at the same time, reduce the risk of combustion instability by absorbing the sonic energy or Reduce the pulsation amplitude of the oscillating pressure. The control methods for combustion instability are mainly divided into active control and passive control. In the active control of combustion instability, the control system inputs control energy into the combustion system through the actuator (high-frequency solenoid valve or speaker, etc.) according to the sampled oscillating pressure signal to interfere with the sound wave or flame; while in the passive control of combustion instability, the There is no need to input additional energy into the controlled system, and the characteristics of the original system are often changed due to the addition of passive controllers, so that the combustion instability of the original system is eliminated or weakened.

一种典型的燃烧不稳定被动控制器为亥姆霍兹共振器,其由短管和声腔体构成,设计亥姆霍兹共振器的共振频率与燃烧不稳定的振荡压力主频一致,则其对振荡压力具有吸收效果,由此降低了燃烧不稳定的振荡强度。但亥姆霍兹共振器或者其他吸声结构在对燃烧不稳定的抑制时存在诸多缺点,比如其工作频率单一、工作频率带宽较窄,当燃烧系统的振荡频率与共振器的共振频率稍有偏差时其控制效果明显变差。因此,对于燃烧不稳定的被动控制器的深入研究,譬如如何扩大其工作频率带宽问题,使其具有更广的适应范围成为研究热点。A typical passive controller for combustion instability is a Helmholtz resonator, which consists of a short tube and an acoustic cavity. Has an absorbing effect on the oscillating pressure, thereby reducing the oscillating intensity of combustion instability. However, Helmholtz resonators or other sound-absorbing structures have many disadvantages in suppressing combustion instability, such as their single operating frequency and narrow operating frequency bandwidth. When the oscillation frequency of the combustion system is slightly different from the resonant frequency of the resonator When the deviation is exceeded, the control effect is obviously deteriorated. Therefore, the in-depth study of the passive controller with unstable combustion, such as how to expand its operating frequency bandwidth to make it have a wider range of adaptation, has become a research hotspot.

发明内容SUMMARY OF THE INVENTION

本发明就是基于现有技术中被动控制器的发展思路,公开了一种新型燃烧不稳定智能抑制器,该抑制器主要由末端可调的吸声管道与控制系统构成。控制系统通过对燃烧不稳定产生的振荡压力实时监测,智能调节波长管末端活塞位置,以此增加其工作频率范围,解决了传统燃烧不稳定被动控制器控制频率单一、工作频段较窄的问题。The invention is based on the development idea of the passive controller in the prior art, and discloses a novel combustion instability intelligent suppressor, which is mainly composed of a sound absorption pipe with an adjustable end and a control system. The control system intelligently adjusts the position of the piston at the end of the wavelength tube through real-time monitoring of the oscillating pressure generated by combustion instability, thereby increasing its working frequency range, solving the problems of single control frequency and narrow working frequency band of the traditional combustion instability passive controller.

本发明是这样实现的:The present invention is realized in this way:

一种新型燃烧不稳定智能抑制器,所述的抑制器包括燃烧装置壁面上分别设置的吸声管道以及振荡压力传感器,所述的吸声管道内部活动设置密封活塞,所述的密封活塞至燃烧装置壁面的距离为吸声管道的工作长度;本发明通过吸声管道来吸收燃烧不稳定产生的振荡压力波,吸声管道内的密封活塞起到封闭作用,密封活塞到底部距离为工作长度。A novel combustion instability intelligent suppressor, the suppressor comprises a sound-absorbing pipe and an oscillating pressure sensor respectively arranged on the wall of the combustion device, a sealing piston is movably arranged inside the sound-absorbing pipe, and the sealing piston is connected to the combustion chamber. The distance from the wall of the device is the working length of the sound absorption pipe; the invention absorbs the oscillating pressure wave generated by combustion instability through the sound absorption pipe, the sealing piston in the sound absorption pipe plays a sealing role, and the distance from the sealing piston to the bottom is the working length.

吸声管道的一端与燃烧系统连接,吸声管道的长度的实际工作长度是可以调节的,由控制系统在线实时调节。通过调节吸声管道中密封活塞的位置,使其共振频率与燃烧不稳定环境中振荡压力主频一致,可以较好的吸收振荡压力。抑制器将被动方式与主动方式相结合,活塞的移动由控制系统完成,控制系统对振荡压力进行采样,分析得到燃烧不稳定的振荡主频,进一步通过执行结构移动活塞到合理位置。One end of the sound-absorbing pipe is connected to the combustion system, and the actual working length of the sound-absorbing pipe can be adjusted, which is adjusted in real time by the control system online. By adjusting the position of the sealing piston in the sound absorption pipe so that its resonance frequency is consistent with the main frequency of the oscillating pressure in an unstable combustion environment, the oscillating pressure can be better absorbed. The suppressor combines passive and active methods. The movement of the piston is completed by the control system. The control system samples the oscillating pressure, analyzes the oscillation frequency of unstable combustion, and further moves the piston to a reasonable position through the execution structure.

密封活塞上设置有精密丝杠,所述的吸声管道顶端设置传动装置,所述的精密丝杠与传动装置连接,所述的传动装置包括旋转升降部件,所述的精密丝杠与旋转升降部件相连接,所述的旋转升降部件在外部设置步进电机;通过步进电机的转动,带动旋转升降部件控制精密丝杠的移动,进而控制密封活塞的移动,调整吸声管道的工作长度。A precision lead screw is arranged on the sealing piston, and a transmission device is arranged at the top of the sound-absorbing pipe. The precision lead screw is connected with the transmission device. The transmission device includes a rotating and lifting component. The components are connected, and the rotating lifting component is provided with a stepping motor outside; through the rotation of the stepping motor, the rotating lifting component is driven to control the movement of the precision lead screw, thereby controlling the movement of the sealing piston, and adjusting the working length of the sound absorption pipe.

进一步,所述的吸声管道的工作长度利用密封活塞的移动调节;所述的吸声管道的直径在10~50mm之间;所述的吸声管道在底部开设有恒定温度空气进口。恒定温度空气进气口安装在吸声管道的底端,该位置不会对活塞造成影响。引入到吸声管道中的空气可以是环境空气或者其他温度稳定的气体即可,其主要是为了维持吸声管道内稳定的温度环境,因此吸声管道的工作长度与其吸收的声波频率呈线性对应关系。Further, the working length of the sound-absorbing pipe is adjusted by the movement of the sealing piston; the diameter of the sound-absorbing pipe is between 10 and 50 mm; the sound-absorbing pipe is provided with a constant temperature air inlet at the bottom. The constant temperature air inlet is installed at the bottom end of the sound absorption duct, and this position does not affect the piston. The air introduced into the sound-absorbing pipe can be ambient air or other gas with stable temperature. It is mainly to maintain a stable temperature environment in the sound-absorbing pipe. Therefore, the working length of the sound-absorbing pipe is linearly corresponding to the frequency of the sound waves it absorbs. relation.

进一步,所述的旋转升降部件在外部设置齿轮,利用齿轮与步进电机连接。在旋转升降部件的外部安装齿轮,使得齿轮与步进电机通过齿轮配合进行传动,方便了旋转升降部件的灵活转动,方便传动控制。抑制器中传动装置的结构设计,使得步进电机角度转动转变为吸声管道中活塞的位置移动。并且将齿轮安装在旋转升降部件外部,旋转升降部件通过轴承与吸声管道连接,此种结构设计方便了零部件的采购与加工,同时保证了安装的简便性与可靠性。Further, the rotating lifting component is provided with a gear outside, and the gear is connected with the stepping motor. Gears are installed on the outside of the rotating lifting part, so that the gears and the stepping motor are driven by the gears, which facilitates the flexible rotation of the rotating lifting parts and facilitates transmission control. The structural design of the transmission device in the suppressor makes the angular rotation of the stepper motor change into the positional movement of the piston in the sound-absorbing pipe. In addition, the gear is installed outside the rotating lifting component, and the rotating lifting component is connected with the sound absorption pipe through the bearing. This structure design facilitates the procurement and processing of the components, and at the same time ensures the simplicity and reliability of the installation.

进一步,所述的旋转升降部件与精密丝杠通过螺纹连接,其中旋转升降部件与精密丝杠通过螺纹连接,当旋转升降部件转动时,精密丝杠带动密封活塞可进行上下移动;所述的旋转升降部件通过轴承与吸声管道安装连接。Further, the rotating lifting component and the precision lead screw are connected by threads, wherein the rotating lifting component and the precision lead screw are connected by threads, and when the rotating lifting component rotates, the precision lead screw drives the sealing piston to move up and down; the rotating The lifting part is installed and connected with the sound absorption pipe through the bearing.

进一步,所述的燃烧装置壁面上设置有振荡压力测量管道,通过在振荡压力测量管道的顶端设置振荡压力传感器,将振荡压力传感器与燃烧装置壁面隔离。由于传感器的长时间耐温受到限制,因此需要设计振荡压力测量管道将振荡压力传感器与燃烧装置壁面隔离,避免振荡压力传感器受到高温破坏。Further, an oscillating pressure measuring pipe is arranged on the wall surface of the combustion device, and the oscillating pressure sensor is isolated from the wall surface of the combustion device by arranging an oscillating pressure sensor at the top of the oscillating pressure measuring pipe. Since the long-term temperature resistance of the sensor is limited, it is necessary to design an oscillating pressure measurement pipeline to isolate the oscillating pressure sensor from the wall of the combustion device, so as to avoid the oscillating pressure sensor from being damaged by high temperature.

进一步,所述的步进电机以及振荡压力传感器分别与数据采集卡的一端连接,所述的数据采集卡的另一端连接控制系统。Further, the stepping motor and the oscillating pressure sensor are respectively connected to one end of the data acquisition card, and the other end of the data acquisition card is connected to the control system.

本发明的核心思想是将主动控制思想应用到了被动控制机构中,可以使得吸收声波管道具有更加灵活的调整方案。吸声管道的工作长度可在一定范围内根据燃烧不稳定主频进行调整,使其具有在线实时智能调整特性,当燃烧不稳定的振荡主频发生变化时,控制系统可以迅速调整吸声管道的工作长度,保证最佳吸声效果。The core idea of the present invention is to apply the active control idea to the passive control mechanism, so that the acoustic wave absorbing pipe can have a more flexible adjustment scheme. The working length of the sound absorption pipe can be adjusted according to the main frequency of unstable combustion within a certain range, so that it has the characteristics of online real-time intelligent adjustment. When the main frequency of the unstable combustion oscillation changes, the control system can quickly adjust the sound absorption pipe. Working length to ensure optimal sound absorption.

本发明与现有技术相比的有益效果在于:The beneficial effects of the present invention compared with the prior art are:

本发明的抑制器能够很方便地安装在燃烧系统的壁面上,燃烧系统外部留有适当空间即可,此种方式不对燃烧系统产生较大的几何破坏;控制系统在对振荡压力采样和分析后,迅速调节抑制器末端活塞位置,这使得抑制器能够实时追踪燃烧不稳定的振荡频率,解决了传统被动控制中频率单一、频段较窄的问题。控制系统实时保证抑制器与燃烧不稳定的共振频率一致,这使得抑制器具有最佳的吸声效果,燃烧不稳定释放的声波被抑制器吸收后其脉动幅值降低,从而进一步减弱了声波对燃烧的干扰;The suppressor of the present invention can be easily installed on the wall surface of the combustion system, as long as there is an appropriate space outside the combustion system, and this method does not cause great geometric damage to the combustion system; after the control system samples and analyzes the oscillating pressure , quickly adjust the position of the piston at the end of the suppressor, which enables the suppressor to track the oscillation frequency of unstable combustion in real time, and solves the problem of single frequency and narrow frequency band in traditional passive control. The control system ensures that the resonant frequency of the suppressor is consistent with the unstable combustion in real time, which makes the suppressor have the best sound absorption effect. burning disturbance;

本发明提出了末端可调的吸声管道用以对燃烧不稳定进行抑制,控制系统根据采样压力智能调节末端活塞位置,结合了被动控制与主动控制,可以在线实时监测振荡压力,这使得被动控制器的工作频率在一定范围内任意可调。实验结果也证实了该种燃烧不稳定智能抑制器可有效降低振荡压力的脉动幅值,能够应用到燃烧系统中对燃烧不稳定进行抑制,可有效降低燃烧不稳定的振荡强度。The invention proposes a sound absorption pipe with an adjustable end to suppress combustion instability. The control system intelligently adjusts the position of the end piston according to the sampling pressure. Combining passive control and active control, the oscillating pressure can be monitored online in real time, which makes passive control The operating frequency of the device can be adjusted arbitrarily within a certain range. The experimental results also confirm that the combustion instability intelligent suppressor can effectively reduce the pulsation amplitude of the oscillating pressure, and can be applied to the combustion system to suppress the combustion instability, and can effectively reduce the oscillation intensity of the combustion instability.

附图说明Description of drawings

图1为本发明的一种新型燃烧不稳定智能抑制器的结构示意图;1 is a schematic structural diagram of a novel combustion instability intelligent suppressor of the present invention;

图2为本发明的燃烧不稳定智能抑制器局部放大图;Fig. 2 is a partial enlarged view of the combustion instability intelligent suppressor of the present invention;

其中, 1-燃烧装置壁面,2-恒定温度空气进口,3-吸声管道,4-密封活塞,5-轴承,6-齿轮,7-旋转升降部件,8-精密丝杠,9-步进电机,10-控制系统,11-数据采集卡,12-振荡压力传感器,13-振荡压力测量管道。Among them, 1-burning device wall, 2-constant temperature air inlet, 3-sound absorbing pipe, 4-sealing piston, 5-bearing, 6-gear, 7-rotating lifting part, 8-precision screw, 9-stepping Motor, 10-control system, 11-data acquisition card, 12-oscillating pressure sensor, 13-oscillating pressure measuring pipeline.

具体实施方式Detailed ways

为使本发明的目的、技术方案及效果更加清楚,明确,以下列举实例对本发明进一步详细说明。应当指出此处所描述的具体实施仅用以解释本发明,并不用于限定本发明。In order to make the objectives, technical solutions and effects of the present invention clearer and clearer, the following examples are given to further describe the present invention in detail. It should be pointed out that the specific implementations described herein are only used to explain the present invention, but not to limit the present invention.

如图1~2所示,本发明设计的燃烧不稳定智能抑制器主要由吸声管道3、密封活塞4、传动装置、步进电机9、振荡压力传感器12、振荡压力测量管道13和控制系统等组成。通常燃烧被局限在封闭的空间内,比如锅炉中燃烧被限制在炉膛内,而燃气轮机中燃烧则被限制在燃烧室内。因此本发明中的燃烧装置壁面1代表了发生了燃烧不稳定的某燃烧装置的壁面,具体的实际中可以是炉膛壁面或者是燃烧室壁面。本发明设计的吸声管道3起到吸收燃烧不稳定产生的振荡声波的作用,其直径设计在一定范围内即可,比如在10~50mm范围内,也可以根据实际效果进行调整。其原理与四分之一波长管的作用一致,即当管道(一端开口一端封闭)长度与声波波长的四分之一长度相等时,管道可以吸收该声波。As shown in Figures 1-2, the intelligent suppressor of combustion instability designed by the present invention mainly consists of a sound absorption pipe 3, a sealing piston 4, a transmission device, a stepping motor 9, an oscillating pressure sensor 12, an oscillating pressure measuring pipe 13 and a control system etc. composition. Combustion is usually confined to an enclosed space, such as the furnace in a boiler, and the combustion chamber in a gas turbine. Therefore, the wall surface 1 of the combustion device in the present invention represents the wall surface of a combustion device in which combustion instability occurs, and may be the furnace wall surface or the combustion chamber wall surface in practice. The sound absorption pipe 3 designed in the present invention plays the role of absorbing the oscillating sound waves generated by unstable combustion, and its diameter can be designed within a certain range, for example, within the range of 10-50 mm, and can also be adjusted according to the actual effect. Its principle is the same as that of a quarter-wavelength tube, that is, when the length of the pipe (one end is open and one end is closed) is equal to a quarter of the wavelength of the sound wave, the pipe can absorb the sound wave.

本发明的吸声管道3内部活动设置密封活塞4,所述的密封活塞4至燃烧装置壁面1的距离为吸声管道3的工作长度。所述的密封活塞4上设置有精密丝杠8,所述的吸声管道3顶端设置传动装置,所述的精密丝杠8与传动装置连接;在传动装置外连接控制系统10;所述的传动装置包括旋转升降部件7,所述的精密丝杠8与旋转升降部件7相连接,所述的旋转升降部件7在外部设置步进电机9;通过步进电机9的转动,带动旋转升降部件7控制精密丝杠8的移动,进而控制密封活塞4的移动,调整吸声管道3的工作长度。A sealing piston 4 is movably arranged inside the sound absorption pipe 3 of the present invention, and the distance from the sealing piston 4 to the wall surface 1 of the combustion device is the working length of the sound absorption pipe 3 . The sealing piston 4 is provided with a precision lead screw 8, the top of the sound absorption pipe 3 is provided with a transmission device, and the precision lead screw 8 is connected with the transmission device; the control system 10 is connected outside the transmission device; The transmission device includes a rotating lifting member 7, the precision screw 8 is connected with the rotating lifting member 7, and the rotating lifting member 7 is provided with a stepping motor 9 outside; the rotation of the stepping motor 9 drives the rotating lifting member 7. Control the movement of the precision lead screw 8, and then control the movement of the sealing piston 4, and adjust the working length of the sound absorption pipe 3.

本发明将密封活塞4和控制传动系统引入到抑制器中,使得管道的工作长度方便调整,使其具有吸收各种频率声波的能力。为了方便密封活塞4的移动,将精密丝杠8与其相连接,并且通过传动装置控制精密丝杠8的移动。In the present invention, the sealing piston 4 and the control transmission system are introduced into the suppressor, so that the working length of the pipeline can be easily adjusted, so that it has the ability to absorb sound waves of various frequencies. In order to facilitate the movement of the sealing piston 4, a precision lead screw 8 is connected to it, and the movement of the precision lead screw 8 is controlled by a transmission device.

本发明的传动装置中,利用旋转升降部件7与精密丝杠8通过螺纹连接,当旋转升降部件7转动时,精密丝杠8带动密封活塞4可进行上下移动。同时旋转升降部件7通过轴承5与吸声管道3安装,方便了旋转升降部件7的灵活转动。为方便传动控制,在旋转升降部件7的外部安装齿轮6,使得齿轮6与步进电机9通过齿轮配合进行传动,细节结构参见图2所示。当步进电机9转动时,吸声管道3内的密封活塞4进行移动,由此可以通过步进电机9调整吸声管道3的工作长度。In the transmission device of the present invention, the rotary lifting member 7 is connected with the precision screw 8 through threads. When the rotary lifting member 7 rotates, the precision screw 8 drives the sealing piston 4 to move up and down. At the same time, the rotating lifting member 7 is installed with the sound absorption pipe 3 through the bearing 5 , which facilitates the flexible rotation of the rotating lifting member 7 . In order to facilitate transmission control, a gear 6 is installed on the outside of the rotating lifting member 7, so that the gear 6 and the stepping motor 9 are driven by gear cooperation. The detailed structure is shown in FIG. 2 . When the stepping motor 9 rotates, the sealing piston 4 in the sound-absorbing pipe 3 moves, so that the working length of the sound-absorbing pipe 3 can be adjusted by the stepping motor 9 .

本发明中的吸声管道3的工作频率是由其工作长度决定的,并且需要根据吸声管道3内空气介质温度进行计算,而在密封活塞4移动过程中难免将燃烧装置内的高温气体引入到吸声管道内,这将改变吸声管道3的工作频率。因此在吸声管道3靠近的燃烧装置壁面1底端开设有恒定温度空气进口2,将少量恒定温度的空气或者氮气等引入到吸声管道中,一方面其可以对吸声管道进行冷却,防止长时间工作导致吸声管道温度升高而改变了工作频率;另一方面其可以防止由于活塞移动吸入高温燃气。本发明向吸声管道内输入恒定温度的介质,比如空气或者氮气等。任何吸声结构均需要根绝介质温度计算其吸收声波的频率,为了避免吸声管道内气体温度的不均匀性及不确定性,需要向吸声管道内通入恒定温度的介质,以此固定了抑制器吸声管道内的介质温度,使得抑制器的工作频率与步进电机的转动角度呈线性对应关系。The working frequency of the sound-absorbing pipe 3 in the present invention is determined by its working length, and needs to be calculated according to the temperature of the air medium in the sound-absorbing pipe 3, and the high-temperature gas in the combustion device is inevitably introduced during the movement of the sealing piston 4 into the sound absorbing duct, which will change the operating frequency of the sound absorbing duct 3. Therefore, a constant temperature air inlet 2 is provided at the bottom end of the wall surface 1 of the combustion device close to the sound absorption pipe 3, and a small amount of constant temperature air or nitrogen is introduced into the sound absorption pipe. On the one hand, it can cool the sound absorption pipe and prevent Working for a long time causes the temperature of the sound-absorbing pipe to increase and changes the working frequency; on the other hand, it can prevent the inhalation of high-temperature gas due to the movement of the piston. The present invention inputs a medium of constant temperature, such as air or nitrogen, into the sound absorption pipe. Any sound-absorbing structure needs to calculate the frequency of the sound wave it absorbs based on the temperature of the medium. In order to avoid the inhomogeneity and uncertainty of the gas temperature in the sound-absorbing pipe, it is necessary to introduce a medium of constant temperature into the sound-absorbing pipe, which is fixed. The temperature of the medium in the sound-absorbing pipe of the suppressor makes the working frequency of the suppressor have a linear correspondence with the rotation angle of the stepping motor.

本发明中的步进电机9具有精确的转动角度,在传动方面具有广泛的应用。通过控制系统10对步进电机9进行控制,根据燃烧不稳定的振荡主频调整吸声管道3的工作长度,而燃烧不稳定的振荡主频通过对振荡压力的采样分析得到。由于一般传感器的长时间耐温受到限制,因此需要设计振荡压力测量管道13将振荡压力传感器12与燃烧装置壁面1隔离,避免振荡压力传感器12受到高温破坏。振荡压力传感器12将振荡压力信号转换为电信号后经过数据采集卡11通过控制系统10进行数据采集,通过频谱分析手段,比如傅里叶变换对振荡压力信号进行频谱分析,得到燃烧不稳定的振荡主频。本发明的控制系统10通过采样的振荡压力分析得到燃烧不稳定的振荡主频,随后控制系统通过步进电机调整吸声管道到合适的工作长度,保证吸声管道可以实时调整工作长度,从而实现实时对燃烧不稳定进行抑制。The stepping motor 9 in the present invention has a precise rotation angle and is widely used in transmission. The stepper motor 9 is controlled by the control system 10, and the working length of the sound absorption pipe 3 is adjusted according to the main oscillation frequency of unstable combustion, which is obtained by sampling and analysis of the oscillation pressure. Since the long-term temperature resistance of the general sensor is limited, it is necessary to design the oscillating pressure measuring pipe 13 to isolate the oscillating pressure sensor 12 from the wall surface 1 of the combustion device, so as to prevent the oscillating pressure sensor 12 from being damaged by high temperature. The oscillating pressure sensor 12 converts the oscillating pressure signal into an electrical signal, and then collects data through the control system 10 through the data acquisition card 11, and performs spectrum analysis on the oscillating pressure signal by means of spectrum analysis, such as Fourier transform, to obtain unstable combustion oscillations. frequency. The control system 10 of the present invention obtains the oscillation main frequency of unstable combustion by analyzing the sampled oscillation pressure, and then the control system adjusts the sound-absorbing pipe to a suitable working length through the stepping motor, so as to ensure that the sound-absorbing pipe can adjust the working length in real time, so as to realize Combustion instability is suppressed in real time.

以上所述仅是本发明的优选实施方式,应当指出,对于本技术领域的普通技术人员来说,在不脱离本发明原理的前提下,还可以做出若干改进,这些改进也应视为本发明的保护范围。The above are only the preferred embodiments of the present invention. It should be pointed out that for those skilled in the art, some improvements can be made without departing from the principles of the present invention, and these improvements should also be regarded as the present invention. the scope of protection of the invention.

Claims (6)

1. The novel intelligent suppressor for unstable combustion is characterized by comprising a sound absorption pipeline (3) and an oscillation pressure sensor (12) which are respectively arranged on a wall surface (1) of a combustion device, wherein a sealing piston (4) is movably arranged in the sound absorption pipeline (3), and the distance from the sealing piston (4) to the wall surface (1) of the combustion device is the working length of the sound absorption pipeline (3);
a precise lead screw (8) is arranged on the sealing piston (4), a transmission device is arranged at the top end of the sound absorption pipeline (3), and the precise lead screw (8) is connected with the transmission device; the control system (10) is connected outside the transmission device;
the transmission device comprises a rotary lifting component (7), the precision lead screw (8) is connected with the rotary lifting component (7), and a stepping motor (9) is arranged outside the rotary lifting component (7); the rotation of the stepping motor (9) drives the rotary lifting component (7) to control the movement of the precision screw rod (8), so as to control the movement of the sealing piston (4) and adjust the working length of the sound absorption pipeline (3).
2. A new type of intelligent suppressor of combustion instability as defined in claim 1, characterized in that the working length of the sound-absorbing duct (3) is adjusted by the movement of the sealing piston (4); the diameter of the sound absorption pipeline (3) is 10-50 mm; the bottom of the sound absorption pipeline (3) is provided with a constant temperature air inlet (2).
3. A new type of intelligent suppresser for combustion instability as defined in claim 1, characterized in that said rotary elevating member (7) is externally provided with a gear (6), and is connected with a stepping motor (9) by means of the gear (6).
4. The novel intelligent suppressor of combustion instability as set forth in claim 1, characterized in that the rotary elevating member (7) is connected with the precision lead screw (8) by a screw thread; the rotary lifting component (7) is connected with the sound absorption pipeline (3) through a bearing (5).
5. The novel intelligent suppressor for combustion instability as recited in claim 1, characterized in that the combustion device wall (1) is provided with an oscillating pressure measuring pipe (13), and the oscillating pressure sensor (12) is isolated from the combustion device wall (1) by arranging the oscillating pressure sensor (12) at the top end of the oscillating pressure measuring pipe (13).
6. The novel intelligent suppressor of combustion instability as set forth in claim 1, characterized in that the stepping motor (9) and the oscillating pressure sensor (12) are respectively connected to one end of a data acquisition card (11), and the other end of the data acquisition card (11) is connected to the control system (10).
CN202010272310.4A 2020-04-09 2020-04-09 A New Intelligent Suppressor of Combustion Instability Pending CN111486476A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010272310.4A CN111486476A (en) 2020-04-09 2020-04-09 A New Intelligent Suppressor of Combustion Instability

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010272310.4A CN111486476A (en) 2020-04-09 2020-04-09 A New Intelligent Suppressor of Combustion Instability

Publications (1)

Publication Number Publication Date
CN111486476A true CN111486476A (en) 2020-08-04

Family

ID=71812685

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010272310.4A Pending CN111486476A (en) 2020-04-09 2020-04-09 A New Intelligent Suppressor of Combustion Instability

Country Status (1)

Country Link
CN (1) CN111486476A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113482777A (en) * 2021-06-28 2021-10-08 浙江大学 Neck optimized Helmholtz silencer with bias flow and application
CN114526479A (en) * 2022-02-23 2022-05-24 浙江科技学院 Method for inhibiting soot generation through pulse combustion
CN114811650A (en) * 2022-06-01 2022-07-29 清华大学 Electric heating stable combustion device and method and storage medium
CN115751379A (en) * 2022-09-27 2023-03-07 南京航空航天大学 Quarter wave tube for suppressing combustion instability and control method thereof

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20070037818A (en) * 2005-10-04 2007-04-09 두산인프라코어 주식회사 Volumetric Resonator for Vehicle
EP2397760A1 (en) * 2010-06-16 2011-12-21 Alstom Technology Ltd Damper Arrangement and Method for Designing Same
CN102434337A (en) * 2011-09-28 2012-05-02 奇瑞汽车股份有限公司 Resonance silencer with dynamically adjustable silencing frequency
US20120204534A1 (en) * 2011-02-15 2012-08-16 General Electric Company System and method for damping pressure oscillations within a pulse detonation engine
CN104373958A (en) * 2013-08-14 2015-02-25 阿尔斯通技术有限公司 Damper for combustion oscillation damping in a gas turbine
CN108870439A (en) * 2018-07-27 2018-11-23 中国东方电气集团有限公司 A kind of combustion oscillation control structure for combustion apparatus

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20070037818A (en) * 2005-10-04 2007-04-09 두산인프라코어 주식회사 Volumetric Resonator for Vehicle
EP2397760A1 (en) * 2010-06-16 2011-12-21 Alstom Technology Ltd Damper Arrangement and Method for Designing Same
US20120204534A1 (en) * 2011-02-15 2012-08-16 General Electric Company System and method for damping pressure oscillations within a pulse detonation engine
CN102434337A (en) * 2011-09-28 2012-05-02 奇瑞汽车股份有限公司 Resonance silencer with dynamically adjustable silencing frequency
CN104373958A (en) * 2013-08-14 2015-02-25 阿尔斯通技术有限公司 Damper for combustion oscillation damping in a gas turbine
CN108870439A (en) * 2018-07-27 2018-11-23 中国东方电气集团有限公司 A kind of combustion oscillation control structure for combustion apparatus

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113482777A (en) * 2021-06-28 2021-10-08 浙江大学 Neck optimized Helmholtz silencer with bias flow and application
CN113482777B (en) * 2021-06-28 2022-09-06 浙江大学 Neck optimized Helmholtz silencer with bias flow and application
CN114526479A (en) * 2022-02-23 2022-05-24 浙江科技学院 Method for inhibiting soot generation through pulse combustion
CN114811650A (en) * 2022-06-01 2022-07-29 清华大学 Electric heating stable combustion device and method and storage medium
CN115751379A (en) * 2022-09-27 2023-03-07 南京航空航天大学 Quarter wave tube for suppressing combustion instability and control method thereof

Similar Documents

Publication Publication Date Title
CN111486476A (en) A New Intelligent Suppressor of Combustion Instability
Morgans et al. Model-based control of combustion instabilities
US8931589B2 (en) Damper arrangement and method for designing same
RU2508506C2 (en) Method and unit for fluid feed in gas turbine engine combustion chamber
Zhao et al. Tuned passive control of acoustic damping of perforated liners
JPH11502032A (en) Active suppression of aircraft engine inlet noise using small sound sources and distributed error sensors
CN101696955B (en) A test device for sound absorption performance of porous metal materials under variable parameter temperature field
Li et al. Experimental evaluation of anti-sound approach in damping self-sustained thermoacoustics oscillations
CN107917337B (en) Liquid helium vessel thermal acoustic oscillation based on capacity damping air reservoir inhibits device
EP2402568A1 (en) Noise elimination method and muffler
Liu et al. Combustion instability control performance of an improved Helmholtz resonator in the presence of bias flow
CN107542514B (en) Self-adaptive bipolar micro-perforated plate silencer
CN108870439A (en) A kind of combustion oscillation control structure for combustion apparatus
CN107727376B (en) A muffler test prototype with adjustable intubation length
CN104358602A (en) Noise control method of wideband composite sound absorption structure-based steam turbine generator unit
CN206609827U (en) A kind of muffler acoustic damping characteristic test system
US20170074515A1 (en) Apparatus and method for dampening acoustics
JP7305839B2 (en) Double-cavity-coupled Helmholtz silencer and control method
Mao et al. Influence of tip end-plate on noise of small axial fan
Howard et al. An adaptive quarter-wave tube that uses the sliding-Goertzel algorithm for estimation of phase
CN114993684B (en) Annular combustion chamber oscillation suppression test device
Liu et al. Study on Suppression of Combustion Instability using Quarter Wavelength Tube
CN113757720A (en) Combustion oscillation control device, method and combustion chamber
CN207960718U (en) A kind of magnetorheological active sound-absorbing muffler for automobile engine exhaust system
Glendinning et al. Experiments on a compressed air loudspeaker

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
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20200804