CN116006331A - Inlet valve opening and closing control structure of centrifugal booster fuel pump - Google Patents
Inlet valve opening and closing control structure of centrifugal booster fuel pump Download PDFInfo
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Abstract
本发明公开了一种离心式加力燃油泵进口活门开闭控制结构,包括整流罩,活塞组件装于杯形件组件内,将整流罩和杯形件组件围成的腔体分隔成调节腔Ⅵ和控制腔Ⅴ,调节腔Ⅵ、控制腔Ⅴ能够分别通过油路与控制油Ⅱ沟通,调节腔Ⅵ能够与进口燃油Ⅰ沟通;电磁阀根据控制信号控制控制腔Ⅴ与系统回油Ⅲ处于沟通状态或断开状态。该结构控制裕度可调节,工作可靠且适用范围更宽,其技术水平达到国内领先水平。该控制结构将在我国新一代航空发动机上快速推广应用,有效提升我国军队战斗力和国家综合国力。
The invention discloses an opening and closing control structure for an inlet valve of a centrifugal afterburner fuel pump, which comprises a fairing, a piston assembly is installed in a cup assembly, and the cavity surrounded by the fairing and the cup assembly is divided into an adjustment chamber Ⅵ and control chamber Ⅴ, the regulating chamber Ⅵ and the control chamber Ⅴ can communicate with the control oil Ⅱ through the oil circuit respectively, and the regulating chamber Ⅵ can communicate with the imported fuel oil Ⅰ; the solenoid valve controls the control chamber Ⅴ to communicate with the system return oil Ⅲ according to the control signal status or disconnected status. The structural control margin can be adjusted, the work is reliable and the application range is wider, and its technical level has reached the domestic leading level. This control structure will be rapidly popularized and applied on my country's new generation of aero-engines, effectively enhancing the combat effectiveness of our army and the country's comprehensive national strength.
Description
技术领域technical field
本发明属于航空发动机燃油控制技术领域,具体涉及一种离心式加力燃油泵进口活门开闭控制结构。The invention belongs to the technical field of aero-engine fuel control, and in particular relates to an opening and closing control structure of an inlet valve of a centrifugal afterburner fuel pump.
背景技术Background technique
某型航空发动机燃油控制系统加力燃油泵的进口活门开闭装置,其控制结构是通过平衡控制腔油压、进口油压和弹簧力来实现进口活门的打开和关闭。这种控制结构的控制裕度不可调节,打开控制裕度很大,而关闭控制裕度却很小。由于燃油控制系统简化改进,系统回油由低压离心泵前调整为低压离心泵后,关闭控制裕度明显降低甚至基本被消除,可能导致进口活门无法正常关闭。The inlet valve opening and closing device of the afterburner fuel pump of a certain type of aero-engine fuel control system, its control structure is to realize the opening and closing of the inlet valve by balancing the oil pressure of the control chamber, the inlet oil pressure and the spring force. The control margin of this control structure is not adjustable, the opening control margin is large, while the closing control margin is very small. Due to the simplification and improvement of the fuel control system, the oil return of the system is adjusted from before the low-pressure centrifugal pump to after the low-pressure centrifugal pump, the closing control margin is significantly reduced or even basically eliminated, which may cause the inlet valve to fail to close normally.
图1所示为原控制结构的工作原理图,该控制结构主要由进口管接头1、整流罩2、螺母3、活塞组件、弹簧5、杯形件组件、进口活门8、壳体10、电磁阀12、节流嘴Ⅰ13等组成。进口管接头1与壳体10端面贴合并固定,内部形成安装空间;整流罩2固定在进口管接头1与壳体10之间;杯形件组件由杯形件7和活门杆11组成,活门杆11穿过杯形件7较小内孔。活门杆11与杯形件7直径较小内孔配合直径为D1,杯形件直径较大内孔直径为D2,杯形件7固定在壳体10上。活塞组件由活塞骨架4和皮碗6组成,活塞组件装于杯形件7内并由螺母3固定在活门杆11的左端,皮碗6装于活塞骨架右端,保证皮碗与活塞骨架和活塞组件与杯形件7内孔之间保持密封,活塞组件右端与杯形件组件形成控制腔Ⅴ,控制腔Ⅴ通过杯形件上的型孔A1和节流嘴Ⅰ13与控制油Ⅱ沟通。活塞组件左端与整流罩2形成空腔Ⅵ,空腔Ⅵ通过整流罩上的孔A2与进口燃油Ⅰ直接沟通。弹簧5安装于整流罩2与活塞骨架4之间,进口活门8通过螺母9固定在活门杆11右端,壳体右端为叶轮腔Ⅳ。壳体10与进口活门贴合密封处直径为D3。电磁阀12根据控制信号控制节流嘴Ⅰ13与型孔A1之间的油嘴与系统回油Ⅲ处于沟通状态或断开状态。Figure 1 shows the working principle diagram of the original control structure, which is mainly composed of
该控制结构的工作原理如下:空腔Ⅵ始终与进口燃油Ⅰ压力相同,活塞组件左端始终承受着弹簧5的弹力和进口燃油Ⅰ的液压力,进口活门8左端始终承受着进口燃油Ⅰ的液压力。当不需要加力燃油泵供油时,电磁阀12切换到打开状态,将节流嘴Ⅰ13与型孔A1之间的油路与系统回油Ⅲ沟通,控制油Ⅱ经节流嘴Ⅰ13节流后压力与系统回油Ⅲ相近,控制腔通过型孔A1与系统回油Ⅲ沟通,弹簧5对活塞骨架4的弹力、活塞组件和进口活门8左端的进口燃油Ⅰ的液压力克服控制腔Ⅴ中燃油对活塞组件向左的液压力和进口活门右端的进口燃油Ⅰ的液压力,将活塞组件、活门杆11和进口活门8向右移动,使控制腔Ⅴ向系统回油Ⅲ放油,直至进口活门8右端顶靠壳体10,进口活门处于图1所示关闭状态,切断进口燃油Ⅰ通向叶轮腔Ⅳ的通路,加力燃油泵不供油,此时叶轮腔Ⅳ中基本无压力;当需要加力燃油泵供油时,电磁阀12切换到关闭位置,切断节流嘴Ⅰ13和型孔A1之间油路与系统回油Ⅲ的沟通,控制油Ⅱ先后通过节流嘴Ⅰ13和型孔A1进入控制腔Ⅴ,使控制腔Ⅴ中压力升高,活塞组件右端的控制腔Ⅴ的液压力克服弹簧5的弹力、活塞组件左端和进口活门8左端的进口燃油Ⅰ的液压力,使活塞组件、活门杆11和进口活门8向左移动,控制油Ⅱ向控制腔Ⅴ注入燃油,直至进口活门8左端与杯形件7右端顶靠,打开进口燃油Ⅰ通向叶轮腔Ⅳ的通路,加力燃油泵开始供油;The working principle of this control structure is as follows: the pressure of the cavity VI is always the same as that of the imported fuel oil I, the left end of the piston assembly always bears the elastic force of the
分析其工作原理可知,进口活门8的打开和关闭过程都是通过平衡弹簧力与油压对活塞组件和进口活门8的推力来实现的。在进口活门8处于关闭状态需要打开时,弹簧力、活塞组件和进口活门8上向右的液压力合力要小于活塞组件承受的向左的液压力;而在进口活门8处于打开状态需要关闭时,弹簧力、活塞组件和进口活门8上向右的液压力合力要大于活塞组件承受的向左的液压力和进口活门8上向左的液压力。由于在该控制结构中弹簧力明显小于液压力,在进口活门8处于关闭状态需要打开时,控制油Ⅱ的压力明显大于进口燃油Ⅰ压力,也就明显大于打开进口活门所需的控制腔Ⅴ压力,即进口活门的打开控制裕度较大;而当进口活门8处于打开状态需要关闭时,进口燃油Ⅰ只是稍大于系统回油Ⅲ的压力(差值为低压离心泵的增压),则进口活门关闭时控制腔Ⅴ中压力也只比系统回油Ⅲ的压力稍大,即进口活门关闭控制裕度基本只有低压离心泵的增压,关闭控制裕度较小。若系统回油Ⅲ由低压离心泵前改为低压离心泵后,则该控制结构的关闭控制裕度被基本消除,进口活门8打开后将无法正常关闭。Analysis of its working principle shows that the opening and closing process of the
发明内容Contents of the invention
发明目的:为了解决上述问题,本发明提供了一种离心式加力燃油泵进口活门开闭控制结构,使进口活门打开和关闭控制裕度可调节,从而做到两者更均衡,扩大进口活门开闭控制结构的适用范围,提高控制功能可靠性,避免在新工作环境下出现任意一项控制裕度过小而使进口活门开闭控制结构工作异常的情况。Purpose of the invention: In order to solve the above problems, the present invention provides a centrifugal afterburner fuel pump inlet valve opening and closing control structure, so that the opening and closing control margin of the inlet valve can be adjusted, so as to make the two more balanced and expand the inlet valve The scope of application of the opening and closing control structure improves the reliability of the control function, and avoids the situation that the opening and closing control structure of the inlet valve is working abnormally due to the small control margin in the new working environment.
本发明的技术方案:Technical scheme of the present invention:
一种离心式加力燃油泵进口活门开闭控制结构,包括整流罩,活塞组件装于杯形件组件内,将整流罩和杯形件组件围成的腔体分隔成调节腔Ⅵ和控制腔Ⅴ,调节腔Ⅵ、控制腔Ⅴ能够分别通过油路与控制油Ⅱ沟通,调节腔Ⅵ能够与进口燃油Ⅰ沟通;电磁阀根据控制信号控制控制腔Ⅴ与系统回油Ⅲ处于沟通状态或断开状态。A centrifugal afterburner fuel pump inlet valve opening and closing control structure, including a fairing, the piston assembly is installed in the cup assembly, and the cavity surrounded by the fairing and the cup assembly is divided into an adjustment chamber VI and a control chamber Ⅴ, the regulating chamber Ⅵ and the control chamber Ⅴ can communicate with the control oil Ⅱ through the oil circuit respectively, and the regulating chamber Ⅵ can communicate with the imported fuel oil Ⅰ; the solenoid valve controls the control chamber Ⅴ to communicate with the system return oil Ⅲ according to the control signal or to disconnect state.
优选的,杯形件组件由杯形件和活门杆组成,活塞组件由活塞骨架和皮碗组成,活门杆穿过杯形件较小内孔,活塞骨架固定在活门杆上将杯形件和整流罩围成的腔体分隔成调节腔Ⅵ和控制腔Ⅴ,皮碗设置在活塞骨架上使活塞骨架与杯形件之间密封。Preferably, the cup assembly is made up of a cup and a valve rod, the piston assembly is made up of a piston skeleton and a leather cup, the valve rod passes through the smaller inner hole of the cup, and the piston skeleton is fixed on the valve rod to connect the cup and the cup. The cavity surrounded by the fairing is divided into an adjustment cavity VI and a control cavity V, and the leather cup is arranged on the piston frame to seal between the piston frame and the cup.
优选的,还包括进口管接头和壳体,进口管接头与壳体端面贴合并固定,活塞组件、杯形件组件均安装在进口管接头和壳体形成的安装空间内;整流罩固定在进口管接头和壳体之间。Preferably, it also includes an inlet pipe joint and a housing, the inlet pipe joint fits and is fixed on the end face of the housing, the piston assembly and the cup assembly are installed in the installation space formed by the inlet pipe joint and the housing; the fairing is fixed on the inlet between the fitting and the housing.
优选的,整流罩和活塞骨架之间设置弹簧。Preferably, a spring is arranged between the fairing and the piston frame.
优选的,调节腔Ⅵ通过杯形件上的型孔A3、壳体上的油路与控制油Ⅱ沟通,油路上设置有节流嘴Ⅱ。Preferably, the adjustment chamber VI communicates with the control oil II through the hole A3 on the cup and the oil passage on the housing, and the oil passage is provided with a throttle nozzle II.
优选的,控制腔Ⅴ通过杯形件上的型孔A1、壳体上的油路与控制油Ⅱ沟通,油路上设置有节流嘴Ⅰ。Preferably, the control chamber V communicates with the control oil II through the hole A1 on the cup and the oil passage on the housing, and the oil passage is provided with a throttle nozzle I.
优选的,整流罩上设置有节流嘴Ⅲ,调节腔Ⅵ通过节流嘴Ⅲ与进口燃油Ⅰ沟通。Preferably, the fairing is provided with a throttle nozzle III, and the regulating chamber VI communicates with the imported fuel oil I through the throttle nozzle III.
优选的,活门杆远离调节腔Ⅵ一端固定有进口活门,进口活门与壳体贴合。Preferably, an inlet valve is fixed at the end of the valve rod away from the adjustment chamber VI, and the inlet valve is attached to the housing.
本发明主要优点是:该结构控制裕度可调节,工作可靠且适用范围更宽,其技术水平达到国内领先水平。该控制结构将在我国新一代航空发动机上快速推广应用,有效提升我国军队战斗力和国家综合国力。The main advantages of the invention are: the control margin of the structure can be adjusted, the work is reliable and the application range is wider, and its technical level reaches the domestic leading level. This control structure will be rapidly popularized and applied on my country's new generation of aero-engines, effectively enhancing the combat effectiveness of our army and the country's comprehensive national strength.
附图说明Description of drawings
图1是现有的某型航空发动机燃油控制系统加力燃油泵的进口活门开闭控制结构示意图。Figure 1 is a schematic diagram of the opening and closing control structure of the inlet valve of the afterburner fuel pump in the existing fuel control system of a certain type of aeroengine.
图2是本发明的一种离心式加力燃油泵进口活门开闭控制结构的示意图。Fig. 2 is a schematic diagram of an opening and closing control structure of an inlet valve of a centrifugal afterburner fuel pump according to the present invention.
图3是本发明的进口活门开闭控制结构仿真时控制油Ⅱ的压力随时间的变化曲线。Fig. 3 is a time-varying curve of the pressure of the control oil II during the simulation of the opening and closing control structure of the inlet valve of the present invention.
图4是本发明的进口活门开闭控制结构仿真时电磁阀的切换情况,0表示关闭,1表示打开。Fig. 4 is the switching situation of the electromagnetic valve during the simulation of the opening and closing control structure of the inlet valve of the present invention, 0 means closed, and 1 means open.
图5是原进口活门控制结构仿真时进口活门的位移响应曲线,0表示完全关闭状态,-8mm表示完全打开状态;Fig. 5 is the displacement response curve of the inlet valve during the simulation of the control structure of the original inlet valve, 0 means fully closed state, -8mm means fully open state;
图6是本发明的进口活门开闭控制结构仿真时进口活门的位移响应曲线,0表示完全关闭状态,-8mm表示完全打开状态。Fig. 6 is the displacement response curve of the inlet valve during the simulation of the opening and closing control structure of the inlet valve of the present invention, where 0 indicates a fully closed state, and -8mm indicates a fully opened state.
图中:1—进口管接头,2—整流罩,3—螺母,4—活塞骨架;5—弹簧,6—皮碗,7—杯形件,8—进口活门,9—螺母,10—壳体,11—活门杆,12—电磁阀,13—节流嘴Ⅰ,14—节流嘴Ⅱ,15—节流嘴Ⅲ,D1—活门杆直径,D2—活塞组件直径,D3—进口活门与壳体贴合密封处直径,L—进口活门行程,A1—孔Ⅰ,A2—孔Ⅱ,A3—孔Ⅲ,Ⅰ—进口燃油,Ⅱ—控制油,Ⅲ—系统回油;Ⅳ—叶轮腔;Ⅴ—控制腔,Ⅵ—调节腔。In the figure: 1—inlet pipe joint, 2—cowl, 3—nut, 4—piston skeleton; 5—spring, 6—skin cup, 7—cup, 8—inlet valve, 9—nut, 10—shell Body, 11—valve rod, 12—solenoid valve, 13—throttle nozzle I, 14—throttle nozzle II, 15—throttle nozzle III, D1—diameter of valve rod, D2—diameter of piston assembly, D3—inlet valve and The diameter of the sealing part of the shell, L—inlet valve stroke, A1—hole I, A2—hole II, A3—hole III, I—inlet fuel oil, II—control oil, III—system oil return; IV—impeller cavity; V - control cavity, VI - regulation cavity.
具体实施方式Detailed ways
下面以某型离心式加力燃油泵进口活门开闭控制结构为例,对本发明作详细说明:Taking the opening and closing control structure of the inlet valve of a certain type of centrifugal afterburning fuel pump as an example, the present invention will be described in detail below:
图2所示为改进后的控制结构的工作原理图,该控制结构主要由进口管接头1、整流罩2、螺母3、活塞组件、弹簧5、杯形件组件、进口活门8、壳体10、电磁阀12、节流嘴Ⅰ13、节流嘴Ⅱ14、节流嘴Ⅲ15等组成。Figure 2 shows the working principle diagram of the improved control structure, the control structure is mainly composed of
进口管接头1与壳体10端面贴合并固定,内部形成安装空间;整流罩2固定在进口管接头1与壳体10之间,整流罩2左端装有节流嘴Ⅲ15;杯形件组件由杯形件7和活门杆11组成,活门杆11穿过杯形件7较小内孔。活门杆11与杯形件7直径较小内孔配合直径为D1,杯形件直径较大内孔直径为D2,杯形件7固定在壳体10上。活塞组件由活塞骨架4和皮碗6组成,活塞组件装于杯形件7内并由螺母3固定在活门杆11的左端,皮碗6套于活塞骨架右端,保证活塞骨架4与皮碗6和皮碗6与杯形件7之间保持密封,活塞组件右端与杯形件组件形成控制腔Ⅴ,控制腔Ⅴ通过杯形件7上的型孔A1和节流嘴Ⅰ13与控制油Ⅱ沟通。活塞组件左端与整流罩2形成调节腔Ⅵ,调节腔Ⅵ通过整流罩2上的节流嘴Ⅲ15与进口燃油Ⅰ沟通,通过杯形件7上的型孔A3和节流嘴Ⅱ14与控制油Ⅱ沟通。弹簧5安装于整流罩2与活塞骨架4之间,进口活门8通过螺母9固定在活门杆11右端,壳体10右端为叶轮腔Ⅳ。壳体10与进口活门8贴合密封处直径为D3。电磁阀12根据控制信号控制节流嘴Ⅰ13与型孔A1之间的油路与系统回油Ⅲ处于沟通状态或断开状态。The
本发明的控制结构的工作原理如下:控制油Ⅱ通过节流嘴Ⅱ14和杯形件7上的型孔A3与调节腔Ⅵ沟通,调节腔Ⅵ通过节流嘴Ⅲ15与进口燃油Ⅰ沟通。通过调节节流嘴Ⅱ14与节流嘴Ⅲ15的通径来调整调节腔Ⅵ中的压力,得到略高于进口燃油Ⅰ压力的合适压力;活塞组件左端始终承受着弹簧5的弹力和调节腔Ⅵ的液压力,进口活门8左端始终承受着进口燃油Ⅰ的液压力。当不需要加力燃油泵供油时,电磁阀12切换到打开状态,将节流嘴Ⅰ13与型孔A1之间的油路与系统回油Ⅲ沟通,控制油Ⅱ经节流嘴Ⅰ13节流后压力与系统回油Ⅲ相近,控制腔Ⅴ通过型孔A1与系统回油Ⅲ沟通,弹簧5对活塞骨架4的弹力、活塞组件和进口活门8左端的进口燃油Ⅰ的液压力克服控制腔Ⅴ中燃油对活塞组件向左的液压力和进口活门8右端的进口燃油Ⅰ的液压力,将活塞组件、活门杆11和进口活门8向右移动,使控制腔Ⅴ向系统回油Ⅲ放油,直至进口活门8右端顶靠壳体10,进口活门8处于图2所示关闭状态,切断进口燃油Ⅰ通向叶轮腔Ⅳ的通路,加力燃油泵不供油,此时叶轮腔Ⅳ中基本无压力;当需要加力燃油泵供油时,电磁阀12切换到关闭位置,切断节流嘴Ⅰ13和型孔A1之间的油路与系统回油Ⅲ的沟通,控制油Ⅱ先后通过节流嘴13和型孔A1进入控制腔Ⅴ,使控制腔Ⅴ中压力升高,活塞组件右端的控制腔Ⅴ的液压力,克服弹簧5的弹力、活塞组件左端调节腔Ⅵ的液压力和进口活门8左端的进口燃油Ⅰ的液压力,使活塞组件、活门杆11和进口活门8向左移动,直至进口活门8左端与杯形件7右端顶靠,打开进口燃油Ⅰ通向叶轮腔Ⅳ的通路,加力燃油泵开始供油;The working principle of the control structure of the present invention is as follows: the control oil II communicates with the regulating chamber VI through the throttle nozzle II14 and the hole A3 on the
分析改进后的进口活门开闭控制结构的工作原理可知,进口活门8的打开和关闭过程主要依靠油压来控制,将原来直接与进口燃油Ⅰ沟通的空腔Ⅵ作为调节腔,通过节流嘴Ⅱ14和节流嘴Ⅲ15调节其中压力,使其中压力大于进口燃油Ⅰ压力,从而加大了活塞组件左端承受的液压力,在进口活门打开时由于活塞组件左端的反向液压力增大,将会导致使进口活门8打开的控制腔Ⅴ压力增大,该压力与控制油Ⅱ之间的压差就下降,从而会降低进口活门打开控制裕度;在进口活门关闭时,由于活塞组件左端的使进口活门8关闭的液压力增大,进口活门8关闭时控制腔Ⅴ中压力同样增大,该压力与系统回油Ⅲ的压力差值就增大了,从而提高了进口活门关闭控制裕度。该控制结构的打开和关闭控制裕度可调节,消除了原控制结构中打开控制裕度过大而关闭控制裕度过小的问题,从而避免了系统回油Ⅲ压力提升后带来的进口活门8无法正常关闭的问题,提高了控制可靠性和适用范围。The analysis of the working principle of the improved inlet valve opening and closing control structure shows that the opening and closing process of the
对于原进口活门开闭控制结构(图1所示),进口燃油压力PⅠ=1.35MPa,控制油压力PⅡ=14MPa,燃油控制系统简化改进后的系统回油压力PⅢ=1.35MPa,空腔Ⅵ中压力与进口燃油压力相同,D1=18mm,D2=46mm,D3=46mm,弹簧刚度K=3.5N/mm,进口活门关闭时弹簧预压缩量△H=44.3mm,进口活门行程L=8mm。进口活门的打开控制裕度:For the original inlet valve opening and closing control structure (shown in Figure 1), the inlet fuel pressure P Ⅰ =1.35MPa, the control oil pressure P Ⅱ =14MPa, the system oil return pressure after the simplified and improved fuel control system P Ⅲ =1.35MPa, the air pressure The pressure in cavity Ⅵ is the same as the inlet fuel pressure, D1=18mm, D2=46mm, D3=46mm, spring stiffness K=3.5N/mm, spring precompression when the inlet valve is closed △H=44.3mm, inlet valve stroke L= 8mm. The opening control margin of the inlet valve:
进口活门的关闭控制裕度:Closing control margin of inlet valve:
可知,进口活门的打开控制裕度富余过大,而关闭控制裕度却很小,系统燃油压力波动和活塞组件的摩擦力足以使进口活门打开后就无法正常关闭。It can be seen that the opening control margin of the inlet valve is too large, but the closing control margin is very small, the system fuel pressure fluctuation and the friction of the piston assembly are enough to make the inlet valve unable to close normally after opening.
在本发明的控制结构中将原空腔Ⅵ作为调整腔,通过选用不同通径的节流嘴Ⅱ14(其通径用d1表示)和节流嘴Ⅲ15(其通径用d2表示)控制该腔的压力,以d1=1mm,d2=1.5mm为例,调节腔中的压力In the control structure of the present invention, the original cavity VI is used as the adjustment cavity, and the cavity is controlled by selecting throttle nozzles II14 (the diameter of which is represented by d1) and throttle nozzles III15 (the diameter of which is represented by d2) of different diameters. The pressure, taking d1=1mm, d2=1.5mm as an example, adjust the pressure in the chamber
则进口活门8的打开控制裕度:Then the opening control margin of the inlet valve 8:
进口活门的关闭控制裕度:Closing control margin of inlet valve:
进口活门的打开控制裕度下降,而关闭控制裕度得到了明显提高,控制裕度更均衡,解决了新环境下进口活门无法正常关闭的问题,提高了进口活门开闭控制结构的工作可靠性和适用范围。The opening control margin of the inlet valve has decreased, while the closing control margin has been significantly improved, and the control margin is more balanced, which solves the problem that the inlet valve cannot be closed normally under the new environment, and improves the working reliability of the inlet valve opening and closing control structure and scope of application.
通过AMEsim软件对改进前、后的进口活门开闭控制结构按提高后的系统回油Ⅲ压力进行系统建模和仿真验证。初始状态进口活门处于关闭位置,控制油Ⅱ按图3所示在20s内从0MPa线性升高到14MPa,然后保持14MPa;电磁阀12延迟25秒打开,随后一个关闭和打开的周期为20秒。原进口活门开闭控制结构的进口活门8位移曲线见图5,进口活门8打开后就无法按电磁阀12的切换正常关闭。新的进口活门开闭控制结构选用通径1mm的节流嘴Ⅱ14和通径1.5mm的节流嘴Ⅲ15时,进口活门8的位移曲线见图6,进口活门8随着电磁阀12的切换而正常打开和关闭,没有出现无法正常关闭的情况;打开控制裕度为10.89MPa,关闭控制裕度为1.6MPa。仿真结果验证了原进口活门开闭控制结构在新的燃油控制系统中工作存在无法正常关闭的问题,而新的进口活门开闭控制结构在新的燃油控制系统中能正常打开和关闭,控制功能可靠。Through the AMEsim software, the system modeling and simulation verification of the inlet valve opening and closing control structure before and after the improvement are carried out according to the improved oil return III pressure of the system. In the initial state, the inlet valve is in the closed position, and the control oil II increases linearly from 0MPa to 14MPa within 20s as shown in Figure 3, and then maintains 14MPa; the
上述实施例只为说明本发明的技术构思及特点,其目的是让熟悉该技术领域的技术人员能够了解本发明的内容并据以实施,并不能以此来限制本发明的保护范围,凡根据本发明精神本质所作出的等同变换或修饰,都应涵盖本发明的保护范围内。本发明未详细描述的技术、形状、构造部分均为公知技术。The above-described embodiments are only to illustrate the technical concept and characteristics of the present invention, and its purpose is to allow those skilled in the art to understand the content of the present invention and implement it accordingly, and cannot limit the protection scope of the present invention with this. The equivalent changes or modifications made by the spirit and essence of the present invention shall fall within the protection scope of the present invention. The technologies, shapes and construction parts not described in detail in the present invention are all known technologies.
Claims (8)
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|---|---|---|---|---|
| FR1292181A (en) * | 1961-06-15 | 1962-04-27 | Dowty Fuel Syst Ltd | Advanced centrifugal pump and its application to the fuel supply of the afterburner burners of a gas turbine |
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| US7878003B1 (en) * | 1985-07-12 | 2011-02-01 | Goodrich Control Systems Limited | Fuel control system for gas turbine engine reheat apparatus |
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| RU2671082C2 (en) * | 2000-02-03 | 2018-10-29 | Российская Федерация в лице Министерства Обороны Российской Федерации | Centrifugal pump |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1292181A (en) * | 1961-06-15 | 1962-04-27 | Dowty Fuel Syst Ltd | Advanced centrifugal pump and its application to the fuel supply of the afterburner burners of a gas turbine |
| US3486458A (en) * | 1967-01-06 | 1969-12-30 | Dowty Fuel Syst Ltd | Centrifugal pumping apparatus |
| US7878003B1 (en) * | 1985-07-12 | 2011-02-01 | Goodrich Control Systems Limited | Fuel control system for gas turbine engine reheat apparatus |
| RU2671082C2 (en) * | 2000-02-03 | 2018-10-29 | Российская Федерация в лице Министерства Обороны Российской Федерации | Centrifugal pump |
| CN103206383A (en) * | 2013-04-11 | 2013-07-17 | 南京航空航天大学 | Vapor-core pump with impeller central pressure supplement regulator |
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