CN112249361B - Cooling ventilation simulation device and control method for high-altitude airborne equipment testing - Google Patents
Cooling ventilation simulation device and control method for high-altitude airborne equipment testing Download PDFInfo
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Abstract
本申请提供一种用于高空机载设备测试的冷却通风模拟装置及控制方法,包括依次连接的:气源、过滤器、减压阀、流量控制单元、制冷机、加热器及背压阀,背压阀输出端与低压舱连接,高空机载设备在低压舱内测试;气源用于输出高压空气,过滤器用于滤除空气中的颗粒和油性杂质,减压阀用于对高压空气减压,流量控制单元用于对减压后的空气进行设定流量控制,制冷机及加热器用于调节空气的温度,背压阀用于稳定冷却通风系统与低压舱之间的压差。本申请的有益效果是:通过本申请的通风装置为低压舱提供低压冷却通风环境,使得测试环境更加接近真实工况;而且本申请的通风装置还可实现通风的流量、压力及温度可控,保证测试环境的稳定性。
The present application provides a cooling and ventilation simulation device and a control method for high-altitude airborne equipment testing, comprising: an air source, a filter, a pressure reducing valve, a flow control unit, a refrigerator, a heater and a back pressure valve connected in sequence, The output end of the back pressure valve is connected to the low-pressure cabin, and the high-altitude airborne equipment is tested in the low-pressure cabin; the air source is used to output high-pressure air, the filter is used to filter out particles and oily impurities in the air, and the pressure reducing valve is used to reduce the high-pressure air. The flow control unit is used to control the set flow of the decompressed air, the refrigerator and the heater are used to adjust the temperature of the air, and the back pressure valve is used to stabilize the pressure difference between the cooling ventilation system and the low pressure chamber. The beneficial effects of the present application are: the low-pressure cooling and ventilation environment is provided for the low-pressure chamber through the ventilation device of the present application, so that the test environment is closer to the real working condition; and the ventilation device of the present application can also realize the controllable flow, pressure and temperature of the ventilation, Ensure the stability of the test environment.
Description
技术领域technical field
本公开涉及低气压环境模拟技术领域,具体涉及一种用于高空机载设备测试的冷却通风模拟装置及控制方法。The present disclosure relates to the technical field of low-pressure environment simulation, in particular to a cooling ventilation simulation device and a control method for high-altitude airborne equipment testing.
背景技术Background technique
在地面进行高空机载设备测试,需要模拟高空低压低温环境,测试其在高空环境下的工作性能。To test high-altitude airborne equipment on the ground, it is necessary to simulate the high-altitude, low-pressure and low-temperature environment to test its working performance in the high-altitude environment.
这种高空低压低温环境通常使用低气压环境模拟装备来模拟,具体的模拟方法为:低气压环境模拟装备具有一个低压舱,通过控制内部压力和温度来模拟不同海拔高度的高空环境。This high-altitude, low-pressure and low-temperature environment is usually simulated by low-pressure environment simulation equipment. The specific simulation method is as follows: the low-pressure environment simulation equipment has a low-pressure chamber, and the internal pressure and temperature are controlled to simulate high-altitude environments at different altitudes.
机载设备在工作工程中常常伴随着大量发热,其散热装置需要飞机的环控系统提供冷却通风,因此其地面测试也应提供冷却通风条件。现有的低气压环境模拟装备难以实现冷却通风环境,无法满足模拟需求。Airborne equipment is often accompanied by a lot of heat during work engineering, and its cooling device needs the aircraft's environmental control system to provide cooling ventilation, so its ground test should also provide cooling ventilation conditions. The existing low-pressure environment simulation equipment is difficult to achieve a cooling and ventilation environment and cannot meet the simulation needs.
现有的冷却通风装置只能在常压下使用,没有针对低气压环境进行设计,因此其在低压环境下使用会带来系统工况不稳定,温度和流量无法控制等问题,严重影响测试效果。Existing cooling and ventilation devices can only be used under normal pressure, and are not designed for low-pressure environments. Therefore, their use in low-pressure environments will lead to unstable system conditions, uncontrollable temperature and flow, and other problems, which seriously affect the test results. .
发明内容SUMMARY OF THE INVENTION
本申请的目的是针对以上问题,提供一种用于高空机载设备测试的冷却通风模拟装置及控制方法。The purpose of this application is to address the above problems, to provide a cooling ventilation simulation device and a control method for high-altitude airborne equipment testing.
第一方面,本申请提供一种用于高空机载设备测试的冷却通风模拟装置,包括依次连接的:气源、过滤器、减压阀、流量控制单元、制冷机、加热器及背压阀,所述背压阀的输出端与所述低压舱连通,所述高空机载设备设置在低压舱内进行测试;所述气源用于输出高压空气,过滤器用于滤除高压空气中的颗粒和油性杂质,减压阀用于对过滤后的高压空气减压,流量控制单元用于对减压后的空气进行设定流量控制,制冷机及加热器用于调节空气的温度,背压阀用于稳定冷却通风系统与低压舱之间的压差。In a first aspect, the present application provides a cooling and ventilation simulation device for high-altitude airborne equipment testing, comprising: an air source, a filter, a pressure reducing valve, a flow control unit, a refrigerator, a heater and a back pressure valve connected in sequence , the output end of the back pressure valve is communicated with the low-pressure cabin, and the high-altitude airborne equipment is set in the low-pressure cabin for testing; the air source is used to output high-pressure air, and the filter is used to filter out particles in the high-pressure air and oily impurities, the pressure reducing valve is used to decompress the filtered high-pressure air, the flow control unit is used to set the flow control of the decompressed air, the refrigerator and the heater are used to adjust the temperature of the air, and the back pressure valve is used for To stabilize the pressure difference between the cooling ventilation system and the low pressure chamber.
根据本申请实施例提供的技术方案,所述流量控制单元包括比例电磁阀及流量计,所述比例电磁阀设置在靠近减压阀的一侧,流量计用于测量冷却通风系统流量,比例电磁阀根据流量计测量的数据调节阀体开度。According to the technical solutions provided in the embodiments of the present application, the flow control unit includes a proportional solenoid valve and a flowmeter, the proportional solenoid valve is arranged on a side close to the pressure reducing valve, the flowmeter is used to measure the flow of the cooling and ventilation system, and the proportional solenoid The valve adjusts the valve body opening according to the data measured by the flow meter.
根据本申请实施例提供的技术方案,所述制冷机和加热器分别单独控制,实现冷却通风系统的温度调节。According to the technical solutions provided in the embodiments of the present application, the refrigerator and the heater are separately controlled to realize the temperature adjustment of the cooling and ventilation system.
第二方面,本申请提供一种用于高空机载设备测试的冷却通风模拟装置控制方法,包括以下步骤:In a second aspect, the present application provides a cooling ventilation simulation device control method for high-altitude airborne equipment testing, comprising the following steps:
设置减压阀输出端第一设定压力值及背压阀输入端第二设定压力值;Set the first set pressure value at the output end of the pressure reducing valve and the second set pressure value at the input end of the back pressure valve;
气源输出高压空气;The air source outputs high pressure air;
过滤器对高压空气进行颗粒及油性杂质的过滤;The filter filters particles and oily impurities from the high-pressure air;
减压阀对过滤后的空气进行减压使得减压阀输出第一设定压力值的空气;The pressure reducing valve decompresses the filtered air so that the pressure reducing valve outputs the air of the first set pressure value;
背压阀对传输至其输入端的空气的压力进行调节使得传输至背压阀输入端空气的压力调节至第二设定压力值;The back pressure valve adjusts the pressure of the air transmitted to its input end so that the pressure of the air transmitted to the input end of the back pressure valve is adjusted to a second set pressure value;
流量控制单元对减压阀及背压阀之间具有第一设定压力值与第二设定压力值恒定压差值的空气进行空气流量调节,使得传输至背压阀输入端的空气具有设定流量;The flow control unit adjusts the air flow of the air with a constant pressure difference between the first set pressure value and the second set pressure value between the pressure reducing valve and the back pressure valve, so that the air transmitted to the input end of the back pressure valve has the set value flow;
制冷机和加热器对减压阀及背压阀之间的空气进行温度调节,使得传输至背压阀输入端的空气具有设定温度;The refrigerator and the heater adjust the temperature of the air between the pressure reducing valve and the back pressure valve, so that the air transmitted to the input end of the back pressure valve has a set temperature;
设定流量、设定温度的空气通过背压阀,输出至低压舱内,实现对低压舱的送风。The air with the set flow and temperature is output to the low pressure chamber through the back pressure valve to realize the air supply to the low pressure chamber.
根据本申请实施例提供的技术方案,所述流量控制单元对减压阀及背压阀之间具有第一设定压力值与第二设定压力值恒定压差值的空气进行空气流量调节,具体包括:According to the technical solution provided by the embodiment of the present application, the flow control unit performs air flow adjustment on the air having a constant pressure difference between the first set pressure value and the second set pressure value between the pressure reducing valve and the back pressure valve, Specifically include:
流量计测量系统流量,并将测量的流量值发送至比例电磁阀;The flow meter measures the system flow and sends the measured flow value to the proportional solenoid valve;
比例电磁阀根据测量的流量值与系统设定流量的数值进行比较后,调整比例电磁阀的开度,使得测量的流量值与设定流量的数值一致。After the proportional solenoid valve compares the measured flow value with the set flow value of the system, adjust the opening of the proportional solenoid valve so that the measured flow value is consistent with the set flow value.
本发明具有以下有益效果:The present invention has the following beneficial effects:
1、满足高空机载设备地面测试时,低气压环境模拟系统中实现冷却通风环境,使得模拟测试环境更加接近实际使用的环境;1. When meeting the ground test of high-altitude airborne equipment, the cooling and ventilation environment is realized in the low-pressure environment simulation system, so that the simulated test environment is closer to the actual use environment;
2、在低压舱不同气压环境中均能保证冷却通风系统的流量、压力及温度的可控性。2. The controllability of the flow, pressure and temperature of the cooling ventilation system can be ensured in different air pressure environments of the low pressure chamber.
附图说明Description of drawings
图1为本申请第一种实施例的结构原理示意图;1 is a schematic diagram of the structural principle of the first embodiment of the application;
图2为本申请第二种实施例的流程图;Fig. 2 is the flow chart of the second embodiment of the application;
图中所述文字标注表示为:1、气源;2、过滤器;3、减压阀;4、流量控制单元;4.1、比例电磁阀;4.2、流量计;5、制冷机;6、加热器;7、背压阀;8、低压舱。The text in the figure is marked as: 1. Air source; 2. Filter; 3. Pressure reducing valve; 4. Flow control unit; 4.1. Proportional solenoid valve; 4.2, Flow meter; 5. Refrigerator; 7. Back pressure valve; 8. Low pressure chamber.
具体实施方式Detailed ways
为了使本领域技术人员更好地理解本发明的技术方案,下面结合附图对本申请进行详细描述,本部分的描述仅是示范性和解释性,不应对本申请的保护范围有任何的限制作用。In order for those skilled in the art to better understand the technical solutions of the present invention, the present application will be described in detail below with reference to the accompanying drawings. The description in this part is only exemplary and explanatory, and should not have any limiting effect on the protection scope of the present application. .
如图1所示为本申请的第一种实施例的示意图,本实施例中,高空机载设备在低压舱8内进行测试,本申请的通风装置包括依次连接的:气源1、过滤器2、减压阀3、流量控制单元4、制冷机5、加热器6及背压阀7,所述背压阀7的输出端与所述低压舱8连接。FIG. 1 is a schematic diagram of the first embodiment of the application. In this embodiment, the high-altitude airborne equipment is tested in the
所述气源1用于输出高压空气,过滤器2用于滤除高压空气中的颗粒和油性杂质,减压阀3用于对过滤后的高压空气减压,流量控制单元4用于对减压后的空气进行设定流量控制,制冷机5及加热器6用于调节空气的温度,背压阀7用于稳定冷却通风系统与低压舱8之间的压差也即通风系统的压力不受低压舱8内压力变化的影响,从而保证在低气压测试过程中也能实现送风温度和流量保持恒定。The
在一优选实施例中,所述流量控制单元4包括比例电磁阀4.1及流量计4.2,所述比例电磁阀4.1设置在靠近减压阀3的一侧,流量计4.2用于测量冷却通风系统流量,比例电磁阀4.1根据流量计4.2测量的数据调节阀体开度。In a preferred embodiment, the
在一优选实施方式中,控制所述制冷机5和加热器6分别单独控制,实现冷却通风系统的温度调节。In a preferred embodiment, the
如图2所示,为本申请第二种实施例的流程图,本实施例是对第一种实施例的装置进行控制的方法,包括以下步骤:As shown in FIG. 2 , it is a flowchart of the second embodiment of the present application. This embodiment is a method for controlling the device of the first embodiment, including the following steps:
S1、设置减压阀输出端第一设定压力值及背压阀输入端第二设定压力值;S1, set the first set pressure value of the output end of the pressure reducing valve and the second set pressure value of the input end of the back pressure valve;
S2、气源输出高压空气;S2, the air source outputs high pressure air;
S3、过滤器对高压空气进行颗粒及油性杂质的过滤;S3. The filter filters the high-pressure air for particles and oily impurities;
S4、减压阀对过滤后的空气进行减压使得减压阀输出第一设定压力值的空气;S4, the pressure reducing valve decompresses the filtered air so that the pressure reducing valve outputs the air of the first set pressure value;
S5、背压阀对传输至其输入端的空气的压力进行调节使得传输至背压阀输入端空气的压力调节至第二设定压力值;S5, the back pressure valve adjusts the pressure of the air transmitted to its input end so that the pressure of the air transmitted to the input end of the back pressure valve is adjusted to the second set pressure value;
S6、流量控制单元对减压阀及背压阀之间具有第一设定压力值与第二设定压力值恒定压差值的空气进行空气流量调节,使得传输至背压阀输入端的空气具有设定流量;S6. The flow control unit adjusts the air flow of the air with a constant pressure difference between the first set pressure value and the second set pressure value between the pressure reducing valve and the back pressure valve, so that the air transmitted to the input end of the back pressure valve has set flow;
S7、制冷机和加热器对减压阀及背压阀之间的空气进行温度调节,使得传输至背压阀输入端的空气具有设定温度;S7, the refrigerator and the heater adjust the temperature of the air between the pressure reducing valve and the back pressure valve, so that the air transmitted to the input end of the back pressure valve has a set temperature;
S8、设定流量、设定温度的空气通过背压阀,输出至低压舱内,实现对低压舱的送风。S8. The air with the set flow and set temperature is output to the low pressure chamber through the back pressure valve, so as to realize the air supply to the low pressure chamber.
在一优选实施方式中,S6步骤,具体包括:In a preferred embodiment, step S6 specifically includes:
S61、流量计测量系统流量,并将测量的流量值发送至比例电磁阀;S61, the flow meter measures the system flow, and sends the measured flow value to the proportional solenoid valve;
S62、比例电磁阀根据测量的流量值与系统设定流量的数值进行比较后,调整比例电磁阀的开度,使得测量的流量值与设定流量的数值一致。S62, after the proportional solenoid valve compares the measured flow value with the system set flow value, adjust the opening of the proportional solenoid valve so that the measured flow value is consistent with the set flow value.
本文中应用了具体个例对本申请的原理及实施方式进行了阐述,以上实例的说明只是用于帮助理解本申请的方法及其核心思想。以上所述仅是本申请的优选实施方式,应当指出,由于文字表达的有限性,而客观上存在无限的具体结构,对于本技术领域的普通技术人员来说,在不脱离本申请原理的前提下,还可以做出若干改进、润饰或变化,也可以将上述技术特征以适当的方式进行组合;这些改进润饰、变化或组合,或未经改进将申请的构思和技术方案直接应用于其它场合的,均应视为本申请的保护范围。Specific examples are used herein to illustrate the principles and implementations of the present application, and the descriptions of the above examples are only used to help understand the methods and core ideas of the present application. The above are only the preferred embodiments of the present application. It should be pointed out that, due to the limited expression of words, there are objectively unlimited specific structures. For those of ordinary skill in the art, without departing from the principles of the present application However, several improvements, modifications or changes can also be made, and the above-mentioned technical features can also be combined in an appropriate manner; these improvements, modifications, or combinations, or the ideas and technical solutions of the application are directly applied to other occasions without improvement. shall be regarded as the protection scope of this application.
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CN209290725U (en) * | 2018-11-30 | 2019-08-23 | 中国航空工业集团公司沈阳飞机设计研究所 | Aircraft dynamic vacuum simulator |
CN110136772A (en) * | 2019-04-08 | 2019-08-16 | 北京强度环境研究所 | A kind of active cooling device inside large structure for low pressure thermal test |
CN110217412A (en) * | 2019-07-04 | 2019-09-10 | 北京瑞尔腾普科技有限公司 | A kind of device for freezing experiment and method |
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