CN106762865A - Retractable oil receiving device test bench - Google Patents

Retractable oil receiving device test bench Download PDF

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Publication number
CN106762865A
CN106762865A CN201710089346.7A CN201710089346A CN106762865A CN 106762865 A CN106762865 A CN 106762865A CN 201710089346 A CN201710089346 A CN 201710089346A CN 106762865 A CN106762865 A CN 106762865A
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CN
China
Prior art keywords
oil
valve
hydraulic system
receiving device
oil return
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Pending
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CN201710089346.7A
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Chinese (zh)
Inventor
王占勇
刘振岗
邹刚
唐元恒
张玎
孔光明
唐有才
郭刚
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Naval Aeronautical University
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Naval Aeronautical University
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Priority to CN201710089346.7A priority Critical patent/CN106762865A/en
Publication of CN106762865A publication Critical patent/CN106762865A/en
Pending legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B1/00Installations or systems with accumulators; Supply reservoir or sump assemblies
    • F15B1/02Installations or systems with accumulators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B11/00Servomotor systems without provision for follow-up action; Circuits therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B13/00Details of servomotor systems ; Valves for servomotor systems
    • F15B13/02Fluid distribution or supply devices characterised by their adaptation to the control of servomotors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B19/00Testing; Calibrating; Fault detection or monitoring; Simulation or modelling of fluid-pressure systems or apparatus not otherwise provided for
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00Circuits for servomotor systems
    • F15B2211/20Fluid pressure source, e.g. accumulator or variable axial piston pump
    • F15B2211/205Systems with pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00Circuits for servomotor systems
    • F15B2211/20Fluid pressure source, e.g. accumulator or variable axial piston pump
    • F15B2211/21Systems with pressure sources other than pumps, e.g. with a pyrotechnical charge
    • F15B2211/212Systems with pressure sources other than pumps, e.g. with a pyrotechnical charge the pressure sources being accumulators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00Circuits for servomotor systems
    • F15B2211/80Other types of control related to particular problems or conditions
    • F15B2211/855Testing of fluid pressure systems

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)

Abstract

收放式受油装置试验台,包括液压系统,所述液压系统包括油箱、与油箱连接的液压系统、回油系统,以及与液压系统和回油系统相连的至少一路试验接出系统;所述液压系统包括手动液压系统和电动液压系统二者之一或包括手动液压系统和电动液压系统;电动液压系统连接有电控系统;所述液压系统与回油系统、试验接出系统之间设置有开关阀,控制液压系统与回油系统和试验接出系统的通断。本发明提供了解决了现有航空试验系统没有专门配备的受油装置测试设备的问题,可应用于飞机平尾折叠与展开系统和起落架收放系统等多种依靠受油装置供油的航空试验,不再需要依靠地方航空工业部门支持方可进行该项检测工作,因此,可极大的改善试验环境和提高试验效率。

The retractable oil receiving device test bench includes a hydraulic system, the hydraulic system includes an oil tank, a hydraulic system connected to the oil tank, an oil return system, and at least one test connection system connected to the hydraulic system and the oil return system; The hydraulic system includes either a manual hydraulic system or an electro-hydraulic system or a manual hydraulic system and an electro-hydraulic system; the electro-hydraulic system is connected with an electric control system; there is a The switch valve controls the on-off of the hydraulic system, the oil return system and the test connection system. The invention solves the problem that the existing aviation test system does not have specially equipped testing equipment for the oil receiving device, and can be applied to various aviation tests relying on the fuel supply of the oil receiving device, such as the aircraft horizontal tail folding and unfolding system and the landing gear retracting system. , It is no longer necessary to rely on the support of the local aviation industry department to carry out the testing work. Therefore, the test environment and test efficiency can be greatly improved.

Description

收放式受油装置试验台Retractable oil receiving device test bench

技术领域technical field

本发明属于航空试验系统技术领域,涉及一种收放式受油装置试验台。The invention belongs to the technical field of aviation test systems, and relates to a retractable oil receiver test bench.

背景技术Background technique

飞机性能测试、检测是飞机设计和研究的重要工作,也是一项综合性工作,需要飞机多系统配合才能完成测试、检测工作。Aircraft performance testing and inspection is an important task in aircraft design and research, and it is also a comprehensive work that requires the cooperation of multiple systems of the aircraft to complete the testing and inspection work.

以飞机平尾折叠与展开系统和起落架收放系统为例,这两个系统是飞机比较重要的系统,其工作性能的好坏直接影响着飞机的良好率。因此,按要求在做定期工作和排故时须对飞机平尾折叠与展开系统和起落架收放系统进行地面相关性能的检查,以保证其性能良好和工作可靠,是机务保障人员一项重要的的工作。而以上系统的试验工作需要依靠受油装置。Take the plane tail folding and unfolding system and the landing gear retracting system as examples. These two systems are relatively important systems of the aircraft, and their working performance directly affects the good rate of the aircraft. Therefore, when doing regular work and troubleshooting as required, it is necessary to check the ground-related performance of the aircraft's horizontal tail folding and unfolding system and landing gear retraction system to ensure its good performance and reliable operation, which is an important task for maintenance personnel. work. The test work of the above system needs to rely on the oil receiving device.

目前,海军航空兵部队还没有配备收放式受油装置测试设备,在日常维修、排故、定检等时机无法对平尾折叠与展开系统和起落架收放系统进行自主检测,必须依靠地方航空工业部门支持方可进行该项检测工作。At present, the naval aviation unit is not equipped with retractable refueling device testing equipment, and cannot independently test the horizontal tail folding and unfolding system and the landing gear retracting system during routine maintenance, troubleshooting, and regular inspections, and must rely on the local aviation industry. The testing work can only be carried out with the support of the department.

除飞机平尾折叠与展开系统和起落架收放系统外,对其他需要受油系统配合工作的系统进行测试、检测工作,也需要应用受油装置测试设备。In addition to the folding and unfolding system of the horizontal tail of the aircraft and the retracting and retracting system of the landing gear, the testing and testing of other systems that require the cooperation of the oil receiving system also require the application of oil receiving device test equipment.

因此,急需一种工作可靠、功能齐全、精度高、操作方便和便于维护的收放式受油装置试验台,这对于确保飞机完成性能检测工作,提高飞机良好率和确保飞行安全都将具有重要意义。Therefore, there is an urgent need for a reliable, fully functional, high-precision, easy-to-operate and easy-to-maintain retractable refueling device test bench, which will play an important role in ensuring that the aircraft completes performance testing, improves the good rate of the aircraft, and ensures flight safety. significance.

发明内容Contents of the invention

本发明的目的在于提供一种应用于飞机性能检测的收放式受油系统试验台。The object of the present invention is to provide a retractable refueling system test bench for aircraft performance testing.

为实现以上目的,本发明提供以下技术方案:To achieve the above object, the present invention provides the following technical solutions:

收放式受油装置试验台,包括液压系统,液压系统包括油箱、与油箱连接的液压系统、回油系统,以及与液压系统和回油系统相连的至少一路试验接出系统;液压系统包括手动液压系统和电动液压系统二者之一或包括手动液压系统和电动液压系统;电动液压系统连接有电控系统;液压系统与回油系统、试验接出系统之间设置有开关阀,控制液压系统与回油系统和试验接出系统的通断。The retractable oil receiving device test bench includes the hydraulic system, the hydraulic system includes the oil tank, the hydraulic system connected to the oil tank, the oil return system, and at least one test connection system connected to the hydraulic system and the oil return system; the hydraulic system includes manual One of the hydraulic system and the electro-hydraulic system or including the manual hydraulic system and the electro-hydraulic system; the electro-hydraulic system is connected with an electric control system; a switch valve is set between the hydraulic system and the oil return system and the test connection system to control the hydraulic system On-off with the oil return system and the test connection system.

进一步,电动液压系统包括电动泵,油箱出油口经吸油滤芯、电泵供油阀接电动泵入油口;电动泵出油口顺次经出油滤芯、单向阀和电泵出油截止阀接开关阀;电动泵出油端还经安全阀与油箱连通;单向阀出油端还经调压截止阀与油箱连通;单向阀出油端连接有电动液压系统压力表;单向阀和电泵出油截止阀之间安装有卸荷溢流阀。Further, the electrohydraulic system includes an electric pump, the oil outlet of the oil tank is connected to the oil inlet of the electric pump through the oil suction filter element, the oil supply valve of the electric pump; the oil outlet of the electric pump passes through the oil outlet filter element, the check valve and the oil outlet cut-off The valve is connected to the on-off valve; the oil outlet of the electric pump is also connected with the fuel tank through the safety valve; the oil outlet of the one-way valve is also connected with the oil tank through the pressure regulating stop valve; the oil outlet of the one-way valve is connected with the pressure gauge of the electrohydraulic system; An unloading overflow valve is installed between the valve and the oil outlet shut-off valve of the electric pump.

进一步,电动液压系统还包括由电泵出油截止阀的入油端接出的蓄能器支路,蓄能器支路上设置有蓄能器和蓄能压力表。Furthermore, the electrohydraulic system also includes an accumulator branch connected to the oil inlet end of the electric pump oil outlet shut-off valve, and an accumulator and an energy storage pressure gauge are arranged on the accumulator branch.

进一步,手动液压系统包括手摇泵,油箱出油口经吸油滤芯、手泵供油阀接手摇泵入油口;手摇泵出油口顺次经出油滤芯、单向阀和手泵截止阀接开关阀;单向阀出油端还经调压截止阀与油箱连通;单向阀出油端还接有手动液压系统压力表。Further, the manual hydraulic system includes a hand pump, the oil outlet of the oil tank is connected to the oil inlet of the hand pump through the oil suction filter element, the oil supply valve of the hand pump; the oil outlet of the hand pump is cut off through the oil outlet filter element, the check valve and the hand pump The valve is connected to the on-off valve; the oil outlet of the one-way valve is also connected with the fuel tank through the pressure regulating stop valve; the oil outlet of the one-way valve is also connected with a pressure gauge of the manual hydraulic system.

进一步,回油系统包括由试验接出系统端向油箱回油口端顺次连接的回油截止阀、回油滤芯和回油阀;回油截止阀的出油端连接至开关阀。Further, the oil return system includes an oil return cut-off valve, an oil return filter element, and an oil return valve sequentially connected from the end of the test connection system to the oil return port of the fuel tank; the oil outlet end of the oil return stop valve is connected to the switch valve.

进一步,包括两路试验接出系统,开关阀为三位四通阀,其进油口接液压系统,其工作油口分别接两路试验接出系统,其回油口接回油系统。Further, it includes a two-way test connection system, the on-off valve is a three-position four-way valve, its oil inlet is connected to the hydraulic system, its working oil port is respectively connected to the two-way test connection system, and its oil return port is connected to the oil return system.

进一步,一路或两路试验接出系统还分出试验接出支路。Further, the one-way or two-way test connection system also divides the test connection branch.

进一步,试验接出系统和试验接出支路包括互连的高压长软管和伸出嘴,伸出嘴端与开关阀相接,高压长软管端与被测试系统相接。Further, the test connection system and the test connection branch include interconnected high-pressure long hoses and extension nozzles, the end of the extension nozzle is connected to the switch valve, and the end of the high-pressure long hose is connected to the system under test.

进一步,包括试验台箱体,试验台箱体包括主操纵面板、组件箱;液压系统、回油系统及试验接出系统设置在组件箱内外;手摇泵设置在组件箱外壁,组件箱外壁还设置有油管嘴和用于缠绕高压长软管的绞轮,其中油管嘴分别于液压系统、回油系统连通。Further, it includes the test bench box, which includes the main control panel and the component box; the hydraulic system, the oil return system and the test connection system are arranged inside and outside the component box; the hand pump is arranged on the outer wall of the component box, and the outer wall of the component box is also It is provided with an oil nozzle and a winch for winding a high-pressure long hose, wherein the oil nozzle communicates with the hydraulic system and the oil return system respectively.

进一步,主操纵板上设置有系统多个压力表,分别连接电动液压系统压力表、手动液压系统压力表和蓄能器压力表;还设置有手泵调压阀、手泵供油阀、电泵调压阀、电泵供油阀和回油开关阀。Furthermore, there are multiple pressure gauges in the system on the main control panel, which are respectively connected to the pressure gauges of the electro-hydraulic system, the pressure gauges of the manual hydraulic system and the pressure gauges of the accumulator; Pump pressure regulating valve, electric pump oil supply valve and oil return switch valve.

本发明的有益效果为:The beneficial effects of the present invention are:

(1)本发明提供了一种可应用于飞机试验的受油装置试验台,解决了现有航空试验系统没有专门配备的受油装置测试设备的问题,可应用于飞机平尾折叠与展开系统和起落架收放系统等多种依靠受油装置供油的航空试验,不再需要依靠地方航空工业部门支持方可进行该项检测工作,因此,可极大的改善试验环境和提高试验效率。(1) The present invention provides a kind of refueling device test bench that can be applied to aircraft test, has solved the problem that existing aviation test system does not have the problem of specially equipped refueling device test equipment, can be applied to aircraft horizontal tail folding and unfolding system and Various aeronautical tests that depend on the oil supply of the oil receiving device, such as the retractable and retractable system of the landing gear, no longer need to rely on the support of the local aviation industry department to carry out the testing work. Therefore, the test environment and test efficiency can be greatly improved.

(2)该受油装置试验系统可外接多条试验管路,且每条试验管路还可延伸设置试验支路,可根据试验需求更换合适的开关阀组件,即可适应试验需求。(2) The test system of the oil receiving device can be externally connected to multiple test pipelines, and each test pipeline can also be extended to set up a test branch, and the appropriate switch valve assembly can be replaced according to the test requirements to meet the test requirements.

(3)该受油装置试验系统配置设计了手动液压系统和电动液压系统,可根据需要选择使用一个或两个液压系统,结构稳定灵活,适应多种应用环境。整个液压系统可输出足够排量的液压油源,能够进行方向转换和压力调节。(3) The test system configuration of the oil receiving device is designed with a manual hydraulic system and an electro-hydraulic system. One or two hydraulic systems can be used according to the needs. The structure is stable and flexible, and it is suitable for various application environments. The entire hydraulic system can output a hydraulic oil source with sufficient displacement, and can perform direction conversion and pressure adjustment.

(4)在适用性和维护性方面使用较长的软导管与飞机部位进行长距离的连接,且在试验完成后,便于进行收起和收藏,确保足够的强度要求。(4) In terms of applicability and maintainability, a longer flexible conduit is used for long-distance connection with the aircraft, and after the test is completed, it is easy to store and store to ensure sufficient strength requirements.

附图说明Description of drawings

图1为收放式受油装置试验台结构示意图。Figure 1 is a schematic diagram of the test bench structure of the retractable oil receiving device.

图2为试验台箱体结构示意图。Figure 2 is a schematic diagram of the box structure of the test bench.

图3为试验台箱体结构示意图。Figure 3 is a schematic diagram of the box structure of the test bench.

图4为试验台箱体结构示意图。Figure 4 is a schematic diagram of the box structure of the test bench.

图5为试验台主操纵面板示意图。Figure 5 is a schematic diagram of the main control panel of the test bench.

其中:1-加油口,2-液位计,3-油箱,4-吸油滤芯,5-手泵供油阀,6-手摇泵,7-出油滤芯,8-单向阀,9-手泵调压阀,10-手动液压系统压力表,11-三位四通阀,12-伸出管嘴,13-高压长软管,14-伸出管嘴,15-高压长软管,16-伸出管嘴,17-高压长软管,18-伸出管嘴,19-高压长软管,20-回油截止阀,21-回油滤芯,22-回油阀,23-手泵出油截止阀,24-吸油滤芯,25-电泵供油阀,26-电动泵,27-出油滤芯,28-单向阀,29-卸荷溢流阀,30-安全阀,31-电泵调压截止阀,32-电动液压系统压力表,33-蓄能器,34-蓄能器压力表,35-电泵出油截止阀,36-试验台箱体,37-绞轮,38-主操纵面板,39-油管嘴,40-放油球阀Among them: 1-refueling port, 2-liquid level gauge, 3-oil tank, 4-oil suction filter element, 5-hand pump oil supply valve, 6-hand pump, 7-oil outlet filter element, 8-one-way valve, 9- Hand pump pressure regulating valve, 10-Manual hydraulic system pressure gauge, 11-Three-position four-way valve, 12-Protruding nozzle, 13-High pressure long hose, 14-Protruding nozzle, 15-High pressure long hose, 16-Extend nozzle, 17-High pressure long hose, 18-Extend nozzle, 19-High pressure long hose, 20-Oil return stop valve, 21-Oil return filter, 22-Oil return valve, 23-Hand Pump oil outlet stop valve, 24-oil suction filter element, 25-electric pump oil supply valve, 26-electric pump, 27-oil outlet filter element, 28-one-way valve, 29-unloading overflow valve, 30-safety valve, 31 - Electric pump pressure regulating cut-off valve, 32- Electrohydraulic system pressure gauge, 33- Accumulator, 34- Accumulator pressure gauge, 35- Electric pump oil outlet cut-off valve, 36- Test bench box, 37- Winding wheel , 38-main control panel, 39-oil nozzle, 40-oil drain ball valve

具体实施方式detailed description

以下将结合附图对本发明的具体实施方式进行清楚完整地描述。显然,具体实施方式所描述的实施例仅为本发明的一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动的前提下所获得的所有其他实施例,都属于本发明的保护范围。The specific implementation manners of the present invention will be clearly and completely described below in conjunction with the accompanying drawings. Apparently, the embodiments described in the specific implementation are only some of the embodiments of the present invention, rather than all the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

收放式受油装置试验台,包括油箱3、与油箱3连接的液压系统、回油系统,以及与液压系统和回油系统相连的至少一路试验接出系统。其中,试验接出系统可根据需要进行的试验进行配置,例如,本实施例中,将以飞机平尾折叠与展开系统和起落架收放系统的试验进行举例说明(由于其可应用于起落架收放等试验,因此试验台也成为收放式受油装置试验台),因此,试验接出系统至少有两路。The retractable oil receiving device test bench includes an oil tank 3, a hydraulic system connected to the oil tank 3, an oil return system, and at least one test output system connected to the hydraulic system and the oil return system. Wherein, the test taking-out system can be configured according to the tests that need to be carried out. For example, in the present embodiment, the tests of the plane tail folding and unfolding system and the landing gear retracting system will be exemplified (because it can be applied to the landing gear retracting system). Release and other tests, so the test bench also becomes a retractable oil receiving device test bench), therefore, there are at least two routes for the test connection system.

液压系统包括手动液压系统和电动液压系统二者之一或包括手动液压系统和电动液压系统;电动液压系统连接有电控系统;液压系统与回油系统、试验接出系统之间设置有开关阀,控制液压系统与回油系统和试验接出系统的通断。开关阀可根据试验需求选择,例如,本实施例中,为配合飞机平尾折叠与展开系统和起落架收放系统的试验,开关阀选用三位四通阀。The hydraulic system includes either the manual hydraulic system or the electro-hydraulic system or the manual hydraulic system and the electro-hydraulic system; the electro-hydraulic system is connected with an electric control system; a switch valve is set between the hydraulic system and the oil return system and the test connection system , control the on-off of the hydraulic system, the oil return system and the test connection system. The switch valve can be selected according to the test requirements. For example, in this embodiment, in order to cooperate with the test of the plane tail folding and unfolding system and the landing gear retraction system, the switch valve is a three-position four-way valve.

其中,手动液压系统靠手动供油,电动液压系统靠电控系统控制供油。根据需要可为受油装置试验台配置手动液压系统,或者配置电动液压系统,亦或者是配置手动和电动两种形式的液压系统。开关阀的作用是控制液压系统的供油管路与试验系统的受油管路之间的开与闭,同时提供一条回油支路。Among them, the manual hydraulic system relies on manual oil supply, and the electrohydraulic system relies on the electric control system to control the oil supply. According to the needs, the oil receiving device test bench can be equipped with a manual hydraulic system, or an electro-hydraulic system, or a manual and electric hydraulic system. The function of the switch valve is to control the opening and closing between the oil supply pipeline of the hydraulic system and the oil receiving pipeline of the test system, and provide an oil return branch at the same time.

以下,将具体说明手动液压系统、电动液压系统和回油系统的具体配置和供油、回油原理。Hereinafter, the specific configuration and principles of oil supply and oil return of the manual hydraulic system, electrohydraulic system and oil return system will be described in detail.

电动液压系统包括电动泵26,油箱出油口经吸油滤芯24、电泵供油阀25接电动泵26入油口;电动泵26出油口顺次经出油滤芯27、单向阀28和电泵出油截止阀35接开关阀;电动泵26出油端还经安全阀30与油箱1连通;单向阀28出油端还经调压截止阀31与油箱1连通;单向阀28出油端连接有电动液压系统压力表32;单向阀28和电泵出油截止阀35之间安装有卸荷溢流阀29。The electrohydraulic system includes an electric pump 26, the oil outlet of the fuel tank is connected to the oil inlet of the electric pump 26 through the oil suction filter element 24, the oil supply valve 25 of the electric pump; the oil outlet of the electric pump 26 passes through the oil outlet filter element 27, the one-way valve 28 and the The oil outlet stop valve 35 of the electric pump is connected to the on-off valve; the oil outlet of the electric pump 26 is also communicated with the fuel tank 1 through the safety valve 30; An electro-hydraulic system pressure gauge 32 is connected to the oil outlet; an unloading overflow valve 29 is installed between the one-way valve 28 and the oil outlet stop valve 35 of the electric pump.

进一步,电动液压系统还包括由电泵出油截止阀35的入油端接出的蓄能器支路,蓄能器支路上设置有蓄能器33和蓄能压力表34。蓄能器支路的作用为稳压和保压,使系统工作更加安全可靠。Further, the electrohydraulic system also includes an accumulator branch connected to the oil inlet end of the electric pump oil outlet shut-off valve 35 , and an accumulator 33 and an accumulator pressure gauge 34 are arranged on the accumulator branch. The function of the accumulator branch is to stabilize and maintain the pressure, which makes the system work safer and more reliable.

手动液压系统包括手摇泵6,油箱3出油口经吸油滤芯4、手泵供油阀5接手摇泵6入油口;手摇泵6出油口顺次经出油滤芯7、单向阀8和手泵出油截止阀23接开关阀;单向阀8出油端还经手动阀9与油箱3连通;单向阀8出油端还接有手动液压系统压力表10。The manual hydraulic system includes a hand pump 6, the oil outlet of the oil tank 3 passes through the oil suction filter element 4, the hand pump oil supply valve 5 is connected to the oil inlet of the hand pump 6; the oil outlet of the hand pump 6 passes through the oil outlet filter element 7, one-way Valve 8 and hand pump oil outlet cut-off valve 23 are connected to the switch valve; the oil outlet of check valve 8 is also communicated with fuel tank 3 through manual valve 9; the oil outlet of check valve 8 is also connected with manual hydraulic system pressure gauge 10.

油箱3中的工作介质采用YH-15号液压油,油箱3的作用是为静压试验提供液压油。作为辅助设计,油箱3内还设置有用于添加液压油的加油口1和用于显示油箱3中液压油液位的液位计3。The working medium in the oil tank 3 adopts No. YH-15 hydraulic oil, and the function of the oil tank 3 is to provide hydraulic oil for the static pressure test. As an auxiliary design, an oil filling port 1 for adding hydraulic oil and a liquid level gauge 3 for displaying the liquid level of the hydraulic oil in the oil tank 3 are also arranged in the oil tank 3 .

采用电动液压系统工作时,电动泵26是电动液压系统的压力源,接通电控系统,为电动液压系统的电动泵26供电。将电泵出油截止阀35处于全开位置。当接上电源、按下电动泵26启动按钮时,电动泵26工作,油箱3中的液压油通过吸油滤24和电泵供油阀25进入电动泵26,通过电动泵26加压后,高压油液经出油滤芯27、单向阀28、卸荷溢流阀29、供电泵出油截止阀35后到达开关阀。When the electrohydraulic system is used, the electric pump 26 is the pressure source of the electrohydraulic system, and the electric control system is connected to supply power for the electric pump 26 of the electrohydraulic system. Put the oil outlet shut-off valve 35 of the electric pump in the fully open position. When the power supply is connected and the start button of the electric pump 26 is pressed, the electric pump 26 works, and the hydraulic oil in the oil tank 3 enters the electric pump 26 through the oil suction filter 24 and the electric pump oil supply valve 25, and after being pressurized by the electric pump 26, the high-pressure The oil liquid reaches the on-off valve after passing through the oil outlet filter element 27, the one-way valve 28, the unloading overflow valve 29, and the oil outlet shut-off valve 35 of the power supply pump.

系统压力由卸荷溢流阀29和调压截止阀31控制。卸荷溢流阀29在系统中主要用于给油泵卸荷和安全溢流的作用,一般卸荷溢流阀29的最高压力(即系统最大工作压力)调至21MPa。当泵源压力和系统压力上升到21MPa(卸荷溢流阀29的卸荷压力)时,卸荷溢流阀29工作,泵出口油压为零,油泵卸荷,系统压力在18~21MPa之间;当系统油压降到18MPa时,油泵停止卸荷,向系统供压至21MPa。System pressure is controlled by unloading overflow valve 29 and pressure regulating cut-off valve 31. The unloading overflow valve 29 is mainly used for oil pump unloading and safety overflow in the system. Generally, the maximum pressure of the unloading overflow valve 29 (that is, the maximum working pressure of the system) is adjusted to 21MPa. When the pump source pressure and system pressure rise to 21MPa (the unloading pressure of the unloading overflow valve 29), the unloading overflow valve 29 works, the oil pressure at the pump outlet is zero, the oil pump is unloaded, and the system pressure is between 18-21MPa When the system oil pressure drops to 18MPa, the oil pump stops unloading and supplies pressure to the system to 21MPa.

采用手动液压系统工作时,手摇泵6将油箱3中的液压油经手泵供油阀5后,再增压供出,油压油源经3μm的出油滤芯7、高压单向阀8、手泵调压阀9和手泵出油截止阀23后送至功试验接出系统。供出的有压油源工作压力为0-28MPa,由高压压力表10指示;供出有压油源工作压力的调节,由手泵调压阀9通过溢流完成。When the manual hydraulic system is used, the hand pump 6 pumps the hydraulic oil in the oil tank 3 through the hand pump oil supply valve 5, and then pressurizes it out. The pump pressure regulating valve 9 and the hand pump oil outlet cut-off valve 23 are then sent to the power test connection system. The working pressure of the supplied pressurized oil source is 0-28MPa, which is indicated by the high pressure gauge 10;

若一个受油装置试验台同时配置电动液压系统和手动液压系统,为防止两种液压系统产生干扰,在使用一个液压系统时,需要先关闭另一个液压系统的管路。具体的说,在电动液压系统工作时,需要关闭手泵出油截止阀23,关闭手动液压系统与试验管路之间的油路;同理,在使用手动液压系统时,需要关闭电泵出油截止阀35,关闭电动液压系统与试验系统的油路。If an oil receiving device test bench is equipped with an electrohydraulic system and a manual hydraulic system at the same time, in order to prevent the two hydraulic systems from interfering, when using one hydraulic system, the pipeline of the other hydraulic system needs to be closed first. Specifically, when the electrohydraulic system is working, it is necessary to close the oil outlet valve 23 of the hand pump, and close the oil circuit between the manual hydraulic system and the test pipeline; The oil cut-off valve 35 closes the oil circuit of the electrohydraulic system and the test system.

回油系统包括由试验接出系统端向油箱回油口端顺次连接的回油截止阀20、回油滤芯21和回油阀22。其中,回油截止阀20的出油端连接至开关阀。The oil return system includes an oil return cut-off valve 20, an oil return filter element 21 and an oil return valve 22 connected in sequence from the end of the test connection system to the oil return port of the oil tank. Wherein, the oil outlet end of the oil return cut-off valve 20 is connected to the switch valve.

回油部分功能主要将试验部分的回油,经回油滤芯21、回油阀22顺利导入油箱3。油箱3内的液位由液位计2指示,放出油箱3打开放油球阀40即可,给油箱3加油可经加油口1加入。The function of the oil return part mainly imports the oil return of the test part into the oil tank 3 smoothly through the oil return filter element 21 and the oil return valve 22 . The liquid level in the fuel tank 3 is indicated by the liquid level gauge 2, and the fuel tank 3 is released to open the oil release ball valve 40, and the fuel tank 3 can be refueled through the filler port 1.

进一步提供一种受油装置试验台的安装结构,包括试验台箱体26,试验台箱体26包括主操纵面板38、组件箱;液压系统、回油系统及试验接出系统设置在组件箱内外,其中各种阀类组件设置在组件箱内部;手摇泵6设置在组件箱外壁,组件箱外壁还设置有油管嘴和用于缠绕高压长软管的绞轮,其中油管嘴分别于液压系统、回油系统连通。Further provide a kind of installation structure of the test bench of the oil receiving device, including the test bench body 26, the test bench body 26 includes the main control panel 38, the component box; the hydraulic system, the oil return system and the test connection system are arranged inside and outside the component box , wherein various valve components are set inside the component box; the hand pump 6 is set on the outer wall of the component box, and the outer wall of the component box is also provided with an oil nozzle and a winch for winding a high-pressure long hose, wherein the oil nozzle is separated from the hydraulic system. , The oil return system is connected.

进一步,主操纵面板38上设置有系统多个压力表分为系统压力表、电泵出口压力表和手摇泵出口压力表,分别连接电动液压蓄能器压力表34、手动液压系统压力表10和电动液压系统压力表32;还设置有手泵调压阀9、手泵出油截止阀23、电泵调压阀31、电泵供油截止阀35和回油阀截止阀20控制键。Further, the main control panel 38 is provided with a plurality of system pressure gauges, which are divided into system pressure gauges, electric pump outlet pressure gauges and hand pump outlet pressure gauges, which are respectively connected to the electrohydraulic accumulator pressure gauge 34 and the manual hydraulic system pressure gauge 10. And electrohydraulic system pressure gauge 32; Also be provided with hand pump pressure regulating valve 9, hand pump oil outlet cut-off valve 23, electric pump pressure regulating valve 31, electric pump oil supply cut-off valve 35 and oil return valve cut-off valve 20 control keys.

试验台箱体36的结构集成了整个受油装置试验台的功能部件结构。The structure of the test bench box 36 integrates the structure of the functional components of the entire oil receiving device test bench.

如前所述,受油装置试验系统可用于飞机平尾折叠与展开系统和起落架收放系统的试验,为实现以上试验目的,本实施例中的开关阀为三位四通阀11,其进油口接液压系统,其工作油口分别接两路试验接出系统,其回油口接回油系统。As mentioned above, the test system of the oil receiving device can be used for the test of the aircraft horizontal tail folding and unfolding system and the landing gear retraction system. The oil port is connected to the hydraulic system, the working oil port is respectively connected to the two test outlet systems, and the oil return port is connected to the oil return system.

设计了两路试验接出系统,一路为伸出管嘴12和高压长软管13所在支路,接飞机平尾折叠与展开系统,其中伸出管嘴12端与三位四通阀11相接;一路为伸出管嘴14与高压长软管15所在支路,接起落架收放系统,其中伸出管嘴14端与三位四通阀11相接;以上两条支路可用于对以上所述两个系统分别进行试验。同时,伸出管嘴14与高压长软管15所在支路还伸出另一条试验支路,即伸出管嘴16与高压长软管17所在支路,其中,其中伸出管嘴16端与三位四通阀11相接。Two-way test connection system is designed, one is the branch where the extension nozzle 12 and the high-pressure long hose 13 are located, and is connected to the plane tail folding and unfolding system, in which the end of the extension nozzle 12 is connected to the three-position four-way valve 11 ; All the way is the branch where the nozzle 14 and the high-pressure long hose 15 are located, connected to the retractable system of the landing gear, wherein the end of the nozzle 14 is connected with the three-position four-way valve 11; the above two branches can be used for The two systems described above were tested separately. At the same time, the branch where the nozzle 14 and the long high-pressure hose 15 are located also extends another test branch, that is, the branch where the nozzle 16 and the long high-pressure hose 17 are located, wherein the end of the nozzle 16 It is connected with the three-position four-way valve 11.

三位四通收放阀11共有收起、中立、放平三个工作位置,与飞机平尾折叠收放作动筒活塞两端油路相连,通过扳动收放阀的手柄,将其置于相应的位置,可实现收放管路的方向转换。由于飞机上管嘴位置距离测试验台箱体26相对较远,高压长软管需设置8-10米的长度为宜。The three-position four-way retractable valve 11 has three working positions: stowed, neutral, and flattened. The corresponding position can realize the direction conversion of the retractable pipeline. Since the position of the nozzle on the aircraft is relatively far away from the test bench casing 26, it is advisable that the high-pressure long hose needs to be provided with a length of 8-10 meters.

Claims (10)

1. extendible oil-receiving device testing stand, it is characterised in that:Including hydraulic system, the hydraulic system includes fuel tank and oil Case connection hydraulic system, oil return system, and be connected with hydraulic system and oil return system at least all the way test pick out system;
The hydraulic system includes hand-hydraulic system and electro-hydraulic system alternative one or including hand-hydraulic system and electricity Hydrodynamic pressure system;
Electro-hydraulic system is connected with electric-control system;
The hydraulic system and oil return system, experiment are provided with switch valve, control hydraulic system and oil return system between picking out system System and experiment pick out the break-make of system.
2. extendible oil-receiving device testing stand as claimed in claim 1, it is characterised in that:The electro-hydraulic system includes electricity Dynamic pump, fuel tank oil-out connects electrodynamic pump oiler through oil suction filter core, electric pump delivery valve;Electrodynamic pump oil-out is sequentially through fuel-displaced filter Core, check valve and electric pump go out oil cut-off valve and connect switch valve;Electrodynamic pump oil outlet end is also connected through safety valve with fuel tank;Check valve is fuel-displaced End also connects through pressure regulation stop valve with fuel tank;Check valve oil outlet end is connected with electro-hydraulic system pressure gauge;Check valve and electric pump Go out between oil cut-off valve and unloading overflow valve is installed.
3. extendible oil-receiving device testing stand as claimed in claim 2, it is characterised in that:Electro-hydraulic system also includes by electricity The accumulator branch road that the oil-inlet end of oil cut-off valve is picked out is pumped out, accumulator and energy-storage pressure are provided with the accumulator branch road Table.
4. extendible oil-receiving device testing stand as claimed in claim 1, it is characterised in that:The hand-hydraulic system includes hand Pump is shaken, fuel tank oil-out shakes and pump into hydraulic fluid port through oil suction filter core, hand pump delivery valve catcher;Hand pump oil-out is sequentially through fuel-displaced filter Core, check valve and hand pump stop valve connect switch valve;Check valve oil outlet end is also connected through pressure regulation stop valve with fuel tank;Check valve is fuel-displaced End is further connected with hand-hydraulic system pressure table.
5. extendible oil-receiving device testing stand as claimed in claim 1, it is characterised in that:The oil return system is included by testing Pick out oil return stop valve, oil return filter core and oil return valve that system end is sequentially connected with to tank drainback mouthful end;Oil return stop valve goes out Oily end is connected to switch valve.
6. the extendible oil-receiving device testing stand as described in any one in claim 1 to 6, it is characterised in that:Including two-way Experiment picks out system, and the switch valve is three-position four-way valve, and its oil inlet connects hydraulic system, and its actuator port connects two the examination of road respectively The system of picking out is tested, its oil return opening takes back oil system.
7. extendible oil-receiving device testing stand as claimed in claim 6, it is characterised in that:All the way or two-way experiment pick out system Also separate experiment and pick out branch road.
8. extendible oil-receiving device testing stand as claimed in claims 6 or 7, it is characterised in that:Experiment picks out system and experiment Pick out branch road include interconnection high pressure long soft-pipe and stretch out mouth, stretch out mouth end and connect with switch valve, high pressure long soft-pipe end be tested Test system connects.
9. the extendible oil-receiving device testing stand as described in any one in claim 1 to 6,8, it is characterised in that:Including examination Platform casing is tested, the testing stand casing includes main control surface plate, module case;The hydraulic system, oil return system and experiment are picked out System is arranged on inside and outside module case;The hand pump is arranged on component box outer wall, and component box outer wall is additionally provided with oil pipe mouth and use In the reel of winding high pressure long soft-pipe, wherein oil pipe mouth is connected respectively at hydraulic system, oil return system.
10. extendible oil-receiving device testing stand as claimed in claim 8, it is characterised in that:Set on the main control surface plate There is system multiple pressure gauge, electro-hydraulic system pressure gauge, hand-hydraulic system pressure table and energy storage pressure table are connected respectively; It is additionally provided with hand pump pressure regulator valve, hand pump delivery valve, electric pump pressure regulator valve, electric pump delivery valve and oil return switch valve.
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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107487442A (en) * 2017-09-28 2017-12-19 辽宁圣华机电设备制造有限公司 A kind of hydraulic actuation system
CN108916131A (en) * 2018-06-28 2018-11-30 中国直升机设计研究所 A kind of folding accumulator system
CN110217407A (en) * 2019-05-17 2019-09-10 陕西飞机工业(集团)有限公司 A kind of experimental rig of hydraulic actuator
RU2809868C1 (en) * 2023-03-17 2023-12-19 Общество с ограниченной ответственностью "Авиатехснаб" Device of hydraulic system of small hydraulic unit and method of its application

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005068849A1 (en) * 2003-12-19 2005-07-28 Dana Corporation Pressurized hydraulic fluid system with remote charge pump
CN102011766A (en) * 2010-11-15 2011-04-13 陕西飞机工业(集团)有限公司 Pressure-resistance and adjustment test bed for aircraft hydraulic system
CN202038460U (en) * 2011-04-11 2011-11-16 新乡平原航空技术工程有限公司 Hydraulic oil test truck for hydraulic system of airplanes
CN105083586A (en) * 2015-08-12 2015-11-25 中国航空工业集团公司西安飞机设计研究所 Device for testing aerial refueling adapter equipment
CN205298098U (en) * 2016-01-22 2016-06-08 安徽工程大学 Press hydraulic system's power servo control device
CN104500504B (en) * 2014-12-19 2017-01-11 上海电气液压气动有限公司 Forward-reverse rotation load sensitivity test system for closed type hydraulic pumps

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005068849A1 (en) * 2003-12-19 2005-07-28 Dana Corporation Pressurized hydraulic fluid system with remote charge pump
CN102011766A (en) * 2010-11-15 2011-04-13 陕西飞机工业(集团)有限公司 Pressure-resistance and adjustment test bed for aircraft hydraulic system
CN202038460U (en) * 2011-04-11 2011-11-16 新乡平原航空技术工程有限公司 Hydraulic oil test truck for hydraulic system of airplanes
CN104500504B (en) * 2014-12-19 2017-01-11 上海电气液压气动有限公司 Forward-reverse rotation load sensitivity test system for closed type hydraulic pumps
CN105083586A (en) * 2015-08-12 2015-11-25 中国航空工业集团公司西安飞机设计研究所 Device for testing aerial refueling adapter equipment
CN205298098U (en) * 2016-01-22 2016-06-08 安徽工程大学 Press hydraulic system's power servo control device

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107487442A (en) * 2017-09-28 2017-12-19 辽宁圣华机电设备制造有限公司 A kind of hydraulic actuation system
CN107487442B (en) * 2017-09-28 2024-01-12 辽宁港泰航空科技有限公司 Hydraulic actuating system
CN108916131A (en) * 2018-06-28 2018-11-30 中国直升机设计研究所 A kind of folding accumulator system
CN108916131B (en) * 2018-06-28 2020-06-09 中国直升机设计研究所 Folding accumulator system
CN110217407A (en) * 2019-05-17 2019-09-10 陕西飞机工业(集团)有限公司 A kind of experimental rig of hydraulic actuator
RU2809868C1 (en) * 2023-03-17 2023-12-19 Общество с ограниченной ответственностью "Авиатехснаб" Device of hydraulic system of small hydraulic unit and method of its application

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