基于轻量化BIM的高空台液压加载试验智能管控技术  

Intelligent Management and Control Technology for Hydraulic Loading System of Altitude Simulation Test Facility Based on Lightweight BIM

作　　者：彭晋 郭鹏飞 刁昕宇 赵万里 郭迎清[2] PENG Jin;GUO Peng-fei;DIAO Xin-yu;ZHAO Wan-li;GUO Ying-qing(AECC Sichuan Gas Turbine Establishment,Mianyang Sichuan 621700,China;School of Power and Energy,Northwestern Polytechnical University,Xi'an 710072,China)

机构地区：[1]中国航发四川燃气涡轮研究院,四川绵阳621000 [2]西北工业大学动力与能源学院,西安710129

出　　处：《航空发动机》2024年第2期153-158,共6页Aeroengine

基　　金：航空动力基础研究项目资助。

摘　　要：为了使航空发动机高空模拟试车中的液压加载试验智能高效地运行,完善并优化其试验平台,提出一种基于轻量化建筑信息模型(BIM)的液压加载试验智能管控技术。建立了支持管控平台运行的高空台液压加载试验软硬件协同运行架构,提出了基于WebGL的数据在Web端3维模型上实时展示的技术,以提高试验操作人员对试验进行监测的直观性。所设计的智能管控平台同时集成了试验设置与试验操作、数据管理、试验过程分析、故障诊断分析等功能。结果表明:所提出的基于轻量化BIM的智能管控技术可使试验操作人员直观、便捷、高效地进行试验流程管控、数据综合管理、设备健康状况分析,提高了高空台液压加载系统试验的智能化、自动化水平。To enable the intelligent and efficient operation of hydraulic loading tests during an aeroengine altitude simulation test,and to improve and optimize its test platform,an intelligent management and control technology of the hydraulic loading system test based on lightweight BIM was proposed.The hardware and software collaborative operation architecture of the hydraulic loading test supporting the management and control platform was established,and the WebGL-based technology of real-time data display on the Web 3D models was proposed to improve the intuitiveness of test monitoring.The designed intelligent management and control platform integrates functions such as test setting and operation,data management,test process analysis,fault diagnosis analysis,etc.The results show that the proposed intelligent management and control technology based on lightweight BIM can make test operators intuitively,conveniently,and efficiently conduct test process management and control,comprehensive data management,and equipment health analysis,improving the intelligence and automation level of the hydraulic loading system of altitude simulation test facility.

关 键 词：高空模拟试验 液压加载系统 智能管控 轻量化建筑信息模型 Web图形库 航空发动机 

分 类 号：V263.14[航空宇航科学与技术—航空宇航制造工程]