{"title":"The ARA large scale thrust measuring rig","authors":"D. Coulton","doi":"10.1109/ICIASF.1995.519123","DOIUrl":null,"url":null,"abstract":"The Large Scale Thrust Measuring Rig (LSTMR) which is installed at the Aircraft Research Association's site at Bedford, England, is a twin stream facility capable of supplying the separate Core and Bypass (Fan) flows to typical engine nozzle/after body models. The rig, which is able to be operated with either cold or hot core flow, provides the means of assessing the performance of single or twin stream nozzle configurations in terms of nozzle discharge and thrust characteristics. Models of jet engine nozzles at typically 1/7 to 1/10 scale can be tested in both forward and reverse thrust modes with mass flows of up to 12 Kg/s (26 lb/s) (Fan) and 5 Kg/s (11 lb/s) (Core) and with core temperatures of up to 600/spl deg/C (1100/spl deg/F). The LSTMR provides the Aircraft Research Association with a test facility that is unique in Europe and which is capable of producing the high quality test results required by the various customers. As such it enhances ARA's capabilities for discharge and thrust measuring facilities by supplementing the two existing Mach Simulation Tanks (MSTI and 2) which are also used for nozzle calibrations. The paper highlights the main features of the rig and discusses in detail the various control and measurement systems that are necessary to provide consistent high quality data.","PeriodicalId":339620,"journal":{"name":"ICIASF '95 Record. International Congress on Instrumentation in Aerospace Simulation Facilities","volume":"11 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1995-07-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"ICIASF '95 Record. International Congress on Instrumentation in Aerospace Simulation Facilities","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICIASF.1995.519123","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
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Abstract

The Large Scale Thrust Measuring Rig (LSTMR) which is installed at the Aircraft Research Association's site at Bedford, England, is a twin stream facility capable of supplying the separate Core and Bypass (Fan) flows to typical engine nozzle/after body models. The rig, which is able to be operated with either cold or hot core flow, provides the means of assessing the performance of single or twin stream nozzle configurations in terms of nozzle discharge and thrust characteristics. Models of jet engine nozzles at typically 1/7 to 1/10 scale can be tested in both forward and reverse thrust modes with mass flows of up to 12 Kg/s (26 lb/s) (Fan) and 5 Kg/s (11 lb/s) (Core) and with core temperatures of up to 600/spl deg/C (1100/spl deg/F). The LSTMR provides the Aircraft Research Association with a test facility that is unique in Europe and which is capable of producing the high quality test results required by the various customers. As such it enhances ARA's capabilities for discharge and thrust measuring facilities by supplementing the two existing Mach Simulation Tanks (MSTI and 2) which are also used for nozzle calibrations. The paper highlights the main features of the rig and discusses in detail the various control and measurement systems that are necessary to provide consistent high quality data.
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ARA大型推力测量装置
大型推力测量装置(LSTMR)安装在英国贝德福德的飞机研究协会基地,是一个双流设备,能够为典型的发动机喷嘴/后车身模型提供单独的核心和旁路(风扇)流。该钻机可以在冷芯流或热芯流条件下操作,可以根据喷嘴排出量和推力特性评估单流或双流喷嘴配置的性能。典型的1/7到1/10比例的喷气发动机喷嘴模型可以在正向和反向推力模式下进行测试,质量流量高达12 Kg/s (26 lb/s)(风扇)和5 Kg/s (11 lb/s)(核心),核心温度高达600/spl度/C (1100/spl度/F)。LSTMR为飞机研究协会提供了一个在欧洲独一无二的测试设施,能够提供各种客户所需的高质量测试结果。因此,通过补充现有的两个用于喷嘴校准的马赫模拟罐(MSTI和2),它增强了ARA的放电和推力测量设施的能力。本文重点介绍了该钻机的主要特点,并详细讨论了提供一致的高质量数据所必需的各种控制和测量系统。
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