欢迎来到毕设资料网! | 帮助中心 毕设资料交流与分享平台
毕设资料网
全部分类
  • 毕业设计>
  • 毕业论文>
  • 外文翻译>
  • 课程设计>
  • 实习报告>
  • 相关资料>
  • ImageVerifierCode 换一换
    首页 毕设资料网 > 资源分类 > DOC文档下载
    分享到微信 分享到微博 分享到QQ空间

    外文翻译--航空发动机状态监测系统设计研究

    • 资源ID:130044       资源大小:83.50KB        全文页数:23页
    • 资源格式: DOC        下载积分:100金币
    快捷下载 游客一键下载
    账号登录下载
    三方登录下载: QQ登录
    下载资源需要100金币
    邮箱/手机:
    温馨提示:
    快捷下载时,用户名和密码都是您填写的邮箱或者手机号,方便查询和重复下载(系统自动生成)。
    如填写123,账号就是123,密码也是123。
    支付方式: 支付宝   
    验证码:   换一换

     
    账号:
    密码:
    验证码:   换一换
      忘记密码?
        
    友情提示
    2、PDF文件下载后,可能会被浏览器默认打开,此种情况可以点击浏览器菜单,保存网页到桌面,就可以正常下载了。
    3、本站不支持迅雷下载,请使用电脑自带的IE浏览器,或者360浏览器、谷歌浏览器下载即可。
    4、本站资源下载后的文档和图纸-无水印,预览文档经过压缩,下载后原文更清晰。

    外文翻译--航空发动机状态监测系统设计研究

    1、 沈阳航空航天大学毕业设计 外文翻译 学 院 自动化学院 专 业 运载器这测试技术 班 级 94070301 学 号 2009040510011 姓 名 李万峰 指导教师 崔建国 负责教师 崔建国 沈阳航空 航天大学 2013 年 6 月 沈阳航空航天大学毕业设计(外文翻译) 1 Aeroengine condition monitoring system design study Design research abstract: the aircraft engine condition monitoring system for a certain type of aircraft en

    2、gine as the research object, discussed the engine state monitoring system design and implementation, this paper mainly discusses the status monitoring system of the overall design, system software and hardware development and testing and redundancy design, and in the design of engine state monitorin

    3、g system, introduced the embedded PC / 104 modules.In order to make the state monitoring system has a better scalability and adaptability, the system designed can work in three ways: airborne operation mode, data playback mode and ground test run mode, through these way for automatic monitoring of e

    4、ngine state parameter, for the state of the engine trend analysis, fault diagnosis, and as to provide scientific basis for maintenance. Key words: the engine condition monitoring;PC / 104;Redundant design. 0. The introduction As the power source of the airplane flight, aircraft engine research is a

    5、very complex process, the aircraft engine test as the development of the three pillars (calculation, manufacture and test), one of its importance is self-evident, it turns out, mainly consisted of 沈阳航空航天大学毕业设计(外文翻译) 2 engine test, rather than by calculation and analysis.For the development of an air

    6、craft engine group, is flat, how we can decide the how developed horizontal engine.For aircraft engine manufacture, condition monitoring is an important examination method of engine performance, by condition monitoring and testing work is to adjust the engine performance and break-in, check the manu

    7、facturing or overhaul quality, finally gives the engine factory performance report purpose, therefore the accurate and reliable test method for state monitoring to ensure the quality of the engine has the vital significance.As we all know, the engine vibration and high noise in the process of work a

    8、nd the strong jamming signal, all parameters to the variety of the monitoring system puts forward higher requirements.Especially with the improvement of engine performance, real-time monitoring of the parameters needed for condition monitoring is becoming more and more people continue to explore new

    9、 testing technology for many years, to adapt to the increasingly development of engine test technology requirements. 1. The condition monitoring system overall design The condition monitoring system is designed for a certain type of turbofan engine, the engine monitoring system of the input signal is part of a total of 17 analog, 3 road 16 way switch frequency and quantity, including 17 analog, 3 road frequency quantity through the


    注意事项

    本文(外文翻译--航空发动机状态监测系统设计研究)为本站会员(泛舟)主动上传,毕设资料网仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请联系网站客服QQ:540560583,我们立即给予删除!




    关于我们 - 网站声明 - 网站地图 - 资源地图 - 友情链接 - 网站客服 - 联系我们
    本站所有资料均属于原创者所有,仅提供参考和学习交流之用,请勿用做其他用途,转载必究!如有侵犯您的权利请联系本站,一经查实我们会立即删除相关内容!
    copyright@ 2008-2025 毕设资料网所有
    联系QQ:540560583