机械工程师
機械工程師
궤계공정사
MECHANICAL ENGINEER
2015年
6期
192-193,194
,共3页
劳黎露%瞿剑苏%夏能海%俞卿%戴志军
勞黎露%瞿劍囌%夏能海%俞卿%戴誌軍
로려로%구검소%하능해%유경%대지군
发动机%叶片%前缘%后缘%测量%校准
髮動機%葉片%前緣%後緣%測量%校準
발동궤%협편%전연%후연%측량%교준
engine%blade%leading edge%trailing edge%measurement%calibration
发动机叶片前后缘的测量对于保证发动机叶片气动性能的优劣至关重要,决定着发动机能量转换的效率。该项测量一直是一项技术难点,也没有专用的测量设备。文中提出了一种针对发动机叶片前后缘的测量方法,解决了前后缘厚度在(0.1~1 mm)范围内的测量,严格控制叶片生产全过程的误差,快速有效地提供叶片任意截面前后缘厚度数据,大大提高测量效率,以期为改善发动机性能作出贡献。同时研究相应的现场校准方法,保证量值溯源。
髮動機葉片前後緣的測量對于保證髮動機葉片氣動性能的優劣至關重要,決定著髮動機能量轉換的效率。該項測量一直是一項技術難點,也沒有專用的測量設備。文中提齣瞭一種針對髮動機葉片前後緣的測量方法,解決瞭前後緣厚度在(0.1~1 mm)範圍內的測量,嚴格控製葉片生產全過程的誤差,快速有效地提供葉片任意截麵前後緣厚度數據,大大提高測量效率,以期為改善髮動機性能作齣貢獻。同時研究相應的現場校準方法,保證量值溯源。
발동궤협편전후연적측량대우보증발동궤협편기동성능적우렬지관중요,결정착발동궤능량전환적효솔。해항측량일직시일항기술난점,야몰유전용적측량설비。문중제출료일충침대발동궤협편전후연적측량방법,해결료전후연후도재(0.1~1 mm)범위내적측량,엄격공제협편생산전과정적오차,쾌속유효지제공협편임의절면전후연후도수거,대대제고측량효솔,이기위개선발동궤성능작출공헌。동시연구상응적현장교준방법,보증량치소원。
The measurement of leading edge and trailing edge is essential to guarantee the pneumatic performance of engine blades, and determine the efficiency of energy transformation of engine. So far, the measurement is carried out with technical difficulties that it has no special device. The paper provides a method of measuring edges of engine blades which can resolve the measurement for thickness of edges between 0.1mm and 1mm. Error of blade is strictly controlled during the whole process of manufacturing. Thickness data of any cross-section of the blade is provided quickly and effectively so that the higher efficiency of measurement can improve the performance of engine. Meanwhile, respective calibration method is studied as well, to ensure the traceability.