A Rapid Method to Achieve Aero-Engine Blade Form Detection
This paper proposes a rapid method to detect aero-engine blade form, according to the characteristics of an aero-engine blade surface. This method first deduces an inclination error model in free-form surface measurements based on the non-contact laser triangulation principle. Then a four-coordinate...
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Format: | Article |
Language: | English |
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MDPI AG
2015-06-01
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Series: | Sensors |
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Online Access: | http://www.mdpi.com/1424-8220/15/6/12782 |
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author | Bin Sun Bing Li |
author_facet | Bin Sun Bing Li |
author_sort | Bin Sun |
collection | DOAJ |
description | This paper proposes a rapid method to detect aero-engine blade form, according to the characteristics of an aero-engine blade surface. This method first deduces an inclination error model in free-form surface measurements based on the non-contact laser triangulation principle. Then a four-coordinate measuring system was independently developed, a special fixture was designed according to the blade shape features, and a fast measurement of the blade features path was planned. Finally, by using the inclination error model for correction of acquired data, the measurement error that was caused by tilt form is compensated. As a result the measurement accuracy of the Laser Displacement Sensor was less than 10 μm. After the experimental verification, this method makes full use of optical non-contact measurement fast speed, high precision and wide measuring range of features. Using a standard gauge block as a measurement reference, the coordinate system conversion data is simple and practical. It not only improves the measurement accuracy of the blade surface, but also its measurement efficiency. Therefore, this method increases the value of the measurement of complex surfaces. |
first_indexed | 2024-04-11T22:27:48Z |
format | Article |
id | doaj.art-b7d8a4ec966646e0a0f5250eee5d5aca |
institution | Directory Open Access Journal |
issn | 1424-8220 |
language | English |
last_indexed | 2024-04-11T22:27:48Z |
publishDate | 2015-06-01 |
publisher | MDPI AG |
record_format | Article |
series | Sensors |
spelling | doaj.art-b7d8a4ec966646e0a0f5250eee5d5aca2022-12-22T03:59:36ZengMDPI AGSensors1424-82202015-06-01156127821280110.3390/s150612782s150612782A Rapid Method to Achieve Aero-Engine Blade Form DetectionBin Sun0Bing Li1State Key Laboratory for Manufacturing Systems Engineering, Xi'an Jiaotong University, Xi'an 710049, ChinaState Key Laboratory for Manufacturing Systems Engineering, Xi'an Jiaotong University, Xi'an 710049, ChinaThis paper proposes a rapid method to detect aero-engine blade form, according to the characteristics of an aero-engine blade surface. This method first deduces an inclination error model in free-form surface measurements based on the non-contact laser triangulation principle. Then a four-coordinate measuring system was independently developed, a special fixture was designed according to the blade shape features, and a fast measurement of the blade features path was planned. Finally, by using the inclination error model for correction of acquired data, the measurement error that was caused by tilt form is compensated. As a result the measurement accuracy of the Laser Displacement Sensor was less than 10 μm. After the experimental verification, this method makes full use of optical non-contact measurement fast speed, high precision and wide measuring range of features. Using a standard gauge block as a measurement reference, the coordinate system conversion data is simple and practical. It not only improves the measurement accuracy of the blade surface, but also its measurement efficiency. Therefore, this method increases the value of the measurement of complex surfaces.http://www.mdpi.com/1424-8220/15/6/12782bladelaser displacement sensorfreeform surfaceerror compensationfour-coordinate measuring system |
spellingShingle | Bin Sun Bing Li A Rapid Method to Achieve Aero-Engine Blade Form Detection Sensors blade laser displacement sensor freeform surface error compensation four-coordinate measuring system |
title | A Rapid Method to Achieve Aero-Engine Blade Form Detection |
title_full | A Rapid Method to Achieve Aero-Engine Blade Form Detection |
title_fullStr | A Rapid Method to Achieve Aero-Engine Blade Form Detection |
title_full_unstemmed | A Rapid Method to Achieve Aero-Engine Blade Form Detection |
title_short | A Rapid Method to Achieve Aero-Engine Blade Form Detection |
title_sort | rapid method to achieve aero engine blade form detection |
topic | blade laser displacement sensor freeform surface error compensation four-coordinate measuring system |
url | http://www.mdpi.com/1424-8220/15/6/12782 |
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