Optical Measurement of Unducted Fan Blade DeflectionsSource: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 004::page 751Author:A. P. Kurkov
DOI: 10.1115/1.2927718Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A nonintrusive optical method for measuring unducted fan (or propeller) blade deflections is described and evaluated. The measurement does not depend on blade surface reflectivity. Deflection of a point at the leading edge and a point at the trailing edge in a plane nearly perpendicular to the pitch axis is obtained with a single light beam generated by a low-power, helium-neon laser. Quantitative analyses are performed from taped signals on a digital computer. Averaging techniques are employed to reduce random errors. Measured static deflections from a series of high-speed wind tunnel tests of a counterrotating unducted fan model are compared with available predicted deflections, which also are used to evaluate systematic errors.
keyword(s): Optical measurement , Blades , Deflection , Errors , Propellers , Signals , Wind tunnels , Helium-neon lasers , Reflectance AND Computers ,
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contributor author | A. P. Kurkov | |
date accessioned | 2017-05-08T23:34:01Z | |
date available | 2017-05-08T23:34:01Z | |
date copyright | October, 1990 | |
date issued | 1990 | |
identifier issn | 0889-504X | |
identifier other | JOTUEI-28606#751_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/107702 | |
description abstract | A nonintrusive optical method for measuring unducted fan (or propeller) blade deflections is described and evaluated. The measurement does not depend on blade surface reflectivity. Deflection of a point at the leading edge and a point at the trailing edge in a plane nearly perpendicular to the pitch axis is obtained with a single light beam generated by a low-power, helium-neon laser. Quantitative analyses are performed from taped signals on a digital computer. Averaging techniques are employed to reduce random errors. Measured static deflections from a series of high-speed wind tunnel tests of a counterrotating unducted fan model are compared with available predicted deflections, which also are used to evaluate systematic errors. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Optical Measurement of Unducted Fan Blade Deflections | |
type | Journal Paper | |
journal volume | 112 | |
journal issue | 4 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.2927718 | |
journal fristpage | 751 | |
journal lastpage | 758 | |
identifier eissn | 1528-8900 | |
keywords | Optical measurement | |
keywords | Blades | |
keywords | Deflection | |
keywords | Errors | |
keywords | Propellers | |
keywords | Signals | |
keywords | Wind tunnels | |
keywords | Helium-neon lasers | |
keywords | Reflectance AND Computers | |
tree | Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 004 | |
contenttype | Fulltext |