2014
DOI: 10.1115/1.4027719
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Algorithm to Construct Line-Shaped Feature Point Clouds of Single-Value Ruled Blades for Gas Turbines

Abstract: A lg o rith m to C onstruct L in e -S h a p e d F e a tu re P o in t C louds of S in g le -V a lu e R u le d B la d e s fo r G as T u rb in e sUsing the geometric features of surfaces, we proposed an algorithm to construct line shaped feature point clouds for the reverse design of a blade surface. Blade surfaces in the gas turbines field require high accuracy and have complex shapes. By quickly recog nizing the border of the scattered point clouds of blades, the back-project method was used to extract the rule… Show more

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Cited by 7 publications
(2 citation statements)
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“…Researchers consider this technology from different engineering perspectives, such as system structure optimization [8], working fluid screening [9], and control strategy optimization [10]. A variety of turbines, such as the radial flow [11], blade [12], and axial flow turbines [13], have been used as organic expanders in ORC systems. However, these expanders have been found to be inefficient due to significant flow losses and high operating speeds [14].…”
Section: Introductionmentioning
confidence: 99%
“…Researchers consider this technology from different engineering perspectives, such as system structure optimization [8], working fluid screening [9], and control strategy optimization [10]. A variety of turbines, such as the radial flow [11], blade [12], and axial flow turbines [13], have been used as organic expanders in ORC systems. However, these expanders have been found to be inefficient due to significant flow losses and high operating speeds [14].…”
Section: Introductionmentioning
confidence: 99%
“…With increasing applications of turbomachinery in various industrial fields, the requirement for multi-objective design methods, such as thermal efficiency, aerodynamic performance and structural life, has considerably increased in the last few decades [ 1 , 2 , 3 ]. As one of the key constraints in blade design, the blade tip clearance (BTC) changes in a complicated manner under various working statuses of rotors.…”
Section: Introductionmentioning
confidence: 99%