In this thesis will be presented an algorithm to analyze the surface of jet engine blades. The purpose of the algorithm is to locate damages and imperfections on the blade and to classify them. In particular, impact caused by foreign object damages, or FODs for brevity, will be distinguished by other forms of damages, like corrosion
The article presents a multi-stage algorithm for automatic (without any human, user – diagnostician ...
This research focuses on the automation of blade inspection, using different Computer Vision (CV) ap...
Evidences suggest that the damages observed on the stator vanes as well as rotor blades of LP compre...
Aircraft gas turbine engines during the operation are exposed to damage of flowing parts. The elemen...
Findings of the analysis of damaged compressor blades (Sl. Nos. 6, 12 and 20) of an aero engine are ...
Damages on the airfoil surface of compressor blades of an aircraft were analyzed. Analysis shows tha...
Findings of the analysis of a damaged first stage LP compressor rotor blade belonging to a SU-30 MKI...
Four damaged compressor blades belonging to the aero engine of an aeroengine were analyzed. Analysis...
Two Foreign Object damaged (FOD) Ist stage compressor blades from an aircraft were analyzed. FOD occ...
Four fan stator blades and three compressor rotor blades belonging to an aeroengine were sent to thi...
The nature of damages observed on the compressor and the gas generator blades suggests that they wer...
Damage to the compressor blades of turbojet engines due to ingestion of foreign objects is a growing...
One 1st stage compressor blade and two turbine blades with suspected FOD were sent to the laboratory...
Evidences show that the damages on the airfoil were caused due to foreign object impact on the conca...
Three I stage compressor rotor blades belonging to an aeroengine were forwarded to the laboratory fo...
The article presents a multi-stage algorithm for automatic (without any human, user – diagnostician ...
This research focuses on the automation of blade inspection, using different Computer Vision (CV) ap...
Evidences suggest that the damages observed on the stator vanes as well as rotor blades of LP compre...
Aircraft gas turbine engines during the operation are exposed to damage of flowing parts. The elemen...
Findings of the analysis of damaged compressor blades (Sl. Nos. 6, 12 and 20) of an aero engine are ...
Damages on the airfoil surface of compressor blades of an aircraft were analyzed. Analysis shows tha...
Findings of the analysis of a damaged first stage LP compressor rotor blade belonging to a SU-30 MKI...
Four damaged compressor blades belonging to the aero engine of an aeroengine were analyzed. Analysis...
Two Foreign Object damaged (FOD) Ist stage compressor blades from an aircraft were analyzed. FOD occ...
Four fan stator blades and three compressor rotor blades belonging to an aeroengine were sent to thi...
The nature of damages observed on the compressor and the gas generator blades suggests that they wer...
Damage to the compressor blades of turbojet engines due to ingestion of foreign objects is a growing...
One 1st stage compressor blade and two turbine blades with suspected FOD were sent to the laboratory...
Evidences show that the damages on the airfoil were caused due to foreign object impact on the conca...
Three I stage compressor rotor blades belonging to an aeroengine were forwarded to the laboratory fo...
The article presents a multi-stage algorithm for automatic (without any human, user – diagnostician ...
This research focuses on the automation of blade inspection, using different Computer Vision (CV) ap...
Evidences suggest that the damages observed on the stator vanes as well as rotor blades of LP compre...