Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Vaishakhi Nandi"'
Publikováno v:
Journal of Failure Analysis and Prevention. 18:465-470
Failure of high-pressure compressor rotor blade in an aero gas turbine engine is analyzed to determine its root cause. Forensic and metallurgical investigations are carried out on the blade and failed parts. The failure of the platform ladder is foun
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c4a1762f7fe64c6781c21c8148fa4342
https://doi.org/10.1007/s11668-018-0425-5
https://doi.org/10.1007/s11668-018-0425-5
Publikováno v:
Engineering Failure Analysis. 79:836-844
Failure of an un-cooled turbine blade in an aero gas turbine engine is analyzed to determine its root cause. The operational condition of the engine was studied and metallurgical investigations are carried out on the fractured blade. The failure has
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f13b2e99610b186f76a9b66351256075
https://doi.org/10.1016/j.engfailanal.2017.05.042
https://doi.org/10.1016/j.engfailanal.2017.05.042
Publikováno v:
Journal of Failure Analysis and Prevention. 15:25-32
An aero gas turbine engine is investigated for foreign object damage. Extensive damage in the low pressure compressor and abnormal noise forced the engine to shut down. Metallic screw type foreign object debris was retrieved from air intake fairing.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c27d45a1b2c8474aa2a6561db6b1a204
https://doi.org/10.1007/s11668-014-9914-3
https://doi.org/10.1007/s11668-014-9914-3
Publikováno v:
Journal of Failure Analysis and Prevention. 14:578-587
Failure of low pressure turbine nozzle guide vane (NGV) in an aero gas turbine engine is analyzed to determine its root cause. Forensic and metallurgical investigations are carried out on the NGV failed as well as the failed components of the downstr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6e6982f775fa394d3515f64406f68732
https://doi.org/10.1007/s11668-014-9858-7
https://doi.org/10.1007/s11668-014-9858-7
Publikováno v:
International Journal of Turbo & Jet-Engines. 34
Failure of a high pressure (HP) turbine blade in a military turbofan engine is investigated to determine the root cause of failure. Forensic and metallurgical investigations are carried out on the affected blades. The loss of coating and the presence
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7bf9ef91cfe298a5a5d641f6def76e10
https://doi.org/10.1515/tjj-2015-0049
https://doi.org/10.1515/tjj-2015-0049
Publikováno v:
Journal of Failure Analysis & Prevention; Apr2018, Vol. 18 Issue 2, p233-240, 8p
Publikováno v:
Journal of Failure Analysis & Prevention; Apr2014, Vol. 14 Issue 2, p160-166, 7p
Publikováno v:
Journal of Failure Analysis & Prevention; Jun2013, Vol. 13 Issue 3, p274-281, 8p