Erosionsbestimmung für Turbomaschinenschaufel
Anmelder: General Electric Company 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP2871459
- Aktenzeichen
- EP14192560
- Anmeldetag
- 10. November 2014
- Veröffentlichung
- 12. April 2017
- Erteilung
- 12. April 2017
- Rechtsraum
- EP
- IPC
- G01M5/00G01B11/24F01D21/00
Abstract
A system (100) may include at least one computer device (104) configured to attain a two-dimensional used profile of a leading edge at a specified radial position on a turbomachine airfoil after use. The system (100) aligns opposing substantially straight alignment portions of the two-dimensional used profile with opposing substantially straight alignment portions of a previously attained, two-dimensional, baseline profile of the turbomachine airfoil. The alignment portions of each profile are in substantially identical radial locations of the turbomachine airfoil. Comparing the used profile to the baseline profile determines whether the leading edge at the specified radial position of the used turbomachine airfoil has erosion. The system may also include a laser profiler (130) for measuring the turbomachine airfoil (132).
Anmelder
- Firma
- General Electric Company
- Land
- 🇺🇸 USA
US-amerikanischer Technologiekonzern mit Sitz in Massachusetts. Historisch aktiv in Energieerzeugung, Luftfahrttriebwerken, Medizintechnik und Industrietechnik über verschiedene Geschäftsbereiche.
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