Dämpfender Stift für Turbinenschaufel und Zugehöriges Turbinenkraftwerk
Anmelder: General Electric Company 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP3138999
- Aktenzeichen
- EP16183857
- Anmeldetag
- 11. August 2016
- Veröffentlichung
- 9. November 2022
- Erteilung
- 9. November 2022
- Rechtsraum
- EP
- IPC
- F01D5/22
Abstract
A damper pin 100 for damping adjacent turbine blades 28 coupled to a rotor shaft 24 includes an elongated body 102 having a center portion 104 disposed between a first end portion 106 and a second end portion 108. The first end portion 106, center portion 104 and second end portion 108 define a generally arcuate top portion 110 of the elongated body 102 that is configured to contact with a groove 48 defined between the adjacent turbine blades 28. The elongated body 102 includes a first side portion 112 laterally opposed to a second side portion 114 and defines a plurality of laterally extending slots 116. The slots 116 are axially spaced along the center portion 104 and each slot 116 extends at least partially through at least one of the first side portion 112 or the second side portion 114.
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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Fachgebiete
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