Flansch mit Gewellten Rändern für Zweireihige Statoranordnung eines Gasturbinenmotors
Anmelder: Pratt & Whitney Canada Corp. 🇨🇦
Details
- Veröffentlichungs-Nr.
- EP4779123
- Anmeldetag
- 20. Januar 2026
- Veröffentlichung
- 22. Juli 2026
- Rechtsraum
- EP
- IPC
- F01D5/14, F01D9/04
Abstract
A double row stator assembly (200) for a gas turbine engine (100) includes a first vane row stator assembly (202) that includes a plurality of first-row vanes, a second vane row stator assembly (204) that includes a plurality of second-row vanes, and a wavy-edged flange (206) configured to secure the first vane row stator assembly to the second vane row stator assembly when the first vane row stator assembly and second vane row stator assembly are assembled to form the double row stator assembly. The second vane row stator assembly is configured to be positioned to be sequentially downstream of the first vane row stator assembly when the first vane row stator assembly and the vane row second stator assembly are assembled to form the double row stator assembly such that trailing edges (202c) of the first-row vanes (202a) overlap leading edges (204b) of the second-row vanes (204a).
Anmelder
- Firma
- Pratt & Whitney Canada Corp.
- Land
- 🇨🇦 Kanada
Kanadische Tochtergesellschaft von Pratt & Whitney mit Sitz in Longueuil, Québec. Entwickelt und fertigt Flugzeugtriebwerke für kleinere Verkehrsflugzeuge, Geschäftsflugzeuge und Hubschrauber.
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