Doppeldichtungsanordnung
Anmelder: PRATT & WHITNEY CANADA CORP. 🇨🇦
Details
- Veröffentlichungs-Nr.
- EP4467859
- Aktenzeichen
- EP24177264
- Anmeldetag
- 22. Mai 2024
- Veröffentlichung
- 27. November 2024
- Rechtsraum
- EP
- IPC
- F16L19/025F16L23/16F16L41/08
Abstract
A tube assembly (10) comprises a tube (12) having a tube flange (18) securable to an associated mounting surface (20) of a turbine engine component (14). A first seal (30) is provided at the bore interface between the tube (12) and a fluid port (34) of the engine component (14). A second seal (32) is provided at the flange interface between the tube flange (18) and the tube mounting surface (20) of the engine component (14). The second seal (32) includes a gasket having a sheet metal body (38) with corrugations (46a, 46b) projecting from the tube facing side (40) of the gasket. Tabs (52) are distributed along a periphery of the gasket for resiliently holding the gasket on the tube flange (18) with the tube facing side (40) of the gasket facing the tube flange (18).
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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