Gasturbinenmotor mit Wasserrückgewinnungssystem
Anmelder: PRATT & WHITNEY CANADA CORP. 🇨🇦
Details
- Veröffentlichungs-Nr.
- EP4477856
- Aktenzeichen
- EP24182412
- Anmeldetag
- 14. Juni 2024
- Veröffentlichung
- 19. März 2025
- Rechtsraum
- EP
- IPC
- F02C3/22F02C3/30F02C6/20F02C7/143F02C7/22F02C7/224
Abstract
An engine system (10) is provided that includes an open propulsor rotor (12), an engine core assembly (14), a bypass flowpath (48) and a condenser (118). The engine core assembly (14) is configured to drive rotation of the open propulsor rotor (12). The engine core assembly (14) includes a core flowpath (30), a compressor section (26), a combustor section (27) and a turbine section (28). The core flowpath (30) extends through the compressor section (26), the combustor section (27) and the turbine section (28) from an inlet (38) into the core flowpath (30) to an exhaust (40) from the core flowpath (30). The bypass flowpath (48) bypasses the engine core assembly (14). The condenser (118) is configured to exchange heat energy between combustion products flowing within the core flowpath (30) downstream of the combustor section (27) and bypass air flowing within the bypass flowpath (48).
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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