System und Verfahren zum Betrieb eines Mehrmotorsystems
Anmelder: Pratt & Whitney Canada Corp. 🇨🇦
Details
- Veröffentlichungs-Nr.
- EP4775825
- Anmeldetag
- 2. Dezember 2022
- Veröffentlichung
- 15. Juli 2026
- Rechtsraum
- EP
- IPC
- F02C9/42
Abstract
A method of operating a multi-engine system of an helicopter includes the multi-engine system having a first turboshaft engine having a first shaft, a second turboshaft engine having a second shaft, a gearbox having a clutch system (152), and a range of rotation speeds defined as a placarded zone. The method includes: rotating the first and second shafts at a first idle rotation speed (NL<LI>) below the placarded zone when clutched to a load; increasing a rotation speed of the first shaft from the first idle rotation speed (NL<LI>) to a flight rotation speed (NL<F>) above the placarded zone; unclutching the second shaft from the load during the increasing; and increasing a rotation speed of the second shaft to a second idle rotation speed (NL<HI>) when the second shaft is unclutched from the load, the second idle rotation speed (NL<HI>) above the placarded zone and below the flight rotation speed (NL<F>).
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.
2.216 Patente in unserer Datenbank