Flugzeugmotorsteuerung mit vereister Temperatursonde
Anmelder: Pratt & Whitney Canada Corp. 🇨🇦
Details
- Veröffentlichungs-Nr.
- EP2412952
- Aktenzeichen
- EP11176212
- Anmeldetag
- 1. August 2011
- Veröffentlichung
- 10. Oktober 2018
- Erteilung
- 10. Oktober 2018
- Rechtsraum
- EP
- IPC
- F02C7/047F01D25/02F02C9/28B64D15/12B64D15/20G01K13/02
Abstract
Methods for controlling an aircraft turbofan engine during icing of a temperature probe and devices for carrying out such methods are described. The methods may comprise: using (46) one or more signals representative of temperature received from a heated temperature probe to generate one or more control signals for use in controlling the engine; determining (44) that an icing condition associated with the probe exists; and using (48) data representing one or more substitute signals in place of signals representative of temperature received from the heated temperature probe to generate the one or more control signals for use in controlling the engine.
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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