System und Verfahren zur Steuerung eines Gasturbinenmotors
Anmelder: United Technologies Corporation 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP3045982
- Aktenzeichen
- EP16151977
- Anmeldetag
- 19. Januar 2016
- Veröffentlichung
- 7. November 2018
- Erteilung
- 7. November 2018
- Rechtsraum
- EP
- IPC
- F01D17/06F01D17/10F01D21/00G05B13/04
Abstract
A control system for a gas turbine engine including a power turbine is disclosed. The control system may include a control module to receive engine operating goals and an estimated current engine state, wherein the estimated current engine state is produced by a model-based estimation module using a bandwidth signal produced by an adaptation logic module. The control module is operative to determine fuel flow, inlet guide vane schedules and stability bleed schedules based at least in part on the received engine operating goals and the estimated current engine state, and to send signals to a gas generator of the gas turbine engine in order to control the gas generator according to the determined fuel flow, inlet guide vane schedules and stability bleed schedules.
Anmelder
- Firma
- United Technologies Corporation
- Land
- 🇺🇸 USA
US-amerikanischer Luft- und Raumfahrt- sowie Verteidigungskonzern, entstanden aus Raytheon und United Technologies. Entwickelt und fertigt Triebwerke, Avionik, Radarsysteme, Raketen- und Verteidigungstechnik für zivile und militärische Kunden.
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