Steuerung eines Gasturbinenmotors
Anmelder: Rolls-Royce plc 🇬🇧
Details
- Veröffentlichungs-Nr.
- EP2937522
- Aktenzeichen
- EP15163815
- Anmeldetag
- 16. April 2015
- Veröffentlichung
- 17. März 2021
- Erteilung
- 17. März 2021
- Rechtsraum
- EP
- IPC
- F01D17/16F02C9/20F02C9/54
Abstract
A method of controlling a gas turbine engine (10) which has a booster compressor (13), a core compressor, combustion equipment, a core turbine, and a low-pressure turbine (18). The low-pressure turbine also drives an external load having a defined speed characteristic. The booster compressor (13) has one or more rows of variable stator vanes. The method includes: scheduling variation in the angle of the variable stator vanes as a function of the speed of the booster compressor such that the vanes open as the booster compressor speed increases; measuring or setting one or more operational parameters which are determinative of the temperature at entry to the core turbine; and biasing the scheduling of the angle variation of the variable stator vanes as a function of the operational parameter(s) to reduce variation in temperature at entry to the core turbine
Anmelder
- Firma
- Rolls-Royce plc
- Land
- 🇬🇧 Großbritannien
Britisches Unternehmen mit Sitz in Derby, das Flugzeugtriebwerke sowie Antriebssysteme für Luftfahrt, Marine und Energieerzeugung entwickelt und herstellt.
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