About 27 results
https://drivepatents.com/patents/1395433 · 21 Jan 2026
La présente invention concerne un procédé de détection d'une ingestion de gaz chauds au sein d'un aéronef (1) ayant au moins une entrée d'air (20) configurée pour alimenter en air frais au moins un moteur (15). Le procédé comporte (i) une mesure d...
https://drivepatents.com/patents/1390611 · 17 Sep 2025
A combustion assembly (68) for a gas turbine engine (20) includes a combustor (40), a monochromator (128), and a photodetector assembly (122). The combustor (40) forms a combustion chamber (98). The monochromator (128) is disposed outside the combustion ch...
https://drivepatents.com/patents/974003 · 4 Jun 2014
It is described a method of controlling a supply of a fuel to a combustor of a gas turbine comprising a compressor upstream of the combustor, the method comprising: supplying the fuel (105) to the combustor (101); obtaining an inlet air pressure (PT7) at a...
https://drivepatents.com/patents/973996 · 4 Jun 2014
It is described a method of controlling a supply of a fuel (105) to a combustor (101) of a gas turbine comprising a compressor upstream of the combustor, the method comprising: supplying the fuel (105) to the combustor (101); obtaining a property value of ...
https://drivepatents.com/patents/974619 · 21 May 2014
A system for reducing modal coupling of combustion dynamics includes a plurality of combustors (42), and at least one fuel injector (66) in each of the plurality of combustors (42). The system also includes structure for dithering a combustion instability ...
https://drivepatents.com/patents/990761 · 15 May 2013
The system (10) has two electronic control units (32, 34) for redundant controlling of an engine (12) of an aircraft. A selection unit (38) selects one of the electronic control units for controlling the engine of the aircraft. The selection unit comprises...
https://drivepatents.com/patents/985346 · 27 Mar 2013
Concepts and technologies are disclosed herein for a sensor system for detecting, characterizing, monitoring, and analyzing data. According to some embodiments disclosed herein, a monitoring system is configured to obtain data from a sensor system. The sen...
https://drivepatents.com/patents/999293 · 15 Aug 2012
The method involves measuring measurement signal values at first and second time points, where the first time point lies before the second time point. Attenuated signal values are generated from the measurement signal values that are subjected to a smoothi...
https://drivepatents.com/patents/1002799 · 2 May 2012
The method involves forming derivation of hot gas temperature at different areas of a gas turbine (10) over pressure measurements by pressure sensors (P1-P3). The pressure measurements are executed in a hot gas flow produced in a combustion chamber (13) of...
https://drivepatents.com/patents/1003273 · 18 Apr 2012
It is described a combustion device control unit and a combustion device, e.g. a gas turbine, which determine on the basis of at least one operating parameter whether the combustion device is in a predefined operating stage. In response hereto, there is ge...