A turbine engine (10) having a compressor section (12), a combustion section (14) and a turbine section (16) in serial flow arrangement. The turbine engine (10) further having a combustor (80), provided within the combustion section (14), defining a combus...

A fluid flow system includes a main valve having a spool (38), a first chamber (37, 137), and a second chamber (34, 134). A pressure difference between the first chamber (37, 137) and the second chamber (34, 134) is configured to move the spool (38) to con...

The invention relates to a surge control method for a gas turbine engine (10). The method includes providing a gas turbine engine (10) having a compressor (20), a combustor (30), downstream of the compressor (20), with a hot gas path, a turbine (40) downst...

The present invention discloses a combustion apparatus 100, which comprises a first device 10 for mixing a fuel with an oxidant, a combustion chamber 12 in which combustion of the fuel/oxidant mix takes place, a pre-chamber 14 located between the first dev...

Power generation system, at least arranged for recovering energy from blast furnace gas, the system comprising at least one gas turbine (GT), at least one heat recovery steam generator (HRSG), and at least one steam turbine (ST), wherein said gas turbine (...

A method and apparatus for the liquefaction of natural gas are described. For reliable operation of the compressors present in natural gas liquefaction plants, it is proposed to obtain the energy for driving the compressors from the combustion of a portion...