MC Hannum, TF Robertson, JN Newby… - US Patent …, 2010 - Google Patents
A submerged combustion vaporizer may include a premix burner with multiple integral mixers for forming premix and discharging the premix into the duct system that …
(57) ABSTRACT A burner is disclosed which includes a vortex generator for a combustion air stream, means for the admission of fuel into the combustion air stream and air inlet ducts …
J Hellat, J Hoffmann - US Patent 9,249,689, 2016 - Google Patents
Baden (CH) 6,202,400 B1 3/2001 Utamura et al. 6.256, 976 B1* 7/2001 Kataoka et al.................. 60,775 (*) Notice: Subject to any disclaimer, the term of this 6,269,624 B1 8 …
ML Joshi, AG Slavejkov, XJ Li - US Patent 7,303,388, 2007 - Google Patents
Combustion system comprising a furnace having a thermal load and a combustion atmosphere disposed therein; one or more fuel lances adapted to inject fuel into the …
KK Venkataraman, WK Hessler, P Popovic - US Patent 8,028,529, 2011 - Google Patents
A gas turbine combustor including: a primary combustion chamber; a secondary combustion chamber downstream of the primary combustion chamber; a venturi having a venturi throat; …
J Hong, JW Wheeler - US Patent App. 13/855,343, 2013 - Google Patents
(57) ABSTRACT A method and apparatus for a burner adapted to heata furnace or other environment of use. In particular, a burner for pro viding a fuel gas in combination with an …
TB Neville, JJ Nowakowski, MC Hannum… - US Patent …, 2008 - Google Patents
A burner has a port facing into a combustion chamber along an axis. A secondary fuel injector structure has secondary fuel injection ports that face into the combustion chamber at …
WR Laster, SM Martin, JEP Bilbao, J Hardes… - US Patent …, 2018 - Google Patents
A secondary fuel stage (14) of a combustor of a gas turbine engine. The combustor has a main combustion zone (43) upstream of the secondary fuel stage to ignite working gas The …
A Eroglu - US Patent 8,033,821, 2011 - Google Patents
BACKGROUND Burners for combusting liquid and/or gaseous fuels, espe cially for use in a gas turbine, are known, which on the one hand have a high stability during operation, and …