|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||600/392.3 ; 600/392.9|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 78 인용 특허 : 2|
Systems for controlling the combustion air to be used with a gas turbine engine for control the products of combustion and reducing emissions emitted therefrom have been used in the past. The present system includes a compressed air plenum being divided into a combustion air supply portion and a dilution or cooling air supply portion. A variable geometry system is positioned between the compressor section and the compressed air plenum. The variable geometry system is movably between an open position and a closed position. Movement of the variable geometr...
[ What is claimed is:] [1.] A gas turbine engine having a compressor section establishing a flow of compressed air, a source of fuel and a combustion section; said gas turbine engine comprising: a fuel injector, a compressed air plenum being divided into a combustion air supply portion and a dilution or cooling air supply portion; a variable geometry system that includes a control mechanism being connected to a divider mechanism having a plurality of holes or openings positioned therein, said system being positioned between said compressor section and sa...