|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/3923 ; ; 60/727|
|발명자 / 주소|
|인용정보||피인용 횟수 : 14 인용 특허 : 41|
An annular combustor system is disclosed in use with a radial turbine-type gas turbine gas generator, the system having an annular housing defining a single stage combustor, an external fuel/air premixer system having a mixing chamber and a fuel valve under the control of a controller, to provide a preselected lean fuel/air ratio mixture for introduction to the combustion zone of the annular housing. A separate compressed air valve under the control of the controller can optionally be included. Compressed air conduits are used to channel a portion of the...
A combustor system for operation with a source of compressed air and a source of fuel, the combustor system comprising: a cylindrical housing defining a single stage combustion chamber, said housing having an axis; at least one fuel/air premixer disposed outside said cylindrical housing; a first conduit interconnecting the source of compressed air and said premixer; a second conduit interconnecting the fuel supply and said premixer; and a fuel valve for determining the fuel flow rate to said premixer through said second conduit, wherein said premixer inc...