|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 4 인용 특허 : 2|
A combustor system for use with a turbocharged combustion engine comprises a combustor connected for continuous passage of engine exhaust gases. The combustor system includes a relatively low pressure fuel injection system for atomizing fuel for combustion in a substantially vitiated atmosphere, a fuel control system for supplying fuel to the combustor in response to engine operating conditions, and a heat exchanger for preheating compressed bypass air prior to supply thereof to the combustor.
In an internal combustion engine having a turbocharger turbine driven by exhaust gases to drive a turbocharger compressor to provide compressed charge air to the engine, a combustor system comprising a combustor coupled between the engine and the turbocharger for in-line passage of engine exhaust gases; means for controllably supplying fuel to the combustor to permit combustor operation with sustained combustion of the fuel to supplement the energy level of gases passing through the combustor; means for selectively and intermittently bypassing a portion ...