|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/3907 ; 60/3929|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 7 인용 특허 : 0|
An air supply system having a combustor whose output drives a turbine. The turbine drives a compressor part of whose output is fed to the combustor. A portion of the compressor output is bled off for utility usage. Instead of varying the fuel rate to the combustor to match varying demand in utility usage, the fuel rate is fixed. Operation of the system at air flows above and below that corresponding to the fixed fuel rate is accommodated by (1) a poppet relief valve which opens at high pressures and (2) a butterfly valve in the bleed (utility) line which...
An air supply system including an air compressor coupled to and rotatably driven by a turbine, a combustor whose gaseous output is coupled to and drives the turbine, the compressor feeding an output line to the input of the combustor, a bleed line leading from the compressor output line, the bleed line adapted to feed compressed air to an external system requiring a pressurized air supply, a fuel line coupled to and adapted to supply a constant rate of fuel for burning to the combustor, the improvement comprising, a first valve, said first valve being a ...