|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/3902 ; 60/3908 ; 60/3983 ; 60/2261|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 57 인용 특허 : 3|
Heat transfer systems for maintaining a thermal balance between a gas turbine engine and heat generating accessory components of the engine are disclosed. In the embodiment illustrated, heat is removed from the cooling system 48 of an electrical generator 46 and is transferred to the fuel supply system 32 of the engine. In one detailed embodiment, the cooling system 48 is in direct heat transfer communication with the downstream portion 62 of the fuel supply system through a heat exchanger 76 and in indirect heat transfer communication with the upstream ...
A method for maintaining a thermal balance in a gas turbine engine operating at variable operating conditions which has a combustion section for burning a first portion of fuel to produce power and which has, a fuel system to supply fuel, the fuel system having a fuel at a temperature which is lower than the freezing point of water under certain operating conditions, wherein a fuel control having an inlet and an outlet for fuel is used to control the flow of fuel in the fuel system and wherein a generator for producing electrical power is driven by the e...