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|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/3908 ; 165/41|
|§371/§102 date||19930618 (19930618)|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 35 인용 특허 : 0|
A gas turbine engine heat exchange apparatus comprises a first heat exchanger (12), which is arranged to receive oil from a lubricating oil system of the engine and put the oil in heat exchange with either a cooling or heating medium (17, 21), and a second heat exchanger (26), which receives the oil from the first heat exchanger, puts the oil in heat exchange with fuel in the engine\s fuel supply system and discharges the oil back to the lubricating oil system. A valve or valves (20, 24) are used to control flow from high and low temperature sources of t...
A heat exchange apparatus for a combustion engine having a lubrication oil system and a fuel supply system, comprising a first heat exchanger receiving oil from the lubrication oil system to put the oil in heat exchange relationship with a heat exchange medium, a second heat exchanger receiving the oil from the first heat exchanger, and placing the oil in heat exchange relationship with fuel in the fuel system and returning the engine oil to the engine, high and low temperature sources for said heat-exchange medium, and valve means for controlling flow f...