Invention Grant
US09097169B2 Gas turbine engine heat management system 有权
燃气轮机发动机热管理系统

Gas turbine engine heat management system
Abstract:
A heat management system of a gas turbine engine for cooling oil and heating fuel, includes an oil circuit having parallel connected first and second branches. The first branch includes a fuel/oil heat exchanger and a first fixed restrictor in series and the second branch includes an air cooled oil cooler and a second fixed restrictor. The first and second fixed restrictors limit respective oil flows through the first and second branch differently, in response to viscosity changes of the oil caused by temperature changes of the oil during engine operation to modify oil distribution between the first and second branches.
Public/Granted literature
Information query
Patent Agency Ranking
0/0