Fuel heating system for gas turbine engine

Power plants – Combustion products used as motive fluid – With lubricators

Patent

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Details

60736, F02C 706

Patent

active

043543456

ABSTRACT:
To accommodate fuel having higher freezing points the continuous bypass flow of fuel from the fuel control is selectively diverted to pick up the rejected heat from the engine's lubrication system to heat the fuel in the aircraft fuel tank.

REFERENCES:
patent: 2865580 (1958-12-01), Marshall
patent: 3080716 (1963-03-01), Cummings et al.
patent: 3300965 (1967-01-01), Sherlaw et al.
patent: 3779007 (1973-12-01), Lavash
patent: 4041697 (1977-08-01), Coffinberry et al.
patent: 4104873 (1978-08-01), Coffinberry

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