Turbojet powerplant with heat exchanger

Details Turbojet powerplant with heat exchanger Turbojet powerplant with heat exchanger

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 3/00 (2006.01) F01D 5/14 (2006.01) F01D 5/18 (2006.01) F01D 9/06 (2006.01) F01D 25/10 (2006.01) F02C 7/08 (2006.01)

Patent

CA 2349994

Turbojet powerplant with at least one compressor (1), at least one combustion chamber (2), a high-pressure turbine (3) and a low-pressure turbine (4), characterised in that a heat exchanger (5) is arranged between the compressor (1) and the combustion chamber (2), in that at least one hot-gas line (6) branches off from an area downstream of the high-pressure turbine (3) and is connected to the heat exchanger (5), and in that at least one cold-gas line (7) connects the heat exchanger (5) with an area upstream of the low-pressure turbine (4).

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