| 摘要 |
#CMT# #/CMT# The engine (1) has a combustion chamber (4) formed with a cylinder (2) for igniting a fuel. A supply line (6) supplies the fuel to the chamber. A discharge line discharges combustion gas from the chamber. A control device (12) controls the supply of the fuel into the chamber. A supply line (8) is separated from the supply line (6) to supply fluid e.g. water, to the chamber besides the fuel. A pump (18) is provided to convey the fluid towards the chamber, where the fluid is selected from fat or oil. A piston (3) is movable opposite to the chamber. #CMT# : #/CMT# An independent claim is also included for a method for operating an internal combustion engine. #CMT#USE : #/CMT# Internal combustion engine e.g. petrol engine and jet engine (all claimed) in an airplane e.g. airliner. Can also be used for a diesel engine, rape oil engine, drive nozzle and turbine. #CMT#ADVANTAGE : #/CMT# The supply line is separated from another supply line to supply the fluid to the chamber besides the fuel, thus increasing the efficiency of the engine, while reducing weight and fuel consumption. #CMT#DESCRIPTION OF DRAWINGS : #/CMT# The drawing shows a schematic view of an internal-combustion engine in form of a petrol engine. 1 : Internal combustion engine 2 : Cylinder 3 : Piston 4 : Combustion chamber 6, 8 : Supply lines 12 : Control device 18 : Pump. |
