Liquid turbojet engine

Power plants – Reaction motor – Motive fluid principally liquid

Patent

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Details

60 3935, 60 3957, 440 45, 123 19, B63H 1100, F02C 330

Patent

active

048979953

ABSTRACT:
A liquid turbojet engine includes an elongated shaft, a housing mounted about the shaft with the shaft being rotatable relative to the housing about the shaft longitudinal axis, a conduit fixed to the shaft within the housing filled with an inert motive liquid and nozzles for inducing combustible gas bubbles in the motive liquid. The conduit has a compression section extending generally radially from the shaft, a combustion section extending generally axially and parallel to the shaft and from the compression section at a radial distance from the shaft, and an expansion section extending generally radially relative to the shaft axis from an end of the combustion section remote from the compression section. The bubble nozzles are located at the inlet of the compression section. The motive liquid enters through an inlet in the housing. The burned bubbles are discharged with the motive liquid through an exit nozzle in the housing.

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