Jet propulsion engines
OwnerAlfred C. Craiginventor
Life of this patent
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Abstract
A jet propulsion engine such as a gas turbine engine has an air compressor for supplying compressed air to the engine compressor stages. The air compressor is controllably and selectively driven by way of a disconnectable drive connection between the air compressor and a freely rotatable fan which is arranged in front of the air compressor and which in operation is rotated by the flow of intake air into the engine. A by-pass duct permits a part of the intake air to be by-passed around the air compressor and passed in variable proportions either to the engine compressor stages or directly out of a by-pass duct outlet.
Claims2
A jet propulsion engine comprising an air intake casing, a fan rotatable in the air intake casing, a main casing, an air compressor in the main casing, compressor means in the main casing rearwardly of the air compressor, a first disconnectable drive coupling between the fan and the air compressor, for the selective controllable driving of the air compressor by the fan, a second disconnectable drive coupling between the air compressor and the compressor means, for the selective controllable driving of the compressor means by the air compressor, a by-pass duct means having a rearwardly directed outlet and an aperture communicating with the compressor means, and valve means for varying the degree of opening of the outlet and the aperture whereby the proportion of the intake air flow passing from the fan to the compressor means and the proportion of the intake air flow passing from the fan through the by-pass duct means and out of the outlet is controllably varied inversely relative to each other.
Dependencies are inferred from the claim text.