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Patent

V/stol aircraft-by-pass engine having a double, thrust diverter valve assembly

E Stevens
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TLDR
In this paper, a double, thrust diverter valve assembly for a bypass engine applicable to the VTOL and V/STOL types of aircraft and having a by-pass annulus and fan for directing the flow of bypass air thereinto, is presented.
Abstract
A double, thrust diverter valve assembly for a by-pass engine applicable to the VTOL and V/STOL-types of aircraft and having a by-pass annulus and fan for directing the flow of bypass air thereinto, and in which an inflatable valve mechanism, operated from a compressed air source and mounted in a first, thrustaugmentation by-pass air flow-passage with a rearwardly-directed exhaust, is combined with a cascade valve mounted in a second, by-pass air flow-passage having a vertically-downward directed exhaust and thereby controlling the flow of by-pass air in the vertical flight mode.

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References
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