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Improvements in axisymmetric nozzles of variable geometry and orientation of flow destinadasa propellant gas turbine
Improvements in axisymmetric nozzles of variable geometry and orientation of flow destinadasa propellant gas turbine
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机译：几何形状和流量可变的destinadasa推进剂燃气轮机的轴对称喷嘴的改进
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摘要
Improvements in invention patent No.. 9401114, filed 20 May 1994 on: Improvements in axisymmetric nozzles of variable geometry and flow orientation propellants aimed at gas turbine. The nozzle comprises control means for regulating the throat area A {sub, 8 and vectoring the thrust, consisting of three concentric rings with the longitudinal axis (14) of the engine, one inside (8), one intermediate (7) and external one (6), and a plurality of linear actuators (9); including the outer ring (6) two ring segments (6a-6b) biarticulated to each other having constrained from pivoting to a single plane and therefore can vector the thrust only in the plane of aircraft pitch. Application in bioreactors aircraft propellers.
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