Axial turbine for aeronautical applications
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United States of America Patent
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-
Mar 1, 2005
Grant Date -
Dec 5, 2002
app pub date -
May 10, 2002
filing date -
May 11, 2001
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
An axial turbine for aeronautical applications has a casing housing a stator, which is provided with an array of airfoil profiles, which are positioned angularly equidistant from one other about the axis of the turbine, define associated spaces between one another for the passage of a flow of gas and are hinged to an annular structure, each one about an associated hinge axis incident to the axis of the turbine; in service, the airfoil profiles are simultaneously actuated to rotate by an identical angle of adjustment by means of a ring actuated by actuators outside the casing and connected to each airfoil profile via an associated lever.
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