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US 4,726,183 AGranted
Self retracting screens for turbomachinery
AssigneeInnerspace Corporation
InventorCalvin A. Gongwer
Life of this patent
Estimating the term…
Abstract
A self retracting screen for turbomachinery comprised of a number of interlocking wires, the wire ends being pivotally attached to the periphery of the normal inlet of the turbomachinery. Preferably, the wires are elliptical, or streamlined, in cross-section such that the major diameters of the elliptical cross-section of the wires when the screen is closed are substantially parallel to the turbomachinery inlet stream.
Claims9
Turbomachinery with a self retracting screen comprising:
- turbomachinery including
- a normal inlet;
- a normal outlet;
- an impeller positioned for axial rotation within said turbo machinery;
- a screen stop which is located at the approximate centerline of the turbomachinery flow path and upstream of said normal inlet to the turbomachinery;
- and,
- a plurality of interlocking wires, said wires having wire ends and a mid section between said wire ends, said wire ends being pivotally attached to the periphery of said normal inlet to the turbomachinery and said mid section between said wire ends being unattached;
- said wires being moveable between a closed position and a retracted position, in said closed position a segment of said mid section between said wire ends of each of said wires rests unattached against said screen stop screening said normal inlet;
- and in said retracted position said mid section between said wire ends do not rest against said screen stop.
6 more elements
A thruster with a self retracting screen comprising:
- a thruster normal inlet;
- a thruster normal outlet;
- a thruster throat section between said normal inlet and said normal outlet;
- an impeller positioned for bi-directional rotation within said throat;
- a screen stop which is located at the approximate centerline of the turbomachinery;
- and
- a plurality of interlocking wires, said wires having wire ends, said wire ends being pivotally attached to the periphery of said normal inlet to the turbomachinery, said wire being moveable between a first position and a second position;
- in said first position a segment of each of said wires intermediate said wire ends rests unattached against said screen stop;
- and, in said second position said wires do not rest against said screen stop.
6 more elements
A thruster having a self retracting screen comprising:
- a thruster normal inlet;
- a thruster normal outlet;
- a thruster throat section located between said thruster normal inlet and normal outlet;
- an impeller positioned for bi-directional rotation within said thruster throat;
- a screen stop which is located at the approximate centerline of the turbomachinery flow path and upstream of said normal inlet to the turbomachinery;
- a motor case;
- and
- two sets of a plurality of interlocking wires, said wires having wire ends, said wire ends of said first set being pivotally attached to the periphery of said thruster normal inlet and said wire ends of said second set being pivotally attached to the periphery of said thruster normal outlet, said first set of interlocking wires and said second set of interlocking wires being moveable between a closed position and a retracted position in said closed position said first set of interlocking wires rests unattached against said screen stop;
- in said retracted position said second set of interlocking wires does not contact said motor case;
- in said retracted position said first set of interlocking wires does not contact said screen stop;
- and, in said closed position said second set of interlocking wires rests unattached against said motor case.
8 more elements
Dependencies are inferred from the claim text.