Regenerative turbine pump impeller
AssigneeVisteon Global Technologies, Inc.
InventorsDequan Yu, Ronald Luce Verkleeren
Life of this patent
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Abstract
A regenerative turbine impeller comprises an annular disk having an annular partition wall extending radially therefrom. A first plurality of circumferentially spaced turbine vanes provided on one side of the partition wall radially projecting from the annular disk and have a radial length greater than the partition wall. A second plurality of circumferentially spaced turbine vanes circumferentially spaced about the disk extend radially therefrom and are provided on a second side of the partition wall. The second plurality of vanes rotationally staggered with respect to the first plurality of turbine vanes.
Claims16
A regenerative fuel pump for supplying fuel to an engine from a fuel tank, the pump comprising:
- a pump housing;
- a rotary pumping element in the form of an impeller within the pump housing, the impeller comprising a disc portion having an outer circumference, a first plurality of vanes circumferentially spaced about the outer circumference of the disc portion and a second plurality of vanes circumferentially spaced about the outer circumference of the disc portion, said second plurality of vanes rotationally staggered with respect to the first plurality of vanes;
- a partition wall formed between the first plurality and the second plurality of vanes, said partition wall extending from the outer circumference for a distance less than the length of the first and second plurality of vanes;
- the first plurality of vanes and said partition wall intersecting to define a first plurality of vane grooves, and said second plurality of vanes and said partition wall intersecting to form a second plurality of vane grooves;
- the second plurality of vanes positioned rotationally immediately adjacent the first plurality of vanes so as to cover a portion of the first plurality of vane grooves immediately adjacent the first plurality of vanes when viewed from an axial end of the impeller.
A regenerative fuel pump for supplying fuel to and engine from a fuel tank, the pump comprising:
- a pump housing;
- a rotary pumping element in the form of an impeller within the pump housing, the impeller comprising a disc portion having an outer circumference, a first plurality of vanes circumferentially spaced about the outer circumference of the disc portion and a second plurality of vanes circumferentially spaced about the outer circumference of the disc portion, said second plurality of vanes rotationally staggered with respect to the first plurality of vanes;
- a partition wall formed between the first plurality and the second plurality of vanes, said partition wall extending from the disc portion outer circumference for a distance less than the length of the first and second plurality of vanes, the first plurality of vanes and the partition wall intersecting to define a first plurality of vane grooves and the second plurality of vanes and said partition wall intersecting to form a second plurality of vane grooves;
- the first and second plurality of vanes having a curved shape when viewed from an end face of the impeller.
A regenerative fuel pump for supplying fuel to an engine from a fuel tank, the pump comprising:
- a pump housing;
- and
- a regenerative turbine impeller having an annular disc having an annular continuous partition wall extending radially therefrom, a first plurality of turbine vanes circumferentially spaced about and radially projecting from said annular disc, and a second plurality of turbine vanes circumferentially spaced about and radially projecting from said annular disc, said first plurality of turbine vanes being provided on a first side of said continuous partition wall while said second plurality of turbine vanes being provided on a second side of said continuous partition wall, said first and second plurality of turbine vanes both having a radial length greater than said continuous partition wall, and said second plurality of turbine vanes being rotationally staggered relative to said first plurality of turbine vanes.
Dependencies are inferred from the claim text.