Turbopump with axially curved vane
A turbopump includes an impeller ( 22 ) that is rotatable about an axis (A). A discharge collector ( 28 ) is located radially outward of the impeller. A passage ( 30 ) fluidly connects the impeller to the discharge collector. The passage is curved.
1. A turbopump comprising:
an impeller rotatable about an axis, wherein the impeller has an axial inlet;
a discharge collector;
a passage having an inlet face at which the passage opens to the impeller and an outlet face at which the passage opens to the discharge collector; and
a vane extending in the passage, the vane is curved axially forward in the direction of the axial inlet, and wherein the vane includes a leading edge at the impeller, a trailing edge that protrudes past the outlet face and extends into the discharge collector, and a height that is uniform from the leading edge to the trailing edge.
2. The turbopump as recited in claim 1 , wherein the discharge collector has a flat side, and the passage opens into the discharge collector at the flat side.
3. The turbopump as recited in claim 2 , wherein the discharge collector has a symmetry with respect to a line of symmetry that intersects the vane.
4. The turbopump as recited in claim 1 , wherein there is a radial direction perpendicular to the axis, and the vane is curved up to 45° with respect to the radial direction.
5. The turbopump as recited in claim 1 , wherein the vane is a guide vane.
6. A turbopump comprising:
an impeller that is rotatable about an axis;
a discharge collector radially outwards of the impeller;
a passage having an inlet face at which the passage opens to the impeller and an outlet face at which the passage opens to the discharge collector; and
a vane in the passage, the vane includes, relative to the axis, a radially inner leading edge at the inlet face and a radially outer trailing edge that protrudes past the outlet face and extends into the discharge collector, and the radially outer trailing edge is axially forward relative to the radially inner leading edge, wherein the vane includes a height that is uniform from the radially inner leading edge to the radially outer trailing edge.
7. The turbopump as recited in claim 6 , wherein the radially outer trailing edge is axially offset from the radially inner leading edge by up to 45° with regard to respective references points and lines at midpoints of the radially outer trailing edge and the radially inner leading edge.
8. The turbopump as recited in claim 6 , wherein the radially outer trailing edge is axially offset from the radially inner leading edge by equal to or less than 30° .
9. The turbopump as recited in claim 6 , wherein the discharge collector has a flat side, and the passage opens into the discharge collector at the flat side.
10. A turbopump comprising:
an impeller rotatable about an axis;
a discharge collector;
a passage having an inlet face at which the passage open to the impeller and an outlet face at which the passage opens to the discharge collector; and
a vane extending in the passage, the vane is axially inclined relative to the axis, and wherein the vane includes a leading edge at the impeller, a trailing edge that protrudes past the outlet face and extends into at the discharge collector, and a height that is uniform from the leading edge to the trailing edge.
11. The turbopump as recited in claim 10 , wherein the vane is inclined at an angle of inclination of greater than 45° .
12. The turbopump as recited in claim 10 , wherein the impeller has an inlet side, and the vane is inclined toward the inlet side.
13. The turbopump as recited in claim 1 , wherein the vane defines axially forward and aft sides that have a constant curvature and do not have any corners.