Multistage radial compressor baffle
An assembly can include a first radial compressor wheel that has a rotational axis and that includes a hub surface; a second radial compressor wheel that comprises a hub surface; and an annular baffle disposed at least in part between the hub surfaces wherein the annular baffle an outer edge and a substantially parabolic portion that extends to a tip portion, where the tip portion includes opposing sides that converge radially inwardly to a blunt end.
1 . An annular baffle configured to a two stage radial compressor assembly, the annular baffle comprising:
an outer edge; and
a substantially parabolic portion that extends to a tip portion, wherein:
the tip portion comprises a bluff body having opposing sides that converge radially inwardly to a blunt end, the opposing sides lacking an annular notch;
wherein the opposing sides comprise a low pressure side complementary to a shape of a backdisk portion of a low pressure radial compressor wheel of a first stage of the two stage radial compressor assembly and a high pressure side complementary to a shape of a backdisk portion of a high pressure radial compressor wheel of a second stage of the two stage radial compressor assembly; and
wherein at least one of the parabolic portion and the tip portion is configured to reduce interstage leakage; and
wherein absence of the annular notch contributes to reduction in the interstage leakage.
2 . The annular baffle according to claim 1 , wherein the tip portion comprises a quadrilateral cross-section.
3 . The annular baffle according to claim 2 , wherein the quadrilateral cross-section is convex.
4 . The annular baffle according to claim 2 , wherein the blunt end comprises a length that is less than a length of at least one of the opposing sides.
5 . The annular baffle according to claim 2 , wherein the quadrilateral cross-section comprises one acute angle and three obtuse angles.
6 . The annular baffle according to claim 1 , wherein the baffle is asymmetrical such that opposing sides comprise a longer side and a shorter side.
7 . The annular baffle according to claim 1 , wherein at least one of the opposing sides of the tip portion converges to the blunt end at an angle less than or equal to 90 degrees and greater than 50 degrees.
8 . The annular baffle according to claim 1 , wherein the blunt end defines an inner perimeter of the annular baffle.
9 . The annular baffle according to claim 1 , comprising a transition region between the substantially parabolic portion and the tip portion.
10 . The annular baffle according to claim 9 , wherein the transition region comprises opposing transition features.
11 . The assembly according to claim 1 , wherein the baffle is arranged offset with respect to low pressure radial compressor wheel and the high pressure radial compressor wheel and the baffle is configured to migrate towards a central position between the low pressure radial compressor wheel and the high pressure radial compressor wheel in response to an increase in operating temperature.
12 . The assembly according to claim 1 , wherein the baffle is further configured to promote at least one vortex between the lower pressure side and the backdisk portion of the low pressure radial compressor wheel.
13 . An assembly comprising:
a first radial compressor wheel that has a rotational axis and that comprises a hub surface;
a second radial compressor wheel that comprises a hub surface; and
an annular baffle disposed at least in part in a space defined between the hub surfaces wherein the annular baffle comprises an outer edge, opposing diffuser surfaces for flow to respective volutes, and a substantially parabolic portion that extends to a tip portion,
wherein the tip portion comprises a bluff body including opposing sides that converge radially inwardly to a blunt end and lack an annual notch,
wherein the baffle is configured to reduce interstage leakage; and
wherein absence of the annular notch contributes to reduction in the interstage leakage.
14 . The assembly according to claim 13 wherein the first radial compressor wheel comprises an axial face defined by a first diameter and wherein the second radial compressor wheel comprises an axial face defined by a second diameter wherein the first diameter exceeds the second diameter.
15 . The assembly according to claim 14 , wherein the first radial compressor wheel is a low pressure stage compressor wheel, wherein the second radial compressor wheel is a high pressure stage compressor wheel, and wherein the opposing diffuser surfaces comprise a low pressure stage diffuser surface and a high pressure stage diffuser surface.
16 . The assembly according to claim 15 , wherein the tip portion of the annular baffle is offset axially toward the high pressure stage compressor wheel.
17 . The assembly according to claim 13 , wherein the baffle is asymmetrical.
18 . The assembly according to claim 13 , wherein the baffle is arranged offset with respect to low pressure radial compressor wheel and the high pressure radial compressor wheel and the baffle is configured to migrate towards a central position between the low pressure radial compressor wheel and the high pressure radial compressor wheel in response to an increase in operating temperature.
19 . The assembly according to claim 13 , wherein the baffle is further configured to promote at least one vortex between the lower pressure side and the backdisk portion of the low pressure radial compressor wheel.