Outlet housing for cabin air compressor
An outlet housing for an aircraft cabin air compressor includes a volute comprising radially inner and outer portions, and having first, second, third, and fourth circumferential regions. The first circumferential region is between the fourth and second circumferential region. The second circumferential region is between the first circumferential region and the third circumferential region. The third circumferential region is between the second circumferential region and the fourth circumferential region. A portion of the volute in the first circumferential region has a first wall thickness. A portion of the volute in the second circumferential region has a second wall thickness. A portion of the volute in the third circumferential region has a third wall thickness. A portion of the volute in the fourth circumferential region has a fourth wall thickness.
1. An outlet housing for an aircraft cabin air compressor, the outlet housing comprising:
a volute comprising:
a radially outer portion;
a radially inner portion;
a first circumferential region having a portion with a wall thickness t 1 on the radially outer portion of the volute;
a second circumferential region having a portion with a wall thickness t 2 on the radially outer portion of the volute and a portion with the wall thickness t 2 on the radially inner portion of the volute;
a third circumferential region having a portion with a wall thickness t 4 between the radially outer portion and the radially inner portion of the volute; and
a fourth circumferential region having a portion with a wall thickness t 3 between the radially outer portion and the radially inner portion of the volute;
wherein the first circumferential region is between the fourth circumferential region and the second circumferential region, the second circumferential region is between the first circumferential region and the third circumferential region, the third circumferential region is between the second circumferential region and the fourth circumferential region, and the fourth circumferential region is between the first circumferential region and the third circumferential region; and
wherein the wall thickness t 1 is greater than the wall thickness t 2 , the wall thickness t 4 , and the wall thickness t 3 ; the wall thickness t 2 is less than the wall thickness t 4 and the wall thickness t 3 ; and the wall thickness t 4 is greater than the wall thickness t 3 ; and
a compressor outlet located in the first circumferential region of the volute.
2. The outlet housing of claim 1 further comprising:
a support ring connected to the radially inner portion of the volute;
a journal bearing support sleeve; and
a web between the journal bearing support sleeve and the support ring.
3. The outlet housing of claim 1 , wherein a ratio of the wall thickness t 1 to the wall thickness t 2 is less than or equal to 4.00 and greater than or equal to 2.18.
4. The outlet housing of claim 1 , wherein a ratio of the wall thickness t 4 to the wall thickness t 2 is less than or equal to 2.58 and greater than or equal to 1.27.
5. The outlet housing of claim 1 , wherein a ratio of the wall thickness t 3 to the wall thickness t 2 is less than or equal to 2.29 and greater than or equal to 1.09.
6. The outlet housing of claim 1 , further comprising:
a fillet in the first circumferential region between a surface of the volute and a surface of the compressor outlet, the fillet having a fillet radius;
wherein the first circumferential region includes an inner radius defined by the intersection of the surface of the volute and the surface of the compressor outlet, and wherein a ratio of the fillet radius to the inner radius is less than or equal to 6.63 and greater than or equal to 3.67.
7. The outlet housing of claim 1 , wherein the first circumferential region includes a portion with the wall thickness t 2 adjacent to the portion with the wall thickness t 1 .
8. The outlet housing of claim 1 , wherein the second circumferential region includes a portion with the wall thickness t 3 between the two portions having the wall thickness t 2 .
9. The outlet housing of claim 1 , wherein the third circumferential region includes a portion with a wall thickness t 5 on the radially outer portion of the volute and a portion with the wall thickness t 5 on the radially inner portion of the volute, wherein the two portions with the wall thickness t 5 are adjacent opposite sides of the portion having the wall thickness t 4 , and wherein the wall thickness t 5 is less than the wall thickness t 4 .
10. The outlet housing of claim 1 , wherein the fourth circumferential region includes a portion with the wall thickness t 2 on the radially outer portion of the volute and a portion with the wall thickness t 2 on the radially inner portion of the volute, wherein the two portions with the wall thickness t 2 are adjacent opposite sides of the portion having the wall thickness t 3 .
11. An aircraft cabin air compressor assembly comprising:
an outlet housing comprising:
a volute comprising:
a radially outer portion;
a radially inner portion;
a first circumferential region having a portion with a wall thickness t 1 on the radially outer portion of the volute;
a second circumferential region having a portion with a wall thickness t 2 on the radially outer portion of the volute and a portion with the wall thickness t 2 on the radially inner portion of the volute;
a third circumferential region having a portion with a wall thickness t 4 between the radially outer portion and the radially inner portion of the volute; and
a fourth circumferential region having a portion with a wall thickness t 3 between the radially outer portion and the radially inner portion of the volute;
a support ring connected to the radially inner portion of the volute;
a journal bearing support sleeve;
a web connected between the journal bearing support sleeve and the support ring; and
a compressor outlet located in the first circumferential region of the volute;
an inlet housing connected to the outlet housing;
a compressor rotor positioned within the inlet housing and having a plurality of blades;
a motor housing connected to the outlet housing at the support ring;
a motor positioned within the motor housing and having a drive shaft that extends through a journal bearing and is connected to the compressor rotor;
wherein the first circumferential region is between the fourth circumferential region and the second circumferential region, the second circumferential region is between the fourth circumferential region and the third circumferential region, the third circumferential region is between the second circumferential region and the fourth circumferential region, and the fourth circumferential region is between the first circumferential region and the third circumferential region; and
wherein the wall thickness t 1 is greater than the wall thickness t 2 , the wall thickness t 4 , and the wall thickness t 3 ; the wall thickness t 2 is less the wall thickness t 4 and the wall thickness t 3 ; and the third wall thickness t 4 is greater than the fourth wall thickness t 3 .
12. The assembly of claim 11 , wherein a ratio of the wall thickness t 1 to the wall thickness t 2 is less than or equal to 4.00 and greater than or equal to 2.18.
13. The assembly of claim 11 , wherein a ratio of the wall thickness t 4 to the wall thickness t 2 is less than or equal to 2.58 and greater than or equal to 1.27.
14. The assembly of claim 11 , wherein a ratio of the wall thickness t 3 to the wall thickness t 2 is less than or equal to 2.29 and greater than or equal to 1.09.
15. The assembly of claim 11 , further comprising:
a fillet in the first circumferential region between a surface of the volute and a surface of the compressor outlet, the fillet having a fillet radius;
wherein the first circumferential region includes an inner radius defined by the intersection of the surface of the volute and the surface of the compressor outlet, and wherein a ratio of the fillet radius to the inner radius is less than or equal to 6.63 and greater than or equal to 3.67.
16. The assembly of claim 11 , wherein the first circumferential region includes a portion having the wall thickness t 2 adjacent to the portion with the wall thickness t 1 .
17. The assembly of claim 11 , wherein the second circumferential region includes a portion with the wall thickness t 3 between two portions having the wall thickness t 2 .
18. The assembly of claim 11 , wherein the third circumferential region includes a portion with a wall thickness t 5 on the radially outer portion of the volute and a portion with the wall thickness t 5 on the radially inner portion of the volute, wherein the two portions with the wall thickness t 5 are adjacent opposite sides of the portion having the wall thickness t 4 , and wherein the wall thickness t 5 is less than the wall thickness t 4 .
19. The assembly of claim 11 , wherein the fourth circumferential region includes two portions with the wall thickness t 2 on the radially outer portion of the volute and a portion with the wall thickness t 2 on the radially inner portion of the volute, wherein the two portions with the wall thickness t 2 are adjacent opposite sides of the portion having the wall thickness t 3 .