Turbine housing for a two wheel air cycle machine

Patent metadata

Field	Value
Publication number	US-11655039-B2
Application number	US-202117218545-A
Country	US
Kind code	B2
Filing date	Mar 31, 2021
Priority date	Apr 3, 2020
Publication date	May 23, 2023
Grant date	May 23, 2023

Abstract

A turbine housing for a two-wheel air cycle machine includes a first side of the turbine housing, a second side of the turbine housing, a central axis, an outer housing portion, an inner housing portion, a plurality of struts between the inner housing portion and the outer housing portion and a plurality of cooling slots between the plurality of supports. The outer housing portion includes an inner surface, an outer surface, a cooling inlet extending from the outer surface of the outer housing portion and a cooling outlet opposite the cooling inlet and extending from the outer surface of the outer housing portion. The inner housing portion includes a thrust bearing support surface substantially parallel to the second side of the turbine housing and a journal bearing bore extending between the first side of the turbine housing and the thrust bearing support surface.

First claim

The invention claimed is:

1. A turbine housing for a two-wheel air cycle machine, the turbine housing comprising:
a first side of the turbine housing;
a second side of the turbine housing;
a central axis;
an outer housing portion comprising:
an inner surface of the outer housing portion;
an outer surface of the outer housing portion comprising:
a mounting flange;
a first parallel wall surface substantially parallel to the central axis with a first end and a second, the first end of the first parallel wall surface being connected to the mounting flange;
a frustoconical wall surface with a first end and a second end, the first end of the frustoconical wall surface being connected to the second end of the first parallel wall surface;
a second parallel wall surface substantially parallel to the central axis with a first end and a second end, the first end of the second parallel wall surface being connected to the second end of the frustoconical wall surface; and
mounting tabs extending from the outer surface of the outer housing portion at the second end of the second parallel wall surface;

a cooling inlet extending from the outer surface of the outer housing portion; and
a cooling outlet opposite the cooling inlet and extending from the outer surface of the outer housing portion;

an inner housing portion comprising:
a thrust bearing support surface substantially parallel to the second side of the turbine housing; and
a journal bearing bore extending between the first side of the turbine housing and the thrust bearing support surface;

a plurality of struts between the inner housing portion and the outer housing portion; and
a plurality of cooling slots between the plurality of struts.

2. The turbine housing of claim 1 , wherein the frustoconical wall portion is at an offset angle from the central axis, and wherein the offset angle is between 14.980 degrees and 15.020 degrees.

3. The turbine housing of claim 2 , wherein the first parallel wall surface of the outer housing portion is positioned a first radius from the central axis, the frustoconical wall portion is positioned a second radius from the offset angle, and the inner surface of the outer surface of the outer housing portion is positioned a third radius from the central axis, and wherein a ratio of the first radius to the second radius is between 0.935 and 0.948, and wherein a ratio of the first radius to the third radius is between 1.015 and 1.041.

4. The turbine housing of claim 1 , wherein the cooling inlet has a first diameter and the cooling outlet has a second diameter, and wherein a ratio of the first diameter to the second diameter is between 0.856 and 0.904.

5. The turbine housing of claim 1 , wherein the journal bearing bore has a third diameter and further comprises:
a first O-seal gland with a first side facing the first side of the turbine housing and a second side facing the thrust bearing support surface; and
a second O-seal gland with a first side facing the first side of the turbine housing and a second side facing the thrust bearing support surface.

6. The turbine housing of claim 5 , wherein the first O-seal gland and the second O-seal gland have a fourth diameter, and wherein the ratio of the third diameter to the fourth diameter is between 0.921 and 0.925.

7. The turbine housing of claim 5 , wherein first O-seal gland and the second O-seal gland have a width from the first side to the second side, respectively, and wherein a ratio of the width to the fourth diameter is between 0.066 and 0.089.

8. The turbine housing of claim 7 , wherein the first O-seal gland is positioned in the journal bearing bore so the second side of the first O-seal gland is a first length from the thrust bearing support surface and the second O-seal gland is positioned in the journal bearing bore so the second side of the second O-seal gland is a second length from the thrust bearing support surface, and wherein a ratio of the first length to the second length is between 5.200 and 6.070.

9. The turbine housing of claim 7 , wherein each edge of the first O-seal gland and the second O-seal gland have a fillet with a fillet radius of a fourth radius, and wherein a ratio of the width to the fourth radius is between 7.125 and 11.000.

10. A two-wheel air cycle machine for an aircraft, the two-wheel air cycle machine comprising:
a turbine assembly comprising:
a turbine rotor;
a turbine housing comprising:
a first side of the turbine housing;
a second side of the turbine housing;
a central axis;
an outer housing portion comprising:
an inner surface of the outer housing portion;
an outer surface of the outer housing portion;
a cooling inlet extending from the outer surface of the outer housing portion; and
a cooling outlet opposite the cooling inlet and extending from the outer surface of the outer housing portion;

an inner housing portion comprising:
a thrust bearing support surface substantially parallel to the second side of the turbine housing; and
a journal bearing bore extending between the first side of the turbine housing and the thrust bearing support surface;

a plurality of struts between the inner housing portion and the outer housing portion; and
a plurality of cooling slots between the plurality of struts; and

a turbine-end journal bearing within the turbine housing;

a compressor assembly comprising:
a compressor inlet housing;
a compressor outlet housing connected to the compressor inlet housing;
a compressor seal housing within the compressor outlet housing;
a bearing housing within the compressor outlet housing and attached at a first side to the compressor seal housing and attached at a second side to the turbine housing; and
a compressor-end journal bearing within the bearing housing;

a tie rod connecting the turbine rotor and the compressor rotor and supported by the turbine-end journal bearing and the compressor-end journal bearing; and
thrust bearings centrally positioned between the turbine assembly and the compressor assembly supported by the turbine housing and the bearing housing.

11. The two-wheel air cycle machine of claim 10 , wherein the outer surface of the outer housing portion of the turbine housing further comprises:
a mounting flange;
a first parallel wall surface substantially parallel to the central axis with a first end and a second, the first end of the first parallel wall surface being connected to the mounting flange;
a frustoconical wall surface with a first end and a second end, the first end of the frustoconical wall surface being connected to the second end of the first parallel wall surface;
a second parallel wall surface substantially parallel to the central axis with a first end and a second end, the first end of the second parallel wall surface being connected to the second end of the frustoconical wall surface; and
mounting tabs extending from the outer surface of the outer housing portion at the second end of the second parallel wall surface.

12. The turbine housing of claim 11 , wherein the frustoconical wall portion is at an offset angle from the central axis, and wherein the offset angle is between 14.980 degrees and 15.020 degrees.

13. The turbine housing of claim 12 , wherein the first parallel wall surface of the outer housing portion is positioned a first radius from the central axis, the frustoconical wall portion is positioned a second radius from the offset angle, and the inner surface of the outer surface of the outer housing portion is positioned a third radius from the central axis, and wherein a ratio of the first radius to the second radius is between 0.935 and 0.948, and whe

Assignees

• Hamilton Sundstrand Corp

Inventors

• Colson Darryl A
• Chrabascz Eric
• Wytas Clarence J

Classifications

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title

• F01D25/265

  Vertically split casings; Clamping arrangements therefor · CPC title

• Y02T50/50

  On board measures aiming to increase energy efficiency · CPC title

• F01D25/125

  of bearings · CPC title

• F04D29/584

  cooling or heating the machine (F04D29/5846, F04D29/5853 take precedence) · CPC title