Fan and compressor housing for an air cycle machine

• US 10,661,906 B2
• Filed: 09/23/2014
• Issued: 05/26/2020
• Est. Priority Date: 09/23/2014
• Status: Active Grant

• Current Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Beers, Craig M., McAuliffe, Christopher, Merritt, Brent J.
• Primary Examiner(s): White, Dwayne J
• Assistant Examiner(s): Christensen, Danielle M.
• Application Number:
  US14/494,282
• Publication Number:
  US 20160083099A1
• Time in Patent Office: 2,072 Days
• Field of Search: 4151682, 4151701, 4152141, 4152151
• CPC Class Codes: B64D 13/06 the air being conditioned pressurising B64D13/02
• CPC Class Codes: F04D 25/024 the driving means being assisted by a power recovery turbine
• CPC Class Codes: F04D 29/4206 especially adapted for elastic fluid pumps
• CPC Class Codes: F04D 29/522 especially adapted for elastic fluid pumps
• CPC Class Codes: F04D 29/624 especially adapted for elastic fluid pumps
• CPC Class Codes: F04D 29/644 especially adapted for elastic fluid pumps

Abstract

A housing for an air cycle machine includes a housing with a first end and a second end opposite the first end, a first duct adjacent the first end of the housing with an air inlet and an air outlet, a second duct adjacent the second end of the housing with an air inlet and an air outlet, and a collar in the housing extending into the second duct. The collar includes a first annular surface facing radially inward and configured to engage a journal bearing and a second annular surface facing radially inward and configured to engage a rotating shaft, wherein the second surface is monolithic with the housing.

Claims

1. A housing for an air cycle machine, the housing comprising:

a housing with a first end and a second end opposite the first end;

a first duct adjacent the first end of the housing with an air inlet and an air outlet;

a second duct adjacent the second end of the housing with an air inlet and an air outlet; and

a collar in the housing extending from a center of the housing towards the first end of the housing, the collar comprising;

a first annular surface facing radially inward and configured to engage a journal bearing;

an annular recess in the first annular surface that is configured to receive a seal ring; and

a second annular surface facing radially inward and configured to engage a rotating shaft, wherein the second annular surface is a uniform, cylindrical surface extending from a first end adjacent a first end of the collar to a second end adjacent the first annular surface, wherein the second annular surface is configured to directly engage the rotating shaft to provide a sealing surface that is monolithic with the housing;

wherein a diameter of the first annular surface is larger than a diameter of the second annular surface; and

wherein the second annular surface is disposed between the first annular surface and the first end of the housing.

2. The housing of claim 1, wherein a ratio of the diameter of the first annular surface of the collar to the diameter of the second annular surface of the collar is between 1.1630 and 1.1653.

3. The housing of claim 1, and further comprising:

a first annular flange adjacent to the second end of the housing with a radially inner surface configured to engage a static part.

4. The housing of claim 3, wherein a ratio of the diameter of the first annular surface of the collar to a diameter of the first annular flange is between 0.2853 and 0.2857.

5. The housing of claim 3, wherein a ratio of the diameter of the second annular surface of the collar to a diameter of the first annular flange is between 0.2451 and 0.2454.

6. The housing of claim 1, and further comprising:

a second annular flange adjacent to the collar; and

a seal positioned against an inner surface of the second annular flange, wherein a radially inner surface of the seal is configured to engage a rotating part.

7. The housing of claim 6, wherein a ratio of the diameter of the first annular surface of the collar to a diameter of the seal on the second annular flange is between 0.9890 and 0.9908.

8. The housing of claim 6, wherein a ratio of the diameter of the second annular surface of the collar to a diameter of the seal on the second annular flange is between 0.8497 and 0.8509.

9. An air cycle machine comprising:

a tie rod that is configured to rotate about an axis;

a fan section with a fan rotor mounted to the tie rod;

a compressor section with a compressor rotor mounted to the tie rod;

a first turbine section with a first turbine rotor mounted to the tie rod;

a first turbine housing; and

a fan and compressor housing connected to the first turbine housing, wherein the fan and compressor housing comprises;

a first end;

a second end adjacent to the first turbine housing and opposite of the first end;

a fan duct adjacent to the first end of the fan and compressor housing, wherein the fan rotor is positioned in the fan duct;

a compressor duct adjacent to the second end of the fan and compressor housing, wherein the compressor rotor is positioned in the compressor duct; and

an annular collar in the fan and compressor housing and extending towards the first end of the fan and compressor housing, wherein the annular collar comprises;

a first annular surface facing radially inward to engage a journal bearing;

an annular recess in the first annular surface that is configured to receive a seal ring; and

a second annular surface facing radially inward to engage a rotating shaft, wherein the second annular surface is a uniform, cylindrical surface extending from a first end adjacent a first end of the collar to a second end adjacent the first annular surface, wherein the second annular surface is configured to directly engage the rotating shaft to provide a sealing surface that is monolithic with the fan and compressor housing;

wherein a diameter of the first annular surface is larger than a diameter of the second annular surface; and

wherein the second annular surface is disposed between the first annular surface and the first end of the fan and compressor housing.

10. The air cycle machine of claim 9, and further comprising:

a second turbine section with a second turbine rotor mounted to the tie rod; and

a second turbine housing connected to the first turbine housing.

11. The air cycle machine of claim 9, wherein a ratio of the diameter of the first annular surface of the collar to the diameter of the second annular surface of the collar is between 1.1630 and 1.1653.

12. The air cycle machine of claim 9, wherein the fan and compressor housing further comprises:

a first annular flange adjacent to the second end of the fan and compressor housing with a radially inner surface configured to engage a diffuser.

13. The air cycle machine of claim 12, wherein a ratio of the diameter of the second annular surface of the collar to a diameter of the first annular flange is between 0.2451 and 0.2454.

14. The air cycle machine of claim 9, wherein the fan and compressor housing further comprises:

a second annular flange adjacent to the collar; and

a seal positioned against an inner surface of the second annular flange, wherein a radially inner surface of the seal is configured to engage the rotating shaft.

15. The air cycle machine of claim 14, wherein a ratio of the diameter of the second annular surface of the collar to a diameter of the seal on the second annular flange is between 0.8497 and 0.8509.