# US 9,752,591 B2 · Compressor diffuser and shroud for a motor driven compressor

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- Number: US 9,752,591 B2
- Document ID: US9752591B2
- Status: Granted
- Kind: B2
- Application number: 14/603,517
- Filed: 2015-01-23
- Published: 2016-07-28
- Granted: 2017-09-05
- Earliest claimed: 2015-01-23
- Assignees: Carrier Corporation
- Applicants: Hamilton Sundstrand Corporation
- Inventors: Craig M. Beers; Darryl A. Colson
- Web page: https://patentgrep.com/patent/US9752591B2

## CPC

- F04D 29/441: {especially adapted for elastic fluid pumps}
- F04D 29/4206: {especially adapted for elastic fluid pumps}
- F04D 29/624: {especially adapted for elastic fluid pumps}
- F04D 29/444: {Bladed diffusers}
- F05D 2250/52: Outlet
- F04D: NON-POSITIVE-DISPLACEMENT PUMPS (engine fuel-injection pumps F02M; ion pumps H01J41/12; electrodynamic pumps H02K44/02)
- F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS

## Abstract

An aspect includes a compressor diffuser and shroud for a motor driven compressor assembly. The motor driven compressor assembly includes a first stage compressor and a second stage compressor. The compressor diffuser and shroud of the first stage compressor includes a diffuser portion, a compressor inlet portion, and a shroud portion. The diffuser portion includes a diffuser portion outer lip having a first sealing lip outer diameter to provide a first sealing interface to a first stage compressor housing. The compressor inlet portion includes an inlet portion outer lip having a second sealing lip outer diameter to provide a second sealing interface. The shroud portion includes a curvature between the diffuser portion outer lip and the inlet portion outer lip to align with a first stage compressor rotor, where a ratio of the first sealing lip outer diameter to the second sealing lip outer diameter is between 1.622 and 1.628.

## Claims

### Claim 1

A compressor diffuser and shroud for a motor driven compressor assembly, the motor driven compressor assembly comprising a first stage compressor and a second stage compressor, the compressor diffuser and shroud of the first stage compressor comprising:
a diffuser portion comprising a diffuser portion outer lip having a first sealing lip outer diameter to provide a first sealing interface to a first stage compressor housing;
a compressor inlet portion comprising an inlet portion outer lip having a second sealing lip outer diameter to provide a second sealing interface to the first stage compressor housing; and
a shroud portion comprising a curvature between the diffuser portion outer lip and the inlet portion outer lip to align with a first stage compressor rotor, wherein a ratio of the first sealing lip outer diameter to the second sealing lip outer diameter is between 1.622 and 1.628.

### Claim 2 (depends on 1)

The compressor diffuser and shroud of claim 1, wherein the diffuser portion comprises a plurality of diffuser fins to diffuse a compressed flow of the first stage compressor with respect to a bearing support plate.

### Claim 3 (depends on 2)

The compressor diffuser and shroud of claim 2, wherein a ratio of the first sealing lip outer diameter to a height of the diffuser fins is between 24.93 and 25.76.

### Claim 4 (depends on 3)

The compressor diffuser and shroud of claim 3, wherein a ratio of the second sealing lip outer diameter to the height of the diffuser fins is between 15.30 and 15.89.

### Claim 5 (depends on 2)

The compressor diffuser and shroud of claim 2, wherein the diffuser portion comprises an outermost group of the diffuser fins and an innermost group of the diffuser fins.

### Claim 6 (depends on 5)

The compressor diffuser and shroud of claim 5, wherein the outermost group of the diffuser fins includes a plurality of holes to fasten the compressor diffuser and shroud to the bearing support plate of the motor driven compressor assembly.

### Claim 7 (depends on 6)

The compressor diffuser and shroud of claim 6, wherein an outermost diameter of the compressor diffuser and shroud is sized to substantially align with an outer diameter of the bearing support plate using an interior portion of a cylindrical alignment tool.

### Claim 8 (depends on 6)

The compressor diffuser and shroud of claim 6, wherein a compressor backing plate is interposed between the compressor diffuser and shroud and the bearing support plate.

### Claim 9

A method of installing a compressor diffuser and shroud in a motor driven compressor assembly comprising a first stage compressor and a second stage compressor, the method comprising:
aligning the compressor diffuser and shroud with a bearing support plate of the motor driven compressor assembly using a cylindrical alignment tool; and
coupling the compressor diffuser and shroud with the bearing support plate based on the aligning to seal a first stage compressor housing with respect to the compressor diffuser and shroud, the compressor diffuser and shroud comprising:
a diffuser portion comprising a diffuser portion outer lip having a first sealing lip outer diameter to provide a first sealing interface to the first stage compressor housing;
a compressor inlet portion comprising an inlet portion outer lip having a second sealing lip outer diameter to provide a second sealing interface to the first stage compressor housing; and
a shroud portion comprising a curvature between the diffuser portion outer lip and the inlet portion outer lip to align with a first stage compressor rotor, wherein a ratio of the first sealing lip outer diameter to the second sealing lip outer diameter is between 1.622 and 1.628.

### Claim 10 (depends on 9)

The method of claim 9, wherein aligning the compressor diffuser and shroud with the bearing support plate further comprises positioning a plurality of diffuser fins of the diffuser portion to diffuse a compressed flow of the first stage compressor with respect to the bearing support plate.

### Claim 11 (depends on 10)

The method of claim 10, wherein a ratio of the first sealing lip outer diameter to a height of the diffuser fins is between 24.93 and 25.76, and a ratio of the second sealing lip outer diameter to the height of the diffuser fins is between 15.30 and 15.89.

### Claim 12 (depends on 11)

The method of claim 11, wherein an outermost diameter of the compressor diffuser and shroud is sized to substantially align with an outer diameter of the bearing support plate using an interior portion of the cylindrical alignment tool.

### Claim 13 (depends on 10)

The method of claim 10, wherein the diffuser portion comprises an outermost group of the diffuser fins and an innermost group of the diffuser fins.

### Claim 14 (depends on 13)

The method of claim 13, wherein the outermost group of the diffuser fins includes a plurality of holes to couple the compressor diffuser and shroud to the bearing support plate of the motor driven compressor assembly.

### Claim 15 (depends on 14)

The method of claim 14, further comprising: interposing a compressor backing plate between the compressor diffuser and shroud and the bearing support plate.
