# US 10,309,410 B2 · Impeller shroud with deflecting outer member for clearance control in a centrifugal compressor

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- Number: US 10,309,410 B2
- Document ID: US10309410B2
- Status: Granted
- Kind: B2
- Application number: 15/165,555
- Filed: 2016-05-26
- Published: 2017-11-30
- Granted: 2019-06-04
- Earliest claimed: 2016-05-26
- Assignees: ROLLS-ROYCE plc
- Applicants: Rolls-Royce Corporation
- Inventors: Nathan Ottow; Jonathan Acker; Nate Cooper
- Web page: https://patentgrep.com/patent/US10309410B2

## CPC

- F04D 29/162: {of a centrifugal flow wheel}
- F04D 27/002: {by varying geometry within the pumps, e.g. by adjusting vanes}
- F04D 27/0246: {by varying geometry within the pumps, e.g. by adjusting vanes}
- F04D 29/284: {for compressors}
- F04D 29/4206: {especially adapted for elastic fluid pumps}
- F01D 11/08: for sealing space between rotor blade tips and stator (specially-shaped blade tips therefor F01D5/20)
- F01D 11/22: by mechanically actuating the stator or rotor components, e.g. moving shroud sections relative to the rotor
- F04D 29/622: {Adjusting the clearances between rotary and stationary parts}
- F05D 2220/32: in gas turbines
- F05D 2240/11: Shroud seal segments
- F05D 2260/50: Kinematic linkage, i.e. transmission of position
- F05D 2260/57: using servos, independent actuators, etc.
- F04D: NON-POSITIVE-DISPLACEMENT PUMPS (engine fuel-injection pumps F02M; ion pumps H01J41/12; electrodynamic pumps H02K44/02)
- F01D: NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES (machines or engines for liquids F03; non-positive displacement pumps F04D)
- F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS

## Abstract

A system for controlling the clearance distance between an impeller blade tip of a centrifugal compressor and a radially inner surface of an impeller shroud in a turbine engine. The system comprises a two-piece integral impeller shroud with a fixed inner member and a variable outer member. An actuator is coupled to an aft end of the variable outer member and imparts axially forward and aft motion on the aft end, causing deflection of the outer member.

## Claims

### Claim 1

A compressor shroud assembly in a turbine engine, said compressor shroud assembly comprising:
a static compressor casing;
an actuator mounted to said casing; and
a double-walled impeller shroud for encasing a rotatable centrifugal compressor, the impeller shroud comprising a pair of nested arcuate shroud members shaped to follow the contour of a rotatable centrifugal compressor, said pair of nested arcuate shroud members comprising a forward member mounted to said casing and an aft member deflectively coupled to said forward member and operatively coupled to said actuator to effect deflection of said aft member relative to said forward member and to the rotatable centrifugal compressor when said actuator is activated.

### Claim 2 (depends on 1)

The compressor shroud assembly of claim 1 wherein said nested arcuate shroud members form a chamber adapted to receive actuating air, said aft member being deflected responsive to the provision of actuating air to said chamber.

### Claim 3 (depends on 2)

The compressor shroud assembly of claim 2 wherein the actuation air is drawn from a discharge air of the rotatable centrifugal compressor.

### Claim 4 (depends on 2)

The compressor shroud assembly of claim 2 wherein said aft member of said nested pair of arcuate shroud members is deflectively coupled to said forward member of said nested pair of arcuate shroud members by a bellows, said bellows being coupled between an aft end of said aft member and an aft end of said forward member.

### Claim 5 (depends on 4)

The compressor shroud assembly of claim 4 wherein said nested arcuate shroud members are statically coupled at a forward end thereof.

### Claim 6 (depends on 1)

The compressor shroud assembly of claim 1 wherein said actuator comprises a mechanical drive member coupled to an aft end of said aft member of said nested pair of arcuate members to effect deflection of said aft member responsive to the provision of a driving force to said aft member by said mechanical drive member.

### Claim 7 (depends on 6)

The compressor shroud assembly of claim 6 wherein said aft member is deflectively coupled to said forward member by a bellows, said bellows being coupled between an aft end of said aft member and an aft end of said forward member.

### Claim 8 (depends on 6)

The compressor shroud assembly of claim 6 wherein said mechanical drive member comprises a cylindrical member coupled to said casing wherein an axial motion of said cylindrical member effects axial translation of said aft member.

### Claim 9 (depends on 6)

The compressor shroud assembly of claim 6 wherein said actuator comprises a pneumatic piston coupled to said casing wherein the actuation of said piston effects axial translation of said aft member.

### Claim 10 (depends on 2)

The compressor shroud assembly of claim 2 further comprising one or more sensors for measuring a fluid pressure in said chamber, said chamber being actuated or vented in response to the measured fluid pressure in said chamber.

### Claim 11 (depends on 2)

The compressor shroud assembly of claim 2 further comprising one or more sensors for measuring the clearance gap between said shroud and the rotatable centrifugal compressor, said chamber being actuated or vented in response to the clearance gap measured by the one or more sensors.

### Claim 12 (depends on 1)

The compressor shroud assembly of claim 1 further comprising a chamber bounded in part by said casing and at least a portion of the impeller shroud proximate an aft end thereof, said chamber being pressurized at a pressure between ambient pressure and 450 pounds per square inch.

### Claim 13

A method of dynamically changing a clearance gap between a rotatable centrifugal compressor and a double-walled shroud encasing the rotatable centrifugal compressor, said method comprising:
mounting a forward shroud member to a static casing;
nesting and deflectively coupling an aft shroud member to the forward shroud member forming the double-walled shroud to follow the contour of the rotatable centrifugal compressor; and
deflecting the aft shroud member relative to the forward shroud member and the rotatable centrifugal compressor.

### Claim 14 (depends on 13)

The method of claim 13 wherein deflecting the aft shroud member comprises providing actuation air to a chamber forming between the shroud members.

### Claim 15 (depends on 14)

The method of claim 14 further comprising providing actuating air from a discharge of the rotatable centrifugal compressor.

### Claim 16 (depends on 14)

The method of claim 14 further comprising sensing air pressure in the chamber, wherein providing the actuating air to the chamber is responsive in response to the sensed air pressure.

### Claim 17 (depends on 14)

The method of claim 14 further comprising sensing the clearance gap between the rotatable centrifugal compressor and the shroud, wherein providing actuating air to the chamber is responsive to the sensed clearance gap.

### Claim 18 (depends on 13)

The method of claim 13 wherein deflecting the aft shroud member comprises providing a mechanical force to the aft shroud member from a mechanical drive member.

### Claim 19 (depends on 18)

The method of claim 18 further comprising:
sensing the clearance gap; and
wherein deflecting the aft shroud member is performed responsive to the sensed clearance gap.

### Claim 20 (depends on 19)

The method of claim 19 wherein the clearance gap is sensed by a plurality of clearance gap sensors positioned along a length of the aft shroud member.

### Claim 21

A turbine engine comprising:
a rotatable centrifugal compressor; and
a compressor shroud assembly at least partly encasing the rotatable centrifugal compressor, the compressor shroud assembly comprising:
a static compressor casing;
an actuator mounted to said casing; and
a double-walled impeller shroud comprising a pair of nested arcuate shroud members shaped to follow the contour of the rotatable centrifugal compressor, the pair of nested arcuate shroud members comprising a forward member mounted to said casing and an aft member deflectively coupled to said forward member and operatively coupled to said actuator to effect deflection of said aft member relative to said forward member and to the rotatable centrifugal compressor when said actuator is activated.