Gas expander

Patent metadata

Field	Value
Publication number	US-10767508-B2
Application number	US-201615771060-A
Country	US
Kind code	B2
Filing date	Feb 9, 2016
Priority date	Feb 9, 2016
Publication date	Sep 8, 2020
Grant date	Sep 8, 2020

Abstract

A gas expander includes: a casing where a swirl chamber for a gas to be expanded is formed; a turbine wheel that is housed in the casing and rotationally driven by the expanded gas; a diffuser that is mounted to the casing in a direction of a rotating shaft of the turbine wheel and includes a flow path for the expanded gas to flow in the direction of the rotating shaft; a swirl stopper that is disposed in the diffuser, faces a downstream front end surface of a boss of the turbine wheel that faces the flow path, and includes a closed swirl stopping surface that is disposed to face the downstream front end surface of the boss with a gap between the closed swirl stopping surface and the downstream front end surface; and a swirl preventing plate that circumferentially partition the flow path in the diffuser.

First claim

The invention claimed is:

1. A gas expander comprising:
a casing where a swirl chamber is formed, wherein a gas to be expanded passes through the swirl chamber;
a turbine wheel that is housed in the casing and rotationally driven by the gas, wherein the gas that rotationally drives the turbine wheel has passed through the swirl chamber and expanded;
a diffuser that:
is mounted to the casing in a direction of a rotating shaft of the turbine wheel, and
includes a flow path where the gas, having passed through the turbine wheel, flows in the direction of the rotating shaft,
a swirl stopper that:
is disposed in the diffuser,
faces a downstream front end surface of a boss of the turbine wheel that faces the flow path, and
includes a closed swirl stopping surface that is disposed to face the downstream front end surface of the boss with a gap between the closed swirl stopping surface and the downstream front end surface; and

a swirl preventing plate that circumferentially partitions the flow path,
wherein L31≥D10≥0.75 is satisfied, where D10 is a diameter of an inlet of the flow path and L31 is a distance from the inlet to an end on the upstream side of the swirl preventing plate.

2. The gas expander according to claim 1 , wherein:
the swirl preventing plate is provided on a downstream side of the flow path,
the flow path includes:
a pressure recovery region on an upstream side, and
a swirl flow stopping region on the downstream side continuous with the pressure recovery region.

3. The gas expander according to claim 2 , wherein L31≥D10×0.75 is satisfied, where D10 is a diameter of an inlet of the flow path and L31 is a distance from the inlet to an end on the upstream side of the swirl preventing plate.

4. The gas expander according to claim 2 , wherein L31≥D10×1.2 is satisfied, where D10 is a diameter of an inlet of the flow path and L31 is a distance from the inlet to an end on the upstream side of the swirl preventing plate.

5. The gas expander according to claim 2 , wherein:
in the diffuser, a flow path area increases from the upstream side toward the downstream side,
the swirl preventing plate is disposed so that the end on the upstream side of the swirl preventing plate is away from the inlet, and
A1×1.6≤A2 is satisfied, where A1 is the flow path area at the inlet of the flow path and A2 is the flow path area at the end on the upstream side of the swirl preventing plate.

6. The gas expander according to claim 2 , wherein L35≥D10×0.45 is satisfied, where L35 is an axial dimension of the swirl preventing plate and D10 is a diameter of the inlet of the flow path.

7. The gas expander according to claim 1 , wherein L31≥D10×1.2 is satisfied, where D10 is a diameter of an inlet of the flow path and L31 is a distance from the inlet to an end on the upstream side of the swirl preventing plate.

8. The gas expander according to claim 1 , wherein:
in the diffuser, a flow path area increases from the upstream side toward the downstream side,
the swirl preventing plate is disposed so that the end on the upstream side of the swirl preventing plate is away from the inlet, and A1×1.6≤A2 is satisfied, where A1 is the flow path area at the inlet of the flow path and A2 is the flow path area at the end on the upstream side of the swirl preventing plate.

9. The gas expander according to claim 1 , wherein:
the gas expander includes a plurality of swirl preventing plates, and the plurality of swirl preventing plates radially partition the flow path.

10. The gas expander according to claim 1 , wherein:
the swirl stopper includes a cylindrical member disposed coaxially with the rotating shaft of the turbine wheel, and D32≥D13×0.95 is satisfied, where D32 is a diameter of the closed swirl stopping surface of the swirl stopper and D13 is a diameter of the downstream front end surface of the boss of the turbine wheel.

11. The gas expander according to claim 10 , wherein D13×1.2≥D32≥D13×0.95 is satisfied.

12. The gas expander according to claim 1 , wherein:
the swirl stopper is secured to the swirl preventing plate and the swirl preventing plate is secured to the diffuser, and
the swirl stopper is mounted to a predetermined position of the diffuser via the swirl preventing plate.

13. The gas expander according to claim 12 , wherein:
the gas expander includes a plurality of swirl preventing plates, and
the plurality of the swirl preventing plates radially partition the flow path in the diffuser around the swirl stopper.

14. The gas expander according to claim 1 , wherein:
the gas expander further includes a plurality of swirl preventing plates, and
the plurality of swirl preventing plates radially partition the flow path.

15. A gas expander comprising:
a casing where a swirl chamber is formed, wherein a gas to be expanded passes through the swirl chamber;
a turbine wheel that is housed in the casing and rotationally driven by the gas, wherein the gas that rotationally drives the turbine wheel has passed through the swirl chamber and expanded;
a diffuser that:
is mounted to the casing in a direction of a rotating shaft of the turbine wheel, and includes a flow path where the gas, having passed through the turbine wheel, flows in the direction of the rotating shaft,

a swirl stopper that:
is disposed in the diffuser,
faces a downstream front end surface of a boss of the turbine wheel that faces the flow path, and
includes a closed swirl stopping surface that is disposed to face the downstream front end surface of the boss with a gap between the closed swirl stopping surface and the downstream front end surface; and

a swirl preventing plate that circumferentially partitions the flow path,
wherein L35≥D10×0.45 is satisfied, where L35 is an axial dimension of the swirl preventing plate and D10 is a diameter of the inlet of the flow path.

16. A gas expander comprising:
a casing where a swirl chamber is formed, wherein a gas to be expanded passes through the swirl chamber;
a turbine wheel that is housed in the casing and rotationally driven by the gas, wherein the gas that rotationally drives the turbine wheel has passed through the swirl chamber and expanded;
a diffuser that:
is mounted to the casing in a direction of a rotating shaft of the turbine wheel, and includes a flow path where the gas, having passed through the turbine wheel, flows in the direction of the rotating shaft,

a swirl stopper that:
is disposed in the diffuser,
faces a downstream front end surface of a boss of the turbine wheel that faces the flow path, and
includes a closed swirl stopping surface that is disposed to face the downstream front end surface of the boss with a gap between the closed swirl stopping surface and the downstream front end surface; and

a swirl preventing plate that circumferentially partitions the flow path, wherein in the swirl stopper, the closed swirl stopping surface has a protruding peripheral edge and an inner side recessed from the peripheral edge, and
the swirl stopper covers the downstream front end surface of the boss and an outer peripheral surface of the turbine wheel continuous with the downstream front end surface of the boss.

Assignees

• Mitsubishi Heavy Ind Compressor Corp

Inventors

• Yonemura Naoto
• Hirata Daisuke
• Higashimori Hirotaka

Classifications

• F01D25/30 Primary

  Exhaust heads, chambers, or the like · CPC title

• F05D2220/30

  in turbines · CPC title

• F02K1/40

  Nozzles having means for dividing the jet into a plurality of partial jets or having an elongated cross-section outlet · CPC title

• F05D2240/12

  Fluid guiding means, e.g. vanes · CPC title

• F02C1/04

  the working fluid being heated indirectly {(in a fluidised-bed combustor F02C3/205)} · CPC title