Centrifugal compressor

Patent metadata

Field	Value
Publication number	US-9714658-B2
Application number	US-201214234447-A
Country	US
Kind code	B2
Filing date	Jan 30, 2012
Priority date	Aug 5, 2011
Publication date	Jul 25, 2017
Grant date	Jul 25, 2017

Abstract

A centrifugal compressor, the capacity of which can be increased with keeping the diameter of the impeller at minimum, is provided. The centrifugal compressor includes: a drive gear ( 11 ); a drive shaft ( 3 ) protruding from one side of the drive gear ( 11 ) in a central axis direction of the drive gear ( 11 ); a no. 1 driven pinion gear ( 12 ) configured for rotation of the drive gear ( 11 ) to be transmitted thereto; a no. 1 driven pinion shaft ( 5 ) protruding from both sides of the no. 1 driven pinion gear ( 12 ) in a central axis direction of the no. 1 driven pinion gear ( 12 ); and a couple of first stage compressor sections ( 7 a, 7 b ), each of which is provided in each end of the no. 1 driven pinion shaft ( 5 ) and is configured to compress fluid by rotation of the no. 1 driven pinion shaft ( 5 ).

First claim

The invention claimed is:

1. A centrifugal compressor comprising:
a drive gear;
a drive shaft protruding from one side of the drive gear in a central axis direction of the drive gear;
a no. 1 driven pinion gear configured for rotation of the drive gear to be transmitted thereto;
a no. 1 driven pinion shaft protruding from both sides of the no. 1 driven pinion gear in a central axis direction of the no. 1 driven pinion gear;
a couple of first stage compressor sections, each of which is provided in each end of the no. 1 driven pinion shaft and is configured to compress fluid by rotation of the no. 1 driven pinion shaft;
a no. 1 idle gear provided between the no. 1 driven pinion gear and the drive gear;
a no. 2 driven pinion gear configured for rotation of the drive gear to be transmitted thereto;
a no. 2 driven pinion shaft protruding from the no. 2 driven pinion gear in a central axis direction of the no. 2 driven pinion gear;
a second stage compressor section provided to the no. 2 driven pinion shaft; and
a no. 2 idle gear provided between the no. 2 driven pinion gear and the drive gear, wherein
rotation axes of the drive shaft, the no. 1 driven pinion shaft, and the no. 2 driven pinion shaft are positioned at the same level in height,
a rotation axis of the no. 1 idle gear is positioned upward or downward with respect to a plane defined by the rotation axes of the drive shaft, the no. 1 driven pinion shaft, and the no. 2 driven pinion shaft, and
a rotation axis of the no. 2 idle gear is positioned at the same side of the rotation axis of the no. 1 idle gear with respect to the plane defined by the rotation axes of the drive shaft, the no. 1 driven pinion shaft, and the no. 2 driven pinion shaft.

2. The centrifugal compressor according to claim 1 , further comprising:
a third stage compressor section provided to the no. 2 driven pinion shaft in an opposite side to the second stage compressor section in the central axis direction of the no. 2 driven pinion gear;
a no. 3 driven pinion gear configured for rotation of the drive gear to be transmitted thereto;
a no. 3 driven pinion shaft protruding from the no. 3 driven pinion gear in a central axis direction of the no. 3 driven pinion gear;
a fourth stage compressor section provided to the no. 3 driven pinion shaft; and
a no. 3 idle gear provided between the no. 3 driven pinion gear and the drive gear, wherein
a rotation axis of the no. 3 idle gear is positioned at on an opposite side of the rotation axes of the no. 1 idle gear and the no . 2 idle gear with respect to the plane defined by the rotation axes of the drive shaft, the no. 1 driven pinion shaft, and the no. 2 driven pinion shaft.

3. The centrifugal compressor according to claim 2 , further comprising a heat exchanger provided to a pipe connecting the pair of the first stage compressor sections and the second stage compressor section, the heat exchanger exchanging heat of the fluid discharged from the pair of the first stage compressor sections, wherein
the heat exchanger comprises: two inlets, each of which is connected to each of the pair of the first stage compressor sections; and an outlet connected to the second stage compressor section.

4. The centrifugal compressor according to claim 3 , further comprising:
an inlet guide vane that is provided to each of the pair of the first stage compressor sections at an upstream side thereof and configured to control an amount of the fluid introduced to the pair of the first stage compressor sections;
a first pressure sensor and a flowmeter provided to each of the pair of the first stage compressor sections at an upstream side thereof;
a second pressure sensor provided to each of the pair of the first stage compressor sections at a downstream side thereof; and
a control unit configured to control the inlet guide vane based on measurements detected by the first pressure sensor, the flow meter, and the second pressure sensor.

5. The centrifugal compressor according to claim 2 , further comprising:
an inlet guide vane that is provided to each of the pair of the first stage compressor sections at an upstream side thereof and configured to control an amount of the fluid introduced to the pair of the first stage compressor sections;
a first pressure sensor and a flowmeter provided to each of the pair of the first stage compressor sections at an upstream side thereof;
a second pressure sensor provided to each of the pair of the first stage compressor sections at a downstream side thereof; and
a control unit configured to control the inlet guide vane based on measurements detected by the first pressure sensor, the flow meter, and the second pressure sensor.

6. The centrifugal compressor according to claim 1 , further comprising a heat exchanger provided to a pipe connecting the pair of the first stage compressor sections and the second stage compressor section, the heat exchanger exchanging heat of the fluid discharged from the pair of the first stage compressor sections, wherein
the heat exchanger comprises: two inlets, each of which is connected to each of the pair of the first stage compressor sections; and an outlet connected to the second stage compressor section.

7. The centrifugal compressor according to claim 6 , further comprising:
an inlet guide vane that is provided to each of the pair of the first stage compressor sections at an upstream side thereof and configured to control an amount of the fluid introduced to the pair of the first stage compressor sections;
a first pressure sensor and a flowmeter provided to each of the pair of the first stage compressor sections at an upstream side thereof;
a second pressure sensor provided to each of the pair of the first stage compressor sections at a downstream side thereof; and
a control unit configured to control the inlet guide vane based on measurements detected by the first pressure sensor, the flow meter, and the second pressure sensor.

8. The centrifugal compressor according to claim 1 , further comprising:
an inlet guide vane that is provided to each of the pair of the first stage compressor sections at an upstream side thereof and configured to control an amount of the fluid introduced to the pair of the first stage compressor sections;
a first pressure sensor and a flowmeter provided to each of the pair of the first stage compressor sections at an upstream side thereof;
a second pressure sensor provided to each of the pair of the first stage compressor sections at a downstream side thereof; and
a control unit configured to control the inlet guide vane based on measurements detected by the first pressure sensor, the flow meter, and the second pressure sensor.

Assignees

• Miyata Hiroyuki
• Yonemura Naoto
• Mitsubishi Heavy Ind Compressor Corp

Inventors

• Miyata Hiroyuki
• Yonemura Naoto

Classifications

• F25J3/04018

  of main feed air · CPC title

• F04D17/12 Primary

  Multi-stage pumps · CPC title

• F25J3/04957

  and inter-connecting equipments upstream of the fractionation unit (s), i.e. at the "front-end" · CPC title

• F04D27/0246

  by varying geometry within the pumps, e.g. by adjusting vanes · CPC title

• F04D25/163

  driven by a common gearing arrangement · CPC title