Geared Compressor

Abstract

To provide a geared compressor which can suppress the enlargement of an occupation space while improving an output.SOLUTION: A geared compressor comprises: a drive gear rotated by the rotation of a motor; an intermediate gear engaged with the drive gear; a first drive-side pinion engaged with the drive gear in a position apart from the intermediate gear; a first intermediate-side pinion engaged with the intermediate gear in a position apart from the drive gear; a second intermediate-side pinion engaged with the intermediate gear in a position apart from the drive gear and the first intermediate-side pinion; a first compression part connected to the first drive-side pinion and compressing a working fluid supplied from the outside by the rotation of the first drive-side pinion; a second compression part connected to the first intermediate-side pinion and compressing a working fluid supplied from the outside by the rotation of the first intermediate-side pinion; and a uniaxial multistage compressor connected to the second intermediate-side pinion and further compressing the working fluid which is compressed by at least either of the first compression part and the second compression part.SELECTED DRAWING: Figure 1

Description

[Technical Field]

[0001] The present disclosure relates to geared compressors. [Background technology]

[0002] For example, Patent Document 1 discloses a transmission (geared compressor) that includes a driving pinion (driving gear) driven by a steam turbine, a large gear as an intermediate gear that meshes with the driving pinion and the turbomachine rotor (compression section), and a driven pinion that is connected to a main compressor while meshing with the driving gear. [Prior art documents] [Patent documents]

[0003] [Patent Document 1] Patent No. 4991789 Summary of the Invention [Problem to be solved by the invention]

[0004] In order to improve the output of a geared compressor, the number of compression sections may be increased. However, due to restrictions on the installation of gears for rotating the compression sections, it may be necessary to install new intermediate gears between the gears and the drive gear or existing intermediate gears. Therefore, as the output of the geared compressor is improved, the space occupied by the geared compressor may increase.

[0005] The present disclosure has been made to solve the above-mentioned problems, and has an object to provide a geared compressor that can improve output while suppressing an increase in the occupied space. [Means for solving the problem]

[0006] In order to solve the above-described problems, a geared compressor according to the present disclosure includes: a drive gear rotated by rotation of a motor; an intermediate gear meshing with the drive gear; a first drive-side pinion meshing with the drive gear at a position spaced apart from the intermediate gear; a first intermediate-side pinion meshing with the intermediate gear at a position spaced apart from the drive gear; a second intermediate-side pinion meshing with the intermediate gear at a position spaced apart from the drive gear and the first intermediate-side pinion; a first compression unit connected to the first drive-side pinion and compressing a working fluid supplied from an outside by rotation of the first drive-side pinion; a second compression unit connected to the first intermediate-side pinion and compressing a working fluid supplied from an outside by rotation of the first intermediate-side pinion; and a single-shaft multi-stage compressor connected to the second intermediate-side pinion and further compressing the working fluid compressed by at least one of the first compression unit and the second compression unit. The intermediate gear meshes with the drive gear at an upper half portion thereof, the second intermediate pinion meshes with the intermediate gear at a lower half portion thereof, and the motor and the single-shaft multi-stage compressor are placed on a base located below the drive gear and the intermediate gear. do. [Effects of the Invention]

[0007] According to the present disclosure, it is possible to provide a geared compressor that can improve output while suppressing an increase in the occupied space. [Brief explanation of the drawings]

[0008] [Figure 1] 1 is a schematic diagram illustrating a general configuration of a geared compressor according to an embodiment of the present disclosure. FIG. [Figure 2] FIG. 2 is a partial cross-sectional view taken along line II-II in FIG. DETAILED DESCRIPTION OF THE INVENTION

[0009] Hereinafter, a geared compressor according to an embodiment of the present disclosure will be described with reference to the drawings.

[0010] (Geared compressor) A geared compressor compresses a process gas as a working fluid generated in, for example, a chemical plant, and supplies the pressurized process gas to a reaction device provided in the chemical plant.

[0011] 1 and 2, the geared compressor 100 has a multi-shaft, multi-stage configuration that drives a compression section 3 having a plurality of impellers. The geared compressor 100 includes a motor 1, a compression section drive mechanism 2, the compression section 3, a single-shaft multi-stage compressor 4, and a shaft coupling 5.

[0012] (Motor) The motor 1 is a drive source that generates power to drive the geared compressor 100. The motor 1 has an output shaft 10 and a motor body 11 that rotates the output shaft 10. The output shaft 10 is a cylindrical drive shaft that extends around an output axis O1 that extends horizontally and is rotatable about this output axis O1.

[0013] The motor body 11 is fixed in a state in which it is placed on a foundation B such as the ground, a stand, or a base plate. The motor body 11 has, for example, a motor stator (not shown) as a stator, and a motor rotor (not shown) as a rotor fixed integrally with the output shaft 10.

[0014] The motor stator is electrically connected to, for example, an external power system. When a current flows through the coil of this motor stator, an electromagnetic force is generated that rotates the motor rotor in the circumferential direction of the output shaft 10. In other words, when electric power is input from the outside to the motor stator of the motor main body 11, the output shaft 10 rotates.

[0015] (Compression section drive mechanism) The compression unit drive mechanism 2 rotates a device that compresses the working fluid G supplied from the outside by transmitting power (torque) generated by the motor 1. The compression unit drive mechanism 2 has a gear case 20, a drive gear 21, a first drive-side pinion 22, a second drive-side pinion 23, an intermediate gear 24, a first intermediate-side pinion 25, a second intermediate-side pinion 26, and a bearing 27.

[0016] (Gear case) The gear case 20 is a casing for accommodating a plurality of gears therein.

[0017] (Drive gear) The drive gear 21 is housed in the gear case 20 and is rotated by the rotation of the motor 1. The drive gear 21 has a drive support shaft 210 and a drive gear body 211. The drive support shaft 210 has a cylindrical shape extending about a drive axis O2 that extends horizontally.

[0018] In this embodiment, the drive shaft 210 is integrally connected to the output shaft 10 of the motor 1 via a flexible coupling C. Therefore, the drive shaft 210 rotates as the output shaft 10 rotates.

[0019] Here, the output axis O1 of the output shaft 10 and the drive axis O2 of the drive support shaft 210 are on the same straight line. The output shaft 10 and the drive support shaft 210 share an axis O as their center line. The axis O is made up of the output axis O1 and the drive axis O2.

[0020] In this embodiment, the direction in which this axis O extends (the vertical direction in FIG. 2) is simply referred to as the "axial direction Da." Furthermore, of both sides of the axial direction Da, one side (the upper side in FIG. 2) is simply referred to as the "one side Dab," and the opposite side (the lower side in FIG. 2) is simply referred to as the "other side Daf."

[0021] The drive gear body 211 is fixed to the drive support shaft 210 from the outer periphery side and is a helical gear that expands around the drive support shaft 210. The drive gear body 211 expands in a direction perpendicular to the axis O. The drive support shaft 210 protrudes from the drive gear body 211 to one side Dab and the other side Daf.

[0022] For ease of explanation, the direction perpendicular to the axis O (the direction in which the drive gear body 211 extends) and along which the imaginary plane X that bisects the drive gear 21 in the axial direction Da will be referred to as the "in-plane direction Pi." In this case, the axial direction Da corresponds to the "out-of-plane direction Po" with respect to the imaginary plane X.

[0023] (First driving pinion) The first drive-side pinion 22 is a gear that is housed in the gear case 20 and rotates in conjunction with the rotation of the drive gear 21. The first drive-side pinion 22 has a first drive-side pinion support shaft 220, a first drive-side pinion body 221, and a first thrust bearing 222. The first drive-side pinion support shaft 220 has a cylindrical shape extending about a first axis A1 that is parallel to the axis O.

[0024] The first drive side pinion body 221 is a helical gear that is fixed to the first drive side pinion spindle 220 from the outer periphery and expands around the first drive side pinion spindle 220. The first drive side pinion body 221 expands in a direction perpendicular to the first axis A1. The first drive side pinion spindle 220 protrudes from the first drive side pinion body 221 to one side Dab and the other side Daf.

[0025] The first drive side pinion body 221 is adjacent to the drive gear body 211 in the in-plane direction Pi and meshes with the drive gear body 211. In this embodiment, the first drive side pinion body 221 meshes only with the drive gear upper half portion 211a of the drive gear body 211.

[0026] In this embodiment, the outer diameter of the first driving side pinion body 221 is smaller than the outer diameter of the driving gear body 211. Therefore, the number of teeth of the first driving side pinion body 221 is smaller than the number of teeth of the driving gear body 211.

[0027] In this embodiment, the drive gear upper half 211a of the drive gear main body 211 means the drive gear main body 211 in the region above the axis O in the vertical direction (up and down direction in Figure 1) when viewing the drive gear main body 211 from the axial direction Da.

[0028] Further, the drive gear lower half 211b of the drive gear body 211 refers to the region of the drive gear body 211 that is vertically below the axis O when the drive gear body 211 is viewed from the axial direction Da.

[0029] In addition, the "outer diameter" of the gear in this embodiment is, for example, the root diameter, tip diameter, or pitch diameter, which can be measured as the distance (dimension) from the center axis of each gear.

[0030] The first thrust bearings 222 are a pair of thrust bearings fixed so as to surround the outer periphery of the first drive-side pinion support shaft 220 of the first drive-side pinion 22. The first thrust bearings 222 are arranged on one side Dab and the other side Daf of the first drive-side pinion body 221 of the first drive-side pinion 22, respectively.

[0031] The first thrust bearing 222 is formed to have a larger diameter than the first drive-side pinion body 221. The first thrust bearing 222 is in sliding contact with, for example, a thrust collar (not shown) that is integral with the first drive-side pinion support shaft 220 and spreads outward in a disk shape from the first drive-side pinion support shaft 220 in the axial direction Da. This restricts the first drive-side pinion body 221 from being displaced in the axial direction Da.

[0032] (Second driving side pinion) The second drive-side pinion 23 is a gear housed in the gear case 20 and rotates in conjunction with the rotation of the drive gear 21. The second drive-side pinion 23 has a second drive-side pinion support shaft 230, a second drive-side pinion body 231, and a second thrust bearing 232. The second drive-side pinion support shaft 230 has a cylindrical shape extending about a second axis A2 that is parallel to the axis O.

[0033] The second drive-side pinion body 231 is a helical gear that expands around the second drive-side pinion support shaft 230. The second drive-side pinion body 231 expands in a direction perpendicular to the second axis A2. The second drive-side pinion support shaft 230 protrudes from the second drive-side pinion body 231 to one side Dab and the other side Daf.

[0034] The second drive side pinion body 231 meshes with the drive gear body 211 at a position separated in the in-plane direction Pi from the first drive side pinion body 221 of the first drive side pinion 22. The second drive side pinion body 231 is adjacent to the drive gear body 211 in the in-plane direction Pi. In this embodiment, the second drive side pinion body 231 meshes only with the portion of the drive gear body 211 where the drive gear upper half portion 211a and the drive gear lower half portion 211b switch.

[0035] In this embodiment, the outer diameter of the second drive side pinion body 231 is the same as the outer diameter of the first drive side pinion body 221 of the first drive side pinion 22. Therefore, the number of teeth of the second drive side pinion body 231 is the same as the number of teeth of the first drive side pinion body 221 of the first drive side pinion 22.

[0036] The second thrust bearings 232 are a pair of thrust bearings fixed so as to surround the outer periphery of the second drive-side pinion support shaft 230 of the second drive-side pinion 23. The second thrust bearings 232 are arranged on one side Dab and the other side Daf of the second drive-side pinion body 231 of the second drive-side pinion 23, respectively.

[0037] The second thrust bearing 232 is formed to have a larger diameter than the second drive-side pinion body 231. The second thrust bearing 232 is in sliding contact with, for example, a thrust collar (not shown) that is integral with the second drive-side pinion support shaft 230 and spreads outward in a disk shape from the second drive-side pinion support shaft 230 in the axial direction Da. This restricts the second drive-side pinion body 231 from being displaced in the axial direction Da.

[0038] (Intermediate gear) The intermediate gear 24 is housed in the gear case 20 and rotates in conjunction with the rotation of the drive gear 21. The intermediate gear 24 has an intermediate support shaft 240 and an intermediate gear body 241. The intermediate support shaft 240 has a cylindrical shape extending about an intermediate axis O3 that is parallel to the axis O.

[0039] The intermediate gear body 241 is fixed to the intermediate support shaft 240 from the outer periphery and is a helical gear that expands around the intermediate support shaft 240. The intermediate gear body 241 expands in a direction perpendicular to the intermediate axis O3. The intermediate support shaft 240 protrudes from the intermediate gear body 241 to one side Dab and the other side Daf.

[0040] The intermediate gear body 241 meshes with the drive gear body 211 at a position spaced apart in the in-plane direction Pi from the first drive side pinion body 221 of the first drive side pinion 22 and the second drive side pinion body 231 of the second drive side pinion 23, and is adjacent to the drive gear body 211 in the in-plane direction Pi.

[0041] 1, the intermediate gear body 241 in this embodiment meshes with the drive gear upper half portion 211a of the drive gear body 211. Therefore, the intermediate axis O3 is located above the axis O in the vertical direction.

[0042] (First intermediate pinion) The first intermediate side pinion 25 is a gear that is housed in the gear case 20 and rotates in conjunction with the rotation of the intermediate gear 24. The first intermediate side pinion 25 has a first intermediate side pinion support shaft 250, a first intermediate side pinion body 251, and a third thrust bearing 252. The first intermediate side pinion support shaft 250 has a cylindrical shape extending about a third axis A3 that is parallel to the axis O.

[0043] The first intermediate side pinion body 251 is a helical gear that is fixed to the first intermediate side pinion support shaft 250 from the outer periphery and expands around the first intermediate side pinion support shaft 250. The first intermediate side pinion body 251 expands in a direction perpendicular to the third axis A3. The first intermediate side pinion support shaft 250 protrudes from the first intermediate side pinion body 251 to one side Dab and the other side Daf.

[0044] The first intermediate side pinion body 251 is adjacent to the intermediate gear body 241 in the in-plane direction Pi and meshes with the intermediate gear body 241. Intermediate gear lower half 241b It only fits in.

[0045] In this embodiment, the intermediate gear upper half 241a of the intermediate gear main body 241 refers to the region of the intermediate gear main body 241 that is vertically above the intermediate axis O3 when the intermediate gear main body 241 is viewed from the axial direction Da.

[0046] The intermediate gear lower half 241b of the intermediate gear main body 241 refers to the region of the intermediate gear main body 241 that is vertically below the intermediate axis O3 when the intermediate gear main body 241 is viewed from the axial direction Da.

[0047] In this embodiment, the outer diameter of the first intermediate side pinion body 251 is the same as the outer diameter of the first driving side pinion body 221 of the first driving side pinion 22. Therefore, the number of teeth of the first intermediate side pinion body 251 is the same as the number of teeth of the first driving side pinion body 221 of the first driving side pinion 22.

[0048] The third thrust bearings 252 are a pair of thrust bearings fixed so as to surround the outer periphery of the first intermediate side pinion support shaft 250 of the first intermediate side pinion 25. The third thrust bearings 252 are arranged on one side Dab and the other side Daf of the first intermediate side pinion body 251 of the first intermediate side pinion 25.

[0049] The third thrust bearing 252 is formed to have a larger diameter than the first intermediate side pinion body 251. The third thrust bearing 252 is in sliding contact with, for example, a thrust collar (not shown) that is integral with the first intermediate side pinion support shaft 250 and spreads outward in a disk shape from the first intermediate side pinion support shaft 250 in the axial direction Da. This restricts the first intermediate side pinion body 251 from being displaced in the axial direction Da.

[0050] (Second intermediate pinion) The second intermediate pinion 26 is housed in the gear case 20, Intermediate gear 24The second intermediate side pinion 26 has a second intermediate side pinion support shaft 260, a second intermediate side pinion body 261, and a fourth thrust bearing 262. The second intermediate side pinion support shaft 260 has a cylindrical shape extending about a fourth axis A4 that is parallel to the axis O.

[0051] The second intermediate side pinion body 261 is a helical gear that is fixed to the second intermediate side pinion support shaft 260 from the outer periphery side and expands around the second intermediate side pinion support shaft 260. 。 The second intermediate side pinion body 261 extends in a direction perpendicular to the fourth axis A4. The second intermediate side pinion support shaft 260 protrudes from the second intermediate side pinion body 261 to one side Dab and the other side Daf.

[0052] The second intermediate side pinion body 261 meshes with the intermediate gear body 241 at a position spaced apart in the in-plane direction Pi from the first intermediate side pinion body 251 of the first intermediate side pinion 25. The second intermediate side pinion body 261 is adjacent to the intermediate gear body 241 in the in-plane direction Pi.

[0053] The second intermediate side pinion body 261 in this embodiment meshes only with the intermediate gear lower half portion 241b of the intermediate gear body 241. Specifically, the second intermediate side pinion body 261 is disposed directly below the intermediate gear body 241.

[0054] In this embodiment, the outer diameter of the second intermediate side pinion body 261 is the same as the outer diameter of the first driving side pinion body 221 of the first driving side pinion 22. Therefore, the number of teeth of the second intermediate side pinion body 261 is the same as the number of teeth of the first driving side pinion body 221 of the first driving side pinion 22.

[0055] The fourth thrust bearings 262 are a pair of thrust bearings fixed so as to surround the outer periphery of the second intermediate side pinion support shaft 260 of the second intermediate side pinion 26. The fourth thrust bearings 262 are arranged on one side Dab and the other side Daf of the second intermediate side pinion body 261 of the second intermediate side pinion 26.

[0056] The fourth thrust bearing 262 is formed to have a larger diameter than the second intermediate side pinion body 261. The fourth thrust bearing 262 is in sliding contact with, for example, a thrust collar (not shown) that is integral with the second intermediate side pinion support shaft 260 and extends in a disk shape from the second intermediate side pinion support shaft 260 toward the outer periphery, in the axial direction Da. This restricts the second intermediate side pinion body 261 from being displaced in the axial direction Da.

[0057] (Compression section) The compression section 3 is rotated by the rotation of the first drive-side pinion 22, the second drive-side pinion 23, and the first intermediate-side pinion 25, thereby compressing the working fluid G supplied from the outside. The compression section 3 is composed of a first compression section 31, a second compression section 32, a third compression section 33, a fourth compression section 34, a fifth compression section 35, and a sixth compression section 36.

[0058] (First compression section) The first compression section 31 is connected to the first drive-side pinion 22 and is rotated by the rotation of the first drive-side pinion 22 to compress the working fluid G. The first compression section 31 has a first rotor 310 and a first compression section casing 311. The first rotor 310 has a first rotary shaft 310a and a first impeller 310b.

[0059] The first rotating shaft 310a is a cylindrical member that extends around the first axis A1 and is rotatable around the first axis A1. The first rotating shaft 310a is integrally connected to the first driving-side pinion support shaft 220 of the first driving-side pinion 22 from one side Dab, and protrudes from the gear case 20 to the one side Dab.

[0060] The first impeller 310b is fixed to the first rotary shaft 310a so as to cover, from the outer circumferential side, a portion of the first rotary shaft 310a that protrudes from the gear case 20 to one side Dab. When the first impeller 310b is fixed to the first rotary shaft 310a, the first impeller 310b has a plurality of blades that are arranged in the circumferential direction of the first rotary shaft 310a.

[0061] The first compression section casing 311 covers the outer periphery of the first impeller 310b and defines a first compression passage therein together with the first impeller 310b. In this embodiment, the first compression section casing 311 is formed integrally with the gear case 20.

[0062] The first compression section casing 311 has a first gas inlet 311a for introducing the working fluid G from the outside into the first compression passage, and a first gas discharge port 311b for discharging the compressed working fluid G from the first compression passage to the outside. Pipes (not shown) through which the working fluid G flows are connected to the first gas inlet 311a and the first gas discharge port 311b.

[0063] In this embodiment, a single-stage compression mechanism is configured by the first rotor 310 and the first compression section casing 311 in the first compression section 31. The first compression section 31 has a single first impeller 310b.

[0064] (Second compression section) The second compression section 32 is connected to the first intermediate side pinion 25 and is rotated by the rotation of the first intermediate side pinion 25 to compress the working fluid G. The second compression section 32 has a second rotor 320 and a second compression section casing 321. The second rotor 320 has a second rotary shaft 320a and a second impeller 320b.

[0065] The second rotating shaft 320a is a cylindrical member that extends about the third axis A3 and is rotatable around the third axis A3. The second rotating shaft 320a is integrally connected to the first intermediate side pinion support shaft 250 of the first intermediate side pinion 25 from one side Dab, and protrudes from the gear case 20 to the one side Dab.

[0066] The second impeller 320b is fixed to the second rotary shaft 320a so as to cover, from the outer circumferential side, a portion of the second rotary shaft 320a that protrudes from the gear case 20 to one side Dab. When the second impeller 320b is fixed to the second rotary shaft 320a, the second impeller 320b has a plurality of blades that are arranged in the circumferential direction of the second rotary shaft 320a.

[0067] The second compression section casing 321 covers the second impeller 320b and defines a second compression passage therein together with the second impeller 320b. The second compression section casing 321 in this embodiment is formed integrally with the gear case 20.

[0068] The second compression section casing 321 has a second gas inlet 321a for introducing the working fluid G from the outside into the second compression passage, and a second gas discharge port 321b for discharging the compressed working fluid G from the second compression passage to the outside. Pipes through which the working fluid G flows are connected to the second gas inlet 321a and the second gas discharge port 321b.

[0069] In this embodiment, a single-stage compression mechanism is configured by the second rotor 320 and the second compression section casing 321 in the second compression section 32. The second compression section 32 has a single second impeller 320b.

[0070] The second compression section 32 compresses the working fluid G supplied from the outside at a stage before the first compression section 31. Therefore, the working fluid G compressed in the second compression passage of the second compression section 32 is introduced through piping into the first compression passage of the first compression section 31 and is further compressed.

[0071] The outer diameter of the second impeller 320b of the second rotor 320 in the second compression section 32 is larger than the outer diameter of the first impeller 310b of the first rotor 310 in the first compression section 31. That is, each blade of the first impeller 310b is larger than each blade of the second impeller 320b. Small It is formed.

[0072] (Third compression section) The third compression section 33 is connected to the second drive-side pinion 23 and is rotated by the rotation of the second drive-side pinion 23 to compress the working fluid G. The third compression section 33 has a third rotor 330 and a third compression section casing 331. The third rotor 330 has a third rotary shaft 330a and a third impeller 330b.

[0073] The third rotating shaft 330a is a cylindrical member that extends about the second axis A2 and is rotatable around the second axis A2. The third rotating shaft 330a is integrally connected to the second driving-side pinion support shaft 230 of the second driving-side pinion 23 from one side Dab, and protrudes from the gear case 20 to the one side Dab.

[0074] The third impeller 330b is fixed to the third rotary shaft 330a so as to cover, from the outer circumferential side, a portion of the third rotary shaft 330a that protrudes from the gear case 20 to one side Dab. When the third impeller 330b is fixed to the third rotary shaft 330a, the third impeller 330b has a plurality of blades that are arranged in the circumferential direction of the third rotary shaft 330a.

[0075] The third compression section casing 331 covers the third impeller 330b and defines a third compression passage therein together with the third impeller 330b. The third compression section casing 331 in this embodiment is formed integrally with the gear case 20.

[0076] The third compression section casing 331 has a third gas inlet 331a for introducing the working fluid G from the outside into the third compression passage, and a third gas discharge port 331b for discharging the compressed working fluid G from the third compression passage to the outside. Pipes through which the working fluid G flows are connected to the third gas inlet 331a and the third gas discharge port 331b.

[0077] In this embodiment, a single-stage compression mechanism is configured by the third rotor 330 and the third compression section casing 331 in the third compression section 33. The third compression section 33 has a single third impeller 330b.

[0078] The third compression section 33 compresses the working fluid G at a stage subsequent to the first compression section 31. Therefore, the working fluid G compressed in the first compression passage of the first compression section 31 is introduced through piping into the third compression passage of the third compression section 33 and further compressed.

[0079] The outer diameter of the third impeller 330b of the third rotor 330 in the third compression section 33 is smaller than the outer diameter of the first impeller 310b of the first rotor 310 in the first compression section 31. That is, each blade of the third impeller 330b is formed smaller than each blade of the first impeller 310b.

[0080] (Fourth compression section) The fourth compression section 34 is connected to the first intermediate side pinion 25 and is rotated by the rotation of the first intermediate side pinion 25 to compress the working fluid G. The fourth compression section 34 has a fourth rotor 340 and a fourth compression section casing 341. The fourth rotor 340 has a fourth rotary shaft 340a and a fourth impeller 340b.

[0081] The fourth rotation shaft 340a is a cylindrical member that extends around the third axis A3 and is rotatable around the third axis A3. The fourth rotation shaft 340a is integrally connected to the first intermediate side pinion support shaft 250 of the first intermediate side pinion 25 from the other side Daf, and protrudes from the gear case 20 to the other side Daf.

[0082] The fourth impeller 340b is fixed to the fourth rotary shaft 340a so as to cover, from the outer circumferential side, a portion of the fourth rotary shaft 340a that protrudes from the gear case 20 to the other side Daf. When fixed to the fourth rotary shaft 340a, the fourth impeller 340b has a plurality of blades that are arranged in the circumferential direction of the fourth rotary shaft 340a.

[0083] The fourth compression section casing 341 covers the fourth impeller 340b and defines a fourth compression passage therein together with the fourth impeller 340b. The fourth compression section casing 341 in this embodiment is formed integrally with the gear case 20.

[0084] The fourth compression section casing 341 has a fourth gas inlet 341a for introducing the working fluid G from the outside into the fourth compression passage, and a fourth gas outlet 341b for discharging the compressed working fluid G from the fourth compression passage to the outside. Pipes through which the working fluid G flows are connected to the fourth gas inlet 341a and the fourth gas outlet 341b.

[0085] In the present embodiment, the fourth rotor 340 and the fourth compression section casing 341 in the fourth compression section 34 constitute a one-stage compression mechanism. The fourth compression section 34 has a single fourth impeller 340b. The fourth compression section 34 in the present embodiment compresses the working fluid G at a stage subsequent to the second compression section 32 and prior to the first compression section 31.

[0086] Therefore, the working fluid G compressed in the second compression passage of the second compression section 32 is introduced through the piping into the fourth compression passage of the fourth compression section 34 and further compressed. The working fluid G compressed in the fourth compression passage of the fourth compression section 34 is introduced through the piping into the first compression passage of the first compression section 31 and further compressed.

[0087] The outer diameter of the fourth impeller 340b of the fourth rotor 340 in the fourth compression section 34 is smaller than the outer diameter of the second impeller 320b of the second rotor 320 in the second compression section 32, and larger than the outer diameter of the first impeller 310b in the first compression section 31. That is, each blade of the fourth impeller 340b is formed smaller than each blade of the second impeller 320b, and larger than each blade of the first impeller 310b.

[0088] (Fifth compression section) The fifth compression section 35 is connected to the first drive-side pinion 22 and is rotated by the rotation of the first drive-side pinion 22 to compress the working fluid G. The fifth compression section 35 has a fifth rotor 350 and a fifth compression section casing 351. The fifth rotor 350 has a fifth rotary shaft 350a and a fifth impeller 350b.

[0089] The fifth rotating shaft 350a is a cylindrical member that extends around the first axis A1 and is rotatable around the first axis A1. The fifth rotating shaft 350a is integrally connected to the first driving-side pinion support shaft 220 of the first driving-side pinion 22 from the other side Daf, and protrudes from the gear case 20 to the other side Daf.

[0090] The fifth impeller 350b is fixed to the fifth rotating shaft 350a so as to cover, from the outer circumferential side, a portion of the fifth rotating shaft 350a that protrudes from the gear case 20 to the other side Daf. When the fifth impeller 350b is fixed to the fifth rotating shaft 350a, the fifth impeller 350b has a plurality of blades that are arranged in the circumferential direction of the fifth rotating shaft 350a.

[0091] The fifth compression section casing 351 covers the fifth impeller 350b and defines a fifth compression passage therein together with the fifth impeller 350b. The fifth compression section casing 351 in this embodiment is formed integrally with the gear case 20.

[0092] The fifth compression section casing 351 has a fifth gas inlet 351a for introducing the working fluid G from the outside into the fifth compression passage, and a fifth gas outlet 351b for discharging the compressed working fluid G from the fifth compression passage to the outside. Pipes through which the working fluid G flows are connected to the fifth gas inlet 351a and the fifth gas outlet 351b.

[0093] In this embodiment, the fifth rotor 350 and the fifth compression section casing 351 in the fifth compression section 35 constitute a one-stage compression mechanism. The fifth compression section 35 has a single fifth impeller 350b. The fifth compression section 35 in this embodiment compresses the working fluid G at a stage subsequent to the first compression section 31 and prior to the third compression section 33.

[0094] Therefore, the working fluid G compressed in the first compression passage of the first compression section 31 is introduced through the piping into the fifth compression passage of the fifth compression section 35 and further compressed. The working fluid G compressed in the fifth compression passage of the fifth compression section 35 is introduced through the piping into the third compression passage of the third compression section 33 and further compressed.

[0095] The outer diameter of the fifth impeller 350b of the fifth rotor 350 in the fifth compression section 35 is smaller than the outer diameter of the first impeller 310b of the first rotor 310 in the first compression section 31, and larger than the outer diameter of the third impeller 330b in the third compression section 33. That is, each blade of the fifth impeller 350b is formed smaller than each blade of the first impeller 310b, and larger than each blade of the third impeller 330b.

[0096] (Sixth compression section) The sixth compression section 36 is connected to the second drive-side pinion 23 and is rotated by the rotation of the second drive-side pinion 23 to compress the working fluid G. The sixth compression section 36 has a sixth rotor 360 and a sixth compression section casing 361. The sixth rotor 360 has a sixth rotary shaft 360a and a sixth impeller 360b.

[0097] The sixth rotating shaft 360a is a cylindrical member that extends around the second axis A2 and is rotatable about the second axis A2. The sixth rotating shaft 360a is integrally connected to the second driving-side pinion support shaft 230 of the second driving-side pinion 23 from the other side Daf, and protrudes from the gear case 20 to the other side Daf.

[0098] The sixth impeller 360b is fixed to the sixth rotating shaft 360a so as to cover, from the outer circumferential side, a portion of the sixth rotating shaft 360a that protrudes from the gear case 20 to the other side Daf. When fixed to the sixth rotating shaft 360a, the sixth impeller 360b has a plurality of blades that are arranged in the circumferential direction of the sixth rotating shaft 360a.

[0099] The sixth compression section casing 361 covers the sixth impeller 360b and defines a sixth compression passage therein together with the sixth impeller 360b. The sixth compression section casing 361 in this embodiment is formed integrally with the gear case 20.

[0100] The sixth compression section casing 361 has a sixth gas inlet 361a for introducing the working fluid G from the outside into the sixth compression passage, and a sixth gas outlet 361b for discharging the compressed working fluid G from the sixth compression passage to the outside.

[0101] In this embodiment, a single-stage compression mechanism is configured by the sixth rotor 360 and the sixth compression section casing 361 in the sixth compression section 36. The sixth compression section 36 has a single sixth impeller 360b.

[0102] The sixth compression section 36 in this embodiment compresses the working fluid G at a stage subsequent to the third compression section 33. Therefore, the working fluid G compressed in the third compression passage of the third compression section 33 is introduced through piping into the sixth compression passage of the sixth compression section 36 and further compressed.

[0103] The outer diameter of the sixth impeller 360b of the sixth rotor 360 in the sixth compression section 36 is smaller than the outer diameter of the third impeller 330b of the third rotor 330 in the third compression section 33. That is, each blade of the sixth impeller 360b is formed smaller than each blade of the third impeller 330b.

[0104] Therefore, the working fluid G supplied to the compression section 3 from the outside is introduced into the second compression section 32, the fourth compression section 34, the first compression section 31, the fifth compression section 35, the third compression section 33, and the sixth compression section 36 in that order, and is compressed (pressurized) sequentially.

[0105] In addition, the sizes of the impellers (first impeller 310b to sixth impeller 360b) in each compression section 3 decrease in the order of the second compression section 32, the fourth compression section 34, the first compression section 31, the fifth compression section 35, the third compression section 33, and the sixth compression section 36.

[0106] (single-shaft multi-stage compressor) The single-shaft multi-stage compressor 4 further compresses the working fluid G compressed in the compression section 3, thereby increasing the pressure. The single-shaft multi-stage compressor 4 in this embodiment further compresses the working fluid G compressed by the sixth compression section 36. The single-shaft multi-stage compressor 4 has a compressor rotor 40 and a compressor casing 41.

[0107] The compressor rotor 40 is connected to the second intermediate pinion 26 and rotates in conjunction with the rotation of the second intermediate pinion 26. The compressor rotor 40 has a compressor rotary shaft 40a and a plurality of compressor impellers 40b. The compressor rotary shaft 40a has a cylindrical shape extending about the fourth axis A4.

[0108] The multiple compressor impellers 40b are arranged on the compressor rotary shaft 40a so as to be aligned in the axial direction Da, and rotate integrally with the compressor rotary shaft 40a about the fourth axis A4. When fixed to the compressor rotary shaft 40a, each compressor impeller 40b has multiple blades arranged in the circumferential direction of the compressor rotary shaft 40a. The compressor rotor 40 in this embodiment has three compressor impellers 40b.

[0109] Each compressor impeller 40b is formed to have the same size. The outer diameter of each compressor impeller 40b is smaller than the outer diameter of the sixth impeller 360b in the sixth compression section 36. That is, each blade of each compressor impeller 40b is formed smaller than each blade of the sixth impeller 360b.

[0110] The compressor casing 41 forms the outer shell of the single-shaft multi-stage compressor 4. The compressor casing 41 is placed and fixed on a foundation B such as the ground, a stand, or a base plate. In this embodiment, the foundation B is located below the drive gear 21 and the intermediate gear 24 in the vertical direction.

[0111] The compressor casing 41 has a casing body 41a, an intake port 41b formed in the casing body 41a, and a discharge port 41c formed in the casing body 41a. Pipes through which the working fluid G flows are connected to the intake port 41b and the discharge port 41c.

[0112] The casing body 41a forms a compressor passage therein that compresses the working fluid G together with the compressor rotor 40. The working fluid G compressed by the sixth compression section 36 flows through a pipe and is then sucked into the casing body 41a through the intake port 41b.

[0113] The working fluid G drawn into the casing body 41a is gradually compressed (pressurized) by the multiple compressor impellers 40b in the compressor passage. The working fluid G compressed inside the casing body 41a is discharged to the outside through the discharge port 41c.

[0114] The working fluid G compressed by the single-shaft multi-stage compressor 4 is supplied to, for example, a reaction device provided outside the geared compressor 100. In this embodiment, the compressor rotor 40 and compressor casing 41 of the single-shaft multi-stage compressor 4 form a multi-stage (three-stage) compression mechanism.

[0115] (shaft coupling) The shaft coupling 5 is a shaft coupling that connects the second intermediate side pinion support shaft 260 of the second intermediate side pinion 26 and the compressor rotating shaft 40a of the single-shaft multi-stage compressor 4. The shaft coupling 5 in this embodiment is, for example, a diaphragm shaft coupling. By connecting the second intermediate side pinion support shaft 260 and the compressor rotating shaft 40a with the shaft coupling 5, the single-shaft multi-stage compressor 4 rotates integrally with the second intermediate side pinion 26.

[0116] The shaft coupling 5 has flexibility. The shaft coupling 5 elastically deforms when the second intermediate side pinion support shaft 260 and the compressor rotating shaft 40a become misaligned while the geared compressor 100 is in operation, thereby suppressing loss of torque transmitted from the second intermediate side pinion support shaft 260 to the compressor rotating shaft 40a.

[0117] (bearings) Here, the bearings 27 of the compression section drive mechanism 2 rotatably support the drive support shaft 210 of the drive gear 21, the intermediate support shaft 240 of the intermediate gear 24, the second intermediate side pinion support shaft 260 of the second intermediate side pinion 26, the first rotating shaft 310a of the first compression section 31, the second rotating shaft 320a of the second compression section 32, the third rotating shaft 330a of the third compression section 33, the fourth rotating shaft 340a of the fourth compression section 34, the fifth rotating shaft 350a of the fifth compression section 35, and the sixth rotating shaft 360a of the sixth compression section 36.

[0118] The bearing 27 is composed of a driving gear bearing 271, an intermediate gear bearing 272, a pinion support shaft bearing 273, a first compression section bearing 274, a second compression section bearing 275, a third compression section bearing 276, a fourth compression section bearing 277, a fifth compression section bearing 278, and a sixth compression section bearing 279.

[0119] A pair of drive gear bearings 271 are fixed to the gear case 20. The drive gear bearings 271 are radial bearings that rotatably support the drive support shaft 210 of the drive gear 21 on one side Dab and the other side Daf of the drive gear main body 211.

[0120] A pair of intermediate gear bearings 272 are fixed to the gear case 20. The intermediate gear bearings 272 are radial bearings that rotatably support the intermediate support shaft 240 of the intermediate gear 24 on one side Dab and the other side Daf of the intermediate gear main body 241.

[0121] The pinion support shaft bearing 273 is fixed to the gear case 20. The pinion support shaft bearing 273 is a radial bearing that rotatably supports the second intermediate side pinion support shaft 260 of the second intermediate side pinion 26 on one side Dab of the second intermediate side pinion main body 261.

[0122] The first compression section bearing 274 is fixed to the gear case 20. The first compression section bearing 274 is a radial bearing that rotatably supports the first rotating shaft 310a of the first rotor 310 in the first compression section 31 on one side Dab of the first drive-side pinion body 221 of the first drive-side pinion 22.

[0123] The second compression section bearing 275 is fixed to the gear case 20. The second compression section bearing 275 is a radial bearing that rotatably supports the second rotating shaft 320a of the second rotor 320 in the second compression section 32 on one side Dab of the first intermediate side pinion body 251 of the first intermediate side pinion 25.

[0124] The third compression section bearing 276 is fixed to the gear case 20. The third compression section bearing 276 is a radial bearing that rotatably supports the third rotating shaft 330a of the third rotor 330 in the third compression section 33 on one side Dab of the second drive-side pinion body 231 of the second drive-side pinion 23.

[0125] The fourth compression section bearing 277 is fixed to the gear case 20. The fourth compression section bearing 277 is a radial bearing that rotatably supports the fourth rotating shaft 340a of the fourth rotor 340 in the fourth compression section 34 on the other side Daf of the first intermediate side pinion 25 relative to the first intermediate side pinion body 251.

[0126] The fifth compression section bearing 278 is fixed to the gear case 20. The fifth compression section bearing 278 is a radial bearing that rotatably supports the fifth rotating shaft 350a of the fifth rotor 350 in the fifth compression section 35 on the other side Daf of the first drive-side pinion 22 relative to the first drive-side pinion body 221.

[0127] The sixth compression section bearing 279 is fixed to the gear case 20. The sixth compression section bearing 279 is a radial bearing that rotatably supports the sixth rotation shaft 360a of the sixth rotor 360 in the sixth compression section 36 on the other side Daf of the second drive-side pinion 23 relative to the second drive-side pinion body 231.

[0128] (Action and effect) In the geared compressor 100 according to the above embodiment, the single-shaft multi-stage compressor 4 having a plurality of compressor impellers 40b is used, and therefore the compression efficiency of the geared compressor 100 can be improved compared to other compression sections 3 that perform compression with a single impeller. As a result, the output of the geared compressor 100 can be improved.

[0129] Furthermore, the drive gear 21 and the second intermediate side pinion 26 are connected via one intermediate gear 24. Therefore, as long as the gear diameters of the drive gear 21 and the second intermediate side pinion 26 are not changed, the relationship between the rotation speed of the drive gear 21 and the rotation speed of the second intermediate side pinion 26 can be maintained constant regardless of how the gear diameter of the intermediate gear 24 is changed.

[0130] As a result, the single-shaft multi-stage compressor 4 can be disposed at any position without reducing the rotation speed of the single-shaft multi-stage compressor 4, simply by changing the gear diameter of the intermediate gear 24. Furthermore, since the relationship between the rotation speed of the drive gear 21 and the rotation speed of the second intermediate side pinion 26 is maintained constant, loss due to gears when the single-shaft multi-stage compressor 4 is driven by the drive gear 21 can be reduced.

[0131] Furthermore, there is no need to dispose a new intermediate gear for driving the single-shaft multi-stage compressor 4 so as to mesh with the drive gear 21 or the intermediate gear 24. That is, there is no need to additionally install a new intermediate gear. In other words, compared to a configuration in which an intermediate gear for the single-shaft multi-stage compressor 4 is additionally installed, it is possible to suppress an increase in the dimension in the in-plane direction Pi. Therefore, it is possible to suppress an increase in the space occupied by the geared compressor 100.

[0132] Furthermore, the single-shaft multi-stage compressor 4 having multiple compressor impellers 40b is larger in size than a compression section 3 consisting of a single impeller. If the second intermediate side pinion 26 to which such a single-shaft multi-stage compressor 4 is connected is configured to directly mesh with the drive gear 21, interference will occur between the motor 1 for rotating the drive gear 21 and the single-shaft multi-stage compressor 4. However, by using the intermediate gear 24, interference between the motor 1 and the single-shaft multi-stage compressor 4 can be suppressed. Furthermore, the size of the geared compressor 100 can be reduced compared to when all of the compression sections 3 are single-shaft multi-stage compressors.

[0133] Furthermore, in the geared compressor 100 according to the above embodiment, the outer diameters of the first drive-side pinion 22, the first intermediate-side pinion 25, and the second intermediate-side pinion 26 are smaller than the outer diameter of the drive gear 21. As a result, the number of teeth of the first drive-side pinion 22, the first intermediate-side pinion 25, and the second intermediate-side pinion 26 are smaller than the number of teeth of the drive gear 21, and therefore the rotation speeds of these pinions are higher than the rotation speed of the drive gear 21.

[0134] That is, the rotation speeds of the first compression section 31 connected to the first drive-side pinion 22, the second compression section 32 connected to the first intermediate-side pinion 25, and the single-shaft multi-stage compressor 4 connected to the second intermediate-side pinion 26 are higher than the rotation speed of the drive gear 21. Therefore, the output of the geared compressor 100 can be improved.

[0135] Furthermore, the dimensions in the in-plane direction Pi can be made smaller compared to a configuration in which the outer diameters of the first drive-side pinion 22, the first intermediate-side pinion 25, and the second intermediate-side pinion 26 are the same as or larger than the outer diameter of the drive gear 21. Therefore, the output of the geared compressor 100 can be further improved while further suppressing an increase in the occupied space.

[0136] Furthermore, in the geared compressor 100 according to the above embodiment, the second compression section 32 is configured to compress the working fluid G at a stage upstream of the first compression section 31. Here, in order to further compress the working fluid G compressed by the second compression section 32 by rotation, the first impeller 310b in the first compression section 31 needs to be smaller than the second impeller 320b in the second compression section 32 which is located at a stage upstream of the first compression section 31. In other words, the second impeller 320b in the second compression section 32 needs to be larger than the first impeller 310b of the first compression section 31.

[0137] According to the above configuration, the first intermediate side pinion 25 to which the second compression section 32 having the second impeller 320b larger than the first impeller 310b in the first compression section 31 is connected meshes with the intermediate gear 24. Therefore, compared to a configuration in which the first intermediate side pinion 25 meshes with the drive gear 21, for example, it is possible to avoid interference of the second compression section 32 with the first compression section 31 and the motor 1.

[0138] Furthermore, in the geared compressor 100 according to the above embodiment, the motor 1 and the single-shaft multi-stage compressor 4 are placed on the base B in a state in which the intermediate gear 24 meshes with the drive gear 21 at the drive gear upper half 211a of the drive gear 21 and the second intermediate side pinion 26 meshes with the intermediate gear 24 at the intermediate gear lower half 241b of the intermediate gear 24. This makes it possible to reduce the dimension in the in-plane direction Pi compared to, for example, a configuration in which the drive gear 21, the intermediate gear 24, and the second intermediate side pinion 26 mesh with each other so as to be aligned in a line. Therefore, the geared compressor 100 can be made compact.

[0139] Furthermore, for example, compared to a configuration in which the second intermediate side pinion 26 meshes with the intermediate gear upper half portion 241a of the intermediate gear 24, the single-shaft multi-stage compressor 4 is disposed at a lower position on the base B on which the motor 1 is mounted. Therefore, the single-shaft multi-stage compressor 4 can be driven stably.

[0140] Furthermore, in the geared compressor 100 according to the above embodiment, the shaft coupling 5 connects the second intermediate side pinion support shaft 260 of the second intermediate side pinion 26 and the compressor rotating shaft 40a of the single-shaft multi-stage compressor 4. As a result, even if misalignment occurs between the second intermediate side pinion support shaft 260 and the compressor rotating shaft 40a, the influence of the misalignment can be suppressed by the shaft coupling 5. As a result, it is possible to reduce rotor dynamics between the second intermediate side pinion support shaft 260 and the compressor rotating shaft 40a.

[0141] Furthermore, the elastic deformation of the shaft coupling 5 can further reduce rotor dynamics occurring in the second intermediate side pinion support shaft 260 and the compressor rotary shaft 40a, thereby enabling smooth transmission of torque between the second intermediate side pinion support shaft 260 and the compressor rotary shaft 40a.

[0142] Furthermore, in the geared compressor 100 according to the above embodiment, the third compression section 33 connected to the second drive-side pinion 23 that meshes with the drive gear 21 compresses the working fluid G in a stage subsequent to the first compression section 31 and prior to the single-shaft multi-stage compressor 4. As a result, the third compression section 33 further compresses the working fluid G that has been compressed by the first compression section 31, thereby further increasing the pressure of the working fluid G. Therefore, the output of the geared compressor 100 can be further improved.

[0143] Furthermore, the first intermediate side pinion 25 and the second intermediate side pinion 26 mesh with the intermediate gear 24, and the first drive side pinion 22 and the second drive side pinion 23 mesh with the drive gear 21. In other words, there is no possibility that many pinions mesh with only one of the drive gear 21 and the intermediate gear 24. This makes it possible to prevent the magnitude of the load acting on the teeth of the drive gear 21 and the intermediate gear 24 from becoming uneven.

[0144] [Other embodiments] Although the embodiments of the present disclosure have been described above in detail with reference to the drawings, the specific configurations are not limited to those of the embodiments, and additions, omissions, substitutions, and other modifications of the configurations are possible within the scope of the gist of the present disclosure. Furthermore, the present disclosure is not limited to the embodiments, but is limited only by the claims.

[0145] In addition, the outer diameter of each pinion body (second drive side pinion body 231, first intermediate side pinion body 251, second intermediate side pinion body 261) of the second drive side pinion 23, the first intermediate side pinion 25, and the second intermediate side pinion 26 does not have to be the same as the outer diameter of the first drive side pinion body 221 of the first drive side pinion 22.

[0146] The outer diameters of the pinion bodies (first drive side pinion body 221, second drive side pinion body 231, first intermediate side pinion body 251, second intermediate side pinion body 261) of the first drive side pinion 22, second drive side pinion 23, first intermediate side pinion 25, and second intermediate side pinion 26 may be different from each other.

[0147] In addition, the outer diameter of the intermediate gear main body 241 in the above embodiment may be the same as the outer diameter of the drive gear main body 211. Also, the outer diameter of the intermediate gear main body 241 may be larger than the outer diameter of the drive gear main body 211. Also, the outer diameter of the intermediate gear main body 241 may be smaller than the outer diameter of the drive gear main body 211.

[0148] Furthermore, the first intermediate side pinion body 251 of the first intermediate side pinion 25 may mesh with the intermediate gear lower half portion 241 b of the intermediate gear body 241 .

[0149] Furthermore, in the above embodiment, the working fluid G compressed by the second compression section 32 is introduced into the fourth compression section 34. However, the present invention is not limited to this configuration. For example, the working fluid G supplied from the outside may be supplied to the second compression section 32 and the fourth compression section 34 simultaneously, compressed in the second compression section 32 and the fourth compression section 34, and then joined together and introduced into the first compression section 31. In this case, the outer diameter of the second impeller 320b in the second compression section 32 and the outer diameter of the fourth impeller 340b in the fourth compression section 34 may be the same.

[0150] In the above embodiment, the working fluid G supplied to the compression section 3 is introduced into the second compression section 32, the fourth compression section 34, the first compression section 31, the fifth compression section 35, the third compression section 33, and the sixth compression section 36 in this order and compressed sequentially, but the present invention is not limited to this configuration. The working fluid G may be introduced into the first compression section 31, the second compression section 32, the third compression section 33, the fourth compression section 34, the fifth compression section 35, and the sixth compression section 36 in any order. In this case, the sizes of the impellers (first impeller 310b to sixth impeller 360b) in each compression section 3 only need to decrease in the order in which the working fluid flows.

[0151] In addition, in the above embodiment, a configuration has been described in which the output axis O1 of the output shaft 10 and the drive axis O2 of the drive gear 21 are on the same straight line, but this does not necessarily mean that they are completely on the same straight line, and also includes cases in which they are slightly misaligned.

[0152] In the above embodiment, the second drive side pinion body 231 meshes with the portion of the drive gear body 211 where the drive gear upper half portion 211a and the drive gear lower half portion 211b switch, but the present invention is not limited to this configuration. The second drive side pinion body 231 may mesh with the drive gear upper half portion 211a of the drive gear body 211. The second drive side pinion body 231 may also mesh with the drive gear lower half portion 211b of the drive gear body 211.

[0153] In the above embodiment, the configuration has been described in which the outer diameter of each compressor impeller 40b in the single-shaft multi-stage compressor 4 is smaller than the outer diameter of the sixth impeller 360b in the sixth compression section 36, but the present invention is not limited to this configuration. The outer diameter of each compressor impeller 40b in the single-shaft multi-stage compressor 4 may be larger than the outer diameter of the sixth impeller 360b in the sixth compression section 36.

[0154] Furthermore, in the above embodiment, the compressor rotor 40 of the single-shaft multi-stage compressor 4 has three compressor impellers 40b, but the number is not limited to three.

[0155] Furthermore, the compressor casing 41 of the single-shaft multi-stage compressor 4 may be formed integrally with the gear case 20 of the compression section drive mechanism 2.

[0156] Furthermore, the shaft coupling 5 is not limited to a diaphragm shaft coupling, and may be, for example, a flange-type shaft coupling, a gear-type shaft coupling, a rubber shaft coupling, a metal spring shaft coupling, a roller chain shaft coupling, or the like.

[0157] [Note] The geared compressor described in the embodiment can be understood, for example, as follows.

[0158] (1) A geared compressor 100 according to a first aspect includes a drive gear 21 rotated by the rotation of a motor 1, an intermediate gear 24 meshing with the drive gear 21, a first drive-side pinion 22 meshing with the drive gear 21 at a position spaced apart from the intermediate gear 24, a first intermediate-side pinion 25 meshing with the intermediate gear 24 at a position spaced apart from the drive gear 21, a second intermediate-side pinion 26 meshing with the intermediate gear 24 at a position spaced apart from the drive gear 21 and the first intermediate-side pinion 25, and a front The compressor includes a first compression section 31 connected to the first drive side pinion 22 and compressing the working fluid G supplied from the outside by the rotation of the first drive side pinion 22, a second compression section 32 connected to the first intermediate side pinion 25 and compressing the working fluid G supplied from the outside by the rotation of the first intermediate side pinion 25, and a single-shaft multi-stage compressor 4 connected to the second intermediate side pinion 26 and further compressing the working fluid G compressed by at least one of the first compression section 31 and the second compression section 32.

[0159] This eliminates the need to additionally provide a new intermediate gear 24 for driving the single-shaft multi-stage compressor 4 to the drive gear 21 or the intermediate gear 24. Therefore, compared to a configuration in which an intermediate gear 24 for the single-shaft multi-stage compressor 4 is additionally provided, it is possible to prevent the size of the geared compressor 100 from increasing.

[0160] (2) The geared compressor 100 according to the second aspect is the geared compressor 100 of (1), wherein the outer diameters of the first drive side pinion 22, the first intermediate side pinion 25, and the second intermediate side pinion 26 may be smaller than the outer diameter of the drive gear 21.

[0161] As a result, the number of teeth of each of the first drive-side pinion 22, the first intermediate-side pinion 25, and the second intermediate-side pinion 26 becomes smaller than the number of teeth of the drive gear 21, and therefore the rotation speeds of these pinions become higher than the rotation speed of the drive gear 21. Therefore, the rotation speeds of the first compression section 31, the second compression section 32, and the single-shaft multi-stage compressor 4 can be made higher than the rotation speed of the drive gear 21.

[0162] (3) The geared compressor 100 according to the third aspect is the geared compressor 100 of (1) or (2), and the second compression section 32 may compress the working fluid G at a stage before the first compression section 31.

[0163] In order to further compress the working fluid G compressed by the second compression section 32 by rotation, the second compression section 32 needs to be larger than the first compression section 31. With the above configuration, compared to a configuration in which the first intermediate side pinion 25 to which the second compression section 32 is connected meshes with the drive gear 21, it is possible to prevent the second compression section 32, which is larger than the first compression section 31, from interfering with the first compression section 31 and the motor 1.

[0164] (4) The geared compressor 100 according to a fourth aspect is the geared compressor 100 of any one of (1) to (3), in which the intermediate gear 24 meshes with the drive gear 21 at an upper half of the drive gear 21 (drive gear upper half 211a), the second intermediate side pinion 26 meshes with the intermediate gear 24 at a lower half of the intermediate gear 24 (intermediate gear lower half 241b), and the motor 1 and the single-shaft multi-stage compressor 4 may be placed on a foundation B located below (vertically lower than) the drive gear 21 and the intermediate gear 24.

[0165] This allows the geared compressor 100 to be made more compact than in a configuration in which the drive gear 21, the intermediate gear 24, and the second intermediate side pinion 26 mesh with each other so as to be aligned in a row. Also, compared to a configuration in which the second intermediate side pinion 26 meshes with the upper half portion of the intermediate gear 24 (intermediate gear upper half portion 241a), the single-shaft multi-stage compressor 4 is disposed at a lower position on the base B on which the motor 1 is placed. Therefore, the single-shaft multi-stage compressor 4 can be driven stably.

[0166] (5) The geared compressor 100 according to a fifth aspect may be the geared compressor 100 of (4), further including a shaft coupling 5 that connects a pinion support shaft (second intermediate side pinion support shaft 260) of the second intermediate side pinion 26 and the compressor rotating shaft 40a of the single-shaft multi-stage compressor 4.

[0167] As a result, even if misalignment occurs between the second intermediate side pinion support shaft 260 and the compressor rotating shaft 40a, the shaft coupling 5 can reduce the rotor dynamics that occur in the second intermediate side pinion support shaft 260 and the compressor rotating shaft 40a.

[0168] (6) The geared compressor 100 according to a sixth aspect is the geared compressor 100 of any one of (1) to (5), further including: a second drive-side pinion 23 that meshes with the drive gear 21 at a position spaced apart from the intermediate gear 24; and a third compression section 33 connected to the second drive-side pinion 23 that compresses the working fluid G by rotation of the second drive-side pinion 23, and the third compression section 33 may compress the working fluid G at a stage subsequent to the first compression section 31 and prior to the single-shaft multi-stage compressor 4.

[0169] As a result, the third compression section 33 further compresses the working fluid G compressed by the first compression section 31, thereby further improving the output of the geared compressor 100. In addition, it is possible to prevent the magnitude of the loads applied to the teeth of the drive gear 21 and the intermediate gear 24 from becoming uneven. [Explanation of symbols]

[0170] 1...motor 2...compression section drive mechanism 3...compression section 4...single-shaft multi-stage compressor 5...shaft coupling 10...output shaft 11...motor body 20...gear case 21...drive gear 22...first drive-side pinion 23...second drive-side pinion 24...intermediate gear 25...first intermediate-side pinion 26...second intermediate-side pinion 27...bearing 31...first compression section 32...second compression section 33...third compression section 34...fourth compression section 35...fifth compression section 36...sixth compression section 40...compressor rotor 40a...compressor rotating shaft 40b...compressor impeller 41...compressor casing 41a...casing body 41b...suction port 41c...discharge port 100...geared compressor 210...drive support shaft 211...drive gear body 211a...drive gear upper half 211b...Drive gear lower half 220...First drive side pinion support shaft 221...First drive side pinion body 222...First thrust bearing 230...Second drive side pinion support shaft 231...Second drive side pinion body 232...Second thrust bearing 240...Intermediate support shaft 241...Intermediate gear body 241a...Intermediate gear upper half 241b...Intermediate gear lower half 250...First intermediate side pinion support shaft 251...First intermediate side pinion body 252...Third thrust bearing 260...Second intermediate side pinion support shaft 261...Second intermediate side pinion body 262...Fourth thrust bearing 271...Drive gear bearing 272...Intermediate gear bearing 273...Pinion support shaft bearing 274...First compression section bearing 275...Second compression section bearing 276...Third compression section bearing 277...Fourth compression section bearing 278...Fifth compression section bearing 279...Sixth compression section bearing 310...First rotor 310a...First rotating shaft 310b...First impeller 311...First compression section casing 311a...First gas inlet 311b...First gas outlet 320...Second rotor 320a...Second rotating shaft 320b...Second impeller 321...Second compression section casing 321a...Second gas inlet 321b...Second gas outlet 330...Third rotor 330a...Third rotating shaft 330b...Third impeller 331...Third compression section casing 331a...Third gas inlet 331b...Third gas outlet 340...Fourth rotor 340a...Fourth rotating shaft 340b...Fourth impeller 341...Fourth compression section casing 341a...Fourth gas inlet port 341b...Fourth gas outlet port 350...Fifth rotor 350a...Fifth rotating shaft 350b...Fifth impeller351...Fifth compression section casing 351a...Fifth gas inlet 351b...Fifth gas outlet 360...Sixth rotor 360a...Sixth rotating shaft 360b...Sixth impeller 361...Sixth compression section casing 361a...Sixth gas inlet 361b...Sixth gas outlet A1...First axis A2...Second axis A3...Third axis A4...Fourth axis B...Foundation C...Coupling Da...Axial direction Dab...One side Daf...Other side G...Working fluid O...Axis O1...Output axis O2...Drive axis O3...Intermediate axis Pi...In-plane direction Po...Out-of-plane direction X...Imaginary plane

Claims

1. a drive gear that is rotated by the rotation of the motor; an intermediate gear that meshes with the drive gear; a first driving pinion that meshes with the driving gear at a position spaced apart from the intermediate gear; a first intermediate pinion that meshes with the intermediate gear at a position spaced apart from the drive gear; a second intermediate pinion that meshes with the intermediate gear at a position spaced apart from the drive gear and the first intermediate pinion; a first compression unit connected to the first drive-side pinion and configured to compress a working fluid supplied from an external source by rotation of the first drive-side pinion; a second compression unit connected to the first intermediate pinion and configured to compress a working fluid supplied from an external source by rotation of the first intermediate pinion; a single-shaft multi-stage compressor connected to the second intermediate pinion and configured to further compress the working fluid compressed by at least one of the first compression section and the second compression section, the intermediate gear meshes with the drive gear at an upper half of the drive gear, the second intermediate pinion meshes with the intermediate gear at a lower half of the intermediate gear, The motor and the single-shaft multi-stage compressor are mounted on a base located below the drive gear and the intermediate gear.

2. The geared compressor according to claim 1 , wherein the first drive pinion, the first intermediate pinion, and the second intermediate pinion have outer diameters smaller than the outer diameter of the drive gear.

3. The geared compressor according to claim 1 or 2, wherein the second compression section compresses the working fluid at an earlier stage than the first compression section.

4. The geared compressor according to claim 1 , further comprising a shaft coupling that connects a pinion support shaft of the second intermediate pinion and a compressor rotary shaft of the single-shaft multi-stage compressor.

5. a second driving pinion that meshes with the driving gear at a position spaced apart from the intermediate gear; a third compression unit connected to the second drive-side pinion that compresses the working fluid by rotation of the second drive-side pinion; Furthermore, The geared compressor according to claim 1 , wherein the third compression section compresses the working fluid at a stage subsequent to the first compression section and prior to the single-shaft multi-stage compressor.

6. The outer diameters of the first drive side pinion, the first intermediate side pinion, and the second intermediate side pinion are smaller than the outer diameter of the drive gear; 6. The geared compressor according to claim 1, wherein, when viewed from an axial direction in which an axis of the drive gear extends, a lowermost end of the second intermediate pinion is located vertically above a lowermost end of the drive gear.

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