阅读说明：本技术 氢气循环泵 (Hydrogen circulating pump ) 是由 张寅� 董宝田 王灿 王坤 于 2021-09-06 设计创作，主要内容包括：本发明涉及一种氢气循环泵。一种氢气循环泵,包括泵壳和位于泵壳内部的转动组件,泵壳由冷却机壳和蜗壳组成,所述冷却机壳和蜗壳共同构成一个用于容设转动组件并与外界密封的内腔,冷却机壳和蜗壳之间气相相通,所述转动组件包括转子轴和叶轮,所述转动组件通过磁悬浮轴承与泵壳间形成悬浮支撑；工作时,所述内腔充满工作介质,转动组件悬浮在工作介质中。本发明具有结构简单、能实现氢气密封,能提高转子轴转速以保证对氢气的增压功能,从而能实现小型化的优点。(The invention relates to a hydrogen circulating pump. A hydrogen circulating pump comprises a pump shell and a rotating assembly positioned in the pump shell, wherein the pump shell consists of a cooling machine shell and a volute, the cooling machine shell and the volute jointly form an inner cavity which is used for accommodating the rotating assembly and is sealed with the outside, the cooling machine shell is communicated with the volute in a gas phase, the rotating assembly comprises a rotor shaft and an impeller, and a suspension support is formed between the rotating assembly and the pump shell through a magnetic suspension bearing; when the rotary assembly works, the inner cavity is filled with working media, and the rotary assembly is suspended in the working media. The invention has the advantages of simple structure, capability of realizing hydrogen sealing, capability of improving the rotating speed of the rotor shaft to ensure the function of pressurizing hydrogen, and capability of realizing miniaturization.)

1. A hydrogen circulating pump is characterized by comprising a pump shell and a rotating assembly positioned in the pump shell, wherein the pump shell consists of a cooling machine shell and a volute, the cooling machine shell and the volute jointly form an inner cavity which is used for accommodating the rotating assembly and is sealed with the outside, the cooling machine shell and the volute are communicated in a gas phase, the rotating assembly comprises a rotor shaft and an impeller, and a suspension support is formed between the rotating assembly and the pump shell through a magnetic suspension bearing; when the rotary assembly works, the inner cavity is filled with working media, and the rotary assembly is suspended in the working media.

2. The hydrogen circulation pump according to claim 1, wherein the volute is disposed at an outer side of an end portion of the cooling casing, an outer limit portion extending to a circumferential outer side is disposed at an offset end portion of the cooling casing, and the volute is located at an axial side of the outer limit portion.

3. The hydrogen circulation pump of claim 1, wherein the magnetic suspension bearings comprise a radial-axial integrated magnetic suspension bearing and a radial magnetic suspension bearing, the radial magnetic suspension bearing is located at the axially extending end of the rotor shaft, and the radial-axial integrated magnetic suspension bearing is located at the non-axially extending end of the rotor shaft.

4. The hydrogen circulation pump of claim 3, wherein the radial magnetic suspension bearing comprises a first magnetic conductor and a second magnetic conductor arranged at an interval along the axial direction of the rotor shaft, a first floating ring is arranged between the first magnetic conductor and the second magnetic conductor, the first floating ring is fixed with a first sensor, the distance between the first floating ring and the rotor shaft is L1, the first magnetic conductor comprises an iron core and a coil, the distance between the iron core of the first magnetic conductor and the rotor shaft is L2, the distance between the first sensor and the rotor shaft is L3, and L1 < L2 ≦ L3.

5. The hydrogen circulation pump according to claim 4, wherein the first floating ring is formed integrally with the cooling casing.

6. The hydrogen circulation pump according to claim 3, wherein the radial-axial integrated magnetic suspension bearing comprises a radial magnetic suspension bearing portion and an axial magnetic suspension bearing portion, and the radial-axial integrated magnetic suspension bearing is provided with a third magnetic conductor, a fourth magnetic conductor and a fifth magnetic conductor which are arranged at intervals in the axial direction of the rotor shaft, wherein the third magnetic conductor and the fourth magnetic conductor constitute magnetic poles of the radial magnetic suspension bearing portion, and the fourth magnetic conductor and the fifth magnetic conductor constitute magnetic poles of the axial magnetic suspension bearing portion.

7. The hydrogen circulation pump of claim 6, wherein the radial magnetic bearing portion and the axial magnetic bearing portion are fixed in a first fixing member having an annular cross section, the first fixing member being fixed to the cooling casing;

a second floating ring is arranged between the third magnetizer and the fourth magnetizer, the third magnetizer comprises an iron core and a coil, the distance between the iron core of the third magnetizer and the rotor shaft is L5, the distance between the second floating ring and the rotor shaft is L4, a second sensor is arranged on the second floating ring, the distance between the second sensor and the rotor shaft is L6, and L4 is more than L5 and is not more than L6;

the second floating ring and the first fixing piece are integrally formed;

the cooling machine shell is characterized in that a first step structure and a second step structure used for positioning a first fixing piece are arranged on the inner wall of the cooling machine shell, one end face of the first fixing piece is close to a step face formed by the first step structure, and the other end of the first fixing piece is provided with an extending portion which extends towards the outer side in the circumferential direction and is fixed with the second step structure.

8. The hydrogen circulation pump according to claim 6, wherein a fifth floating ring and a sixth floating ring are provided between the fourth magnetizer and the fifth magnetizer, and a thrust plate provided between the fifth floating ring and the sixth floating ring is provided on the rotor shaft;

the fifth floating ring is fixed on the end face of the fourth magnetizer, and the sixth floating ring is fixed on the end face of the fifth magnetizer;

and the distance L7 between the end surface of the thrust disc and the fifth floating ring or the sixth floating ring is smaller than the distance L8 between the impeller and the end surface of the cooling machine shell, which is closest to the impeller.

9. The hydrogen circulating pump according to claim 1, wherein the cooling casing is a structure with openings at two axial ends and an annular cross section, a closed casing is arranged at one end of the cooling casing far away from the volute, and the closed casing and the cooling casing are fixedly connected in a sealing manner;

the end face of the closed shell is provided with a mounting hole, an aviation plug is arranged at the mounting hole, the aviation plug is fixed with the closed shell and closes the mounting hole, and the aviation plug and the closed shell are sealed; the closed shell is provided with a cavity for yielding the outgoing line, and the outgoing line is electrically connected with the aviation plug.

10. The hydrogen circulation pump according to claim 1, wherein the outer surface of the rotating member is provided with a protective layer; and a stator is arranged in the cooling machine shell and is sealed by pouring sealant.

Technical Field

The invention relates to a hydrogen circulating pump.

Background

The hydrogen fuel cell system needs to integrate a hydrogen circulation system, leads out unreacted hydrogen in the fuel cell stack, leads the unreacted hydrogen into the hydrogen fuel cell stack again after filtration and pressurization to participate in reaction together with fresh hydrogen, and can lead out moisture and impurities accumulated in the stack and wet the newly led-in hydrogen in the process. At present, a hydrogen circulating pump or an ejector is mainly adopted to pressurize the part of hydrogen and then send the hydrogen into the fuel cell for use.

The centrifugal hydrogen circulating pump has high working efficiency and large flow rate, but needs higher rotating speed. Compared with air, hydrogen is more difficult to compress, and the centrifugal hydrogen circulating pump can effectively compress the hydrogen only by reaching higher rotating speed, so the centrifugal hydrogen circulating pump also needs to face the bearing support problem under high rotating speed in a hydrogen environment. The impeller of hydrogen circulating pump is in under the environment of hydrogen and vapor, and the motor rotor shaft is supported by mechanical bearing, and vapor can lead to revealing of mechanical bearing lubricating oil, not only influences the motor life-span but also can pollute the hydrogen environment. Conventional mechanical bearings must therefore solve the problem of sealing of the lubricating oil, otherwise normal use at very high rotational speeds cannot be guaranteed. .

The Chinese patent with the application number of 201820734220.0 discloses a full-shielding high-speed centrifugal hydrogen circulating pump, which adopts a shielding sleeve mode to perform hydrogen isolation sealing, but has the defects of complex structure and difficult processing.

Disclosure of Invention

The invention aims to provide a hydrogen circulating pump which is simple in structure, can realize hydrogen sealing, can improve the rotating speed to ensure the function of pressurizing hydrogen, and can realize miniaturization.

In order to achieve the purpose, the invention adopts the following technical scheme: a hydrogen circulating pump comprises a pump shell and a rotating assembly positioned in the pump shell, wherein the pump shell consists of a cooling machine shell and a volute, the cooling machine shell and the volute jointly form an inner cavity which is used for accommodating the rotating assembly and is sealed with the outside, the cooling machine shell is communicated with the volute in a gas phase, the rotating assembly comprises a rotor shaft and an impeller, and a suspension support is formed between the rotating assembly and the pump shell through a magnetic suspension bearing; when the rotary assembly works, the inner cavity is filled with working media, and the rotary assembly is suspended in the working media.

The inner cavity of the cooling machine shell is directly communicated with the inner cavity of the volute, dynamic sealing of the rotor shaft and the volute is not needed, and hydrogen sealing can be realized only by sealing the pump shell and the outside, so that hydrogen leakage is avoided. The invention adopts the magnetic suspension bearing to support the rotation of the impeller, the magnetic suspension bearing has no rotation speed limitation of a mechanical bearing, the mechanical bearing is not required to support, the lubrication and sealing problems which need to be faced by the mechanical bearing are avoided, the hydrogen is not polluted by lubricating oil, and the high-speed rotation of the rotor shaft can be realized. Compared with a claw type hydrogen circulating pump, the hydrogen pressurizing device has the advantages that the hydrogen pressurizing effect can be guaranteed, the structure is simple, and the miniaturization of the hydrogen circulating pump can be realized.

The magnetic suspension bearing can isolate the vibration transmission of the stator part and the rotor part of the motor to a great extent, and has the advantages of low noise, high reliability and longer service life; meanwhile, compared with other pneumatic bearings, the passive non-contact bearing with the active control can also realize more active control of the motor and feedback of the state of the rotating shaft. Wherein, hydrogen gets into in the cooling machine shell, can also cool rotating assembly.

Preferably, the volute is sleeved on the outer side of the end portion of the cooling casing, an outer limiting portion extending towards the circumferential outer side is arranged at the position of the cooling casing deviated from the end portion, and the volute is located on the axial side of the outer limiting portion. Various sealing methods can be adopted between the volute and the cooling machine shell, such as glue sealing, sealing ring sealing and the like. The end part of the volute is sleeved outside the end part of the cooling casing and fixed, so that the volute cannot move radially relative to the cooling casing, an effective avoiding space between the impeller and the inner wall of the volute can be ensured, and the impeller is prevented from floating upwards to be in contact with the volute after the motor is powered on and started. The outer limiting part is used for limiting the volute, so that a set position is ensured between an air inlet and an air outlet of the volute and the impeller, and the impeller can be prevented from being driven by the rotor shaft to float upwards to contact and collide with the inner wall of the volute after the motor part is electrified. Wherein, outer spacing portion not only is used for spacing, can also be used for fixed with the fastener of spiral case.

Preferably, the magnetic suspension bearing comprises a radial-axial integrated magnetic suspension bearing and a radial magnetic suspension bearing, the radial magnetic suspension bearing is positioned at the shaft extension end of the rotor shaft, and the radial-axial integrated magnetic suspension bearing is positioned at the non-shaft extension end of the rotor shaft. The three degrees of freedom of the rotating assembly are kept through the radial-shaft integrated magnetic suspension bearing, and the two degrees of freedom of the rotating assembly are guaranteed through the radial magnetic suspension bearing.

Preferably, the radial magnetic suspension bearing comprises a first magnetizer and a second magnetizer which are arranged along the axial direction of the rotor shaft at intervals, a first floating ring is positioned between the first magnetizer and the second magnetizer, a first sensor is fixed on the first floating ring, the distance between the first floating ring and the rotor shaft is L1, the first magnetizer comprises an iron core and a coil, the distance between the iron core of the first magnetizer and the rotor shaft is L2, the distance between the first sensor and the rotor shaft is L3, and L1 is more than L2 and is not more than L3.

Wherein, L1 is more than L2 is less than or equal to L3, which can avoid the rotor shaft contacting with the first magnetizer and the second magnetizer when the invention is not used, so as to ensure the rotor shaft to suspend and rotate quickly and stably when the invention is started.

Preferably, the first floating ring is integrally formed with the cooling casing. The first floating ring and the cooling shell are integrated, so that the structure of the magnetic bearing is simplified, and the positioning and cooling of the magnetic bearing are facilitated.

Preferably, the radial-axial integrated magnetic suspension bearing comprises a radial magnetic suspension bearing portion and an axial magnetic suspension bearing portion, the radial-axial integrated magnetic suspension bearing is provided with a third magnetizer, a fourth magnetizer and a fifth magnetizer which are axially arranged along the rotor shaft at intervals, wherein the third magnetizer and the fourth magnetizer form a magnetic pole of the radial magnetic suspension bearing portion, and the fourth magnetizer and the fifth magnetizer form a magnetic pole of the axial magnetic suspension bearing portion. The radial magnetic suspension bearing part and the axial magnetic suspension bearing part share the same magnetizer, so that the axial structure of the invention is more compact, and the miniaturization of the invention is convenient to realize.

Preferably, the radial magnetic suspension bearing portion and the axial magnetic suspension bearing portion are fixed in a first fixing piece with an annular cross section, and the first fixing piece is fixed with the cooling machine shell; a second floating ring is arranged between the third magnetizer and the fourth magnetizer, the third magnetizer comprises an iron core and a coil, the distance between the iron core of the third magnetizer and the rotor shaft is L5, the distance between the second floating ring and the rotor shaft is L4, a second sensor is arranged on the second floating ring, the distance between the second sensor and the rotor shaft is L6, and L4 is more than L5 and is not more than L6; the second floating ring and the first fixing piece are integrally formed; the cooling machine shell is characterized in that a first step structure and a second step structure used for positioning a first fixing piece are arranged on the inner wall of the cooling machine shell, one end face of the first fixing piece is close to a step face formed by the first step structure, and the other end of the first fixing piece is provided with an extending portion which extends towards the outer side in the circumferential direction and is fixed with the second step structure.

The radial-axial integrated magnetic suspension bearing is made into an independent component assembly through the first fixing piece, so that the radial-axial integrated magnetic suspension bearing is convenient to store in the assembling and production processes, and is convenient to subsequently maintain and replace. And L6 is more than L4 and less than L5, so that the rotor shaft can be prevented from contacting with the third magnetizer and the fourth magnetizer when the motor is not used, and the rotor shaft can be quickly and stably suspended and rotated when the motor is started. The inner wall of the cooling machine shell is provided with a step structure, so that the first fixing piece is convenient to position and fix, and the assembly of the cooling machine shell is convenient. The second floating ring and the first fixing piece are integrally formed, so that positioning and fixing are facilitated, assembly of parts of the radial-axial integrated magnetic suspension bearing is facilitated, and the first fixing piece can play a role in improving a cooling effect when made of a heat-conducting aluminum material and the like.

Preferably, a fifth floating ring and a sixth floating ring are arranged between the fourth magnetizer and the fifth magnetizer, and a thrust disc positioned between the fifth floating ring and the sixth floating ring is arranged on the rotor shaft; the fifth floating ring is fixed on the end face of the fourth magnetizer, and the sixth floating ring is fixed on the end face of the fifth magnetizer; and the distance L7 between the end surface of the thrust disc and the fifth floating ring or the sixth floating ring is smaller than the distance L8 between the impeller and the end surface of the cooling machine shell, which is closest to the impeller. The fifth floating ring and the sixth floating ring are used for avoiding the contact between a thrust disc of the rotor shaft and the magnetizer, and the rotor shaft can be ensured to be quickly and stably suspended and rotated when the motor is started. Wherein, L7 is less than L8, which can avoid the contact between the impeller and the cooling casing when the invention is not used.

Preferably, the cooling machine shell is of a structure with openings at two axial ends and an annular cross section, a closed shell is arranged at one end, away from the volute, of the cooling machine shell, and the closed shell is fixedly connected with the cooling machine shell in a sealing manner; the end face of the closed shell is provided with a mounting hole, an aviation plug is arranged at the mounting hole, the aviation plug is fixed with the closed shell and closes the mounting hole, and the aviation plug and the closed shell are sealed; the closed shell is provided with a cavity for yielding the outgoing line, and the outgoing line is electrically connected with the aviation plug.

Preferably, a protective layer is arranged on the outer surface of the rotating assembly; and a stator is arranged in the cooling machine shell and is sealed by pouring sealant. The protective layer and the pouring sealant are used for preventing hydrogen and water vapor from corroding the rotating assembly and the stator. Wherein, a protective layer can be formed on the surface of the rotor shaft by means of titanium plating or DLC treatment.

The invention has the advantages of simple structure, capability of realizing hydrogen sealing, capability of improving the rotating speed of the rotor shaft to ensure the function of pressurizing hydrogen, and capability of realizing miniaturization.

Drawings

FIG. 1 is a schematic structural diagram of the present invention;

FIG. 2 is a schematic structural diagram of a first radial magnetic suspension bearing according to the present invention;

FIG. 3 is an enlarged view taken at A in FIG. 2;

FIG. 4 is a schematic structural diagram of a radial-axial integrated magnetic suspension bearing of the present invention;

FIG. 5 is an enlarged view of FIG. 4 at B;

FIG. 6 is an enlarged view at C in FIG. 4;

fig. 7 is a schematic structural diagram of a radial magnetic suspension bearing portion of the radial-axial integrated magnetic suspension bearing of the present invention.

Detailed Description

The invention is further described below with reference to the figures and specific embodiments.

As shown in fig. 1, 2 and 4, the hydrogen circulation pump of the present invention comprises a pump housing and a rotating assembly located inside the pump housing, wherein the pump housing is composed of a cooling machine shell 1 and a volute 2, the cooling machine shell 1 and the volute 2 jointly form an inner cavity for accommodating the rotating assembly and sealing with the outside, the cooling machine shell 1 and the volute 2 are in gas phase communication, when the hydrogen circulation pump of the present invention works, the inner cavity of the pump housing is filled with a working medium, and the rotating assembly is suspended in the working medium. The rotating assembly comprises a rotor shaft 3 and an impeller 31, and the rotor shaft 3 and the impeller 31 form a suspension support with the pump shell through a magnetic suspension bearing.

The magnetic suspension bearing comprises a radial-axial integrated magnetic suspension bearing 100 and a radial magnetic suspension bearing 200, the radial magnetic suspension bearing 200 is positioned at the axial extension end of the rotor shaft 3, and the radial-axial integrated magnetic suspension bearing 100 is positioned at the non-axial extension end of the rotor shaft 3. Wherein, the outer surface of the rotating component is provided with a protective layer, or the rotor shaft is made of stainless steel; the stator 10 is arranged in the cooling machine shell 1, the stator 10 is fixed with the cooling machine shell 1 and is positioned between the radial-axial integrated magnetic suspension bearing 100 and the radial magnetic suspension bearing 200, and pouring sealant is wrapped outside the stator 10.

The volute 2 is directly connected with the cooling casing 1 and is sealed by a first sealing ring 21. The volute 2 is sleeved on the outer side of the end part of the cooling casing 1, an outer limiting part 11 extending towards the outer circumferential side is arranged at the position of the deviated end part of the cooling casing 1, the volute 2 is located at the axial side of the outer limiting part 11 and is fixed with the outer limiting part 11 through a fastening piece, and a first sealing ring 21 for sealing is arranged between the circumferential inner wall of the volute 2 and the circumferential outer wall of the end part of the cooling casing 1.

The cooling machine shell 1 is of a structure with openings at two axial ends and an annular cross section, a closed shell 4 is arranged at one end, away from the volute 2, of the cooling machine shell 1, the end part of the closed shell 4 and the end part of the cooling machine shell 1 are sleeved with each other and fixed together in a fastening piece or thread fixing mode, and the connection part 41 of the end part of the closed shell 4 and the end part of the cooling machine shell 1 is sealed. The end face of the closed shell 4 is provided with a mounting hole, the mounting hole is provided with an aviation plug 42, the aviation plug 42 is fixed with the closed shell 4 and seals the mounting hole, and the aviation plug 42 and the closed shell 4 are sealed through a second sealing ring 43. The enclosure 4 is formed with a cavity 40 for abdicating the outlet wires for electrical connection with an aviation plug 42.

As shown in fig. 1 to fig. 3, the radial magnetic suspension bearing 200 includes a first magnetizer 201 and a second magnetizer 202 axially spaced along the rotor shaft, a first floating ring 204 is disposed between the first magnetizer 201 and the second magnetizer 202, the first floating ring 204 is integrally formed with the cooling casing 1, a plurality of axially penetrating fixing grooves are disposed at a position of the first floating ring 204 adjacent to the cooling casing 1, a first permanent magnet 203 is fixed in each fixing groove, the plurality of first permanent magnets 203 are annularly and uniformly spaced and surround the rotor shaft, and a first sensor 205 is fixed on the first floating ring 204. The distance between the first floating ring 204 and the rotor shaft 3 is L1, the first magnetizer 201 includes an iron core and a coil, the distance between the iron core of the first magnetizer 201 and the rotor shaft 3 is L2, the distance between the first sensor 205 and the rotor shaft 3 is L3, and L1 is greater than L2 and is equal to or less than L3.

As shown in fig. 1 and 4, the radial-axial integrated magnetic levitation bearing 100 includes a radial magnetic levitation bearing portion 110 and an axial magnetic levitation bearing portion 120, the radial magnetic levitation bearing portion 110 and the axial magnetic levitation bearing portion 120 are both fixed in a first fixing member 130 having an annular cross section, and the first fixing member 130 is fixed to the cooling casing 1.

The radial-axial integrated magnetic suspension bearing 100 includes a third magnetic conductor 111, a fourth magnetic conductor 112, and a fifth magnetic conductor 121 disposed at intervals along the axial direction of the rotor shaft, wherein the third magnetic conductor 111 and the fourth magnetic conductor 112 constitute magnetic poles of the radial magnetic suspension bearing portion 110, the fourth magnetic conductor 112 and the fifth magnetic conductor 121 constitute magnetic poles of the axial magnetic suspension bearing portion 120, and the radial magnetic suspension bearing portion 110 and the axial magnetic suspension bearing portion 120 of the present embodiment share the same fourth magnetic conductor 112. As is well known, the radial magnetically levitated bearing portion 110 and the axial magnetically levitated bearing portion 120 further include components constituting a magnetic levitation bearing, such as permanent magnets. A second floating ring 114 is disposed between the third magnetic conductor 111 and the fourth magnetic conductor 112, and the second floating ring 114 and the first fixing member 130 are integrally formed.

As shown in fig. 3 to 7, the radial magnetic suspension bearing portion 110 of the present embodiment has the same structure as the radial magnetic suspension bearing 200, a second permanent magnet 113 is disposed between a third magnetizer 111 and a fourth magnetizer 112 of the radial magnetic suspension bearing portion 110, a second floating ring 114 has the same shape and structure as the first floating ring 204, the second permanent magnet 113 is fixed in a fixing groove of the second floating ring 114, and the first magnetizer 201 and the third magnetizer 111 both include an iron core and a coil 119.

The distance between the iron core of the third magnetizer 111 and the rotor shaft 3 is L5, the distance between the second floating ring 114 and the rotor shaft 3 is L4, the second floating ring 114 is provided with a second sensor 115, the distance between the second sensor 115 and the rotor shaft 3 is L6, and L4 is greater than L5 and is equal to or greater than L6.

A fifth floating ring 122 and a sixth floating ring 123 are arranged between the fourth magnetizer 112 and the fifth magnetizer 121, a thrust plate 30 positioned between the fifth floating ring 122 and the sixth floating ring 123 is arranged on the rotor shaft 3, the fifth floating ring 122 is fixed at the end surface of the fourth magnetizer 112, and the sixth floating ring 123 is fixed at the end surface of the fifth magnetizer 121. As shown in fig. 3 and 4, the distance between the end surface of the thrust disc 30 and the fifth floating ring 122 or the sixth floating ring 123 is L7, the distance between the impeller 31 and the end surface of the cooling casing 1 closest to the impeller 31 is L8, and L7 < L8.

As shown in fig. 1 and 4, the inner wall of the cooling housing 1 is provided with a first step structure 12 and a second step structure 13 for positioning a first fixing member 130, one end face of the first fixing member 130 is adjacent to the step face formed by the first step structure 12, and the other end of the first fixing member 130 is provided with an extending portion 131 extending to the outside in the circumferential direction and fixed with the second step structure 13. The second fixing member 140 is fixed to a side of the first fixing member 130 away from the impeller 31, the second fixing member 140 is fixed to the first fixing member 130 by a fastener, the axial magnetic levitation bearing portion 120 is limited to an axial side of the second fixing member 140, and an axial displacement sensor 150 is disposed at an inner edge of a fifth magnetizer 121 of the axial magnetic levitation bearing portion 120.

As shown in fig. 1, the inner diameter of the inner wall of the cooling housing 1 is gradually reduced from the volute 2 side to the closed housing 4 side and is in a multi-section structure, the inner diameter of the inner wall of each section of the cooling housing is different, the radial magnetic suspension bearing 200 is located at the section with the smaller inner diameter of the cooling housing, and the radial-axial integrated magnetic suspension bearing 100 is located at the section with the larger inner diameter of the cooling housing.

The invention has the advantages of simple structure, capability of realizing hydrogen sealing, capability of improving the rotating speed of the rotor shaft to ensure the function of pressurizing hydrogen, and capability of realizing miniaturization.