CN219282026U

CN219282026U - Breathing machine and turbine fan assembly thereof

Info

Publication number: CN219282026U
Application number: CN202223600650.9U
Authority: CN
Inventors: 黄嘉伟; 方飞村; 张文桂
Original assignee: Resvent Medical Technology Co Ltd
Current assignee: Resvent Medical Technology Co Ltd
Priority date: 2022-12-27
Filing date: 2022-12-27
Publication date: 2023-06-30
Anticipated expiration: 2032-12-27

Abstract

The application provides a turbo fan assembly, comprising: the shell comprises a main body, an air inlet cover and a sealing cover, wherein the main body comprises a side wall and a bottom wall, the bottom wall is connected to one end of the side wall, the sealing cover is arranged at one end of the main body far away from the bottom wall, a containing cavity is formed by surrounding between the side wall, the bottom wall and the sealing cover, the air inlet cover is arranged at one end of the main body close to the bottom wall, an air inlet channel communicated with the containing cavity is formed between the air inlet cover and the bottom wall, and the air inlet cover is provided with an air inlet communicated with the air inlet channel; and the turbine fan is accommodated in the accommodating cavity and fixedly arranged between the main body and the sealing cover. In addition, the application also provides a breathing machine. The application provides a turbofan subassembly can effectively fall the noise that the turbofan produced and make an uproar.

Description

Breathing machine and turbine fan assembly thereof

Technical Field

The application relates to the technical field of turbine fans, in particular to a breathing machine and a turbine fan assembly thereof.

Background

With the increasing development of medical technology, more and more people are aware of the hazards of respiratory diseases. As a medical device for treating a part of respiratory diseases, a ventilator is required to have high reliability. In the field of ventilator products, turbines are the most central critical device for generating a flow of gas. The vortex box is a bearing piece of the turbine and plays various roles of gas mixing, stabilizing airflow, reducing noise and noise, isolating vibration, conducting heat, reducing temperature and the like. However, the turbine may generate noise during operation, which may affect the user of the ventilator. At present, the main flow scheme mainly comprises the steps of completely filling the inner cavity of the vortex box by using sponge, or covering the surfaces of main noise sources such as an air inlet/an air outlet outside the vortex box by using sponge, and the like, and absorbing noise through a sponge micropore structure to achieve the purpose of noise reduction. The prior art mainly depends on the material property of the sponge to achieve the noise reduction effect, but can be limited by the material defect of the sponge.

Disclosure of Invention

In view of the foregoing, it is desirable to provide a ventilator and a turbo fan assembly thereof that can effectively reduce noise generated by the turbo fan.

In a first aspect, embodiments of the present application provide a turbine fan assembly comprising:

the shell comprises a main body, an air inlet cover and a sealing cover, wherein the main body comprises a side wall and a bottom wall, the bottom wall is connected to one end of the side wall, the sealing cover is arranged at one end of the main body far away from the bottom wall, a containing cavity is formed by surrounding between the side wall, the bottom wall and the sealing cover, the air inlet cover is arranged at one end of the main body close to the bottom wall, an air inlet channel communicated with the containing cavity is formed between the air inlet cover and the bottom wall, and the air inlet cover is provided with an air inlet communicated with the air inlet channel; and

the turbine fan is accommodated in the accommodating cavity and fixedly arranged between the main body and the sealing cover.

In a second aspect, embodiments of the present application provide a ventilator comprising a housing and a turbo-fan assembly as described above, the housing being provided with a mounting cavity, the turbo-fan assembly being disposed in the mounting cavity.

Above-mentioned breathing machine and turbine fan subassembly thereof have abandoned the cotton scheme of inhaling the sound bubble, through the holistic structural design of turbine fan subassembly's casing to reach the purpose that gives sound insulation, amortization, leading sound, fall noise. The air inlet groove and the air inlet channel are the air passages, and can be used for reducing noise, so that the noise reduction effect is optimized, and the whole volume of the shell is reduced. The annular radial stacked shell design can form a plurality of cavities and walls for physical silencing, so that the whole air channel is of a concentrated, divergent and re-concentrated air channel design. The shell is used as a bearing part of the turbine fan, so that the number of parts of the whole assembly of the turbine fan assembly can be effectively reduced, the assembly and material cost is greatly reduced, the effects of mixing air flow, stabilizing air flow, reducing noise, isolating vibration, conducting heat, reducing temperature and the like are also achieved, and the stability and the user experience of the turbine fan assembly are greatly improved.

Drawings

In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings that are required in the embodiments or the description of the prior art will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present application, and that other drawings may be obtained from the structures shown in these drawings without inventive effort to a person of ordinary skill in the art.

Fig. 1 is a perspective view of a turbine fan assembly provided in an embodiment of the present application.

FIG. 2 is a first exploded schematic view of a turbofan assembly provided in an embodiment of the present application.

FIG. 3 is a second exploded schematic view of a turbofan assembly provided in an embodiment of the present application.

Fig. 4 is a first schematic cross-sectional view of a turbofan assembly provided in an embodiment of the present application.

Fig. 5 is a second cross-sectional schematic view of a turbofan assembly provided in an embodiment of the present application.

FIG. 6 is a perspective view of the main body of the turbofan assembly shown in FIG. 1.

FIG. 7 is a schematic cross-sectional view of a main body of the turbofan assembly shown in FIG. 1.

Fig. 8 is a schematic diagram of a ventilator according to an embodiment of the present application.

The realization, functional characteristics and advantages of the present application will be further described with reference to the embodiments, referring to the attached drawings.

Detailed Description

In order to make the objects, technical solutions and advantages of the present application more apparent, the present application will be further described in detail with reference to the accompanying drawings and examples. It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the present application. All other embodiments, which can be made by one of ordinary skill in the art without undue burden from the present disclosure, are within the scope of the present disclosure.

The terms "first," "second," "third," "fourth" and the like in the description and in the claims of this application and in the above-described figures, if any, are used for distinguishing between similar elements of a plan and not necessarily for describing a particular sequential or chronological order. It is to be understood that the data so used may be interchanged under appropriate circumstances, or in other words, the described embodiments may be implemented in other sequences than those illustrated or otherwise described herein. Furthermore, the terms "comprises," "comprising," and "having," and any variations thereof, may also include other items, such as processes, methods, systems, articles, or apparatus that include a series of steps or elements, are not necessarily limited to only those steps or elements explicitly listed, but may include other steps or elements not explicitly listed or inherent to such processes, methods, articles, or apparatus.

It should be noted that the description herein of "first," "second," etc. is for descriptive purposes only and is not to be construed as indicating or implying a relative importance or implying an indication of the number of technical features being indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include one or more such feature. In addition, the technical solutions of the embodiments may be combined with each other, but it is necessary to base that the technical solutions can be realized by those skilled in the art, and when the technical solutions are contradictory or cannot be realized, the combination of the technical solutions should be regarded as not exist and not within the protection scope of the present application.

Referring to fig. 1 to 5 in combination, fig. 1 is a perspective view of a turbo fan assembly provided in an embodiment of the present application, fig. 2 is a first exploded schematic view of the turbo fan assembly provided in an embodiment of the present application, fig. 3 is a second exploded schematic view of the turbo fan assembly provided in an embodiment of the present application, fig. 4 is a first cross-sectional schematic view of the turbo fan assembly provided in an embodiment of the present application, and fig. 5 is a second cross-sectional schematic view of the turbo fan assembly provided in an embodiment of the present application. The turbine fan assembly 1 is applied to ventilation treatment equipment such as a breathing machine and is a key device of the most core of the ventilation treatment equipment. In some possible embodiments, the turbo-fan assembly 1 may also be applied to a vacuum cleaner, a blower, or the like provided with a turbo-fan, which is not limited herein.

The turbo-fan assembly 1 comprises a housing 10 and a turbo-fan 20. Wherein, the shell 10 is provided with a containing cavity 110, and the turbine fan 20 is contained in the containing cavity 110.

The housing 10 includes a main body 11, an intake cover 12, and a sealing cover 13. In the present embodiment, the main body 11 includes a side wall 111 and a bottom wall 112, and the bottom wall 112 is connected to one end of the side wall 111. Specifically, the side wall 111 includes a first side wall 1111 and a second side wall 1112, the bottom wall 112 is connected to one end of the first side wall 1111, and the second side wall 1112 is sleeved outside the first side wall 1111. Wherein an air intake slot 1110 is formed between the first sidewall 1111 and the second sidewall 1112. It will be appreciated that the body 11 has a double-layer solid wall.

In the present embodiment, the side wall 111 is circular and the bottom wall 112 is circular. Specifically, the first sidewall 1111 and the second sidewall 1112 are each generally hollow circular tube-shaped. Accordingly, the air intake slot 1110 between the first sidewall 1111 and the second sidewall 1112 is substantially circular. In some possible embodiments, the outer portion of the sidewall 111 may be square or shaped and the inner portion of the sidewall 111 is circular. That is, the second sidewall 1112 may be square or shaped, but the first sidewall 1111 is hollow and circular-tubular regardless of the shape of the second sidewall 1112.

The sealing cover 13 is arranged at one end of the main body 11 far away from the bottom wall 112, and the air inlet cover 12 is arranged at one end of the main body 11 near the bottom wall 112. A receiving chamber 110 is defined between the side wall 111, the bottom wall 112 and the sealing cover 13. Specifically, the sealing cover 13 is disposed on an end of the second side wall 1112 far away from the bottom wall 112, the air inlet cover 12 is disposed on an end of the second side wall 1112 near the bottom wall 112, and the accommodating cavity 110 is defined among the first side wall 1111, the bottom wall 112 and the sealing cover 13. The second side wall 1112 is sleeved on a side of the first side wall 1111 away from the accommodating chamber 110. In this embodiment, an end of the first side wall 1111 away from the bottom wall 112 is flush with an end of the second side wall 1112 away from the bottom wall 112, and the first side wall 1111 and the second side wall 1112 are fixedly connected by a fixing portion 1113.

The air inlet cover 12 is covered on one side of the bottom wall 112 away from the accommodating cavity 110, and an air inlet channel 102 communicated with the accommodating cavity 110 is formed between the air inlet cover 12 and the bottom wall 112. The intake cover 12 is provided with an intake port 120, and the intake port 120 communicates with the intake passage 102. The air intake channel 1110 communicates the air intake passage 102 with the accommodating chamber 110. It will be appreciated that the air inlet 120, the air inlet passage 102, the air inlet channel 1110 and the receiving cavity 110 are in communication in sequence. In the present embodiment, the intake cover 12 is circular as a whole, and the intake port 120 is located at the center of the intake cover 12.

When the turbo fan 20 accommodated in the accommodating chamber 110 is operated, air flow needs to enter the housing 10 from the air inlet 120 and pass through the air inlet passage 102 and the air inlet groove 1110 in order to reach the accommodating chamber 110. The air intake slot 1110 between the first side wall 1111 and the second side wall 1112 is substantially circular, and the cross-sectional area of the air intake slot 1110 increases as the radius of the side wall 111 increases.

Further, when the turbo fan 20 accommodated in the accommodating chamber 110 is operated, noise generated from the turbo fan 20 needs to pass through the accommodating chamber 110, the air inlet groove 1110, the air inlet passage 102 and the air inlet 120 in order to be transmitted to the outside of the housing 10 through the air passage. The arrangement and the cooperation between the main body 11, the air inlet cover 12 and the sealing cover 13 effectively increase the distance that noise needs to travel, and can greatly reduce the noise so as to achieve the aim of multiple noise reduction.

The air intake cover 12 includes a cover body 121 and an air intake wall 122, one end of the air intake wall 122 is connected to the cover body 121, and the other end of the air intake wall 122 extends in a direction approaching the bottom wall 112. In the present embodiment, the size of the air inlet wall 122 near the end of the bottom wall 112 is smaller than the size of the air inlet wall 122 far from the end of the bottom wall 112. The air inlet wall 122 encloses the air inlet 120. Accordingly, the cover 121 is circular; the air intake wall 122 is provided at the center of the cover 121.

In the present embodiment, a rib 123 is provided on a side of the lid 121 facing the bottom wall 112, and the rib 123 extends from the side of the lid 121 in a direction approaching the bottom wall 112. Specifically, the rib 123 is circumferentially disposed around the air inlet wall 122.

The bottom wall 112 includes a plurality of projections 1121 and depressions 1122. Wherein, the concave part 1122 is concave from the bottom wall 112 to the direction away from the air inlet cover 12 and is arranged opposite to the air inlet wall 122 and the convex rib 123; the protruding portion 1121 protrudes from the bottom wall 112 in a direction approaching the intake cover 12, and is provided opposite to the intake port 120 or between the intake wall 122 and the rib 123. In the present embodiment, the concave portions 1122 are alternately arranged with the convex portions 1121. A portion of the recess 1122 is disposed opposite the intake wall 122, and another portion of the recess 1122 is disposed opposite the rib 123. One of the protrusions 1121 is disposed opposite the air inlet 120, and the remaining protrusions 1121 are disposed between the air inlet wall 122 and the rib 123. It will be appreciated that the protruding

portions

1121, 1122 of the bottom wall 112 are mutually engaged with the air intake wall 122, the ribs 123 of the air intake cover 12, and are alternately arranged, so that the air intake passage 102 is overall in a meandering S-shape in cross-section, and the length of the air intake passage 102 can be increased. Meanwhile, the S-shaped tortuous air inlet channel 102 can also form channel wall projection overlapping in the radial direction, and the thickness of the overlapping is 5 times or more than that of a conventional wall thickness, so that noise can be effectively reduced, and a better sound insulation effect is achieved.

In this embodiment, the protrusion 1121 includes a boss 1120 disposed opposite the air inlet 120. Specifically, the end of the boss 1120 remote from the receiving cavity 110 extends from the end of the intake wall 122 proximate the bottom wall 112 to the intake port 120. It will be appreciated that the end of the boss 1120 remote from the receiving cavity 110 is further from the bottom wall 112 than the end of the inlet wall 122 closer to the receiving cavity 110.

The outer wall of the boss 1120 is inclined, and the size of the boss 1120 near one end of the accommodating chamber 110 is larger than the size of the boss 1120 far from the one end of the accommodating chamber 110. That is, the boss 1120 is generally trapezoidal and cylindrical, i.e., is generally circular. The boss 1120 is designed to effectively weaken the rigidity of the bottom wall 112 in the axial direction, and guide most of the noise generated by the turbofan 20 to the boss 1120 for dispersion in the form of resonance propagation. Meanwhile, the boss 1120 divides the air inlet channel from a solid circle into a state of annular tiling, so that the clustered air flows flowing in from the air inlet 120 can be effectively dispersed and uniformly distributed to the whole air inlet channel 102, the clustered air flows are dispersed into a plurality of dispersed air flows, the flow speed of the dispersed air flows can be effectively slowed down, and the wind noise of the air flows is reduced. In some possible embodiments, the boss 1120 may also be hemispherical, ellipsoidal, conical, etc., without limitation. In other possible embodiments, the boss 1120 may be integrally formed as a recess, i.e., extending from the bottom wall 112 in a direction away from the air inlet 120.

The housing 10 is provided with a limiting aperture 100. In this embodiment, the sealing cover 13 is provided with a notch 130, the main body 11 is correspondingly provided with a through hole 114, and the notch 130 and the through hole 114 together form the limiting hole 100. Specifically, the through hole 114 is opened at one end of the side wall 111 near the seal cover 13.

Referring to fig. 6 and 7 in combination, fig. 6 is a perspective view of a main body provided in an embodiment of the present application, and fig. 7 is a schematic cross-sectional view of the main body provided in an embodiment of the present application. In the present embodiment, a plurality of reinforcing ribs 113 are provided on a side of the bottom wall 112 facing the turbo fan 20. The reinforcing ribs 113 are disposed at intervals along the circumferential direction of the bottom wall 112, and disposed on the bottom wall 112 along a preset direction. Specifically, each rib 113 is formed in a sheet shape as a whole, and is connected to a side of the bottom wall 112 facing the accommodating chamber 110 and a side of the first side wall 1111 facing the accommodating chamber 110. The reinforcement rib 113 may increase the rigidity of the junction of the bottom wall 112 and the first side wall 1111, and reduce the occurrence of resonance between the bottom wall 112 and the first side wall 1111, thereby reducing the propagation of noise.

In the present embodiment, the turbo blower 20 is fixedly installed between the main body 11 and the sealing cover 13. Specifically, the turbo fan 20 is fixedly installed between the bottom wall 112 and the seal cover 13. The turbo fan 20 includes a fan blade 21 and an air inlet pipe 22, the air inlet pipe 22 is disposed at one side of the turbo fan 20 facing the bottom wall 112, and the air inlet 201 is disposed at the air inlet pipe 22. The air inlet pipe 22 is in a circular tube shape, and the air inlet 201 is opposite to the boss 1120.

The fan blade 21 includes a rotation direction, and the reinforcement rib 113 is disposed along the bottom wall 112 in the same circumferential direction as the rotation direction. That is, if the rotation direction of the fan blade 21 is clockwise, the reinforcing ribs 113 are sequentially provided in the clockwise direction; if the rotation direction of the fan blade 21 is counterclockwise, the ribs 113 are disposed in order in the counterclockwise direction. The preset included angle is formed between the preset direction of the reinforcing rib 113 and the diameter of the fan blade 21, and the straight line where the preset direction is located is tangent to the pipe wall of the air inlet pipe 22. In this embodiment, the preset angle is 30 °. In some possible embodiments, the preset included angle may also be a degree of other values such as 20 °, 25 °, 35 °, 40 °, or 45 °, which is not limited herein.

The preset included angle between the preset direction of the reinforcing rib 113 and the diameter of the fan blade 21 is 30 degrees, and the preset direction is tangential to the pipe wall of the air inlet pipe 22, so that the reinforcing rib 113 can play a role in guiding the flow direction of the air flow, the flow direction of the air flow entering the turbine fan 20 from the air inlet 201 is consistent and tangential to the rotation direction of the fan blade 21, the turbulence amplitude generated by the impact of the air flow and the fan blade 21 is reduced, and the purposes of noise reduction and noise reduction are finally achieved.

Referring again to fig. 2, the turbo fan 20 further includes an air outlet pipe 23, and the air outlet pipe 23 protrudes from the limiting hole 100 to the outside of the housing 10. The turbine fan assembly 1 further comprises a sealing member 40, wherein the sealing member 40 is sleeved at one end of the air outlet pipe 23 far away from the accommodating cavity 110, and is sealed between the air outlet pipe 23 and the shell 10.

The turbo-fan assembly 1 further includes a damper 30, the damper 30 being disposed between the turbo-fan 20 and the reinforcing ribs 113. It will be appreciated that the damper 30 is fixed to the end of the rib 113 remote from the bottom wall 112, and the turbo fan 20 is fixedly disposed between the damper 30 and the sealing cover 13. In the present embodiment, the damper 30 is provided with a through hole 31, and the air inlet pipe 22 is accommodated in the through hole 31. Wherein the shock absorbing member 30 is a disc spring type member. When the turbo fan 20 is operated, the air pressure of the air flow at the air inlet 201 will float and change, so that the whole turbo fan 20 may vibrate up and down along with the rotation of the fan blades 21, and noise is generated. The damping piece 30 is arranged at the air inlet 201 of the turbofan 20, and when the turbofan 20 vibrates up and down, the damping piece 30 can correspondingly generate deformation damping to provide stable damping and damping, so that the amplitude of the turbofan 20 is slowed down, and the purpose of noise reduction is achieved. In this embodiment, the shock absorbing member 30 is made of a silicone material. In some possible embodiments, the shock absorbing member 30 may also be made of a non-rigid material including, but not limited to, soft materials such as TPU, TPE, etc.

In the above embodiment, the scheme of sound absorbing foam is abandoned, and the purposes of sound insulation, noise reduction, sound guiding and noise reduction are achieved through the integral structural design of the shell of the turbine fan assembly. The air inlet groove and the air inlet channel are the air passages, and can be used for reducing noise, so that the noise reduction effect is optimized, and the whole volume of the shell is reduced. The annular radial stacked shell design can form a plurality of cavities and walls for physical silencing, so that the whole air channel is of a concentrated, divergent and re-concentrated air channel design. The shell is used as a bearing part of the turbine fan, so that the number of parts of the whole assembly of the turbine fan assembly can be effectively reduced, the assembly and material cost is greatly reduced, the effects of mixing air flow, stabilizing air flow, reducing noise, isolating vibration, conducting heat, reducing temperature and the like are also achieved, and the stability and the user experience of the turbine fan assembly are greatly improved.

Please refer to fig. 8 in combination, which is a schematic diagram of a ventilator according to an embodiment of the present application. The ventilator 9 includes a housing 2 and a turbo fan assembly 1. The specific structure of the turbo fan assembly 1 refers to the above-described embodiment.

In this embodiment, the housing 2 is provided with a mounting cavity 3, and the turbo fan assembly 1 is provided in the mounting cavity 3.

In the above embodiments, since the ventilator 9 adopts all the technical solutions of all the embodiments, at least the advantages brought by the technical solutions of the embodiments are provided, and will not be described in detail herein.

It will be apparent to those skilled in the art that various modifications and variations can be made in the present application without departing from the spirit or scope of the application. Thus, if and when such modifications and variations of the present application fall within the scope of the claims and their equivalents, the present application is intended to cover such modifications and variations.

The foregoing list of preferred embodiments of the present application is, of course, not intended to limit the scope of the claims hereof, and therefore, equivalent changes as set forth in the claims hereof are intended to fall within the scope of the present application.

Claims

1. A turbofan assembly, the turbofan assembly comprising:

2. The turbofan assembly of claim 1 wherein the side wall comprises a first side wall and a second side wall, the bottom wall is connected to one end of the first side wall, and the first side wall, the bottom wall and the sealing cover enclose the receiving cavity therebetween; the second side wall is sleeved on one side, far away from the accommodating cavity, of the first side wall, an air inlet groove is formed between the first side wall and the second side wall, and the air inlet groove is communicated with the air inlet channel and the accommodating cavity.

3. The turbofan assembly of claim 2 wherein the intake cover comprises a cover body and an intake wall, one end of the intake wall being connected to the cover body, the other end of the intake wall extending in a direction toward the bottom wall, the intake wall surrounding the intake opening; a rib is arranged on one side of the cover body, which faces the bottom wall, and extends from one side of the cover body to a direction close to the bottom wall; the bottom wall comprises a plurality of protruding parts and recessed parts, the recessed parts are recessed from the bottom wall towards the direction away from the air inlet cover, are opposite to the air inlet wall and the convex edges, and the protruding parts protrude from the bottom wall towards the direction close to the air inlet cover, are opposite to the air inlet or are arranged between the air inlet wall and the convex edges.

4. The turbofan assembly of claim 3 wherein the size of the inlet wall proximate one end of the bottom wall is smaller than the size of the inlet wall distal one end of the bottom wall; the protruding portion comprises a boss which is arranged opposite to the air inlet, and one end, away from the accommodating cavity, of the boss extends from one end, close to the bottom wall, of the air inlet wall to the air inlet.

5. The turbofan assembly of claim 4 wherein the side wall is tubular and the bottom wall is generally circular; the diapire orientation one side of turbo fan is equipped with a plurality of strengthening ribs, a plurality of strengthening ribs are followed the circumference direction interval setting of diapire.

6. The turbofan assembly of claim 5 wherein the turbofan includes blades that include a direction of rotation; the reinforcing ribs are arranged on the bottom wall along a preset direction, and a preset included angle is formed between the preset direction and the diameter of the fan blade; the circumferential direction is the same as the rotational direction.

7. The turbofan assembly of claim 6 further comprising a shock absorber disposed between the turbofan and the stiffener; the turbine fan is towards one side of diapire is equipped with the air intake, the turbine fan includes the air-supply line, the air intake set up in the air-supply line, the damping member is equipped with the through-hole, the air-supply line holding in the through-hole.

8. The turbofan assembly of claim 7 wherein the air inlet is disposed opposite the boss; the air inlet pipe is in a circular pipe shape, and a straight line in which the preset direction is located is tangent to the pipe wall of the air inlet pipe; the preset included angle is 30 degrees.

9. The turbofan assembly of claim 1 wherein the turbofan includes an outlet duct, the housing having a limiting aperture, the outlet duct protruding from the limiting aperture to the exterior of the housing; the turbine fan assembly further comprises a sealing piece, wherein the sealing piece is sleeved at one end, far away from the accommodating cavity, of the air outlet pipe and is sealed in a gap between the air outlet pipe and the shell.

10. A ventilator comprising a housing provided with a mounting cavity and a turbo fan assembly according to any one of claims 1 to 9, the turbo fan assembly being arranged in the mounting cavity.