The present invention generally pertains to centrifugal particle separators. More particularly, the invention relates to a construction which improves the functional, structural and volumetric characteristics of molded or cast inlet vane assemblies of centrifugal particle separators.
Generally, air precleaners are used for removing particulates from the air prior to introducing the air through an air cleaner or filter of an internal combustion engine. The function of the air precleaner is to remove as many contaminants from the air as possible before it flows into an air filter medium upstream from the internal combustion engine.
Precleaners operate on the principle of centrifugal separation. Outside air, with its entrained contaminants, is drawn into the precleaner by the vacuum created by the engine. The air and contaminants traverse a set of fixed, static, vanes which cause the air to circulate at a great speed. Centrifugal force throws the contaminants and moisture towards the outer wall of the precleaner. The contaminants follow the wall until they reach an opening where they are discharged back into the atmosphere or collected. Clean, dry air is then allowed to enter the air filter and subsequently the internal combustion engine.
Undesirable contaminants in the atmosphere include particulate matter such as dirt, dust, sand, snow and the like. While most engines include air filters which are meant to remove such contaminants from the air that feeds the engine, engine precleaners are also used in order to extend the life of the air filter and extend the engine's life.
As air precleaners work on centrifugal separation, greater air flow velocity will result in better separation between air and contaminants. As the velocity of air flow decreases, the centrifugal force on the contaminants also decreases reducing the separation efficiency of the precleaner.
Several different designs of air precleaners are commercially available in the marketplace. In one design, a precleaner uses a rotatable impeller or spinner to separate particles from air, discharge the dirty air and particle mixture circumferentially from a housing and direct the clean air to the air intake structure of an engine. The clean air moves centrally through a stack to the engine in response to a vacuum pressure on the air moving to the engine. Known air precleaners have also included a design in which air flows into the top of the precleaner and flows axially downwardly through the precleaner and into the intake stack of the engine. Also, some air precleaners are only useable when positioned in one orientation, i.e. positioned on a vertical axis or positioned on a horizontal axis.
Typically, air precleaners of molded construction utilize a centrifugal particle separator having a one-piece inlet vane. This inlet vane generally has a gap between each blade on the vane for tooling clearances. This gap (commonly referred to as a “shut-off” clearance) allows a portion of the air to pass axially through the particle separator, effectively bypassing the intended swirling route established by the vane blades. This “shut-off” clearance increases as the designed maximum flow of the precleaner increases. This necessitates a particle separator of an undesirably large axial and circumferential volume, having a narrow operational flow range and less than optimum separation efficiency.
Accordingly, it has been considered desirable to develop a new and improved centrifugal particle separator incorporating overlapping inlet vanes assemblies which would overcome the foregoing difficulties and others while providing better and more advantageous overall results.
In an exemplary embodiment of the invention, a centrifugal particle separator is provided.
More particularly, in accordance with this aspect of the present invention, the centrifugal particle separator comprises a first vane assembly and a second vane assembly. The first vane assembly includes a centrally positioned hub, a collar encircling the hub and a plurality of first vanes. Each first vane has at least one of an inner end connected to the hub and an outer end connected to the collar, wherein a trailing edge of at least one of the plurality of first vanes extends past an edge of the collar. The second vane assembly includes a centrally positioned hub, a collar encircling the hub and a plurality of second vanes circumferentially disposed about the hub. Each second vane has at least one of an inner end connected to the hub and an outer end connected to the collar. When the first and second vane assemblies are secured together, at least one of the plurality of first vanes protrudes into the second vane assembly.
In accordance with another aspect of the present invention, a centrifugal particle separator comprises a first vane assembly and a second vane assembly. The first vane assembly includes a centrally positioned hub, a collar encircling the hub, and a plurality of first vanes circumferentially disposed about the hub. Each first vane has at least one of a radially inner end connected to the hub and a radially outer end connected to the collar, wherein a trailing edge of at least one first vane extends past an edge of the collar. The second vane assembly includes a centrally positioned hub, a collar encircling the hub, and a plurality of second vanes circumferentially disposed about the hub. Each second vane has at least one of a radially inner end connected to the hub and a radially outer end connected to the collar, wherein a leading edge of at least one second vane extends past an edge of the collar. The first vane assembly is selectively secured to the second vane assembly so as to allow the trailing edge of at least one first vane to be masked by the leading edge of at least one second vane.
In accordance with still another aspect of the present invention, a centrifugal particle separator comprises a first vane assembly and a second vane assembly. The first vane assembly includes a central portion including a sidewall, a collar encircling the central portion, and a plurality of first vanes circumferentially disposed about the central portion. At least one first vane includes a radially inner end connected to the central portion sidewall and a radially outer end connected to an inner sidewall of the collar. A trailing edge of at least one of the plurality of first vanes extends past an edge of the collar. The second vane assembly includes a central portion including a sidewall, a collar encircling the central portion, and a plurality of second vanes circumferentially disposed about the hub. At least one second vane includes a radially inner end connected to the central portion sidewall and a radially outer end connected to an inner sidewall of the collar. A leading edge of at least one of the plurality of second vanes extends past an edge of the collar. Fastening means are provided for selectively securing the first vane assembly to the second vane assembly.
Still other aspects of the invention will become apparent from a reading and understanding of the detailed description of the preferred embodiments hereinbelow.
The present invention may take physical form in certain parts and arrangements of parts, preferred embodiments of which will be described in detail in this specification and illustrated in the accompanying drawings which form a part of the invention.
Referring now to the drawings, wherein the showings illustrate the preferred embodiments of the invention only and are not intended to limit same,
In this embodiment, the first vane assembly 10 is mounted atop the second vane assembly 50 because the air precleaner assembly A is orientated along a vertical axis. Therefore, the first vane assembly 10 will be termed hereafter the upper vane assembly and the second vane assembly 50 will be termed hereafter the lower vane assembly. It should be recognized, however, that if the air precleaner assembly A were to extend along a horizontal axis, the terms “upper” and “lower” would lose their respective meaning.
With reference to
With continued reference to
With reference to
With continued reference to
The masking assembly 100, as shown in
With reference again to
Located at the distal end of each of the arms 126 is a respective second blade 134. Each second blade can be of compound shape. Each second blade 134 includes a first section 136 which is substantially aligned with its respective arm 126 and a second section 138 which is oriented at an angle to the first section 136. The second blades of the impeller are of a shape that will not unload with increasing static pressure. The relationship of the sizeable first blades 128 and the compound second blades 134 combine to provide a blade assembly which will not unload at increasing static pressures. These blades combine to convert the rotational velocity of the impeller to static pressure at ejection ports better than straight, forward or backward curved blades. The unique shape of the second blades 134 combined with the fact that these blades are rotating in the perimeter of the air leaving the inlet vanes 26, 76 of the centrifugal particle separator B provides for particle extraction by both low pressure and centrifugal force as well as by mechanical separation.
A pair of bearings 144 and 146 can be positioned in the hub bore 124. The bearings 144 and 146 enable the rotating impeller assembly to smoothly rotate in relation to the centrifugal particle separator B. A washer 148 can be positioned between a head of the bolt and the lower bearing 144. Also provided in this embodiment is a tubular bearing spacer 150 and a step washer 152 adjacent the upper bearing 146. The spacer is inserted in the bore 124 between the two bearings to prevent side loading of the bearings. The step washer 152 is illustrated with the smaller diameter end of the washer resting on the adjacent bearing 146 and the larger diameter end resting on the bottom seal plate 104. Alternatively, two washers of different diameters can be stacked.
To assemble the air precleaner A, the collar 32 of the upper vane assembly 10 is first releasably secured to the collar 82 of the lower vane assembly 50 by inserting the axially extending flange 40 in the recess 92. As shown in
Also provided is a fastening means for securing the rotating impeller assembly 120 to the centrifugal particle separator B. The fastening means can comprise the bolt 140 and the lock nut 142. The lock nut is generally hexagonally shaped and is positioned in the hexagonally shaped socket section 64, which is best shown in
With the air precleaner assembly A illustrated herein, atmospheric air flows around the hub 12 and across the vanes 26 of the upper vane assembly 10 and the vanes 76 of the lower vane assembly 50. Due to the overlapping vane design and the smooth curved shape of the inlet vanes 26 and 76, the air acquires a strong swirling motion as it flows into the rotating impeller assembly 120. The concave inlet vanes 26 and 76 illustrated in
With reference to
It should be apparent that the hub 12 of the upper vane assembly blocks direct access of the inlet air into an air inlet pipe of a vehicle's internal combustion engine (not shown) on which the air precleaner assembly A can be mounted. Further, the location of the collar 82 of the lower vane assembly 50 is such as to partially mask the second blades 134 providing higher vane speed for better ejection of particulates in the air stream.
Similar to the aforementioned first preferred embodiment, a second preferred embodiment is shown in
With reference to
The hood assembly 200 includes an end wall 202 and a skirt 204 depending therefrom. The end wall and the skirt together form a first chamber 205 for accommodating the impeller assembly 120′. As shown in
Positioned beneath the hood assembly 200 is the rotating impeller assembly 120′. The rotating impeller assembly comprises a hub 122′ having a bore 124′ extending axially therethrough. In this embodiment, four arms 220 radiate away from the hub. Of course, more or less than four arms could be employed for the rotating impeller assembly. Secured to the hub 122′ is a plurality of first blades 222, each of which is aligned with a respective one of the arms 220. The first blades are located at the proximal ends of the several arms. Located at the distal ends of each of the arms 220 is a respective second blade 134′. Each second blade includes a first section 136′ which is substantially aligned with its respective arm 220 and a second section 138′ which is oriented at an angle to the first section 136′.
A pair of bearings 144′ and 146′ can be positioned in the hub bore 124′. The bearings 144′ and 146′ enable the rotating impeller assembly to smoothly rotate in relation to the centrifugal particle separator B′. A first washer 224 can be positioned between a head of a bolt 230 and the lower bearing 144′. Also provided is a tubular bearing spacer 150′ and a step washer 226 adjacent the upper bearing 146′. The spacer is inserted in the bore 124′ between the two bearings to prevent side loading of the bearings. The step washer 226 is illustrated with the smaller diameter end of the washer resting on the adjacent bearing 146′ and the larger diameter end resting on a second washer 228.
Also provided is a fastening means for securing the rotating impeller assembly 120′ to the hood assembly 200. The fastening means can comprise a bolt 230, a lock nut 232, and two second washers 228. The lock nut can be generally hexagonally shaped and is positioned adjacent the second washer and end wall 202. The bolt extends upwardly through the hub 122′ from a bottom end of the rotating impeller assembly 120′. As the bolt 230 is being secured to the lock nut 232, the rotating impeller assembly 120′ is rotatably secured to the hood assembly 200.
With reference now to
With continued reference to
As shown in
A plurality of vanes 284 is circumferentially disposed about the hub 270. In this embodiment, each lower vane has a radially inner end 286 secured to the sidewall 272 of the hub 270 and a radially outer end 288 secured to a collar 290 encircling the hub. Each lower vane can be angled downwardly and laterally about the hub and can have a concave surface 292 along which inlet air flows. If desired, the degree of concavity of each vane can change along the length of the vane. A leading edge 294 of each lower vane can extend above an upper edge 296 of the collar. As with the trailing edges 256 of the upper vanes 242, not all of the leading edges 294 need extend above the upper edge 294 of the collar 290 in all embodiments of the invention.
As shown in
Extending radially outwardly of the collar 290, at a bottom edge thereof, is a horizontal ledge 300. Extending radially outwardly from the ledge is a plurality of spaced protrusions 302. As shown in
With the air precleaner assembly A′ including the centrifugal particle separator B′ illustrated in the second preferred embodiment, and with the air precleaner positioned in an upright orientation, atmospheric air flows upwardly over the vanes 284 of the lower vane assembly 50′ and the vanes 242 of the upper vane assembly 10′ into the centrifugal particle separator B′. As the air flows upwardly across the vanes 284 and 242, the air is caused to spin in a spiral direction as the air flows into the first chamber 205. As is best illustrated in
Typically, the masking assembly 100, the rotating impeller assembly 120 and hood assembly 200 are all made of a suitable conventional thermoplastic material. Of course, it should be recognized that one or more of these components could also be made from any other conventional type of material, such as a metal (e.g. aluminum or the like) and composite materials (e.g. carbon fiber reinforced resin material). In the preferred embodiments of the present invention, the upper vane assembly 10 and the lower vane assembly 50 are each of one piece and can be made of a conventional polymer material or a composite material including resin such that the vane assemblies are formed in a single molding operation.
In accordance with the present disclosure, the air precleaner assembly A removes undesirable contaminants from an airstream prior to the airstream reaching an air filter (not illustrated) of an internal combustion engine. The overlapping inlet vanes 26 and 76 of the upper and lower vane assemblies 10 and 50 of the centrifugal particle separator B increase the ability of the air precleaner assembly to remove contaminants from the intake air and reduce the required axial and radial dimensions of the air precleaner for any designed airflow capability.
Prior to the present invention, plastic and polymer precleaners had to include mold “shut-off clearances” for tooling purposes. This “shut-off clearance” allowed a portion of the airstream to travel axially (referred to as “blow-by”) through the air precleaner A, effectively bypassing the intended swirling route established by a centrifugal particle separator B. The present invention eliminates this “blow-by” by overlapping the inlet vanes 26 and 76, which can have identical vane profiles. While the “shut-off clearance” is maintained to produce each of the upper and lower vane assemblies, it is eliminated from the assembled centrifugal particle separator due to the stacking of the upper and lower vane assemblies 10 and 50 together.
One aspect of the present invention resides in the improved efficiency over prior single inlet vane centrifugal particle separators by eliminating the “blow-by” caused by the “shut-off clearance.” Other aspects of the present invention reside in improved corrosion resistance, manufacturing economy, structural integrity and weight reduction over prior centrifugal particle separators with overlapping inlet vanes due to the upper vane assembly 10 and the lower vane assembly 50 being of one piece and made of a conventional polymer material or composite.
The exemplary embodiments of the present invention have been described with reference to several preferred embodiments. Obviously, modifications and alterations will occur to others upon reading and understanding the preceding detailed description. It is intended that the invention not be limited to the embodiments described. Rather, the present invention should be construed as including all such modifications and alterations which come within the scope of the appended claims or the equivalents thereof.
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Number | Date | Country | |
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20060045731 A1 | Mar 2006 | US |