US20190195225A1 - Rotary blower - Google Patents
Rotary blower Download PDFInfo
- Publication number
- US20190195225A1 US20190195225A1 US15/852,570 US201715852570A US2019195225A1 US 20190195225 A1 US20190195225 A1 US 20190195225A1 US 201715852570 A US201715852570 A US 201715852570A US 2019195225 A1 US2019195225 A1 US 2019195225A1
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- United States
- Prior art keywords
- lobe
- seal insert
- tip
- housing
- rotary blower
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/08—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
- F04C18/12—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type
- F04C18/126—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with radially from the rotor body extending elements, not necessarily co-operating with corresponding recesses in the other rotor, e.g. lobes, Roots type
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C27/00—Sealing arrangements in rotary-piston pumps specially adapted for elastic fluids
- F04C27/001—Radial sealings for working fluid
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C27/00—Sealing arrangements in rotary-piston pumps specially adapted for elastic fluids
- F04C27/001—Radial sealings for working fluid
- F04C27/004—Radial sealing elements specially adapted for intermeshing-engagement type pumps, e.g. gear pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C27/00—Sealing arrangements in rotary-piston pumps specially adapted for elastic fluids
- F04C27/008—Sealing arrangements in rotary-piston pumps specially adapted for elastic fluids for other than working fluid, i.e. the sealing arrangements are not between working chambers of the machine
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2240/00—Components
- F04C2240/20—Rotors
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2240/00—Components
- F04C2240/30—Casings or housings
Definitions
- the present application generally relates to blowers and more particularly, but not exclusively, to rotary blowers.
- Rotary blowers of various types e.g., Roots blowers
- Some existing systems have various shortcomings, drawbacks and disadvantages relative to certain applications.
- undesirable amounts of leakage between the rotors and/or between the housing and the rotors may occur. Accordingly, there remains a need for further contributions in this area of technology.
- a rotary blower includes a housing and a pair of meshed rotors.
- the meshed rotors are disposed in the housing.
- Each rotor has a plurality of lobes.
- Each lobe includes a lobe tip seal insert mounted thereon.
- the lobe tip seal insert is disposed at a tip of each lobe.
- Each lobe tip seal insert is constructed to seal against the housing and to prevent or reduce leakage between each lobe and the housing.
- FIG. 1 schematically illustrates a cross-sectional view depicting some aspects of a non-limiting example of a rotary blower in accordance with an embodiment of the present invention.
- FIG. 2 schematically illustrates a cross-sectional view depicting some aspects of a non-limiting example of the rotary blower of FIG. 1 with the rotors at a first rotational position, which is the rotational position illustrated in FIG. 1 .
- FIG. 3 schematically illustrates a cross-sectional view depicting some aspects of a non-limiting example of the rotary blower of FIG. 1 , from the perspective of FIG. 2 but with the rotors at a second rotational position.
- FIG. 4 schematically illustrates a cross-sectional view depicting some aspects of a non-limiting example of the rotary blower of FIG. 1 , from the perspective of FIG. 2 but with the rotors at a third rotational position.
- FIG. 5 schematically illustrates a cross-sectional view depicting some aspects of a non-limiting example of a 3-lobed rotary blower in accordance with an embodiment of the present invention.
- FIGS. 6A-6C illustrate cross-sectional views depicting some aspects of non-limiting examples of lobe side seal inserts and a lobe tip seal insert in accordance with an embodiment of the present invention.
- FIG. 7 depicts a cross-section illustrating some aspects of a non-limiting example of a lobe side seal insert in accordance with an embodiment of the present invention.
- FIG. 8 depicts a cross-section illustrating some aspects of a non-limiting example of a lobe tip seal insert in accordance with an embodiment of the present invention.
- FIG. 9 depicts a cross-section illustrating some aspects of a non-limiting example of a pusher weight in accordance with an embodiment of the present invention.
- rotary blower 10 is a Roots blower. In other embodiments, rotary blower 10 may take other forms.
- rotary blower 10 includes a pair of rotors, i.e., a driving rotor 12 in mesh with a driven rotor 14 .
- each of driving rotor 12 and driven rotor 14 are 2-lobed rotors.
- driving rotor 12 and driven rotor 14 may be 3-lobed rotors, 4-lobed rotors, or rotors having any number of lobes.
- Driving rotor 12 and driven rotor 14 are supported by respective shafts 16 , 18 and 20 , 22 .
- Shafts 16 , 18 , 20 and 22 may be integral with rotors 12 , 14 , or may be separate components affixed or mounted onto or into rotors 12 , 14 .
- Shafts 16 , 18 , 20 and 22 are supported by respective bearings 24 , 26 , 28 and 30 .
- Driving rotor 12 and driven rotor 14 are disposed radially within a housing 32 , which cooperates with driving rotor 12 and driven rotor 14 to pump or compress a fluid, such as air.
- Driving rotor 12 and driven rotor 14 are disposed axially between head plates 34 and 36 .
- Housing 32 is coupled, e.g., bolted, to head plates 34 and 36 .
- Bearings 24 , 26 , 28 and 30 are mounted in and supported by head plates 34 and 36 .
- Bearings 24 , 26 , 28 and 30 transmit radial and thrust loads from rotors 12 and 14 to head plates 34 and 36 .
- bearings 24 , 26 , 28 and 30 are rolling element bearings.
- bearings 26 and 30 are ball thrust bearings
- bearings 24 and 28 are roller bearings.
- one or more of bearings 24 , 26 , 28 and 30 may be one or more other types of bearings.
- Driving rotor 12 is supplied with shaft power via a shaft power source, such as an electric motor (not shown).
- Driving rotor 12 is operative to supply mechanical power to driven rotor 14 via gears 38 and 40 .
- Gears 38 and 40 are mounted on respective shafts 16 and 20 of respective driving and driven rotors 12 and 14 , and are in mesh with each other.
- Gears 38 and 40 are operative to maintain a desired angular relationship between driving rotor 12 and driven rotor 14 , and to transmit rotational motion and power from driving rotor 12 to driven rotor 14 .
- a plurality of seals may be employed to prevent the leakage of oil and/or compressed gas/fluids into undesired portions of rotary blower 10 .
- End plate covers (not shown) may be employed to cover the bearings 24 , 26 , 28 , 30 and gears 38 , 40 .
- FIGS. 2-4 in conjunction with FIG. 1 , during operation of rotary blower 10 , an inlet gas stream to be pumped or compressed enters rotary blower 10 through an inlet 42 , and the inlet gas is trapped in chambers formed between lobes 44 and the blower body or housing 32 , and is forced out of rotary blower 10 at an outlet 46 .
- three types of clearances are typically used in order to allow rotation of the rotors relative to the housing and relative to each other. Examples of such clearances that occur in conventional blowers are illustrated in FIGS. 2-4 , which are exaggerated for purposes of illustration. In the depictions of FIG.
- lobe seal inserts 58 , 60 illustrated in and described with respect to FIG. 5-9 are not shown in order to illustrate the clearances.
- One such clearance is lateral clearance 48 , which is the clearance between the rotors 12 , 14 (including lobes 44 ) and the head plates, e.g., such as head plates 34 and 36 .
- Another such clearance is diameter or diametral clearance 50 , which is the radial clearance between the rotor lobes and the housing, e.g., housing 32 .
- a third such clearance is the clearance between rotors, or between lobes, e.g., parallel lobes, such as 30° clearance 52 .
- clearances are typically calculated in consideration of thermal effects, such as dilation or thermal expansion.
- the blower may crash or seize or otherwise be damaged if the clearances are too small.
- the size of the clearances or amount of clearance impacts blower efficiency. For example, efficiency decreases with increasing clearance, e.g., due to leakage through the clearances.
- Embodiments of the present invention reduce or eliminate the diameter clearance and the clearance between rotors (lobes), e.g., the 30° clearance, via the use of lobe seal inserts (not shown in FIG. 1-4 ).
- Rotary blower 10 A includes meshed driving rotor 12 A and driven rotor 14 A. Each of driving rotor 12 A and driven rotor 14 A have three lobes 44 A. Each lobe 44 A has a tip 54 and two sides 56 . Each lobe 44 A includes a lobe tip seal insert 58 mounted thereon. Some aspects of a non-limiting example of lobe tip seal insert 58 are illustrated in FIG. 5 , FIG. 6A and FIG. 8 .
- Each lobe 44 A also includes two lobe side seal inserts 60 mounted thereon, one lobe side seal insert 60 on each side 56 .
- Some aspects of a non-limiting example of lobe side seal insert 60 are illustrated in FIG. 5 , FIG. 6B , FIG. 6C and FIG. 7 .
- a greater amount of lobe tip seal inserts 58 and lobe side seal inserts 60 may be employed.
- Some embodiments may include only lobe tip seal insert(s) 58 or only lobe side seal insert(s) 60 .
- lobe tip seal inserts 58 and lobe side seal inserts 60 are flexible and compliant.
- portions of lobe tip seal inserts 58 and lobe side seal inserts 60 may be rigid.
- the material used to form lobe tip seal inserts 58 and lobe side seal inserts 60 is different than the material used to form the balance of rotors 12 A and 14 A.
- the material used to form lobe tip seal inserts 58 and lobe side seal inserts 60 may be non-metallic, whereas the material used to form the balance of rotors 12 A and 14 A may be metallic in some embodiments.
- lobe tip seal inserts 58 and lobe side seal inserts 60 may be formed from, for example, a polymeric or composite or other non-metallic material.
- preferable materials used to make lobe tip seal inserts 58 and lobe side seal inserts 60 are capable of continuous use at temperatures up to 180° C.; supports sliding speeds up to 40 m/s, and have a relatively low coefficient of friction.
- the materials used to make lobe tip seal inserts 58 and lobe side seal inserts 60 , and the corresponding coefficients of friction, may vary with the needs of the particular application.
- Each lobe tip seal insert 58 is disposed at tip 54 of each lobe 44 A.
- each lobe tip seal insert 58 is constructed and operative to seal against housing 32 and to prevent or reduce leakage between each lobe 44 A and housing 32 .
- each lobe tip seal insert 58 is also constructed and operative to seal against portions of the opposite rotor, e.g., at a location 12 A 1 , 14 A 1 between the lobes 44 A, and also at the base or bottom or radially inward portion 44 A 1 of the lobes 44 A, to prevent or reduce leakage between each lobe 44 A of one rotor and location 12 A 1 , 14 A 1 of the other rotor, and between each lobe 44 A of one rotor and the base portions 44 A 1 of lobes 44 A on the other rotor.
- each lobe tip seal insert 58 is constructed to contact housing 32 during the operation of blower 10 .
- each lobe tip seal insert 58 is constructed to engage in sliding contact with housing 32 during rotation of the rotors, i.e., during operation of rotary blower 10 .
- each lobe tip seal insert 58 is constructed to have an interference fit 64 with housing 32 , e.g., as illustrated in FIG. 6A , wherein a free surface boundary 66 of a free lobe tip seal insert 58 (e.g., the sealing surface boundary of a lobe tip seal insert 58 not compressed by housing 32 or an adjacent rotor) extends beyond the compressed surface boundary 68 of a lobe tip seal insert 58 in the interference condition.
- the interference condition occurs when lobe tip seal 58 on one lobe 44 A is compressed by interference with housing 32 or with an adjacent rotor at a location 12 A 1 , 14 A 1 between lobes or at the base or bottom portion 44 A 1 of the meshing lobe 44 A.
- the compressed boundary 68 is the boundary of the installed lobe tip seal insert 58 after being compressed due to the interference fit with housing 32 or with an adjacent rotor, e.g., as depicted in FIG. 6A , which illustrates the interference with housing 32 .
- lobe tip seal inserts 58 may be constructed to reduce diameter clearance 50 ( FIG. 2 ) without contacting housing 32 under some or all operating conditions, or may be constructed to reduce diameter clearance 50 by contacting housing 32 with little or no interference, e.g., under some or all operating conditions.
- each lobe 44 A includes a pusher weight 62 , e.g., a rod.
- pusher weight 62 is a rod having a circular cross section. In other embodiments, pusher weight 62 may have any suitable geometric configuration.
- Each pusher weight 62 is constructed and operative to impart a radially outward, centrifugal load on a corresponding lobe tip seal insert 58 , e.g., to aid in loading lobe tip seal insert 58 in a direction toward housing 32 and toward the lobe and rotor that the lobe 44 A is meshing with.
- the radially outward loading may, for example, aid in maintaining desired contact loading between lobe tip seal insert 58 and housing 32 , and between the lobe tip seal insert 58 and the lobe and rotor it is meshing with.
- Other embodiments may not employ a pusher weight.
- each lobe 44 A includes a tip recess 70 disposed at the tip 54 of the lobe.
- Lobe tip seal insert 58 is mounted in tip recess 70 .
- Other embodiments may not include a tip recess.
- tip recess 70 includes a dovetail 72 for mating with a corresponding dovetail 74 on lobe tip seal insert 58 for retaining lobe tip seal insert 58 on lobe 44 A.
- other geometric configurations and/or fasteners may be employed to retain lobe tip seal insert 58 onto lobe 44 A.
- Each lobe side seal insert 60 is disposed at side 56 of the each lobe 44 A.
- each lobe side seal insert 60 of one rotor is constructed to seal against an adjacent lobe 44 A in mesh therewith of the other rotor, including against an adjacent lobe side seal insert 60 .
- Each lobe side seal insert 60 is constructed and operative to prevent or reduce leakage between adjacent lobes 44 A in mesh with each other, e.g., while the lobes are meshing.
- each lobe side seal insert 60 is constructed to contact and seal against the adjacent lobe in mesh therewith (including contacting and sealing against the lobe side seal insert 60 on the adjacent lobe) during operation of blower 10 .
- each lobe side seal insert 60 is constructed to engage in sliding contact with the adjacent lobe 44 A in mesh therewith (including sliding contact with an adjacent lobe side seal insert 60 ) during rotation of the rotors, i.e., during operation of rotary blower 10 .
- each lobe side seal insert 60 is constructed to have an interference fit 76 with the adjacent meshing lobe 44 A, e.g., as illustrated in FIG. 6B , wherein a free surface boundary 78 of a free lobe side seal insert 60 (e.g., the sealing surface boundary of a lobe side seal insert 60 not compressed by an adjacent lobe 44 A, including the adjacent lobe side seal 60 ) extends beyond the compressed surface boundary 80 of a lobe side seal insert 60 in the interference condition.
- the interference condition occurs when lobe side seal insert 60 is compressed by interference with the adjacent meshing lobe 44 A, including the adjacent lobe side seal insert 60 , e.g., as depicted in FIG. 6B .
- lobe side seal inserts 60 may be constructed to reduce 30° clearance 52 ( FIGS. 3 and 4 ) without contacting the adjacent lobe 44 A in mesh therewith under some or all operating conditions, or may be constructed to reduce 30° clearance 52 by contacting the adjacent lobe 44 A in mesh therewith with little or no interference, e.g., under some or all operating conditions.
- the interference may be generated, for example, by constructing the sealing surface of lobe side seal inserts 60 to protrude beyond the surface of the balance of lobe 44 A by a desired distance 82 .
- each lobe 44 A includes a side recess 84 disposed on each side 56 of the lobe.
- Lobe side seal insert 60 is mounted in side recess 84 .
- Other embodiments may not include a side recess.
- side recess 84 includes a dovetail 86 for mating with a corresponding dovetail 88 on lobe side seal insert 60 for retaining lobe side seal insert 60 on lobe 44 A.
- other geometric configurations and/or fasteners may be employed to retain lobe side seal insert 60 onto lobe 44 A.
- Embodiments of the present invention include a rotary blower, comprising: a housing; a pair of meshed rotors disposed in the housing, each rotor having a plurality of lobes; and each lobe including a lobe tip seal insert mounted thereon and disposed at a tip of the each lobe, each lobe tip seal insert being constructed to seal against the housing and to prevent or reduce leakage between each lobe and the housing.
- each lobe tip seal insert is constructed to engage in sliding contact with the housing during rotation of the rotors.
- the rotary blower further comprises a plurality of pusher weights, each pusher weight being constructed to impart a radially outward load on a corresponding lobe tip seal insert.
- each lobe includes a tip recess formed at the tip of the lobe; wherein the lobe tip seal insert is mounted in the tip recess.
- each lobe tip seal insert on one rotor is constructed to contact and seal against the other rotor at a location between the lobes and at a base of the lobes.
- each lobe further includes a lobe side seal insert mounted thereon and disposed on a side of the each lobe, each lobe side seal insert on each lobe on one rotor being constructed to contact and seal against an adjacent lobe in mesh therewith of the other rotor and to prevent or reduce leakage between adjacent lobes in mesh with each other.
- each lobe side seal insert is constructed to engage in sliding contact with the adjacent lobe during rotation of the rotors.
- each lobe includes a side recess formed at the side of the lobe; and wherein the lobe side seal insert is mounted in the side recess.
- each lobe side seal insert and each lobe tip seal insert is non-metallic.
- Embodiments of the present invention include a rotary blower, comprising: a pair of meshed rotors, each rotor having a plurality of lobes; and each lobe including a lobe side seal insert mounted thereon and disposed on a side of the each lobe, each lobe side seal insert on each lobe on one rotor being constructed to seal against an adjacent lobe in mesh therewith of the other rotor and to prevent or reduce leakage between adjacent lobes in mesh with each other.
- each lobe side seal insert is constructed to engage in sliding contact with the adjacent lobe during rotation of the rotors.
- each lobe includes a side recess formed at the side of the lobe; and wherein the lobe side seal insert is mounted in the side recess.
- the rotary blower further comprises a housing, wherein the pair of meshed rotors is disposed in the housing; and wherein each lobe further includes a lobe tip seal insert mounted thereon and disposed at a tip of the each lobe, each lobe tip seal insert being constructed to contact and seal against the housing and to prevent or reduce leakage between each lobe and the housing.
- each lobe tip seal insert is constructed to engage in sliding contact with the housing during rotation of the rotors.
- each lobe tip seal insert and each lobe side seal insert is non-metallic.
- each lobe includes a tip recess formed at the tip of the lobe; and wherein the lobe tip seal insert is mounted in the tip recess.
- each lobe tip seal insert on one rotor is constructed to contact and seal against the other rotor at a location between the lobes and at a base of the lobes.
- the rotary blower further comprises a plurality of pusher weights, each pusher weight being constructed to impart a radially outward load on a corresponding lobe tip seal insert.
- Embodiments of the present invention include a rotary blower, comprising: a housing; a pair of meshed rotors disposed in the housing, each rotor having a plurality of lobes; and means for contacting and sealing against the housing and to prevent or reduce leakage between each lobe and the housing.
- the rotary blower further comprises means on each lobe for contacting and sealing against an adjacent lobe in mesh therewith and to prevent or reduce leakage between adjacent lobes in mesh with each other.
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Abstract
Description
- The present application generally relates to blowers and more particularly, but not exclusively, to rotary blowers.
- Rotary blowers of various types, e.g., Roots blowers, remain an area of interest. Some existing systems have various shortcomings, drawbacks and disadvantages relative to certain applications. For example, in some rotary blowers, undesirable amounts of leakage between the rotors and/or between the housing and the rotors may occur. Accordingly, there remains a need for further contributions in this area of technology.
- A rotary blower includes a housing and a pair of meshed rotors. The meshed rotors are disposed in the housing. Each rotor has a plurality of lobes. Each lobe includes a lobe tip seal insert mounted thereon. The lobe tip seal insert is disposed at a tip of each lobe. Each lobe tip seal insert is constructed to seal against the housing and to prevent or reduce leakage between each lobe and the housing.
- The description herein makes reference to the accompanying drawings wherein like reference numerals refer to like parts throughout the several views, and wherein:
-
FIG. 1 schematically illustrates a cross-sectional view depicting some aspects of a non-limiting example of a rotary blower in accordance with an embodiment of the present invention. -
FIG. 2 schematically illustrates a cross-sectional view depicting some aspects of a non-limiting example of the rotary blower ofFIG. 1 with the rotors at a first rotational position, which is the rotational position illustrated inFIG. 1 . -
FIG. 3 schematically illustrates a cross-sectional view depicting some aspects of a non-limiting example of the rotary blower ofFIG. 1 , from the perspective ofFIG. 2 but with the rotors at a second rotational position. -
FIG. 4 schematically illustrates a cross-sectional view depicting some aspects of a non-limiting example of the rotary blower ofFIG. 1 , from the perspective ofFIG. 2 but with the rotors at a third rotational position. -
FIG. 5 schematically illustrates a cross-sectional view depicting some aspects of a non-limiting example of a 3-lobed rotary blower in accordance with an embodiment of the present invention. -
FIGS. 6A-6C illustrate cross-sectional views depicting some aspects of non-limiting examples of lobe side seal inserts and a lobe tip seal insert in accordance with an embodiment of the present invention. -
FIG. 7 depicts a cross-section illustrating some aspects of a non-limiting example of a lobe side seal insert in accordance with an embodiment of the present invention. -
FIG. 8 depicts a cross-section illustrating some aspects of a non-limiting example of a lobe tip seal insert in accordance with an embodiment of the present invention. -
FIG. 9 depicts a cross-section illustrating some aspects of a non-limiting example of a pusher weight in accordance with an embodiment of the present invention. - For the purposes of promoting an understanding of the principles of the invention, reference will now be made to the embodiments illustrated in the drawings and specific language will be used to describe the same. It will nevertheless be understood that no limitation of the scope of the invention is thereby intended. Any alterations and further modifications in the described embodiments, and any further applications of the principles of the invention as described herein are contemplated as would normally occur to one skilled in the art to which the invention relates.
- Referring to
FIG. 1 , some aspects of a non-limiting example of arotary blower 10 are illustrated in accordance with an embodiment of the present invention. In one form,rotary blower 10 is a Roots blower. In other embodiments,rotary blower 10 may take other forms. In one form,rotary blower 10 includes a pair of rotors, i.e., adriving rotor 12 in mesh with a drivenrotor 14. In one form, each of drivingrotor 12 and drivenrotor 14 are 2-lobed rotors. In other embodiments, drivingrotor 12 and drivenrotor 14 may be 3-lobed rotors, 4-lobed rotors, or rotors having any number of lobes.Driving rotor 12 and drivenrotor 14 are supported by 16, 18 and 20, 22.respective shafts 16, 18, 20 and 22 may be integral withShafts 12, 14, or may be separate components affixed or mounted onto or intorotors 12, 14.rotors 16, 18, 20 and 22 are supported byShafts 24, 26, 28 and 30.respective bearings - Driving
rotor 12 and drivenrotor 14 are disposed radially within ahousing 32, which cooperates with drivingrotor 12 and drivenrotor 14 to pump or compress a fluid, such as air.Driving rotor 12 and drivenrotor 14 are disposed axially between 34 and 36.head plates Housing 32 is coupled, e.g., bolted, to 34 and 36.head plates 24, 26, 28 and 30 are mounted in and supported byBearings 34 and 36.head plates 24, 26, 28 and 30 transmit radial and thrust loads fromBearings 12 and 14 torotors 34 and 36. In one form,head plates 24, 26, 28 and 30 are rolling element bearings. For example, in the depicted embodiment ofbearings FIG. 1 , 26 and 30 are ball thrust bearings, whereasbearings 24 and 28 are roller bearings. In other embodiments, one or more ofbearings 24, 26, 28 and 30 may be one or more other types of bearings.bearings -
Driving rotor 12 is supplied with shaft power via a shaft power source, such as an electric motor (not shown).Driving rotor 12 is operative to supply mechanical power to drivenrotor 14 via 38 and 40.gears 38 and 40 are mounted onGears respective shafts 16 and 20 of respective driving and driven 12 and 14, and are in mesh with each other.rotors 38 and 40 are operative to maintain a desired angular relationship between drivingGears rotor 12 and drivenrotor 14, and to transmit rotational motion and power from drivingrotor 12 to drivenrotor 14. In various embodiments, a plurality of seals (not shown) may be employed to prevent the leakage of oil and/or compressed gas/fluids into undesired portions ofrotary blower 10. End plate covers (not shown) may be employed to cover the 24, 26, 28, 30 andbearings 38, 40.gears - Referring to
FIGS. 2-4 , in conjunction withFIG. 1 , during operation ofrotary blower 10, an inlet gas stream to be pumped or compressed entersrotary blower 10 through aninlet 42, and the inlet gas is trapped in chambers formed betweenlobes 44 and the blower body orhousing 32, and is forced out ofrotary blower 10 at anoutlet 46. In conventional rotary blowers, three types of clearances are typically used in order to allow rotation of the rotors relative to the housing and relative to each other. Examples of such clearances that occur in conventional blowers are illustrated inFIGS. 2-4 , which are exaggerated for purposes of illustration. In the depictions ofFIG. 1-4 , some aspects of the present invention, such as the 58, 60 illustrated in and described with respect tolobe seal inserts FIG. 5-9 are not shown in order to illustrate the clearances. One such clearance islateral clearance 48, which is the clearance between therotors 12, 14 (including lobes 44) and the head plates, e.g., such as 34 and 36. Another such clearance is diameter orhead plates diametral clearance 50, which is the radial clearance between the rotor lobes and the housing, e.g.,housing 32. A third such clearance is the clearance between rotors, or between lobes, e.g., parallel lobes, such as 30°clearance 52. These clearances are typically calculated in consideration of thermal effects, such as dilation or thermal expansion. In conventional rotary blowers, the blower may crash or seize or otherwise be damaged if the clearances are too small. The size of the clearances or amount of clearance impacts blower efficiency. For example, efficiency decreases with increasing clearance, e.g., due to leakage through the clearances. Embodiments of the present invention reduce or eliminate the diameter clearance and the clearance between rotors (lobes), e.g., the 30° clearance, via the use of lobe seal inserts (not shown inFIG. 1-4 ). - Referring to
FIGS. 5-9 , some aspects of a non-limiting example of a 3-lobed rotary blower 10A in accordance with an embodiment of the present invention is illustrated.Rotary blower 10A includes meshed drivingrotor 12A and drivenrotor 14A. Each of drivingrotor 12A and drivenrotor 14A have threelobes 44A. Eachlobe 44A has atip 54 and twosides 56. Eachlobe 44A includes a lobetip seal insert 58 mounted thereon. Some aspects of a non-limiting example of lobetip seal insert 58 are illustrated inFIG. 5 ,FIG. 6A andFIG. 8 . Eachlobe 44A also includes two lobe side seal inserts 60 mounted thereon, one lobeside seal insert 60 on eachside 56. Some aspects of a non-limiting example of lobeside seal insert 60 are illustrated inFIG. 5 ,FIG. 6B ,FIG. 6C andFIG. 7 . In other embodiments, a greater amount of lobe tip seal inserts 58 and lobe side seal inserts 60 may be employed. Some embodiments may include only lobe tip seal insert(s) 58 or only lobe side seal insert(s) 60. In one form, lobe tip seal inserts 58 and lobe side seal inserts 60 are flexible and compliant. In other embodiments, portions of lobe tip seal inserts 58 and lobe side seal inserts 60 may be rigid. - In one form, the material used to form lobe tip seal inserts 58 and lobe side seal inserts 60 is different than the material used to form the balance of
12A and 14A. For example, the material used to form lobe tip seal inserts 58 and lobe side seal inserts 60 may be non-metallic, whereas the material used to form the balance ofrotors 12A and 14A may be metallic in some embodiments. For instance, in some embodiments, lobe tip seal inserts 58 and lobe side seal inserts 60 may be formed from, for example, a polymeric or composite or other non-metallic material. In some embodiments, preferable materials used to make lobe tip seal inserts 58 and lobe side seal inserts 60 are capable of continuous use at temperatures up to 180° C.; supports sliding speeds up to 40 m/s, and have a relatively low coefficient of friction. The materials used to make lobe tip seal inserts 58 and lobe side seal inserts 60, and the corresponding coefficients of friction, may vary with the needs of the particular application.rotors - Each lobe
tip seal insert 58 is disposed attip 54 of eachlobe 44A. In one form, each lobetip seal insert 58 is constructed and operative to seal againsthousing 32 and to prevent or reduce leakage between eachlobe 44A andhousing 32. In some embodiments, each lobetip seal insert 58 is also constructed and operative to seal against portions of the opposite rotor, e.g., at a location 12A1, 14A1 between thelobes 44A, and also at the base or bottom or radially inward portion 44A1 of thelobes 44A, to prevent or reduce leakage between eachlobe 44A of one rotor and location 12A1, 14A1 of the other rotor, and between eachlobe 44A of one rotor and the base portions 44A1 oflobes 44A on the other rotor. In some embodiments, each lobetip seal insert 58 is constructed to contacthousing 32 during the operation ofblower 10. In some embodiments, each lobetip seal insert 58 is constructed to engage in sliding contact withhousing 32 during rotation of the rotors, i.e., during operation ofrotary blower 10. - In a particular embodiment, each lobe
tip seal insert 58 is constructed to have an interference fit 64 withhousing 32, e.g., as illustrated inFIG. 6A , wherein afree surface boundary 66 of a free lobe tip seal insert 58 (e.g., the sealing surface boundary of a lobetip seal insert 58 not compressed byhousing 32 or an adjacent rotor) extends beyond the compressed surface boundary 68 of a lobetip seal insert 58 in the interference condition. The interference condition occurs whenlobe tip seal 58 on onelobe 44A is compressed by interference withhousing 32 or with an adjacent rotor at a location 12A1, 14A1 between lobes or at the base or bottom portion 44A1 of themeshing lobe 44A. The compressed boundary 68 is the boundary of the installed lobetip seal insert 58 after being compressed due to the interference fit withhousing 32 or with an adjacent rotor, e.g., as depicted inFIG. 6A , which illustrates the interference withhousing 32. In other embodiments, lobe tip seal inserts 58 may be constructed to reduce diameter clearance 50 (FIG. 2 ) without contactinghousing 32 under some or all operating conditions, or may be constructed to reducediameter clearance 50 by contactinghousing 32 with little or no interference, e.g., under some or all operating conditions. - In one form, each
lobe 44A includes apusher weight 62, e.g., a rod. In the depiction ofFIG. 5 andFIG. 9 ,pusher weight 62 is a rod having a circular cross section. In other embodiments,pusher weight 62 may have any suitable geometric configuration. Eachpusher weight 62 is constructed and operative to impart a radially outward, centrifugal load on a corresponding lobetip seal insert 58, e.g., to aid in loading lobetip seal insert 58 in a direction towardhousing 32 and toward the lobe and rotor that thelobe 44A is meshing with. The radially outward loading may, for example, aid in maintaining desired contact loading between lobetip seal insert 58 andhousing 32, and between the lobetip seal insert 58 and the lobe and rotor it is meshing with. Other embodiments may not employ a pusher weight. - In one form, each
lobe 44A includes atip recess 70 disposed at thetip 54 of the lobe. Lobetip seal insert 58 is mounted intip recess 70. Other embodiments may not include a tip recess. In one form,tip recess 70 includes adovetail 72 for mating with a correspondingdovetail 74 on lobetip seal insert 58 for retaining lobetip seal insert 58 onlobe 44A. In other embodiments, other geometric configurations and/or fasteners may be employed to retain lobetip seal insert 58 ontolobe 44A. - Each lobe
side seal insert 60 is disposed atside 56 of the eachlobe 44A. In one form, each lobeside seal insert 60 of one rotor is constructed to seal against anadjacent lobe 44A in mesh therewith of the other rotor, including against an adjacent lobeside seal insert 60. Each lobeside seal insert 60 is constructed and operative to prevent or reduce leakage betweenadjacent lobes 44A in mesh with each other, e.g., while the lobes are meshing. In some embodiments, each lobeside seal insert 60 is constructed to contact and seal against the adjacent lobe in mesh therewith (including contacting and sealing against the lobeside seal insert 60 on the adjacent lobe) during operation ofblower 10. In some embodiments, each lobeside seal insert 60 is constructed to engage in sliding contact with theadjacent lobe 44A in mesh therewith (including sliding contact with an adjacent lobe side seal insert 60) during rotation of the rotors, i.e., during operation ofrotary blower 10. - In a particular embodiment, each lobe
side seal insert 60 is constructed to have an interference fit 76 with theadjacent meshing lobe 44A, e.g., as illustrated inFIG. 6B , wherein a free surface boundary 78 of a free lobe side seal insert 60 (e.g., the sealing surface boundary of a lobeside seal insert 60 not compressed by anadjacent lobe 44A, including the adjacent lobe side seal 60) extends beyond thecompressed surface boundary 80 of a lobeside seal insert 60 in the interference condition. The interference condition occurs when lobeside seal insert 60 is compressed by interference with theadjacent meshing lobe 44A, including the adjacent lobeside seal insert 60, e.g., as depicted inFIG. 6B . In other embodiments, lobe side seal inserts 60 may be constructed to reduce 30° clearance 52 (FIGS. 3 and 4 ) without contacting theadjacent lobe 44A in mesh therewith under some or all operating conditions, or may be constructed to reduce 30°clearance 52 by contacting theadjacent lobe 44A in mesh therewith with little or no interference, e.g., under some or all operating conditions. The interference may be generated, for example, by constructing the sealing surface of lobe side seal inserts 60 to protrude beyond the surface of the balance oflobe 44A by a desireddistance 82. - In one form, each
lobe 44A includes aside recess 84 disposed on eachside 56 of the lobe. Lobeside seal insert 60 is mounted inside recess 84. Other embodiments may not include a side recess. In one form,side recess 84 includes adovetail 86 for mating with a correspondingdovetail 88 on lobeside seal insert 60 for retaining lobeside seal insert 60 onlobe 44A. In other embodiments, other geometric configurations and/or fasteners may be employed to retain lobeside seal insert 60 ontolobe 44A. - Embodiments of the present invention include a rotary blower, comprising: a housing; a pair of meshed rotors disposed in the housing, each rotor having a plurality of lobes; and each lobe including a lobe tip seal insert mounted thereon and disposed at a tip of the each lobe, each lobe tip seal insert being constructed to seal against the housing and to prevent or reduce leakage between each lobe and the housing.
- In a refinement, each lobe tip seal insert is constructed to engage in sliding contact with the housing during rotation of the rotors.
- In another refinement, the rotary blower further comprises a plurality of pusher weights, each pusher weight being constructed to impart a radially outward load on a corresponding lobe tip seal insert.
- In yet another refinement, each lobe includes a tip recess formed at the tip of the lobe; wherein the lobe tip seal insert is mounted in the tip recess.
- In still another refinement, each lobe tip seal insert on one rotor is constructed to contact and seal against the other rotor at a location between the lobes and at a base of the lobes.
- In yet still another refinement, each lobe further includes a lobe side seal insert mounted thereon and disposed on a side of the each lobe, each lobe side seal insert on each lobe on one rotor being constructed to contact and seal against an adjacent lobe in mesh therewith of the other rotor and to prevent or reduce leakage between adjacent lobes in mesh with each other.
- In a further refinement, each lobe side seal insert is constructed to engage in sliding contact with the adjacent lobe during rotation of the rotors.
- In a yet further refinement, each lobe includes a side recess formed at the side of the lobe; and wherein the lobe side seal insert is mounted in the side recess.
- In a still further refinement, each lobe side seal insert and each lobe tip seal insert is non-metallic.
- Embodiments of the present invention include a rotary blower, comprising: a pair of meshed rotors, each rotor having a plurality of lobes; and each lobe including a lobe side seal insert mounted thereon and disposed on a side of the each lobe, each lobe side seal insert on each lobe on one rotor being constructed to seal against an adjacent lobe in mesh therewith of the other rotor and to prevent or reduce leakage between adjacent lobes in mesh with each other.
- In a refinement, each lobe side seal insert is constructed to engage in sliding contact with the adjacent lobe during rotation of the rotors.
- In another refinement, each lobe includes a side recess formed at the side of the lobe; and wherein the lobe side seal insert is mounted in the side recess.
- In yet another refinement, the rotary blower further comprises a housing, wherein the pair of meshed rotors is disposed in the housing; and wherein each lobe further includes a lobe tip seal insert mounted thereon and disposed at a tip of the each lobe, each lobe tip seal insert being constructed to contact and seal against the housing and to prevent or reduce leakage between each lobe and the housing.
- In still another refinement, each lobe tip seal insert is constructed to engage in sliding contact with the housing during rotation of the rotors.
- In yet still another refinement, each lobe tip seal insert and each lobe side seal insert is non-metallic.
- In a further refinement, each lobe includes a tip recess formed at the tip of the lobe; and wherein the lobe tip seal insert is mounted in the tip recess.
- In a yet further refinement, each lobe tip seal insert on one rotor is constructed to contact and seal against the other rotor at a location between the lobes and at a base of the lobes.
- In a still further refinement, the rotary blower further comprises a plurality of pusher weights, each pusher weight being constructed to impart a radially outward load on a corresponding lobe tip seal insert.
- Embodiments of the present invention include a rotary blower, comprising: a housing; a pair of meshed rotors disposed in the housing, each rotor having a plurality of lobes; and means for contacting and sealing against the housing and to prevent or reduce leakage between each lobe and the housing.
- In a refinement, the rotary blower further comprises means on each lobe for contacting and sealing against an adjacent lobe in mesh therewith and to prevent or reduce leakage between adjacent lobes in mesh with each other.
- While the invention has been illustrated and described in detail in the drawings and foregoing description, the same is to be considered as illustrative and not restrictive in character, it being understood that only the preferred embodiments have been shown and described and that all changes and modifications that come within the spirit of the inventions are desired to be protected. It should be understood that while the use of words such as preferable, preferably, preferred or more preferred utilized in the description above indicate that the feature so described may be more desirable, it nonetheless may not be necessary and embodiments lacking the same may be contemplated as within the scope of the invention, the scope being defined by the claims that follow. In reading the claims, it is intended that when words such as “a,” “an,” “at least one,” or “at least one portion” are used there is no intention to limit the claim to only one item unless specifically stated to the contrary in the claim. When the language “at least a portion” and/or “a portion” is used the item can include a portion and/or the entire item unless specifically stated to the contrary.
- Unless specified or limited otherwise, the terms “mounted,” “connected,” “supported,” and “coupled” and variations thereof are used broadly and encompass both direct and indirect mountings, connections, supports, and couplings. Further, “connected” and “coupled” are not restricted to physical or mechanical connections or couplings.
Claims (20)
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US15/852,570 US20190195225A1 (en) | 2017-12-22 | 2017-12-22 | Rotary blower |
| EP18215096.1A EP3502477A1 (en) | 2017-12-22 | 2018-12-21 | Rotary blower |
| CN201811569396.6A CN110017278A (en) | 2017-12-22 | 2018-12-21 | Rotary blower |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US15/852,570 US20190195225A1 (en) | 2017-12-22 | 2017-12-22 | Rotary blower |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20190195225A1 true US20190195225A1 (en) | 2019-06-27 |
Family
ID=64899222
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US15/852,570 Abandoned US20190195225A1 (en) | 2017-12-22 | 2017-12-22 | Rotary blower |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US20190195225A1 (en) |
| EP (1) | EP3502477A1 (en) |
| CN (1) | CN110017278A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1023360A (en) * | 1911-02-06 | 1912-04-16 | August Brauer | Rotary engine. |
| US2270222A (en) * | 1941-06-23 | 1942-01-13 | Rea | Fluid brake |
| US2380752A (en) * | 1941-08-15 | 1945-07-31 | Grieb Benjamin Curtis | Rotary engine or blower device |
| US3444843A (en) * | 1966-11-22 | 1969-05-20 | Huschang Sabet | Rotary sealing element having centrifugal force compensation |
| US20130216417A1 (en) * | 2012-02-10 | 2013-08-22 | Randy Dixon | Rotary lobe pump with wiper blades |
| US20150285248A1 (en) * | 2012-02-10 | 2015-10-08 | Randy Dixon | Rotary lobe pump with wiper blades |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2063600A5 (en) * | 1969-10-23 | 1971-07-09 | Saviem | |
| US5335640A (en) * | 1992-06-19 | 1994-08-09 | Feuling Engineering, Inc. | Rotor to casing seals for roots type superchargers |
| WO2016209868A1 (en) * | 2015-06-22 | 2016-12-29 | Dixon Pumps | Rotary lobe pump with wiper blades |
-
2017
- 2017-12-22 US US15/852,570 patent/US20190195225A1/en not_active Abandoned
-
2018
- 2018-12-21 EP EP18215096.1A patent/EP3502477A1/en not_active Withdrawn
- 2018-12-21 CN CN201811569396.6A patent/CN110017278A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1023360A (en) * | 1911-02-06 | 1912-04-16 | August Brauer | Rotary engine. |
| US2270222A (en) * | 1941-06-23 | 1942-01-13 | Rea | Fluid brake |
| US2380752A (en) * | 1941-08-15 | 1945-07-31 | Grieb Benjamin Curtis | Rotary engine or blower device |
| US3444843A (en) * | 1966-11-22 | 1969-05-20 | Huschang Sabet | Rotary sealing element having centrifugal force compensation |
| US20130216417A1 (en) * | 2012-02-10 | 2013-08-22 | Randy Dixon | Rotary lobe pump with wiper blades |
| US20150285248A1 (en) * | 2012-02-10 | 2015-10-08 | Randy Dixon | Rotary lobe pump with wiper blades |
Also Published As
| Publication number | Publication date |
|---|---|
| EP3502477A1 (en) | 2019-06-26 |
| CN110017278A (en) | 2019-07-16 |
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