referring now to the drawings , there is shown a vacuum powered device 10 in the form of a combined rotary brush and vacuum nozzle cleaning tool . the major parts of the illustrated tool 10 comprise a housing 11 and a center assembly 12 received within the housing . the center assembly 12 , in turn , has as its principle parts a rotary disc brush 13 , a stator 14 and a turbine wheel 15 . the housing 11 is preferably formed of injection molded plastic components . a main body part 16 of the housing 11 is a hollow member having a generally cup shaped portion 17 and inclined tubular handle portion 18 . as illustrated most clearly in fig5 the interior space of the cup and handle portions 17 , 18 communicate directly where the handle portion generally merges with an inclined end wall 19 of the cup portion and a generally cylindrical sidewall 20 of the cup - shaped portion . a brush ring unit 25 forms a forward part of the housing 11 . the brush ring unit 25 is releasably retained in position against a forward face 26 of the main housing body cup portion 17 by a hook 27 integral with the ring 25 and a diametrically opposed pin 28 which snaps into a spring steel clothespin - type catch 29 anchored in a hollow projection 30 of the main housing body 16 . the brush ring 25 is released from the main housing body 16 by depressing a release button 31 carried in the projection 30 . the release button 31 includes an operating pin 32 which is adapted to press the opposed ring pin 28 out of the spring catch 29 . brush tufts 33 each formed of a plurality of bristles 34 are pressed into associated holes , in a known manner , across a forward face 35 of the ring 25 and an integral projection 36 . radially inward of the brush tufts 33 , the ring 25 is formed with an annular bellmouthed surface 37 which forms an inlet for air to be drawn through the housing 11 . the ring 25 , preferably , is injection molded of polypropylene or other known plastic material suitable for receiving the brush tufts 33 under pressure without significant distortion or damage . as indicated in fig5 the bellmouthed surface 37 merges smoothly with an annular interior surface 38 formed by the main housing body cup portion 17 . this annular interior housing surface 38 , along the axial zone subtended by the center assembly 12 , has the general configuration of a shallow cone and but for a draft angle , is nearly cylindrical . the tubular handle portion 18 of the main housing body 16 preferably has a series of gently formed exterior ribs 46 on its forward side to provide a comfortable finger grip zone . the handle portion 18 is grasped in the hand of the user to permit the tool 10 to be conveniently hand - carried and manipulated . the interior , designated 47 of the tubular handle portion 18 , ideally , is in the form of a shallow cone or taper to provide a friction lock fit with a mating tubular end fitting of a flexible vacuum hose , as is customary in the domestic vacuum cleaner industry . an oil impregnated bronze bushing 51 , having a cup shape with a blind end 52 is press fitted or otherwise retained in the hollow of a boss 53 formed on the housing end wall 19 . the bushing or bearing 51 has a central blind bore 54 aligned with the axis of the interior conical or annular housing surface 38 . the turbine wheel 15 includes a hemi - spheroidal shell or cup portion 60 such that it forms a hollow space 61 . on a sidewall area 62 of the hemi - spheroidal part 60 of the turbine wheel 15 , there are intergrally formed a plurality of peripherally spaced turbine blades 63 . the turbine blades 63 have a configuration which takes advantage of the principles of the pelton wheel . the blades 63 ( fig4 ) can each be described generally as a curved plane of changing radius having its imaginary axii extending radially of the turbine wheel axis i . e . the axis of revolution of the hemi - spheroidal portion 60 . in the illustrated case , the turbine blades 63 extend radially from the wheel sidewall 62 almost to the interior housing surface 38 , but for a limited amount of radial clearance as indicated at 64 . aligned with the axis of the turbine wheel 15 is a hub portion 65 integrally formed with an end wall 66 of the hemi - spheroidal portion 60 . the hub portion 65 has a central cylindrical bore 67 . the bore 67 is stepped with a generally radial shoulder 68 . the turbine wheel 15 is preferably injection molded of abs or other suitable rigid plastic . a cylindrical steel shaft 71 is permanently assembled to the turbine wheel 15 by press fitting it into the bore 67 . ribs 72 formed as upsets on the shaft 71 , or otherwise , rotationally lock the shaft and wheel 15 together . a rearward end 73 of the shaft 71 protrudes from the hub portion 65 and includes a spherical area 74 . the spherical shaft end area 74 is received in the bushing bore 54 so that the bushing 51 serves as a radial and end thrust bearing for the shaft end 73 . the spherical shaft end 74 permits the shaft 71 to be self - aligning to the bushing 51 . at its opposite end , the shaft 71 has an elongated flat 75 . assembled in succession on the shaft 71 are a thrust washer 76 , a bushing 77 carried in the stator 14 , a felt washer 78 , a spring cup shield 79 , a spring 81 , an insert 82 in the disc brush 13 and a retaining washer 83 . the thrust washer 76 is formed of acetal or other low friction , low noise material and eliminates wear between the wheel hub portion 65 and bushing 77 . the stator 14 in its illustrated form includes a shallow cup or pan - shaped body having a generally cylindrical sidewall 84 and a generally radial end wall 85 . the sidewall 84 and end wall 85 bound a hollow space 86 . the end wall 85 is stepped axially at 87 to form a recess for reception of the felt washer 78 . integrally formed with the end wall 85 is a hub 88 which is coaxial with the sidewall 84 . the bronze bushing or bearing 77 is press fitted in a central cylindrical bore 89 of the stator hub 88 . the bearing 77 is of the oil impregnated type . integrally formed on the periphery of the stator sidewall 84 are a plurality of spaced stator blades 90 . each blade 90 ( fig4 ) lies in a generally flat plane that is both radial and inclined with respect to the axis of the center assembly 12 , i . e . the axis of the shaft 71 . the blades 90 are effective to direct air passing through the housing 11 towards the turbine wheel blades 63 at an angle which , in conjunction with the configuration of such turbine wheel blades , increases torque at relatively low rotational speeds . as indicated , the stator blades 90 extend radially from the stator sidewall 84 to the housing surface 38 with minimal clearance . the stator 14 is locked in position against rotation in the housing 11 by spider legs 91 which in the illustrated case are four in number and are at 90 ° intervals on the periphery of the stator . the spider legs 91 are received with a friction fit in associated cavities 92 formed in the main housing body forward face 26 . the spiders 91 are locked in their respective cavities 92 or released therefrom by installation or removal of the brush ring unit 25 . in its installed position , the brush ring unit 25 bears against the forwardmost surfaces of the spiders 91 to retain them in the cavities 92 . removal of the brush ring unit 25 from the main housing body 16 releases the spider legs 91 and permits the center assembly 12 to be removed from the housing for inspection and / or cleaning . it will be understood that with the stator 14 locked in position in the main housing body 16 by virtue of the spider legs 91 being received in the associated cavitites 92 , the stator bearing or bushing 77 is spatially fixed in relation to the housing 11 . the bearing 77 thus cooperates with the cup bushing 51 to rigidly support the shaft 71 in the housing 11 . endwise motion of the shaft 71 is limited by the cup bushing 51 and a shoulder or flange portion 93 of a bushing 77 which operates through the thrust washer 76 to restrict axial motion of the turbine wheel hub portion 65 to which the shaft is fixed as aforementioned . the spring cup shield 79 has a generally cylindrical sidewall 98 and a circular end wall 97 . the free end of the sidewall 98 is notched at three uniformly spaced angular zones 99 which provide clearance for three corresponding ribs 101 formed on a rear face 102 of an end wall 103 of the rotary disc brush 13 . the cup shield end wall 97 has a central aperture 104 of d - shape which rotationally interlocks with the flat 75 of the shaft 71 . rearward thrust loads on the spring shield 79 are transmitted to the shaft 71 by virtue of abutment of radial faces 106 , 107 of the cup shield and shaft respectively . the spring cup shield 79 reduces the risk of threads , string and like filaments from being wrapped around the shaft 71 and the spring 81 . alternative constructions for the shield 79 include cages or spider legs as substitutes for the notched sidewall 98 . the end wall 103 and an annular sidewall 108 of the rotary disc brush 13 form a hollow space 109 . an exterior surface 130 of the brush sidewall 108 varies in radial spacing from the rotational axis of the brush 13 . as shown , this surface 130 is a composite of a plurality of reverse cylindrical segments 129 , angularly spaced about the outer periphery of the sidewall 108 . the end view of the rear face of the disc brush 13 illustrated in fig6 shows these cylindrical surface segments 129 as scallops . in the illustrated case , the rotary disc brush 13 has a set of three rows 114 of brush tufts 115 which are formed of individual bristles that are pressed into corresponding holes 116 . like the brush ring 25 , the disc brush 13 is preferably injection molded of polypropylene or other suitable plastic which accepts the force fitting of the brush tufts 115 without significant distortion or detrimental effects to the appearance of this part . the brush tuft 114 rows on a forward face 117 of the disc brush 13 are arranged in an offset y pattern . the ribs 101 have a corresponding offset y pattern on the rear face 102 of the disc brush end wall 103 to provide stock surrounding the holes 116 for the tufts 115 . integrally formed at the center of the disc brush end wall 103 is a hollow hub 121 in which is locked an insert 82 of low friction material such as acetal . the insert 82 has a d - shaped bore 123 which rotationally interlocks on the shaft flat area 75 but which permits axial movement of the disc brush 13 along the shaft 71 . the disc brush 13 is axially retained on the shaft 71 by the retaining washer 83 . from the foregoing , it will be understood that the disc brush 13 is rotationally interlocked to the turbine wheel 15 by the shaft 71 . the rotary disc brush 13 is resiliently biased away from the stator 14 and turbine wheel 15 by the spring 81 . the spring 81 is a helical compression spring sized to normally maintain the disc brush 13 in the solid line position illustrated in fig5 where the disc brush tufts 115 extend forwardly of the brush ring tufts 33 . an exterior surface 130 of the disc brush sidewall 108 is in telescoping relation with an interior generally cylindrical surface 131 of the stator sidewall 84 . air inlet holes 132 extend through the disc brush end wall 103 . in the illustrated example , the holes are three in number , each being associated with one of the rows 114 of brush tufts 115 . as viewed in fig2 the rotary brush 13 turns counterclockwise and , as shown , the air inlet holes 132 lead their respective tuft rows 114 . in operation , the tubular handle 18 is connected to a source of vacuum such a domestic vacuum cleaner by means of conventional flexible hose having its end fitting inserted into the interior 47 . suction applied to the housing handle interior 47 causes air to be drawn through the housing 11 . the bellmouthed surface 37 of the brush ring 25 serves as the inlet for air flow through the housing 11 and the handle interior 47 serves as the outlet . between these inlet and outlet points , the interior housing surface 38 forms the main outer peripheral boundary for such air flow . air rushes through the annular space between this peripheral housing surface 38 and the center assembly 12 . the stator blades 90 channel this air flow in a helical - like direction as it passes through the axial zone of these blades . this orientation of air flow improves the efficiency of the turbine wheel 15 in developing a high torque at relatively low speed . after the air flow transfers its momentum by the pelton wheel effect to the turbine wheel 15 , it exhausts through an opening 141 into the handle 18 from the main housing body 16 . as air impinges on the turbine wheel blades 63 , the turbine wheel 15 is caused to rotate . rotary motion of the turbine wheel 15 is imparted to the disc brush 13 permitting the latter to be used to sweep over a surface to be cleaned . at the same time , air rushing into the inlet 37 causes dirt and debris which is swept up by the bristle tufts 33 , 115 or which is relatively loose to be collected at the vacuum source . an air flow circuit for purging the hollow cavity 109 of the disc brush 13 and the hollow cavity 86 of the stator 14 is provided , in part by the air inlet holes 132 in the disc brush end wall 103 . air indicated by the arrows 151 flows into these inlet holes 132 and circulates through the respective cavities of the disc brush 13 and stator 14 and is drawn out of this hollow or cavity area through a peripheral gap 152 between the disc brush sidewall 108 and stator sidewall 84 . it will be understood that the major outside diameter of the scalloped disc brush sidewall 108 is somewhat less than the minor inside diameter of the stator sidewall 84 , for purposes of maintaining rotating clearance and for maintaining this purge air flow . during rotation of the disc brush 13 , the scallops or irregular surface segments 129 of the outer periphery 130 of the sidewall 108 produce turbulence in the adjacent air , which develops a slight relative increase in air pressure at this point to prevent back flow of ambient air through the gap 152 into the disc brush and stator cavities . it has been found that a positive flow of ambient air through these cavity areas , entering the holes 132 and exiting through the peripheral gap 152 is effective in sweeping these cavity areas free of accumulations of dirt and debris which otherwise occur when such holes 132 and related flow circuit is not provided . as mentioned , the holes 132 each associated with a tuft row 114 leads such row during rotation , and it has been found that this relation develops the most effective positive air flow current through the disc brush and stator cavities . the disc brush 13 is capable of floating axially with respect to the housing brush ring 25 so as to limit and otherwise control the brushing force which can be developed by the tool 10 . at high brush force levels , the axial resistance of the resilient spring 81 is overcome and the disc brush 13 retracts towards the interior of the housing 11 . in this mode , the disc brush insert 122 slides along the shaft 71 . the retracted position of the disc brush 13 is indicated at 161 by phantom lines representing the rearward edge of the disc brush sidewall 108 . although the preferred embodiment of this invention has been shown and described , it should be understood that various modifications and rearrangements of the parts may be resorted to without departing from the scope of the invention as disclosed and claimed herein .
a rotary brush vacuum sweeper having a directly coupled disc brush and turbine wheel . the disc brush floats axially within the sweeper housing to control brush force and is in telescopic relation with rearward motor components to promote favorable air flow characteristics . hollow space between the disc brush and turbine wheel is continuously purged of dirt and debris by ambient air passing through an associated internal circuit .