SELF REGULATING FLUID BEARING HIGH PRESSURE ROTARY RETARDER NOZZLE

Abstract

A rotary nozzle having a rotating shaft operating within a cylindrical housing is balanced by allowing passage of a small amount of pressurized fluid to be bled to an area between the outside of the opposite end of the shaft and the inside of the housing where the fluid force acts axially in an opposing direction upon the shaft to balance the axial inlet force exerted by the pressurized fluid. The balance of axial forces is self-regulating by controlling escape of the fluid through a tapered or frusto-conical region between the shaft and housing. A plurality of centrifugal weight segments around the inlet end of the shaft are thrust outwardly against the cylindrical housing to retard rotational speed while pressurized fluid around the centrifugal weight segments provides a fluid bearing between the weights and the housing.

Claims

1. A nozzle assembly for spraying high pressure fluid against an object, the nozzle assembly comprising: a cylindrical housing body; a tubular shaft member coaxially and rotatably carried within the cylindrical housing body and having an inlet end within and near one end of the cylindrical housing body, the tubular shaft member having an outlet end near a second end of the cylindrical housing body for securing a spray head thereto for rotation with the tubular shaft member, the tubular shaft member having a central passage to conduct fluid from the inlet end of the tubular shaft member to the outlet end of the tubular shaft member, the tubular shaft member having a regulating passage formed between the cylindrical housing body and an outer surface of the tubular shaft member; one or more bores communicating between the central passage of the tubular shaft member and the regulating passage, wherein pressure of the fluid within the regulating passage acts axially upon the tubular shaft member to counterbalance axial force on the tubular shaft member exerted by fluid pressure acting upon the inlet end of the tubular shaft member; and a plurality of partial annular segments disposed on the tubular shaft member in the cylindrical housing body and captured between the inlet end of the tubular shaft member and the cylindrical housing body and constrained to rotate with the tubular shaft member and constrained to ride on a rail extending across the central passage through the tubular shaft member near the inlet end of the tubular shaft member, wherein the plurality of partial annular segments are free to separate outwardly from the tubular shaft member on the rail and press against the cylindrical housing body thereby reducing rotational speed of the tubular shaft member within the cylindrical housing body during nozzle operation.

2. The nozzle assembly according to claim 1 wherein the regulating passage is a tapered frusto-conical gap defined between the tubular shaft member and the cylindrical housing body.

3. The nozzle assembly according to claim 1 wherein each of the plurality of partial annular segments is a half annular segment disposed on the tubular shaft member between the regulating passage and an inlet bearing area of the cylindrical housing body.

4. The nozzle assembly according to claim 3 wherein each half annular segment rides on the rail formed on the tubular shaft member extending across the central passage between the inlet end of the tubular shaft member and a tapered surface portion of the tubular shaft member.

5. The nozzle assembly according to claim 1 wherein the rail is formed between the inlet end of the tubular shaft member and a tapered surface portion of the tubular shaft member, wherein the rail extends laterally across the central passage through the tubular shaft member.

6. The nozzle assembly according to claim 1 wherein each of the plurality of partial annular segments has one or more peripheral grooves in its external surface.

7. The nozzle assembly according to claim 1 wherein each of the plurality of partial annular segments has one or more angled axial channels in its external surface.

8. The nozzle assembly according to claim 1 wherein each of the plurality of partial annular segments has a partial internal recess facing the tubular shaft member.

9. A nozzle assembly for spraying high pressure fluid against an object, the nozzle assembly comprising: a cylindrical housing body; a tubular shaft member coaxially and rotatably carried within the cylindrical housing body and having an inlet end within and near one end of the cylindrical housing body, the tubular shaft member having an outlet end near a second end of the cylindrical housing body for securing a spray head thereto for rotation with the tubular shaft member, the tubular shaft member having a central passage to conduct fluid from the inlet end of the tubular shaft member to the outlet end of the tubular shaft member; a regulating passage formed between the cylindrical housing body and an outer surface of the tubular shaft member; one or more bores communicating between the central passage through the tubular shaft member and the regulating passage, wherein pressure of the fluid within the regulating passage acts axially upon the tubular shaft member to counterbalance axial force on the tubular shaft member exerted by fluid pressure acting upon the inlet end of the tubular shaft member, the tubular shaft member having formed thereon a transverse rail extending across the central passage through the tubular shaft member; and a plurality of partial annular segments slidably disposed on the transverse rail formed on the tubular shaft member in the cylindrical housing body, wherein the plurality of partial annular segments are free to separate outwardly from the tubular shaft member along the transverse rail and press against the cylindrical housing body thereby reducing rotational speed of the tubular shaft member within the cylindrical housing body during nozzle operation.

10. The nozzle assembly according to claim 9 wherein the transverse rail includes a feature preventing axial movement of the plurality of partial annular segments.

11. The nozzle assembly according to claim 9 wherein each of the plurality of partial annular segments is a half annular segment disposed on the transverse rail formed on the tubular shaft member and positioned between the regulating passage and an inlet bearing area of the cylindrical housing body.

12. The nozzle assembly according to claim 9 wherein each of the plurality of partial annular segments has one or more peripheral grooves in its external surface.

13. The nozzle assembly according to claim 9 wherein each of the plurality of partial annular segments has one or more angled axial channels in its external surface.

14. The nozzle assembly according to claim 9 wherein the transverse rail has a constant cross sectional shape and carries the plurality of partial annular segments.

15. The nozzle assembly according to claim 14 wherein each of the plurality of partial annular segments has a shape complementary to a cross sectional shape of the transverse rail.

16. The nozzle assembly according to claim 14 wherein the transverse rail includes at least one rib or ridge and each segment has a groove complementary to the at least one rib or ridge to constrain movement of the plurality of partial annular segments in a radial direction toward or away from the central passage through the tubular shaft member.

17. The nozzle assembly according to claim 14 wherein the tubular shaft member has a feature on the transverse rail operable to constrain movement of the plurality of partial annular segments to only toward and away from the central passage through the tubular shaft member during nozzle operation.

18. The nozzle assembly according to claim 17 wherein the feature is a rib on the transverse rail extending laterally across the tubular shaft member adjacent the central passage.

19. The nozzle assembly according to claim 16 wherein each segment engages the at least one rib or ridge to preclude axial movement of the plurality of partial annular segments.

20. The nozzle assembly according to claim 16 wherein each of the plurality of partial annular segments has a partial axially flat outer surface.

Description

DESCRIPTION OF THE DRAWINGS

[0018] FIG. 1 is a longitudinal cross-section of a prior art nozzle in which a tapered regulator passage also serves as a balancing chamber.

[0019] FIG. 2 is a longitudinal cross-section of a nozzle in accordance with the present disclosure in which a portion of the inlet portion of the shaft carries a separate pair of centrifugal weight segments.

[0020] FIG. 3 is a separate partial exploded perspective view of the rotary shaft removed from the nozzle shown in FIG. 2 showing one of the centrifugal segments separated laterally from the shaft.

[0021] FIG. 4 is a longitudinal cross-section view of an alternative nozzle shown in FIG. 2 in which a rib on the lateral straight rail engages a complementary recess or groove in each segment to prevent axial movement of the centrifugal segments along the inlet end of the shaft.

[0022] FIG. 5 is separate partial exploded perspective view of the rotary shaft shown in FIG. 4 showing one of the separable centrifugal segments separated laterally from the shaft.

[0023] FIG. 6 is a separate perspective view of a first alternative configuration of a separable centrifugal segment having peripheral grooves and a straight peripheral axial flat surface.

[0024] FIG. 7 is a separate perspective view of a second alternative configuration of a separable centrifugal segment having peripheral grooves as in FIG. 6 and a radial bore through the centrifugal segment into the axial flat surface.

[0025] FIG. 8 is a separate perspective view of a third alternative embodiment of a centrifugal segment as shown in FIGS. 2 and 3 having a pair of opposite axially extending flat surfaces.

[0026] FIG. 9 is a fourth alternative embodiment of a rotational shaft from the nozzle shown in FIGS. 2 and 3 with a fourth alternative set of centrifugal weight segments with an O-ring positioned between the segments and around the inlet end of the rotational shaft.

[0027] FIG. 10 is a separate perspective view of a fourth alternative configuration of a separable centrifugal segment shown in FIG. 4 including peripheral axial slots or grooves.

[0028] FIG. 11 is an end view of the separable centrifugal segment shown in FIG. 10.

[0029] FIG. 12 is an end view of a fifth alternative configuration of a separable centrifugal segment.

DETAILED DESCRIPTION OF THE DISCLOSURE

[0030] One exemplary embodiment of a nozzle assembly 100 in accordance with the present disclosure is shown in FIGS. 2 and 3. FIG. 2 shows a longitudinal cross sectional view of the nozzle 100 without a spray head attached. The nozzle assembly 100 includes a hollow cylindrical housing body 102 threadably fastened to a hollow cylindrical inlet nut 104 that forms an inlet end portion of the cylindrical housing body 102 and which has a central axial passage 106. The inlet nut 104 is in turn fastened to a high pressure fluid hose (not shown) for directing high pressure fluid into and through the nozzle 100. A hollow tubular rotatable shaft member 108 is coaxially carried within the housing body 102 and captured therein by the inlet nut 104. Thus the inlet nut 104 together with the housing body 102 constrain and capture the rotatable shaft member 108 therein. This tubular shaft member 108 has a fluid inlet end 110 within and near one end of the housing body 102, which is supported by the inlet nut 104. The tubular shaft member 108 has an outlet end 112 near a second end of the housing body 102 for securing a spray head thereto (not shown) for rotation with the shaft member 108 and directing fluid against an object.

[0031] The tubular shaft member 108 has an axial central passage 114 to conduct fluid from the inlet end 110 to and through the outlet end 112 to a spray head 130, shown in FIG. 4. The high pressure fluid inlet passage 106 in the housing body 102 through inlet nut 104 coaxially communicates with the central passage 114 of the tubular shaft member 108. The housing body 102 has an inlet bearing area 116 formed by the inlet nut 104 supporting the inlet end 110 of the tubular shaft member 108.

[0032] A regulating passage 118 is formed between the housing body 102 and an outer surface of the shaft 108. In preferred embodiments, the regulating passage 118 is a tapered frusto-conical gap defined between the tubular shaft 108 and the cylindrical housing body 102. One or more bores 120 extend between the central passage 114 of the tubular shaft member 108 and the regulating passage 118. Pressure of fluid within the regulating passage 118 acts axially upon the shaft member 108 to counterbalance axial force on the tubular shaft member 108 exerted by fluid pressure acting upon the inlet end 110 of the tubular shaft member 108.

[0033] A plurality of partial annular segments 122 are disposed on the shaft member 108 adjacent the distal end of the inlet nut 104 between the inlet bearing area 116 of the housing body 102 and the regulating passage 118, captured between the inlet end 110 of the shaft member 108 and the cylindrical housing body 102 and constrained to rotate with the shaft member 108. In the exemplary embodiment shown in FIGS. 2 and 3, there are two half annular segments 122. These segments 122 are free to separate outwardly, in this case laterally, i.e. radially, from the shaft member 108 and press against the inside wall surface of the cylindrical housing body 102 to reduce rotational speed of the shaft member 108 within the cylindrical housing body 102 during nozzle operation.

[0034] Each of the segments 122 slides laterally on a transverse straight rail 124 formed in the tubular shaft 108. This transverse straight rail 124 formed in the shaft 108 includes a feature 128 thereon which prevents axial movement of the weight segments 122 toward the inlet end 110 of the shaft member 108. Preferably this feature 128 is a raised rib or tab extending outward from the rail 124. Each of the segments 122 has a complementary shape feature 130 to engage the rail 124 with its tab or rib feature 128 so as to slide or ride on the rail 124 only laterally, i.e. radially, during nozzle operation.

[0035] As the shaft 108 rotates in the housing body 102, contact between the weight segments 122 and the rail 124 causes the segments to rotate with the shaft 108. As the shaft rotates, centrifugal force pushes the segments 122 radially outward, eventually contacting the inner wall of the housing body 102 and providing a drag force against further rotational speed. Some of the high pressure fluid from the regulating passage 118 leaks past and provides some lubrication to the segments 122. This leakage fluid then exits through the discharge ports 126 through the housing body 102.

[0036] In the embodiment shown in FIGS. 2 and 3, the semi-annular centrifugal weight segments 122 are constrained to rotate with the shaft 108 because of the transverse rail 124. The centrifugal weight segments 122 are prevented from movement axially back and forth along the inlet end of the shaft 108 by engagement between the tab or rib feature 128 with its complementary feature 130 on the weight segments 122.

[0037] Another embodiment of a nozzle assembly 150 in accordance with the present disclosure is shown in FIGS. 4 and 5. Again, the nozzle 150 includes a hollow cylindrical housing body 102 threadably fastened to a hollow cylindrical inlet nut 104 that forms an inlet end portion of the cylindrical housing body 102 and which has a central axial passage 106. The inlet nut 104 is in turn fastened to a high pressure fluid hose (not shown) for directing high pressure fluid into and through the nozzle 150. A hollow tubular rotatable shaft member 108 is coaxially carried within the housing body 102 and captured therein by the inlet nut 104. Thus the inlet nut 104 together with the housing body 102 constrain and capture the rotatable shaft member 108 therein. This shaft member 108 has a fluid inlet end 110 within and near one end of the housing body 102, which is supported by the inlet nut 104. The shaft member 108 has an outlet end 112 near a second end of the housing body 102 for securing a spray head thereto (not shown) for rotation with the shaft member 108.

[0038] The shaft member 108 has an axial central passage 114 to conduct fluid from the inlet end 110 to and through the outlet end 112 to a spray head 130, shown in FIG. 4. The high pressure fluid inlet passage 106 in the housing body 102 through inlet nut 104 coaxially communicates with the central passage 114 of the shaft member 108. The housing body 102 has an inlet bearing area 116 formed by the inlet nut 104 supporting the inlet end 110 of the tubular shaft member 108.

[0039] A regulating passage 118 is formed between the housing body 102 and an outer surface of the shaft 108. One or more bores 120 communicate between the central passage 114 of the shaft member 108 and the regulating passage 118. Pressure of fluid within the regulating passage 118 acts axially upon the shaft member 108 to counterbalance axial force on the shaft member 108 exerted by fluid pressure acting upon the inlet end 110 of the shaft member 108.

[0040] A pair of partial annular weight segments 122a are disposed on the shaft member 108 adjacent distal end of the inlet nut 104 and between the inlet bearing area 116 of the housing body 102 and the regulating passage 118 and captured between the inlet end 110 of the shaft member 108 and the cylindrical housing body 102 and constrained to rotate with the shaft member 108, wherein the segments are free to separate laterally from the shaft member 108 and press against the inside wall surface of the cylindrical housing body 102 adjacent the inner, or distal, end of the inlet nut 104 to reduce rotational speed of the shaft member 108 within the cylindrical housing body 102 during nozzle operation.

[0041] Each of the weight segments 122a slides laterally on a transverse straight rail 124 formed in the shaft 108 that extends fully across the shaft 108. As the shaft 108 rotates in the housing body 102, contact between the segments 122a and the rail 124 causes the segments to rotate with the shaft 108. As the shaft rotates, centrifugal force pushes the segments 122a radially outward, eventually contacting the inner wall of the housing body 102 and providing a drag force against further rotational speed. Some of the high pressure fluid from the regulating passage 118 leaks past and provides some lubrication to the segments 122a. This leakage fluid then exits through the discharge ports 126 through the housing body 102.

[0042] This nozzle 150 is the same as that shown in FIGS. 2 and 3 wherein the shaft 108 is provided with a feature such as a rib 128 along each side of the rail 124 and each semi-annular segment 122a has a complementary feature such as a slot 130 to accommodate the ridge or rib 128 of the rail 124. This configuration with each segment 122a having a complementary slot 130 prevents any axial movement of the centrifugal segments 122a along the axis of the shaft 108. However, in this nozzle 150, each of the weight segments 122a has a series of spaced peripheral grooves 132 formed in its outer surface. These grooved weight segments 122a unexpectedly results in a further reduction in rotational speed of the nozzle 150 during operation than the configuration shown in FIGS. 2 and 3.

[0043] The following table illustrates this result:

TABLE-US-00001 Standard Grooved Torque, Tool Counterweight Counterweight in-lb RPM RPM RPM .09 16000 5000 4100 .19 20000 8100 5000 .29 28000 9200 6600 .38 30000 10700 8100 .48 35000 12200 9800 .58 38000 14400 11500

[0044] The high pressure nozzle cylindrical housing body 102 and tubular shaft member 108 are preferably made of a high strength stainless steel. Each of the partial annular weight segments in the embodiments described herein is preferably made of a non-galling metal or a metal coated with an anti-galling material to prevent galling of the segment against the rail 124 or the inner surface of the cylindrical housing body 102. One such non-galling metal is 660 Bronze, which was used in the above example and in the embodiments described below.

[0045] Many changes may be made to the rotary nozzle assembly described above without departing from the scope of the present disclosure. For example, the weighted segments may be three, four or five or more partial annular segments wherein at least two are restrained by a radially extending rail such that the segments cannot rotate about the shaft member and can only move outward radially as the shaft member rotates about the central passage. The rail 124 and/or ribs 128 may be other than as specifically shown. For example, the rail 124 may include discrete tabs rather than continuous ribs. The rail 124 may have a dovetail cross-sectional shape rather than utilizing a raised rib or ridge 128 at right angles as illustrated to prevent axial movement of the segments 122 or 122a along the rail 124.

[0046] A first exemplary alternative configuration 122b of a weight segment 122 is shown in FIG. 6. In this embodiment of a nozzle 150, segment 122b is the same as 122a except for a partial axially extending flat surface 152 formed or milled on the outer surface of each of the segments 122b extending axially across each of the peripheral grooves 132. This flat surface 152 provides an axial fluid leakage path during nozzle operation. Alternatively the axially extending flat surface 152 may be replaced with an axially grooved outer curved surface (not shown).

[0047] A second exemplary alternative configuration 122c of a weight segment 122 in accordance with the present disclosure is shown in FIG. 7. In this exemplary configuration each weight segment 122c has a radial bore 154 extending radially through the segment 122c to the axial flat surface 152. This configuration provides another fluid leakage path.

[0048] A third exemplary alternative configuration of a weight segment 122d in accordance with the present disclosure is shown in FIG. 8. In this embodiment, the weight segment 122d has a smooth outer surface as the segments 122 shown in FIGS. 2 and 3, but has a pair of axially extending external flats 156 in its outer surface adjacent the edges mating with the corresponding opposite segment 122d and has a recessed out portion 158 over the slot 130. Again, this configuration changes the leakage path as the segments are centrifugally thrust radially outward during nozzle operation.

[0049] Another variation is shown in FIG. 9. In this embodiment of a nozzle 150 a silicon O-ring 162 is slipped onto the stem 110 of the shaft 108 and each of the segments 122e has a corresponding half annular groove 164 or recess formed in its inner surface sized to receive the O-ring 162 therein. The outer cylindrical surface of each segment 122e may be smooth as shown in FIG. 3, or may be configured with peripheral circular grooves 132, a radial bore 154 such as is shown in FIG. 7, or axial flats 156 as shown in FIG. 8, or any combination of these configurations so as to cause a desired reduction of rotational speed.

[0050] A fourth exemplary alternative configuration of a weight segment 122f in accordance with the present disclosure is shown in FIG. 10. In this embodiment, the weight segment 122f is the same as that shown in FIGS. 4 and 5 in which the outer surface has a plurality of spaced peripheral circular grooves 132. However, in this embodiment each weight segment 122f also has a series of radially spaced axial channels or slots 170, 172, 174, 176, 178 and 180. The sides of each of the slots may be parallel and each of the slots angled identically with reference to a tangent line to the periphery of the segment 122f in a direction of rotation of the nozzle 150 as shown or may be straight radial slots.

[0051] An end view of the segment 122f is shown in FIG. 11. In this embodiment 122f there are six peripheral axial slots shown. Each of the slots 170-180 may preferably be angled with reference to a line tangent to the periphery of the segment to act on or add to the flowing stream of leakage or balancing water passing from the tapered portion of the shaft 108 to the discharge ports 126 in the nozzle body 102 generated during operation of the nozzle 150. These slots as shown have parallel sides as in a saw kerf. Alternatively the slots may be V or U shaped in cross section.

[0052] A fifth alternative embodiment of a weight segment 122g is shown in an end view in FIG. 12. This weight segment is the same as that shown in FIGS. 10 and 11 except that it has an enlarged inlet end diameter which, when the pair of weight segments 122g are disposed on the shaft 108 as in FIG. 5, causes the weight segments 122g to form an annular recess 190 around the inlet end 110 of the shaft 108.

[0053] Again, as the shaft 108 rotates, centrifugal force pushes the segments 122g radially outward along the rail 124, eventually contacting the inner wall of the housing body 102 and exerting a drag force against the inner wall of the housing body 102 thereby reducing further rotational speed. Some of the high pressure fluid from the regulating passage 118 leaks past and provides some lubrication to the segments 122g. This leakage fluid then exits through the discharge ports 126 through the housing body 102. Each of the segments 122g has an inner diameter larger than the inlet end 110 of the shaft 108 toward the inlet end 110 so as to form an annular recess 190 around the shaft 108 at the inlet end 110 when both semi annular segments are mounted to the shaft 108 together on the rail 124. Each of the segments 122g may also be provided with peripheral annular grooves 132 and slanted axial grooves 170-180 as in the embodiment described above with reference to FIGS. 10 and 11 to enhance the speed retarding effect. During nozzle operation, this annular recess 190 facing the inlet end 110 of the tubular shaft member 108 effectively moves the applied counter force exerted by the leakage water closer to the rail 124 so that the segments 122g more uniformly exert force pressing outward against the inner wall of the housing 102. This tends to reduce uneven wear on the exterior surface of the segments 122g.

[0054] Many variations and combinations may be made to the above various embodiments of the retarding partial annular weight segments 122a-g described above. For example, in the weight segments 122a shown in FIG. 5, each segment 122a may be provided with a recess 190 formed at the inlet end of the segment 122a as is shown in the alternative embodiment 122g in FIG. 12. Weight segments 122a or 122b for example, may alternatively each include a radial bore 154 as shown in FIG. 7. Therefore all such changes, alternatives and equivalents in accordance with the features and benefits described herein, are within the scope of the present disclosure. Any or all of such changes and alternatives may be introduced without departing from the spirit and broad scope of this disclosure as defined by the claims below and their equivalents.