US20060153721A1 - Dual inlet rotary tool - Google Patents
Dual inlet rotary tool Download PDFInfo
- Publication number
- US20060153721A1 US20060153721A1 US11/032,805 US3280505A US2006153721A1 US 20060153721 A1 US20060153721 A1 US 20060153721A1 US 3280505 A US3280505 A US 3280505A US 2006153721 A1 US2006153721 A1 US 2006153721A1
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- United States
- Prior art keywords
- fluid
- housing
- fluid inlet
- recited
- rotor
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- 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.)
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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
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
- F04B39/12—Casings; Cylinders; Cylinder heads; Fluid connections
- F04B39/121—Casings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
Definitions
- This invention relates generally to rotary tools.
- this invention relates to machine mounted pressurized fluid driven rotary tools.
- the present invention relates to a rotary device having a housing that has a first fluid inlet and a second fluid inlet.
- a rotor is rotatably mounted in the housing and is in communication with the first and second fluid inlets.
- the present invention also relates to a method for connecting a rotary tool to a fluid source by providing a housing and a rotor mounting in the housing.
- First and second fluid inlets are provided in the housing, which are each in communication with the rotor.
- a plug is inserted into the first fluid inlet and the second fluid inlet is connected to a high pressure fluid source.
- FIG. 1 is a cross-sectional view of a rotary tool according to the present invention.
- FIGS. 2A and 2B are side views of the rotary tool according to the present invention as mounted to a CNC machine.
- FIGS. 3A and 3B are side views of the rotary tool according to the present invention as mounted to a machine fixture.
- an exemplary rotary device according to the present invention is shown generally at 10 .
- the exemplary device described herein is a pneumatic tool having a turbine rotor powered by oil-free high pressure air, however, it will be understood that the concepts of the current invention could be used or adapted for use for any rotary tool having any type of fluid driven motor, such as a vane motor, and powered by any type of compressed fluid.
- the rotary tool 10 generally has a housing 13 formed by a front section 12 , a back section 14 threaded to the front section 12 , and an end cap 24 threaded to the back section 14 .
- the front section 12 includes a portion having a relatively large diameter to which a fixture can be attached, as described in more detail below.
- the portion of the front section 12 having the relatively large diameter includes a motor chamber 15 formed on an inside portion thereof and a rotor 16 mounted within the motor chamber 15 .
- the back section 14 of the housing 13 includes a first fluid inlet 34 that has a longitudinal axis B that is generally perpendicular to an axis of rotation A of the rotor 16 .
- the first fluid inlet 34 is in communication with the rotor 16 and is adapted to receive a pressurized fluid and transmit the pressurized fluid to the rotor 16 .
- the first fluid inlet 34 is formed by a bore extending through the sidewall of the back section 14 of the housing 13 and is adapted to receive a hose from a high pressure air source, an inlet adapter, or a plug, as described in more detail below, for example by having threads formed on at least a portion of the bore.
- An inlet adapter 36 is threaded into the first fluid inlet 34 and has a bore 37 therethrough that is in communication with the first fluid inlet 34 .
- the inlet adapter 36 is adapted to receive a hose from a high pressure air source or a plug, as described in more detail below, for example by having threads 38 formed on at least a portion of the bore.
- the back section 14 of the housing 13 also includes a second fluid inlet 32 that has a longitudinal axis that is generally parallel to the axis of rotation A of the rotor 16 .
- the second fluid inlet 32 is in communication with the rotor 16 and is adapted to receive a pressurized fluid and transmit the pressurized fluid to the rotor 16 .
- the second fluid inlet 32 is formed by a bore extending through the end of the back section 14 of the housing 13 .
- a generally cylindrical shank 30 having a longitudinal axis that is generally parallel to the axis of rotation A of the rotor 16 is integrally formed to the back section 14 of the housing 13 , extends from the end of the back section 14 , and can be used as a mount to connect the rotary tool 10 to a machine, as is described in more detail below.
- the shank 30 has a bore 33 extending therethrough, which is in communication with the second fluid inlet 32 , to allow the shank 30 to receive a pressurized fluid and transmit the pressurized fluid to the second fluid inlet 32 , as described in more detail below.
- the shank 30 is adapted to receive a hose from high pressure air source or a plug, as described in more detail below, for example by having threads 35 formed on at least a portion of the bore.
- a pair of o-rings 31 sit within indentations in the outer wall of the shank 30 .
- a muffler 26 Inside of the back section 14 is a muffler 26 , which may be composed of a felt-like material and is adapted for muffling the noise caused by exhausted fluids.
- the end cap 24 includes one or more holes 21 each having a predetermined diameter which are adapted to allow the pressurized fluid to escape from the motor chamber 15 .
- a rotor 16 having an axis of rotation A, is mounted within the motor chamber 15 such that the rotor 16 can rotate therein.
- the rotor 16 is a reaction turbine-type rotor, such as that described in U.S. Pat. No. 4,776,752 to Davis, which has a common assignee with the present invention, and the disclosure of which is hereby incorporated by reference.
- the present invention is not so limited and may be applied to rotary devices having other types of motors.
- pressurized air is directed to the rotor 16 from the first fluid inlet 34 and/or the second fluid inlet 32 .
- the air enters the rotor 16 it enters a first annular chamber 50 , flows around a resilient valve ring 52 through radial holes 54 in annular wall 60 into a second annular chamber 56 , where it is directed through nozzles 58 , thereby imparting rotation to the rotor 16 and therefore the rotatable shaft 18 .
- the pressurized fluid is expelled from the rotor 16 through the nozzles 58 and passes into the motor chamber 15 , through the muffler 26 , and exits the rotary tool 10 through the holes 21 in the end cap 24 to atmosphere.
- rotation increases to a pre-selected maximum.
- Centrifugal forces acting on resilient valve ring 52 tend to cause radial expansion of the ring 52 , however, the inner surface of the annular wall 60 supports the valve ring 60 , except at radial holes 54 . This enables the radial expansion of the valve ring 52 to be directed into the holes 54 so as to cause a controlled elastic deformation of valve ring 52 .
- the resilient valve ring 52 deforms, it approaches the ends of radial holes 54 . As the distance narrows sufficiently, fluid flow through the radial holes 54 is restricted and rotating forces reduced. As drag forces acting on the system and rotating forces reach equilibrium, the forces acting on the resilient valve ring 52 will also be in equilibrium. This results in a constant rotary speed.
- a rotatable shaft 18 is attached at one end to the rotor 16 and at the other end to a collet 22 , which is used to hold a tool (not shown), such as a grinding-type tool.
- the shaft 18 is rotatably supported by bearings 20 which, in turn, are respectively secured to the front section 12 of the housing 13 .
- the tool 10 is secured to the machine by inserting the shank 30 into the chuck 40 of the machine (not shown) and securing it thereto. If the machine provides high pressure air through the chuck 40 , the bore 33 in the shank 30 (see FIG. 1 ) is left open and the high pressure air is supplied to the rotor 16 through the second fluid inlet 32 (see FIG. 1 ). When secured in the chuck 40 , the o-rings 31 (see FIG. 1 ) prevent the high pressure air from escaping around the outside of the shank 30 .
- the first fluid inlet 34 see FIG.
- the first fluid inlet 34 can be blocked by threading a plug 42 directly into the first fluid inlet 34 .
- air from the high pressure air source enters the tool 10 through the shank 30 , passes through the bore 33 in the shank 30 to the second fluid inlet 32 , and from the second fluid inlet 32 to the rotor 16 , where the high pressure air drives the rotor 16 .
- the high pressure air that is expelled from the rotor 16 enters the motor chamber 15 , passes through the muffler 26 , and is expelled from the tool 10 through the holes 21 in the end cap 24 .
- the second fluid inlet 32 could be blocked by threading a plug 42 into the shank 30 and the hose 46 of a high pressure air source (not shown) could be connected to the inlet adapter 36 to provide high pressure air to the rotor 16 through the first fluid inlet 34 (see FIG. 1 ).
- the hose 46 could be connected directly into the first fluid inlet 34 . As can best be seen in FIG.
- air from the high pressure air source enters the tool 10 through the inlet adapter 36 , passes through the bore 37 in the inlet adapter 36 to the first fluid inlet 34 , and from the first fluid inlet 34 to the rotor 16 , where the high pressure air drives the rotor 16 .
- the high pressure air that is expelled from the rotor 16 enters the housing 13 , passes through the muffler 26 , and is expelled from the tool 10 through the holes 21 in the end cap 24 .
- the tool 10 is secured to the fixture 44 by clamping the housing 13 within the fixture 44 .
- the tool 10 can also be secured to the fixture 44 by clamping the shank 30 , rather than the housing 13 , within the fixture 44 , as shown in phantom.
- the shank 30 is connected to the hose 46 of a high pressure air source (not shown) to provide high pressure air to the rotor 16 through the second fluid inlet 32 (see FIG. 1 ).
- the first fluid inlet 34 (see FIG. 1 ) is blocked by threading a plug 42 into the inlet adapter 36 .
- the first fluid inlet 34 can be blocked by threading a plug 42 directly into the first fluid inlet 34 .
- air from the hose 46 enters the tool 10 through the shank 30 , passes through the bore 33 in the shank 30 to the second fluid inlet 32 , and from the second fluid inlet 32 to the rotor 16 , where the high pressure air drives the rotor 16 .
- the high pressure air that is expelled from the rotor 16 enters the housing 13 , passes through the muffler 26 , and is expelled from the tool 10 through the holes 21 in the end cap 24 .
- the inlet adapter 36 could be attached to the hose 46 of the high pressure air source (not shown) to provide high pressure air to the rotor 16 (see FIG. 1 ) through the first fluid inlet 34 (see FIG. 1 ).
- the hose 46 could be attached directly to the first fluid inlet 34 .
- the second fluid inlet 32 (see FIG. 1 ) is then blocked by threading a plug 42 into the end of the shank 30 . As can best be seen in FIG.
- air from the high pressure air source enters the tool 10 through the inlet adapter 36 , passes through the bore 37 in the inlet adapter 36 to the first fluid inlet 34 , and from the first fluid inlet 34 to the rotor 16 , where the high pressure air drives the rotor 16 .
- the high pressure air that is expelled from the rotor 16 enters the housing 13 , passes through the muffler 26 , and is expelled from the tool 10 through the holes 21 in the end cap 24 .
- the current invention allows a single rotary tool to be used with almost any machine, any mounting configuration, and any fluid inlet configuration desired, rather than having different tools for each.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Auxiliary Devices For Machine Tools (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Automatic Tool Replacement In Machine Tools (AREA)
- Finish Polishing, Edge Sharpening, And Grinding By Specific Grinding Devices (AREA)
- Hydraulic Motors (AREA)
- Joints Allowing Movement (AREA)
- Dental Tools And Instruments Or Auxiliary Dental Instruments (AREA)
- Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
- Constituent Portions Of Griding Lathes, Driving, Sensing And Control (AREA)
- Gripping On Spindles (AREA)
Abstract
A rotary device having a housing that has a first fluid inlet and second fluid inlet. A rotor is rotatably mounted in the housing and is in communication with the first and second fluid inlets.
Description
- This invention relates generally to rotary tools. In particular, this invention relates to machine mounted pressurized fluid driven rotary tools.
- In one embodiment, the present invention relates to a rotary device having a housing that has a first fluid inlet and a second fluid inlet. A rotor is rotatably mounted in the housing and is in communication with the first and second fluid inlets.
- The present invention also relates to a method for connecting a rotary tool to a fluid source by providing a housing and a rotor mounting in the housing. First and second fluid inlets are provided in the housing, which are each in communication with the rotor. A plug is inserted into the first fluid inlet and the second fluid inlet is connected to a high pressure fluid source.
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FIG. 1 is a cross-sectional view of a rotary tool according to the present invention. -
FIGS. 2A and 2B are side views of the rotary tool according to the present invention as mounted to a CNC machine. -
FIGS. 3A and 3B are side views of the rotary tool according to the present invention as mounted to a machine fixture. - Referring to
FIG. 1 , an exemplary rotary device according to the present invention is shown generally at 10. The exemplary device described herein is a pneumatic tool having a turbine rotor powered by oil-free high pressure air, however, it will be understood that the concepts of the current invention could be used or adapted for use for any rotary tool having any type of fluid driven motor, such as a vane motor, and powered by any type of compressed fluid. - As shown in
FIG. 1 , therotary tool 10 generally has ahousing 13 formed by afront section 12, aback section 14 threaded to thefront section 12, and anend cap 24 threaded to theback section 14. Thefront section 12 includes a portion having a relatively large diameter to which a fixture can be attached, as described in more detail below. The portion of thefront section 12 having the relatively large diameter includes amotor chamber 15 formed on an inside portion thereof and arotor 16 mounted within themotor chamber 15. - The
back section 14 of thehousing 13 includes afirst fluid inlet 34 that has a longitudinal axis B that is generally perpendicular to an axis of rotation A of therotor 16. Thefirst fluid inlet 34 is in communication with therotor 16 and is adapted to receive a pressurized fluid and transmit the pressurized fluid to therotor 16. Thefirst fluid inlet 34 is formed by a bore extending through the sidewall of theback section 14 of thehousing 13 and is adapted to receive a hose from a high pressure air source, an inlet adapter, or a plug, as described in more detail below, for example by having threads formed on at least a portion of the bore. Aninlet adapter 36 is threaded into thefirst fluid inlet 34 and has abore 37 therethrough that is in communication with thefirst fluid inlet 34. Theinlet adapter 36 is adapted to receive a hose from a high pressure air source or a plug, as described in more detail below, for example by havingthreads 38 formed on at least a portion of the bore. - The
back section 14 of thehousing 13 also includes asecond fluid inlet 32 that has a longitudinal axis that is generally parallel to the axis of rotation A of therotor 16. Thesecond fluid inlet 32 is in communication with therotor 16 and is adapted to receive a pressurized fluid and transmit the pressurized fluid to therotor 16. Thesecond fluid inlet 32 is formed by a bore extending through the end of theback section 14 of thehousing 13. A generallycylindrical shank 30 having a longitudinal axis that is generally parallel to the axis of rotation A of therotor 16 is integrally formed to theback section 14 of thehousing 13, extends from the end of theback section 14, and can be used as a mount to connect therotary tool 10 to a machine, as is described in more detail below. Theshank 30 has abore 33 extending therethrough, which is in communication with thesecond fluid inlet 32, to allow theshank 30 to receive a pressurized fluid and transmit the pressurized fluid to thesecond fluid inlet 32, as described in more detail below. Theshank 30 is adapted to receive a hose from high pressure air source or a plug, as described in more detail below, for example by havingthreads 35 formed on at least a portion of the bore. A pair of o-rings 31 sit within indentations in the outer wall of theshank 30. - Inside of the
back section 14 is amuffler 26, which may be composed of a felt-like material and is adapted for muffling the noise caused by exhausted fluids. In addition, theend cap 24 includes one ormore holes 21 each having a predetermined diameter which are adapted to allow the pressurized fluid to escape from themotor chamber 15. - A
rotor 16, having an axis of rotation A, is mounted within themotor chamber 15 such that therotor 16 can rotate therein. As described herein, therotor 16 is a reaction turbine-type rotor, such as that described in U.S. Pat. No. 4,776,752 to Davis, which has a common assignee with the present invention, and the disclosure of which is hereby incorporated by reference. However, the present invention is not so limited and may be applied to rotary devices having other types of motors. In operation, pressurized air is directed to therotor 16 from thefirst fluid inlet 34 and/or thesecond fluid inlet 32. As the air enters therotor 16 it enters a firstannular chamber 50, flows around aresilient valve ring 52 throughradial holes 54 inannular wall 60 into a secondannular chamber 56, where it is directed throughnozzles 58, thereby imparting rotation to therotor 16 and therefore therotatable shaft 18. The pressurized fluid is expelled from therotor 16 through thenozzles 58 and passes into themotor chamber 15, through themuffler 26, and exits therotary tool 10 through theholes 21 in theend cap 24 to atmosphere. As the pressurized fluid is directed into therotor 16, rotation increases to a pre-selected maximum. Centrifugal forces acting onresilient valve ring 52 tend to cause radial expansion of thering 52, however, the inner surface of theannular wall 60 supports thevalve ring 60, except atradial holes 54. This enables the radial expansion of thevalve ring 52 to be directed into theholes 54 so as to cause a controlled elastic deformation ofvalve ring 52. In operation, as theresilient valve ring 52 deforms, it approaches the ends ofradial holes 54. As the distance narrows sufficiently, fluid flow through theradial holes 54 is restricted and rotating forces reduced. As drag forces acting on the system and rotating forces reach equilibrium, the forces acting on theresilient valve ring 52 will also be in equilibrium. This results in a constant rotary speed. If drag forces increase, the equilibrium would be disrupted, and the forces on theresilient valve ring 52 will retract thevalve ring 52 from its closest proximity toradial holes 54, allowing additional fluid flow until another equilibrium is established. If for any reason the turbine should exceed the desired governed speed, theresilient valve ring 52 will move to restrict pressure fluid flow even further until sufficient overspeed will cause all flow to stop, thereby incorporating an overspeed safety. - A
rotatable shaft 18 is attached at one end to therotor 16 and at the other end to acollet 22, which is used to hold a tool (not shown), such as a grinding-type tool. Theshaft 18 is rotatably supported bybearings 20 which, in turn, are respectively secured to thefront section 12 of thehousing 13. - As shown in
FIG. 2A , to mount therotary tool 10 to a CNC machine, or other machine having a chuck for mounting the tool, thetool 10 is secured to the machine by inserting theshank 30 into thechuck 40 of the machine (not shown) and securing it thereto. If the machine provides high pressure air through thechuck 40, thebore 33 in the shank 30 (seeFIG. 1 ) is left open and the high pressure air is supplied to therotor 16 through the second fluid inlet 32 (seeFIG. 1 ). When secured in thechuck 40, the o-rings 31 (seeFIG. 1 ) prevent the high pressure air from escaping around the outside of theshank 30. The first fluid inlet 34 (seeFIG. 1 ) is blocked by threading aplug 42 into theinlet adapter 36. Alternatively, if aninlet adapter 36 is not used, thefirst fluid inlet 34 can be blocked by threading aplug 42 directly into thefirst fluid inlet 34. As can best be seen inFIG. 1 , when connected in this way, air from the high pressure air source enters thetool 10 through theshank 30, passes through thebore 33 in theshank 30 to thesecond fluid inlet 32, and from thesecond fluid inlet 32 to therotor 16, where the high pressure air drives therotor 16. The high pressure air that is expelled from therotor 16 enters themotor chamber 15, passes through themuffler 26, and is expelled from thetool 10 through theholes 21 in theend cap 24. - Alternatively, as shown in
FIG. 2B , the second fluid inlet 32 (seeFIG. 1 ) could be blocked by threading aplug 42 into theshank 30 and thehose 46 of a high pressure air source (not shown) could be connected to theinlet adapter 36 to provide high pressure air to therotor 16 through the first fluid inlet 34 (seeFIG. 1 ). Alternatively, if aninlet adapter 36 is not used, thehose 46 could be connected directly into thefirst fluid inlet 34. As can best be seen inFIG. 1 , when connected in this way, air from the high pressure air source enters thetool 10 through theinlet adapter 36, passes through thebore 37 in theinlet adapter 36 to thefirst fluid inlet 34, and from thefirst fluid inlet 34 to therotor 16, where the high pressure air drives therotor 16. The high pressure air that is expelled from therotor 16 enters thehousing 13, passes through themuffler 26, and is expelled from thetool 10 through theholes 21 in theend cap 24. - As shown in
FIG. 3A , to mount therotary tool 10 to a machine having afixture 44, such as a robotic arm, thetool 10 is secured to thefixture 44 by clamping thehousing 13 within thefixture 44. Alternatively, depending on the machine and the desired usage, thetool 10 can also be secured to thefixture 44 by clamping theshank 30, rather than thehousing 13, within thefixture 44, as shown in phantom. Theshank 30 is connected to thehose 46 of a high pressure air source (not shown) to provide high pressure air to therotor 16 through the second fluid inlet 32 (seeFIG. 1 ). The first fluid inlet 34 (seeFIG. 1 ) is blocked by threading aplug 42 into theinlet adapter 36. Alternatively, if aninlet adapter 36 is not used, thefirst fluid inlet 34 can be blocked by threading aplug 42 directly into thefirst fluid inlet 34. As can best be seen inFIG. 1 , when connected in this way, air from thehose 46 enters thetool 10 through theshank 30, passes through thebore 33 in theshank 30 to thesecond fluid inlet 32, and from thesecond fluid inlet 32 to therotor 16, where the high pressure air drives therotor 16. The high pressure air that is expelled from therotor 16 enters thehousing 13, passes through themuffler 26, and is expelled from thetool 10 through theholes 21 in theend cap 24. - Alternatively, as shown in
FIG. 3B , theinlet adapter 36 could be attached to thehose 46 of the high pressure air source (not shown) to provide high pressure air to the rotor 16 (seeFIG. 1 ) through the first fluid inlet 34 (seeFIG. 1 ). Alternatively, if aninlet adapter 36 is not used, thehose 46 could be attached directly to thefirst fluid inlet 34. The second fluid inlet 32 (seeFIG. 1 ) is then blocked by threading aplug 42 into the end of theshank 30. As can best be seen inFIG. 1 , when connected in this way, air from the high pressure air source enters thetool 10 through theinlet adapter 36, passes through thebore 37 in theinlet adapter 36 to thefirst fluid inlet 34, and from thefirst fluid inlet 34 to therotor 16, where the high pressure air drives therotor 16. The high pressure air that is expelled from therotor 16 enters thehousing 13, passes through themuffler 26, and is expelled from thetool 10 through theholes 21 in theend cap 24. - As can be seen from the above description, the current invention allows a single rotary tool to be used with almost any machine, any mounting configuration, and any fluid inlet configuration desired, rather than having different tools for each.
- The foregoing description of the preferred embodiment of the invention has been presented for purposes of illustration and description, and is not intended to be exhaustive or to limit the invention to the precise form disclosed. The descriptions were selected to best explain the principles of the invention and their practical application to enable other skills in the art to best utilize the invention in various embodiments and various modifications as are suited to the particular use contemplated. It is intended that the scope of the invention not be limited by the specification, but be defined by the claims set forth below.
Claims (21)
1. A rotary device, comprising:
a housing having a first fluid inlet and a second fluid inlet;
a rotor rotatably mounted in the housing and in communication with the first and second fluid inlets.
2. A rotary device, as recited in claim 1 , wherein the first fluid inlet has a longitudinal axis transverse to an axis of rotation of the rotor and is adapted to receive a pressurized fluid and transmit the pressurized fluid to the rotor.
3. A rotary device, as recited in claim 2 , wherein the first fluid inlet comprises a bore extending through a side of the housing.
4. A rotary device, as recited in claim 1 , wherein the second fluid inlet has a longitudinal axis parallel to an axis of rotation of the rotor and is adapted to receive a pressurized fluid and transmit the pressurized fluid to the rotor.
5. A rotary device, as recited in claim 4 , wherein the second fluid inlet comprises a bore extending through an end of the housing.
6. A rotary device, as recited in claim 1 , further comprising a mount connected to an end of the housing for connecting the rotary device to a machine.
7. A rotary device, as recited in claim 6 , wherein the mount is adapted to receive a pressurized fluid and transmit the pressurized fluid to the second fluid inlet.
8. A rotary device, as recited in claim 6 , wherein the mount comprises a bore therethrough, the bore being in communication with the second fluid inlet.
9. A rotary device, as recited in claim 6 , wherein the mount is integral with the housing.
10. A rotary device, as recited in claim 6 , wherein the mount comprises a shank connected to and extending from the end of the housing.
11. A rotary device, as recited in claim 10 , wherein the shank is adapted to receive a pressurized fluid and transmit the pressurized fluid to the second fluid inlet.
12. A rotary device, as recited in claim 10 , wherein the shank comprises a bore therethrough, the bore being in communication with the second fluid inlet.
13. A rotary device, as recited in claim 10 , wherein the shank is integral with the housing.
14. A rotary device, as recited in claim 1 , further comprising an inlet adapter, removably connected to the housing and in communication with the first fluid inlet, for connecting the housing to a high pressure fluid source.
15. A rotary device, as recited in claim 14 , further comprising a plug adapted to prevent the flow of fluid through the inlet adapter.
16. A rotary device, as recited in claim 1 , further comprising a plug adapted to prevent the flow of fluid through the first or second fluid inlet.
17. A method for connecting a rotary tool to a fluid source, comprising the steps of:
providing a housing and a rotor mounted in the housing;
providing a first fluid inlet in the housing in communication with the rotor;
providing a second fluid inlet in the housing in communication with the rotor;
inserting a plug into the first fluid inlet; and
connecting the second fluid inlet to a high pressure fluid source.
18. A method for connecting a rotary tool to a fluid source, as recited in claim 17 , further comprising the step of providing a mount connected to an end of the housing for connecting the housing to a machine.
19. A method for connecting a rotary tool to a fluid source, as recited in claim 17 , further comprising the step of providing a shank connected to and extending from an end of the housing for connecting the housing to a machine.
20. A method for connecting a rotary tool to a fluid source, as recited in claim 19 , further comprising the step of providing a bore through the shank adapted to receive a pressurized fluid and transmit the pressurized fluid to the first or second fluid inlet.
21. A method for connecting a rotary tool to a fluid source, as recited in claim 17 , further comprising the step of providing an inlet adapter for connection to the first or second fluid inlet for connecting the fluid inlet to a high pressure fluid source.
Priority Applications (11)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/032,805 US20060153721A1 (en) | 2005-01-11 | 2005-01-11 | Dual inlet rotary tool |
JP2007550355A JP2008527238A (en) | 2005-01-11 | 2005-09-22 | Two-neck rotating tool |
KR1020077015841A KR20070108149A (en) | 2005-01-11 | 2005-09-22 | Dual inlet rotary tool |
RU2007126321/02A RU2007126321A (en) | 2005-01-11 | 2005-09-22 | ROTATING TOOL WITH TWO INLETS |
MX2007008453A MX2007008453A (en) | 2005-01-11 | 2005-09-22 | Dual inlet rotary tool. |
AU2005324445A AU2005324445A1 (en) | 2005-01-11 | 2005-09-22 | Dual inlet rotary tool |
EP05800228A EP1853819A2 (en) | 2005-01-11 | 2005-09-22 | Dual inlet rotary tool |
PCT/US2005/034103 WO2006076055A2 (en) | 2005-01-11 | 2005-09-22 | Dual inlet rotary tool |
CNA2005800072403A CN101389854A (en) | 2005-01-11 | 2005-09-22 | Dual inlet rotary tool |
CA002593698A CA2593698A1 (en) | 2005-01-11 | 2005-09-22 | Dual inlet rotary tool |
TW095136130A TWI345611B (en) | 2005-01-11 | 2006-09-29 | Rotary tool |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/032,805 US20060153721A1 (en) | 2005-01-11 | 2005-01-11 | Dual inlet rotary tool |
Publications (1)
Publication Number | Publication Date |
---|---|
US20060153721A1 true US20060153721A1 (en) | 2006-07-13 |
Family
ID=36653426
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/032,805 Abandoned US20060153721A1 (en) | 2005-01-11 | 2005-01-11 | Dual inlet rotary tool |
Country Status (11)
Country | Link |
---|---|
US (1) | US20060153721A1 (en) |
EP (1) | EP1853819A2 (en) |
JP (1) | JP2008527238A (en) |
KR (1) | KR20070108149A (en) |
CN (1) | CN101389854A (en) |
AU (1) | AU2005324445A1 (en) |
CA (1) | CA2593698A1 (en) |
MX (1) | MX2007008453A (en) |
RU (1) | RU2007126321A (en) |
TW (1) | TWI345611B (en) |
WO (1) | WO2006076055A2 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9333611B2 (en) | 2013-09-13 | 2016-05-10 | Colibri Spindles, Ltd. | Fluid powered spindle |
US10207379B2 (en) | 2016-01-21 | 2019-02-19 | Colibri Spindles Ltd. | Live tool collar having wireless sensor |
Citations (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2462997A (en) * | 1944-11-30 | 1949-03-01 | Roush James Leigh | Attachment for milling machines |
US2801415A (en) * | 1955-03-25 | 1957-08-06 | Bostitch Inc | Fastener-applying implement |
US2818570A (en) * | 1952-09-25 | 1958-01-07 | Harlan N Faccou | Pneumatic stapler |
US2881589A (en) * | 1956-06-25 | 1959-04-14 | Aro Equipment Corp | Pneumatic drill |
US2896677A (en) * | 1957-10-04 | 1959-07-28 | Timber Structures Inc | Air drill |
US3101014A (en) * | 1961-10-02 | 1963-08-20 | Henry H G Rowe | Ultra-high-speed pneumatically driven machine tools, such as drills and the like |
US3119304A (en) * | 1961-04-12 | 1964-01-28 | Roland E Doeden | Air operated tool |
US3383805A (en) * | 1963-10-24 | 1968-05-21 | Westwind Turbines Ltd | Air-driven turbines |
US3610770A (en) * | 1968-05-31 | 1971-10-05 | Koninkl Maschf Stork Nv | Compressible fluid turbine |
US3803981A (en) * | 1972-01-17 | 1974-04-16 | Owens Illinois Inc | Independent drive sub-spindle mounted for eccentric adjustment in prime spindle |
US3893487A (en) * | 1973-12-26 | 1975-07-08 | Caterpillar Tractor Co | High pressure hydraulic fitting |
US4468897A (en) * | 1982-09-27 | 1984-09-04 | Joseph V. Munoz | Universal pneumatic grinding bar |
US4654956A (en) * | 1985-04-16 | 1987-04-07 | Protocad, Inc. | Drill apparatus for use with computer controlled plotter |
US4776752A (en) * | 1987-03-02 | 1988-10-11 | Davis Lynn M | Speed governed rotary device |
US5180019A (en) * | 1991-04-15 | 1993-01-19 | Ingersoll-Rand Company | Power tool having selectable inlet location |
US5228523A (en) * | 1990-10-19 | 1993-07-20 | Atlas Copco Tools Ab | Pneumatic power tool |
US6193461B1 (en) * | 1999-02-02 | 2001-02-27 | Varian Inc. | Dual inlet vacuum pumps |
US6311487B1 (en) * | 1999-07-15 | 2001-11-06 | Paul C. Ferch | Electromechanical hydraulic drive system for vehicle |
US20040146368A1 (en) * | 2003-01-28 | 2004-07-29 | Konishi M Howard | Autonomous power interface for modifying limited rotation speed of a machine |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2682428B1 (en) * | 1991-10-11 | 1993-12-24 | Michele Martinez | DEVICE FOR CONTROLLING AND CONTROLLING THE ROTATION OF A PNEUMATIC TURBINE. |
-
2005
- 2005-01-11 US US11/032,805 patent/US20060153721A1/en not_active Abandoned
- 2005-09-22 KR KR1020077015841A patent/KR20070108149A/en not_active Application Discontinuation
- 2005-09-22 WO PCT/US2005/034103 patent/WO2006076055A2/en active Search and Examination
- 2005-09-22 AU AU2005324445A patent/AU2005324445A1/en not_active Abandoned
- 2005-09-22 EP EP05800228A patent/EP1853819A2/en not_active Withdrawn
- 2005-09-22 RU RU2007126321/02A patent/RU2007126321A/en not_active Application Discontinuation
- 2005-09-22 CA CA002593698A patent/CA2593698A1/en not_active Abandoned
- 2005-09-22 CN CNA2005800072403A patent/CN101389854A/en active Pending
- 2005-09-22 MX MX2007008453A patent/MX2007008453A/en not_active Application Discontinuation
- 2005-09-22 JP JP2007550355A patent/JP2008527238A/en active Pending
-
2006
- 2006-09-29 TW TW095136130A patent/TWI345611B/en not_active IP Right Cessation
Patent Citations (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2462997A (en) * | 1944-11-30 | 1949-03-01 | Roush James Leigh | Attachment for milling machines |
US2818570A (en) * | 1952-09-25 | 1958-01-07 | Harlan N Faccou | Pneumatic stapler |
US2801415A (en) * | 1955-03-25 | 1957-08-06 | Bostitch Inc | Fastener-applying implement |
US2881589A (en) * | 1956-06-25 | 1959-04-14 | Aro Equipment Corp | Pneumatic drill |
US2896677A (en) * | 1957-10-04 | 1959-07-28 | Timber Structures Inc | Air drill |
US3119304A (en) * | 1961-04-12 | 1964-01-28 | Roland E Doeden | Air operated tool |
US3101014A (en) * | 1961-10-02 | 1963-08-20 | Henry H G Rowe | Ultra-high-speed pneumatically driven machine tools, such as drills and the like |
US3383805A (en) * | 1963-10-24 | 1968-05-21 | Westwind Turbines Ltd | Air-driven turbines |
US3610770A (en) * | 1968-05-31 | 1971-10-05 | Koninkl Maschf Stork Nv | Compressible fluid turbine |
US3803981A (en) * | 1972-01-17 | 1974-04-16 | Owens Illinois Inc | Independent drive sub-spindle mounted for eccentric adjustment in prime spindle |
US3893487A (en) * | 1973-12-26 | 1975-07-08 | Caterpillar Tractor Co | High pressure hydraulic fitting |
US4468897A (en) * | 1982-09-27 | 1984-09-04 | Joseph V. Munoz | Universal pneumatic grinding bar |
US4654956A (en) * | 1985-04-16 | 1987-04-07 | Protocad, Inc. | Drill apparatus for use with computer controlled plotter |
US4776752A (en) * | 1987-03-02 | 1988-10-11 | Davis Lynn M | Speed governed rotary device |
US5228523A (en) * | 1990-10-19 | 1993-07-20 | Atlas Copco Tools Ab | Pneumatic power tool |
US5180019A (en) * | 1991-04-15 | 1993-01-19 | Ingersoll-Rand Company | Power tool having selectable inlet location |
US6193461B1 (en) * | 1999-02-02 | 2001-02-27 | Varian Inc. | Dual inlet vacuum pumps |
US6311487B1 (en) * | 1999-07-15 | 2001-11-06 | Paul C. Ferch | Electromechanical hydraulic drive system for vehicle |
US20040146368A1 (en) * | 2003-01-28 | 2004-07-29 | Konishi M Howard | Autonomous power interface for modifying limited rotation speed of a machine |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9333611B2 (en) | 2013-09-13 | 2016-05-10 | Colibri Spindles, Ltd. | Fluid powered spindle |
US10207378B2 (en) | 2013-09-13 | 2019-02-19 | Colibri Spindles Ltd. | Fluid powered spindle |
US10207379B2 (en) | 2016-01-21 | 2019-02-19 | Colibri Spindles Ltd. | Live tool collar having wireless sensor |
Also Published As
Publication number | Publication date |
---|---|
KR20070108149A (en) | 2007-11-08 |
TW200815681A (en) | 2008-04-01 |
RU2007126321A (en) | 2009-02-20 |
AU2005324445A1 (en) | 2006-07-20 |
EP1853819A2 (en) | 2007-11-14 |
CA2593698A1 (en) | 2006-07-20 |
MX2007008453A (en) | 2008-03-13 |
JP2008527238A (en) | 2008-07-24 |
TWI345611B (en) | 2011-07-21 |
WO2006076055A3 (en) | 2008-06-12 |
CN101389854A (en) | 2009-03-18 |
WO2006076055A2 (en) | 2006-07-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: AIR TURBINE TECHNOLOGY, INC., FLORIDA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:DODDS, KEMMA S.;REEL/FRAME:015685/0654 Effective date: 20050110 |
|
STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |