US20050150671A1 - Turbine motor for pneumatic tools - Google Patents
Turbine motor for pneumatic tools Download PDFInfo
- Publication number
- US20050150671A1 US20050150671A1 US10/829,586 US82958604A US2005150671A1 US 20050150671 A1 US20050150671 A1 US 20050150671A1 US 82958604 A US82958604 A US 82958604A US 2005150671 A1 US2005150671 A1 US 2005150671A1
- Authority
- US
- United States
- Prior art keywords
- rotor
- turbine motor
- pneumatic tool
- casing
- tool according
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25B—TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
- B25B21/00—Portable power-driven screw or nut setting or loosening tools; Attachments for drilling apparatus serving the same purpose
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01D15/06—Adaptations for driving, or combinations with, hand-held tools or the like control thereof
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
- F01D17/165—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
Definitions
- the present invention relates to a turbine motor for a pneumatic tool, particularly to a turbine motor which transforms pneumatic energy of air at high pressure into rotational energy, combining high power output of pneumatic tools and high efficiency with simple structure and compact design.
- Pneumatic tools like air levers generally are driven by turbines that transform pneumatic energy of air at high pressure into rotational energy.
- a turbine motor for an air lever with a regulating device has been disclosed in Taiwan patent no. 482075, mainly comprising a pneumatic tool main body a and an adjusting rod b.
- the pneumatic tool main body a further comprises: a tool case c; an air inlet controlling device d; a rotor e; and a motor body f.
- a chamber g lies inside the pneumatic tool main body a, with inlet and outlet tubes leading into the chamber g.
- the motor body f is fixed inside the chamber g. Compressed air is led into the chamber g, driving a rotational movement of the rotor e in the motor body f.
- a rotating head h is set on the rotor e and is used as a rotating tool.
- the motor body f has a valve i, which is an integral hollow body, and is placed in the chamber g.
- the valve i has forward and reverse flow grooves and on a lower side an inlet hole j.
- the adjusting rod b passes through the valve i. Longitudinal shifting of the adjusting rod b controls flow of air into the valve i by causing air to enter different forward and reverse flow grooves, allowing to control directions of the rotational movement of the rotating head h.
- U.S. publication no. 2003/0121680 has disclosed a turbine motor for an air lever with a regulating device, as taught in Taiwan patent no. 482075 cited above.
- the turbine motor is placed within the dash-dotted circle. Both publications describe similar turbine motors for use in pneumatic tools.
- a conventional turbine motor for pneumatic tools has an arrangement of the rotor and the flow grooves that makes it complicated to regulate airflow. Furthermore, air of high pressure entering the rotor from a perpendicular direction hits rotor blades at a certain angle, causing high material stress and reduced efficiency, therefore not allowing for operation under high load and at high speed.
- the present inventor has designed a turbine motor which, following physical laws of conservation of angular momentum and gas dynamics, offers higher effectivity, better efficiency and a simplified passage of air.
- the turbine motor for a pneumatic tool of the present invention comprises: a casing 10 ; a rotor 20 ; and an axis 30 , on which the rotor 20 is set.
- the casing 10 is a hollow body surrounding a chamber 11 and having a hole accommodating the axis 30 .
- An air inlet 12 and an air outlet 13 are attached to the casing 10 .
- the rotor 20 is placed in the chamber 11 , having an axis body and a plurality of rotor blades 21 . Compressed air entering the chamber 11 through the air inlet 12 drives a rotational movement of the rotor 20 .
- the axis 30 has a rear end borne by the casing 10 and a front end passing through the hole of the casing 10 , providing torque.
- Operation of the turbine motor for a pneumatic tool of the present invention is as follows: Compressed air enters the chamber 11 through the inlet 12 , flows towards the axis body of the axis 20 and hits the rotor blades 21 , exerting torque on the axis 30 . Since the direction of air flow leaves the rotor blades 21 of the rotor 20 exposed longer and more effective as compared to conventional art, higher output power and better efficiency are attained, making the present invention suitable for high speed and high load.
- a stator 40 is inserted between the rotor 20 and an inner wall of the casing 10 .
- the stator 40 has a plurality of stator blades 41 which surround the rotor blades 21 of the rotor 20 and are radially oriented, being placed opposite the inlet 12 . Compressed air entering the chamber 11 through the inlet 12 is deflected by the stator 40 to hit the rotor blades 21 uniformly, increasing efficiency.
- stator 40 for regulating forward and reverse directions of the rotating movement, two orientations of the stator blades 41 are adjustable.
- the stator 40 has a ring body with a plurality of blade supports 42 .
- the stator blades 41 are turnable on the blade supports 42 , allowing to control in which directions the rotor blades 21 are hit by compressed air, in particular, to regulate forward and reverse directions of the rotating movement.
- an air whirling device 70 is placed around the stator 40 , reducing turbulence.
- a shield 60 and an outlet passageway 61 placed in the chamber 11 along airflow to the stator 40 contribute to minimizing power loss.
- a multiple bearing 50 carries the axis 30 , so that the axis 30 and the rotor 20 are disposed within the shield 60 , without friction between the axis 30 and the shield 60 being generated, so that no power is wasted.
- the present invention in another embodiment has a rear casing 80 substituted for the shield 60 and the stator 40 , tightly surrounding the rotor 20 and the rotor blades 21 .
- a valve 90 allows to switch incoming airflow on and off.
- An air direction adjusting knob 91 moving either axially or in an angular direction and directing compressed air from the inlet 12 , allows to control forward and reverse directions of the rotational movement of the rotor 20 .
- the present invention as compared to conventional art, has the following effects:
- FIG. 1 is a sectional side view of the turbine motor for a pneumatic tool of the present invention.
- FIG. 2 is a sectional side view of the turbine motor for a pneumatic tool of the present invention in an embodiment with a stator.
- FIG. 3 is a sectional front view of the stator of the present invention.
- FIG. 4 is a sectional side view of the turbine motor for a pneumatic tool of the present invention in an embodiment with an air whirling device, a shield and an outlet passageway.
- FIGS. 5A and 5B are sectional views of the turbine motor for a pneumatic tool of the present invention in another embodiment.
- FIG. 6 (prior art) is a perspective view of a conventional turbine motor for a pneumatic tool.
- FIG. 7 (prior art) is a sectional side view of a conventional turbine motor for a pneumatic tool.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Actuator (AREA)
- Motor Or Generator Cooling System (AREA)
Abstract
A turbine motor for a pneumatic tool, comprising a casing, a rotor and an axis. Compressed air enters the casing through an inlet and is directed towards blades of the rotor in a radial direction, so that torque is exerted on the axis. The blades of the rotors are to a large part hit by compressed air, each for an extended time, so that high effectivity and good efficiency result, allowing for operation at high speed and under high load.
Description
- The present invention relates to a turbine motor for a pneumatic tool, particularly to a turbine motor which transforms pneumatic energy of air at high pressure into rotational energy, combining high power output of pneumatic tools and high efficiency with simple structure and compact design.
- Pneumatic tools like air levers generally are driven by turbines that transform pneumatic energy of air at high pressure into rotational energy.
- A turbine motor for an air lever with a regulating device, as shown in
FIG. 6 , has been disclosed in Taiwan patent no. 482075, mainly comprising a pneumatic tool main body a and an adjusting rod b. The pneumatic tool main body a further comprises: a tool case c; an air inlet controlling device d; a rotor e; and a motor body f. A chamber g lies inside the pneumatic tool main body a, with inlet and outlet tubes leading into the chamber g. The motor body f is fixed inside the chamber g. Compressed air is led into the chamber g, driving a rotational movement of the rotor e in the motor body f. A rotating head h is set on the rotor e and is used as a rotating tool. The motor body f has a valve i, which is an integral hollow body, and is placed in the chamber g. The valve i has forward and reverse flow grooves and on a lower side an inlet hole j. The adjusting rod b passes through the valve i. Longitudinal shifting of the adjusting rod b controls flow of air into the valve i by causing air to enter different forward and reverse flow grooves, allowing to control directions of the rotational movement of the rotating head h. - Referring to
FIG. 7 , U.S. publication no. 2003/0121680 has disclosed a turbine motor for an air lever with a regulating device, as taught in Taiwan patent no. 482075 cited above. InFIG. 7 , the turbine motor is placed within the dash-dotted circle. Both publications describe similar turbine motors for use in pneumatic tools. - A conventional turbine motor for pneumatic tools, as described above, has an arrangement of the rotor and the flow grooves that makes it complicated to regulate airflow. Furthermore, air of high pressure entering the rotor from a perpendicular direction hits rotor blades at a certain angle, causing high material stress and reduced efficiency, therefore not allowing for operation under high load and at high speed.
- Considering the shortcomings of conventional art, the present inventor has designed a turbine motor which, following physical laws of conservation of angular momentum and gas dynamics, offers higher effectivity, better efficiency and a simplified passage of air.
- It is the object of the present invention to provide a turbine motor for a pneumatic tool having a rotor hit by air in a radial direction, thus achieving high effectivity, good efficiency and a compact design.
- The present invention can be more fully understood by reference to the following description and accompanying drawings.
- As shown in
FIG. 1 , the turbine motor for a pneumatic tool of the present invention comprises: acasing 10; arotor 20; and anaxis 30, on which therotor 20 is set. Thecasing 10 is a hollow body surrounding achamber 11 and having a hole accommodating theaxis 30. Anair inlet 12 and anair outlet 13 are attached to thecasing 10. Therotor 20 is placed in thechamber 11, having an axis body and a plurality ofrotor blades 21. Compressed air entering thechamber 11 through theair inlet 12 drives a rotational movement of therotor 20. Theaxis 30 has a rear end borne by thecasing 10 and a front end passing through the hole of thecasing 10, providing torque. - Operation of the turbine motor for a pneumatic tool of the present invention is as follows: Compressed air enters the
chamber 11 through theinlet 12, flows towards the axis body of theaxis 20 and hits therotor blades 21, exerting torque on theaxis 30. Since the direction of air flow leaves therotor blades 21 of therotor 20 exposed longer and more effective as compared to conventional art, higher output power and better efficiency are attained, making the present invention suitable for high speed and high load. - Referring to
FIG. 2 , for more effective driving of therotor 20, astator 40 is inserted between therotor 20 and an inner wall of thecasing 10. Thestator 40 has a plurality ofstator blades 41 which surround therotor blades 21 of therotor 20 and are radially oriented, being placed opposite theinlet 12. Compressed air entering thechamber 11 through theinlet 12 is deflected by thestator 40 to hit therotor blades 21 uniformly, increasing efficiency. - Referring to
FIG. 3 , for regulating forward and reverse directions of the rotating movement, two orientations of thestator blades 41 are adjustable. Thestator 40 has a ring body with a plurality of blade supports 42. Thestator blades 41 are turnable on the blade supports 42, allowing to control in which directions therotor blades 21 are hit by compressed air, in particular, to regulate forward and reverse directions of the rotating movement. Thus a greatly simplified structure, as compared to conventional art, is achieved. - Referring to
FIG. 4 , for even higher power output of therotor 20, an air whirling device 70 is placed around thestator 40, reducing turbulence. Ashield 60 and anoutlet passageway 61 placed in thechamber 11 along airflow to thestator 40 contribute to minimizing power loss. - Furthermore, a multiple bearing 50 carries the
axis 30, so that theaxis 30 and therotor 20 are disposed within theshield 60, without friction between theaxis 30 and theshield 60 being generated, so that no power is wasted. - As shown in
FIGS. 5A and 5B , the present invention in another embodiment has arear casing 80 substituted for theshield 60 and thestator 40, tightly surrounding therotor 20 and therotor blades 21. Avalve 90 allows to switch incoming airflow on and off. An airdirection adjusting knob 91, moving either axially or in an angular direction and directing compressed air from theinlet 12, allows to control forward and reverse directions of the rotational movement of therotor 20. - As above explanation shows, the present invention, as compared to conventional art, has the following effects:
-
- 1. By guiding incoming compressed air onto the rotor blades in directions of rotation and having air hit the rotor blades at high speed, the rotor blades are exposed to compressed air for long time intervals and to a large part. In conventional art, rotor blades are hit by compressed air in a perpendicular direction, being exposed shorter times and to a minor part, so that a lower power output and lower speed than in the present invention are achieved.
- 2. By employing a stator with a variable angular position, the present invention allows to vary the direction of airflow, controlling forward and reverse directions of the rotational movement within a simple structure. Conventional art requires a penetrating, complicated structural part for controlling forward and reverse directions of the rotational movement.
- 3. The present invention has an air whirling device, directing compressed air to hit all of the rotor blades simultaneously, greatly increasing effectivity. Conventional art allows compressed air only to hit one rotor blade in a given time unit, obviously resulting in lower effectivity than the present invention.
- 4. Higher output power and greater effectivity make the present invention suitable for high speed and high load.
- While the invention has been described with reference to preferred embodiments thereof, it is to be understood that modifications or variations may be easily made without departing from the spirit of this invention which is defined by the appended claims.
-
FIG. 1 is a sectional side view of the turbine motor for a pneumatic tool of the present invention. -
FIG. 2 is a sectional side view of the turbine motor for a pneumatic tool of the present invention in an embodiment with a stator. -
FIG. 3 is a sectional front view of the stator of the present invention. -
FIG. 4 is a sectional side view of the turbine motor for a pneumatic tool of the present invention in an embodiment with an air whirling device, a shield and an outlet passageway. -
FIGS. 5A and 5B are sectional views of the turbine motor for a pneumatic tool of the present invention in another embodiment. -
FIG. 6 (prior art) is a perspective view of a conventional turbine motor for a pneumatic tool. -
FIG. 7 (prior art) is a sectional side view of a conventional turbine motor for a pneumatic tool.
Claims (14)
1. A turbine motor for a pneumatic tool, comprising:
a casing, surrounding a chamber, with an air inlet and an air outlet being attached to said casing;
a rotor, disposed inside said chamber, performing a rotational movement driven by compressed air from said air inlet; and
an axis, carrying said rotor, having a rear end borne by said casing and a front end passing through said casing, from which torque is taken.
2. The turbine motor for a pneumatic tool according to claim 1 , wherein a stator is inserted between said rotor and an inner wall of said casing.
3. The turbine motor for a pneumatic tool according to claim 2 , wherein said stator has a plurality of stator blades.
4. The turbine motor for a pneumatic tool according to claim 2 , wherein said stator is radially oriented and placed opposite said air inlet.
5. The turbine motor for a pneumatic tool according to claim 3 , wherein said stator is radially oriented and placed opposite said air inlet.
6. The turbine motor for a pneumatic tool according to claim 2 , wherein an air whirling device surrounds said stator.
7. The turbine motor for a pneumatic tool according to claim 1 , wherein in said chamber a shield and an outlet passageway are placed along airflow towards said stator.
8. The turbine motor for a pneumatic tool according to claim 1 , wherein said axis has a plurality of bearings, so that said axis and said rotor are borne inside said shield of said rotor.
9. The turbine motor for a pneumatic tool according to claim 7 , wherein said axis has a plurality of bearings, so that said axis and said rotor are borne inside said shield of said rotor.
10. A turbine motor for a pneumatic tool, comprising:
a casing, surrounding a chamber, with an air inlet and an air outlet air being attached to said casing;
a rotor, disposed inside said chamber, performing a rotational movement driven by compressed air from said air inlet;
an axis, carrying said rotor, having a rear end borne by said casing and a front end passing through said casing, from which torque is taken;
a rear casing, placed at a rear end of said casing, closely surrounding said rotor and blades thereof; and
an air direction adjusting knob, placed close to said air inlet and allowing, by an axial or an angular movement, to switch directing of incoming compressed air onto said rotor between forward and reverse directions.
11. The turbine motor for a pneumatic tool according to claim 10 , wherein a valve is installed at said air inlet, allowing to switch incoming airflow on and off.
12. The turbine motor for a pneumatic tool according to claim 3 , wherein said plurality of stator blades have adjustable orientations.
13. The turbine motor for a pneumatic tool according to claim 3 , wherein said plurality of stator blades are turnably set on a plurality of blade supports.
14. The turbine motor for a pneumatic tool according to claim 12 , wherein said plurality of stator blades are turnably set on a plurality of blade supports.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
TW093100481 | 2004-01-08 | ||
TW093100481A TWI283199B (en) | 2004-01-08 | 2004-01-08 | A turbine motor of an air tool |
Publications (1)
Publication Number | Publication Date |
---|---|
US20050150671A1 true US20050150671A1 (en) | 2005-07-14 |
Family
ID=32592257
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US10/829,586 Abandoned US20050150671A1 (en) | 2004-01-08 | 2004-04-21 | Turbine motor for pneumatic tools |
Country Status (3)
Country | Link |
---|---|
US (1) | US20050150671A1 (en) |
DE (1) | DE202004005998U1 (en) |
TW (1) | TWI283199B (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20090017737A1 (en) * | 2004-12-03 | 2009-01-15 | Juergen Hesse | Flow medium-driven hand-held power tool |
US20090152319A1 (en) * | 2007-12-12 | 2009-06-18 | Cooper Brands, Inc. | Pneumatic tool design |
US20150273679A1 (en) * | 2014-03-27 | 2015-10-01 | Basso Industry Corp. | Pneumatic tool |
US11685036B2 (en) | 2020-07-27 | 2023-06-27 | Techtronic Cordless Gp | Motor mounting assembly for a power tool |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2617527A1 (en) * | 2012-01-19 | 2013-07-24 | Bülent Sentürk | Pneumatic torque wrench |
DE102013222111A1 (en) * | 2013-10-30 | 2015-04-30 | Henkel Ag & Co. Kgaa | Dynamic mixing device |
Citations (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3556230A (en) * | 1969-01-13 | 1971-01-19 | Earl G Roggenburk | Rotary impact tool |
US3734515A (en) * | 1971-01-29 | 1973-05-22 | Thor Power Tool Co | Power wrench with interchangeable adapters |
US3880245A (en) * | 1973-11-21 | 1975-04-29 | Chicago Pneumatic Tool Co | Exhaust noise attenuating system with muffler for pneumatic tools |
US3988076A (en) * | 1974-01-30 | 1976-10-26 | Robert Bosch G.M.B.H. | Rotary vane machine with spring-biased vanes |
US4326846A (en) * | 1977-04-01 | 1982-04-27 | Kabushiki Kaisha Morita Seisakusho | Dental handpiece |
US4380270A (en) * | 1981-01-23 | 1983-04-19 | Allan Air Products, Inc. | Tool device |
US4589161A (en) * | 1984-08-10 | 1986-05-20 | The Scott & Fetzer Company | Vacuum driven tool |
US5083619A (en) * | 1989-09-25 | 1992-01-28 | Chicago Pneumatic Tool Company | Powered impact wrench |
US5277769A (en) * | 1991-11-27 | 1994-01-11 | The United States Of America As Represented By The Department Of Energy | Electrochemical thinning of silicon |
US5525097A (en) * | 1994-08-09 | 1996-06-11 | Uht Corporation | Air motor |
US5562446A (en) * | 1994-02-10 | 1996-10-08 | J. Morita Mfg. Corp. | Small handpiece with fluid driven turbine |
US5632578A (en) * | 1996-02-23 | 1997-05-27 | Ryobi North America | Exhaust stator and fan for a power tool |
US5902108A (en) * | 1997-02-25 | 1999-05-11 | J. Morita Manufacturing Corporation | Air turbine handpiece |
US6273718B1 (en) * | 1999-05-05 | 2001-08-14 | M & H DENTALWERK BüRMOOS GMBH | Dental handpiece |
US6796386B2 (en) * | 2000-09-08 | 2004-09-28 | S.P. Air Kabusiki Kaisha | Pneumatic rotary tool |
-
2004
- 2004-01-08 TW TW093100481A patent/TWI283199B/en not_active IP Right Cessation
- 2004-04-16 DE DE202004005998U patent/DE202004005998U1/en not_active Expired - Lifetime
- 2004-04-21 US US10/829,586 patent/US20050150671A1/en not_active Abandoned
Patent Citations (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3556230A (en) * | 1969-01-13 | 1971-01-19 | Earl G Roggenburk | Rotary impact tool |
US3734515A (en) * | 1971-01-29 | 1973-05-22 | Thor Power Tool Co | Power wrench with interchangeable adapters |
US3880245A (en) * | 1973-11-21 | 1975-04-29 | Chicago Pneumatic Tool Co | Exhaust noise attenuating system with muffler for pneumatic tools |
US3988076A (en) * | 1974-01-30 | 1976-10-26 | Robert Bosch G.M.B.H. | Rotary vane machine with spring-biased vanes |
US4326846A (en) * | 1977-04-01 | 1982-04-27 | Kabushiki Kaisha Morita Seisakusho | Dental handpiece |
US4380270A (en) * | 1981-01-23 | 1983-04-19 | Allan Air Products, Inc. | Tool device |
US4589161A (en) * | 1984-08-10 | 1986-05-20 | The Scott & Fetzer Company | Vacuum driven tool |
US5083619A (en) * | 1989-09-25 | 1992-01-28 | Chicago Pneumatic Tool Company | Powered impact wrench |
US5277769A (en) * | 1991-11-27 | 1994-01-11 | The United States Of America As Represented By The Department Of Energy | Electrochemical thinning of silicon |
US5562446A (en) * | 1994-02-10 | 1996-10-08 | J. Morita Mfg. Corp. | Small handpiece with fluid driven turbine |
US5525097A (en) * | 1994-08-09 | 1996-06-11 | Uht Corporation | Air motor |
US5632578A (en) * | 1996-02-23 | 1997-05-27 | Ryobi North America | Exhaust stator and fan for a power tool |
US5902108A (en) * | 1997-02-25 | 1999-05-11 | J. Morita Manufacturing Corporation | Air turbine handpiece |
US6273718B1 (en) * | 1999-05-05 | 2001-08-14 | M & H DENTALWERK BüRMOOS GMBH | Dental handpiece |
US6796386B2 (en) * | 2000-09-08 | 2004-09-28 | S.P. Air Kabusiki Kaisha | Pneumatic rotary tool |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20090017737A1 (en) * | 2004-12-03 | 2009-01-15 | Juergen Hesse | Flow medium-driven hand-held power tool |
US20090152319A1 (en) * | 2007-12-12 | 2009-06-18 | Cooper Brands, Inc. | Pneumatic tool design |
US20150273679A1 (en) * | 2014-03-27 | 2015-10-01 | Basso Industry Corp. | Pneumatic tool |
US11685036B2 (en) | 2020-07-27 | 2023-06-27 | Techtronic Cordless Gp | Motor mounting assembly for a power tool |
Also Published As
Publication number | Publication date |
---|---|
DE202004005998U1 (en) | 2004-06-09 |
TW200523076A (en) | 2005-07-16 |
TWI283199B (en) | 2007-07-01 |
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Legal Events
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AS | Assignment |
Owner name: INDUSTRIAL TECHNOLOGY RESEARCH INSTITUTE, TAIWAN Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:KUO, CHIL-RON;WU, JIA-RUEY;CHANG, CHIA-YANG;AND OTHERS;REEL/FRAME:015260/0340 Effective date: 20040212 |
|
STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |