Blower wheel and power tool with an internal combustion engine and a blower wheel
11268534 · 2022-03-08
Assignee
Inventors
- Andreas Wolf (Leutenbach, DE)
- Wolfgang Weissert (Winnenden, DE)
- Volker Lempges (Eschfeld, DE)
- Helmut Zimmermann (Berglen, DE)
- Günter Wolf (Oppenweiler, DE)
- Holger Vollmer (Hilzingen, DE)
- Marcel Förster (Schwaikheim, DE)
- Ute Dawin (Waiblingen, DE)
- Jonas Lank (Winnenden, DE)
Cpc classification
H02K7/1815
ELECTRICITY
F04D29/281
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/441
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01P1/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/668
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/662
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
H02K21/22
ELECTRICITY
F16F15/315
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D25/084
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B63/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/023
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2260/43
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/624
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F04D29/28
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/66
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/44
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
H02K7/18
ELECTRICITY
H02K21/22
ELECTRICITY
F01P1/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B63/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A blower wheel is provided with a base member having an axis of rotation and with a rotor of a generator, wherein the rotor is fixedly secured on the blower wheel. At least one magnet is arranged on the rotor. An inertia ring is fixedly secured on the base member at a spacing to the at least one magnet. The inertia ring is made of a first material having a first density and the base member is made of a second material having a second density. The first density is greater than the second density. An internal combustion engine is provided with such a blower wheel.
Claims
1. A blower wheel comprising: a base member having an axis of rotation; a rotor of a generator, wherein the rotor is fixedly secured on the blower wheel; at least one magnet arranged on the rotor; an inertia ring fixedly secured on the base member at a spacing to the at least one magnet; wherein the inertia ring is made of a first material having a first density and wherein the base member is made of a second material having a second density; wherein the first density is greater than the second density.
2. The blower wheel according to claim 1, wherein the inertia ring comprises at least one section in which a thickness of the inertia ring measured in a direction of the axis of rotation decreases in a radial outward direction relative to the axis of rotation.
3. The blower wheel according to claim 1, wherein the inertia ring is attached by an adhesive to the base member.
4. The blower wheel according to claim 1, wherein the rotor is fixedly secured on the base member of the blower wheel.
5. The blower wheel according to claim 1, wherein the inertia ring is a closed continuous ring extending concentrically about the axis of rotation of the base member.
6. The blower wheel according to claim 1, further comprising a metallic magnetic return ring configured to reinforce a magnetic flux of the at least one magnet.
7. The blower wheel according to claim 6, wherein the inertia ring is arranged radially outside of the metallic magnetic return ring in a radial direction relative to the axis of rotation.
8. The blower wheel according to claim 1, wherein the base member comprises an annular wall arranged on one side of the base member, wherein the annular wall extends in an annular shape about the axis of rotation, and wherein the at least one magnet is arranged radially inside the annular wall in a radial direction relative to the axis of rotation.
9. The blower wheel according to claim 8, wherein the inertia ring is arranged outside of the annular wall in the radial direction.
10. The blower wheel according to claim 1, wherein the base member comprises a first side and a second side, wherein the first side and the second side face in opposite axial directions relative to the axis of rotation, and further comprises flow guiding elements that are arranged on the second side of the base member.
11. The blower wheel according to claim 10, wherein the inertia ring is arranged on the first side of the base member.
12. The blower wheel according to claim 10, wherein the flow guiding elements are arranged in a circular ring area of the base member, wherein the circular ring area has a center point positioned on the axis of rotation, wherein an inner radius of the circular ring area corresponds to at most 0.5 times an outer radius of the base member, wherein an outer radius of the circular ring area corresponds to at least 0.9 times the outer radius of the base member.
13. A blower wheel comprising: a base member having an axis of rotation; a rotor of a generator, wherein the rotor is fixedly secured on the blower wheel; at least one magnet arranged on the rotor; an inertia ring fixedly secured on the base member at a spacing to the at least one magnet; wherein the inertia ring is made of a first material having a first density and wherein the base member is made of a second material having a second density; wherein the first density is greater than the second density; wherein the base member comprises a first side and a second side, wherein the first side and the second side face in opposite axial directions relative to the axis of rotation, and further comprises flow guiding elements that are arranged on the second side of the base member; wherein the base member has an imaginary terminal plane positioned perpendicular to the axis of rotation, wherein the imaginary terminal plane is arranged on the first side of the base member, wherein the imaginary terminal plane extends through an outermost boundary of the base member provided in the axial direction, wherein the base member on the second side of the base member comprises a flow guiding surface, and wherein a first measured spacing of the flow guiding surface, measured relative to the imaginary terminal plane, increases as a second measured spacing of the flow guiding surface, measured in a radial direction relative to the axis of rotation, decreases.
14. The blower wheel according to claim 13, wherein the rotor is fixedly secured on the base member of the blower wheel.
15. The blower wheel according to claim 13, wherein the inertia ring is a closed continuous ring extending concentrically about the axis of rotation of the base member.
16. The blower wheel according to claim 13, wherein, on a side of the inertia ring that is facing the flow guiding surface, a contour of the inertia ring follows a contour of the flow guiding surface.
17. The blower wheel according to claim 13, wherein, between the first side and the second side of the base member, a separating wall is arranged and wherein the inertia ring is arranged adjacent to the separating wall.
18. The blower wheel according to claim 17, wherein the flow guiding surface is formed at least partially by the separating wall of the base member.
19. The blower wheel according to claim 17, wherein a contour of the separating wall on the first side of the base member follows a contour of the flow guiding surface on the second side of the base member.
20. A power tool comprising: an internal combustion engine; a blower wheel comprising: a base member having an axis of rotation; a rotor of a generator, wherein the rotor is fixedly secured on the blower wheel; at least one magnet arranged on the rotor; an inertia ring fixedly secured on the base member at a spacing to the at least one magnet, wherein the inertia ring is made of a first material having a first density and the base member is made of a second material having a second density, wherein the first density is greater than the second density.
21. The power tool according to claim 20, wherein the rotor is fixedly secured on the base member of the blower wheel.
22. The power tool according to claim 20, wherein the inertia ring is a closed continuous ring extending concentrically about the axis of rotation of the base member.
Description
BRIEF DESCRIPTION OF THE DRAWING
(1)
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DESCRIPTION OF THE PREFERRED EMBODIMENTS
(15)
(16) The motor chainsaw comprises a motor housing 36 on which a guide bar 68 is secured. A saw chain 69 is guided in circulation about the guide bar 68. In the motor housing 36, an internal combustion engine 19 is arranged which is indicated in
(17) For guiding the motor chainsaw, there is also a grip 66 provided that is extending across the motor housing 36 of the motor chainsaw. The motor chainsaw comprises a hand guard 67 which is extending on the side of the grip 66 facing the guide bar 68. The hand guard 67 serves advantageously for triggering a braking device, not illustrated in the embodiment.
(18)
(19) A blower wheel 1 is provided that rotates together with the crankshaft 27 and is secured fixedly on the crankshaft 27. For fixation of the blower wheel 1, a fixation nut 31 is provided which is screwed onto one end of the crankshaft 27 and secures thereby the blower wheel 1 axially on the crankshaft 27. The blower wheel 1 serves for conveying cooling air to the internal combustion engine 19. The blower wheel 1 serves at the same time as a flywheel. Moreover, the blower wheel 1 comprises a rotor 3 of a generator 4.
(20) The blower wheel 1 comprises a base member 2. The base member 2 of the blower wheel 1 comprises a first side 9 illustrated in
(21) The internal combustion engine 19 comprises a crankcase 48 in which the crankshaft 27 is rotatably supported. On the crankcase 48 a stator 20 of the generator 4 is fixedly secured. The stator 20 comprises at least one coil 63. The blower wheel 1 engages across the circumference of the stator 20 so that the stator 20 is positioned in radial direction inside the rotor 3. Upon rotation of the blower wheel 1 about the axis of rotation 100, the magnets 5 of the rotor 3 induce voltage in the coil 63 of the stator 20.
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(24) The inertia ring 6 is embodied separate from the magnetic return ring 7. In a section plane perpendicular to the axis of rotation 100, the inertia ring 6 is of a circular ring shape. The density of the material of the inertia ring 6 is greater than the density of the material of the base member 2 of the blower wheel 1. The base member 2 is comprised advantageously of lightweight construction material, in particular lightweight metal such as aluminum or magnesium, or of plastic material. In the embodiments, the base member 2 is comprised of magnesium. The inertia ring 6 is comprised advantageously of steel. Other materials for the inertia ring 6 can be selected, for example, die-cast zinc, copper, ceramic material, titanium or the like. The inertia ring 6 can be comprised of metallic or non-metallic materials. The density of the material of the inertia ring 6 amounts advantageously to at least two times, in particular at least three times, preferably at least four times, the density of the material of the base member 2.
(25) The magnets 5 of the magnetic return ring 7 are preferably arranged, uniformly spaced from each other, on the inner circumferential edge of the magnetic return ring 7. As a whole, twelve magnets 5 are provided. The magnets 5 and the magnetic return ring 7 form together the rotor 3 of the generator 4 illustrated in
(26) The second side 10 of the base member 2 is facing away from the inertia ring 6 and the magnetic return ring 7. In the area of the axis of rotation 100, a receptacle 55 is formed preferably on the second side 10 of the base member 2. The receptacle 55 is a substantially of a hollow-cylindrical shape. The receptacle 55 serves in the embodiment for receiving a follower 46, illustrated in
(27) On the second side 10 of the base member 10, flow guiding elements 11 are arranged. As a whole, fifteen flow guiding elements 11 are uniformly arranged relative to each other at uniform angular spacings relative to the axis of rotation 100 on the second side 10 of the base member 2. The flow guiding elements 11 extend in radial direction outside of the outer wall 21. The flow guiding elements 11 are of a vane-shape design. They extend substantially radially relative to the axis of rotation 100. The flow guiding elements 11 are attached to a flow guiding surface 12 of the blower wheel 1. The flow guiding elements 11 generate a cooling air flow for the internal combustion engine 19 in operation upon rotation of the blower wheel 1.
(28)
(29) The base member 2 comprises a partition or separating wall 14 between its first side 9 and its second side 10. The separating wall 14 comprises on the first side 9 of the base member 2 a first face 38. The first face 38 of the separating wall 14 in the assembled state of the blower wheel 1 is facing the inertia ring 6. The first face 38 of the separating wall 14 forms the bottom of the receptacle 51 for the inertia ring 6 in the base member 2.
(30) The base member 2 of the blower wheel 1 comprises preferably an annular wall 8. The annular wall 8 extends annularly about the axis of rotation 100. The annular wall 8 is positioned in radial direction within the outer wall 15. In the assembled state of the blower wheel 1, the annular wall 8 is positioned between the inertia ring 6 and the magnetic return ring 7. The annular wall 8 is positioned in the assembled state of the blower wheel 1 between the inertia ring and the fastening ring 32.
(31) The annular wall 8 comprises a radial outwardly positioned side 70. The outwardly positioned side 70 of the annular wall 8 extends in axial direction of the axis of rotation 100 and in a circular shape so as to surround the axis of rotation 100. The outwardly positioned side 70 of the annular wall 8 delimits the receptacle 51 for the inertia ring 6. The outwardly positioned side 70 of the annular wall 8 extends in the embodiment parallel to an inwardly positioned flank 53 of the outer wall 15. Between the outwardly positioned side 70 of the annular wall 8 and the inwardly positioned flank 53 of the outer wall 15 the first face 38 of the separating wall 14 is extending. The receptacle 51 for the inertia ring 6 is delimited by the inwardly positioned flank 53 of the outer wall 15, the first face 38 of the separating wall 14, and the outwardly positioned side 70 of the annular wall 8.
(32) The annular wall 8 comprises a radial inwardly positioned side 72. The radial inwardly positioned side 72 of the annular wall 8 extends preferably parallel to the radial outwardly positioned side 70 of the annular wall. The radial inwardly positioned side 72 is positioned radially within the outwardly positioned side 70. In the assembled state of the blower wheel 1, the fastening ring 32 is contacting (rests on) the radial inwardly positioned side 72 of the annular wall 8.
(33) In radial direction inwardly relative to the radial inwardly positioned side 72 of the annular wall 8, a projection 73 of the base member 2 adjoins the radial inwardly positioned side 72. The projection 73 extends in a circular ring shape about the axis of rotation 100 in a plane which is oriented substantially perpendicular to the axis of rotation 102 and to the annular wall 8. In the assembled state of the blower wheel 1, the magnetic return ring 7 is contacting (rests on) the projection 73. In the assembled state of the blower wheel 1, the fastening ring 32 is contacting (rests on) the projection 73.
(34) The projection 73 comprises in the embodiment several first positioning members 40 for positioning the magnetic return ring 7 in the base member 2. The first positioning member 40 in the embodiment is designed as a recess in the projection 73. The recess which forms the first positioning member 40 extends substantially in the direction of the axis of rotation 100. On the magnetic return ring 7 several second positioning members 47 are formed in correspondence with the first positioning members 40. In the embodiment according to
(35) In the area of the axis of rotation 100, the base member 2 of the blower wheel 1 has a hub 34. The hub 34 comprises in the embodiment a conical fastening opening 28 which completely penetrates the base member 2 in the direction of the axis of rotation 100. Another, in particular a round, configuration of the fastening opening 28 can however be advantageous also. Also, a form-fit connection, in particular by means of a feather key, can be advantageous.
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(38) The inertia ring 6 comprises an inner radius rit. The inner radius rit of the inertia ring 6 amounts advantageously to at least 0.6 times the outer radius rag of the base member 2. In the embodiment according to
(39) The inertia ring 6 is arranged adjacent to the first face 38, illustrated in
(40) As illustrated in
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(43) The inertia ring 6 is fixedly secured at a spacing d relative to the magnet 5 on the base member 2 of the blower wheel 1. The spacing d is measured perpendicular to the axis of rotation 100. The spacing d amounts advantageously to at least 0.5 mm, in particular at least 1 mm. The magnet 5 is arranged radially within the annular wall 8. The magnet 5 is arranged radially within the magnetic return ring 7.
(44) The base member 2 of the blower wheel 1 comprises an imaginary terminal plane E. The imaginary terminal plane E is illustrated in
(45) In the embodiment, the spacing B2 of the flow guiding surface 12 relative to the axis of rotation 100 is greater than the spacing B1. The spacing a1 is greater than the spacing a2. The spacing a1, a2 of the flow guiding surface 12 relative to the terminal plane E increases with decreasing spacing B1, B2. The father outwardly a point is positioned in the radial direction on the flow guiding surface 12, the closer it is to the terminal plane E, i.e., the closer it is to the crankcase 48 of the internal combustion 19 on which the blower wheel 1 is secured. The flow guiding surface 12 is slanted in radial direction outwardly in the direction of the crankcase 48.
(46) As can be seen in
(47) The separating wall 14 comprises a second face 39. The second face 39 of the separating wall 14 is facing away from the inertia ring 6 and from the magnetic return ring 7. The flow guiding surface 12 is formed at least partially by the second face 39 of the separating wall 14 of the base member 2. The flow guiding surface 12 is at least partially formed by the separating wall 14 of the base member 2. The separating wall 14 extends circumferentially about axis of rotation 100 between the annular wall 8 and the outer wall 15 of the base member 2. On the second side 10 of the base member 2 where the separating wall 14 is part of the flow guiding surface 12, the flow guiding elements 11 are arranged on the separating wall 14. The separating wall 14 has a thickness t measured in the direction of the axis of rotation 100. The thickness t of the separating wall 14 is constant in the embodiment. The first face 38 of the separating wall 14 extends at least partially parallel to the second face 39 of the separating wall 14. The flow guiding surface 12 extends on the second face 39 of the separating wall 14. A contour of the separating wall 14 on the first side 9 of the base member 2 follows a contour of the flow guiding surface 12 on the second side 10 of the base member 2.
(48) The first face 38 of the separating wall 14 forms the bottom for the receptacle 51 in the base member 2. The receptacle 51 serves for receiving the inertia ring 6. The inertia ring 6 is arranged on the bottom of the receptacle 51 or arranged to rest on knobs 41 (
(49) The inertia ring 6 comprises first side face 74. The first side face 74 is facing away from the base member 2. The first side face 74 in the embodiment is of a planar configuration and is positioned approximately in a plane which is substantially perpendicular to the axis of rotation 100.
(50) The inertia ring 6 comprises a thickness s1 measured in the direction of the axis of rotation 100. The thickness s1 is measured at the outer radius rat of the inertia ring 6. The inertia ring 6 comprises a thickness s2 measured in the direction of the axis of rotation 100. The thickness s2 is measured at the inner radius rit of the inertia ring 6. The thickness s1 of the inertia ring 6 relative to the axis of rotation 100 is preferably positioned radially farther outwardly, i.e., measured at a greater radial distance to the axis of rotation 100 than the thickness s2. The thickness s1 is smaller than the thickness s2. The inertia ring 6 comprises at least one section in which the thickness s1, s2 of the inertia ring 6 that is measured in the direction of the axis of rotation 100 decreases in radial direction outwardly. The thickness of the inertia ring 6 decreases advantageously continuously from the inner radius rit toward the outer radius rat. The thickness s1 of the inertia ring 6 at the outer radius rat of the inertia ring 6 is advantageously approximately 60% to approximately 80%, in particular approximately 70%, of the thickness s2 at the inner radius rit of the inertia ring 6.
(51) The side face 16 of the inertia ring 6 extends conically. As is shown in
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(53) The first face 38 of the separating wall 14 in the embodiment is slanted relative to the annular wall 8 at an angle α that is smaller than 90°. The angle α in this context is measured relative to the outwardly positioned side 70 of the annular wall 8 in a section plane that contains the axis of rotation 100. The angle α advantageously amounts to 50° to 85°, in particular 60° to 80°. The outwardly positioned side 70 of the annular wall 8 extends advantageously parallel to the axis of rotation 100.
(54) The first face 38 of the separating wall 14 is slanted relative to the axis of rotation 100 at an angle β that is smaller than 90°. In this context, the angle β is measured in a section plane which contains the axis of rotation 100. The angle β advantageously amounts to 50° to 85°, in particular 60° to 80°. Advantageously, the angles α and β are identical.
(55) The contour of the side of the inertia ring 6 which is facing the separating wall 14 follows the contour of the first face 38 of the separating wall 14. In this way, an approximately triangular, outwardly narrowing cross-section of the inertia ring 6 is created.
(56)
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(58) The receptacle 55 of the base member 2 of the blower wheel 1 is substantially hollow-cylindrical. In the assembled state, the longitudinal cylinder axis coincides with the axis of rotation 100. The receptacle 55 comprises a sidewall 60. The inner surface of the sidewall 60 of the receptacle 55 which is positioned opposite the outer circumferential surface of the hollow cylinder of the receptacle 55 comprises preferably a cam contour 54. In the outwardly pivoted state, the pawls 43 engage the cam contour 54. In this way, a rotationally fixed coupling of the follower 46 with the base member 2 and the blower wheel 1 and thus with the crankshaft 27 of the internal combustion engine 19 illustrated in
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(61) The specification incorporates by reference the entire disclosure of German priority document 10 2015 016 482.1 having a filing date of Dec. 15, 2015.
(62) While specific embodiments of the invention have been shown and described in detail to illustrate the inventive principles, it will be understood that the invention may be embodied otherwise without departing from such principles.