Actuator with open-loop control direct drive
11852055 · 2023-12-26
Assignee
Inventors
- Antoine Foucaut (Montarlot lès Rioz, FR)
- Pierre Gemberlé (Biel/Bienn, CH)
- Antoine Bourgade (Biel/Bienne, CH)
Cpc classification
F01L2009/2107
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L2009/213
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L2820/041
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L9/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
H02K7/12
ELECTRICITY
F01L1/047
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L2820/032
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L2009/25
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L9/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F01L9/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L1/047
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L9/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
Travel of a brushless rotary actuator is limited by two stops, including a wound stator and a magnetic cylindrical rotor rigidly attached to a shaft having a first end rigidly attached to a control member. A second end of the shaft is rigidly attached to a travel limiting part acting as stops, and the travel limiting part has bending, resilient beam shapes. The actuator is electrically controlled in an open-loop. A control system controls a lift value of valves of an internal combustion engine by a lever driven by such an actuator.
Claims
1. A brushless rotary actuator comprising: two stops; a wound stator; a magnetic cylindrical rotor; a shaft rigidly attached to the rotor, the shaft having a first end and a second end; a control member rigidly attached to the first end of the shaft, wherein the control member has a resilient beam configured to damp movement when the rotor reaches an end of travel position; and a travel limiter rigidly attached to the second end of the shaft, wherein the travel limiter has one or more resilient beams configured to elastically bend when the travel limiter comes into contact with the two stops; wherein the actuator is configured to be electrically controlled in an open-loop.
2. The brushless rotary actuator according to clean 1, wherein the one or more resilient beams of the travel limiter and the control member are made of a material with a ratio between a breaking stress and a modulus of elasticity greater than 0.020 and a Charpy notched impact strength greater than 20 kJ/m.sup.2.
3. The brushless rotary actuator according to claim 2, wherein one or both of the travel limiter and the control member comprise an unfilled thermoplastic material.
4. The brushless rotary actuator according to claim 1, wherein the one or more resilient beams of the travel limiter are symmetrical to allow identical damping from one end of travel to the other.
5. The brushless rotary actuator according to claim 1, further comprising a mechanical spring configured to return the rotor to a predefined position.
6. The brushless rotary actuator according to a claim 1, wherein the travel limiter includes: at least two engaging pads configured to engage with the rotor; at least two travel limiting pads movable between the two stops; an anchor configured to receive a spiral end of a spring; and a centering element of the travel limiter with respect to the shaft; wherein at least one of the one or more resilient beams of the travel limiter connect an engaging pad of the at least two engaging pads to a travel limiting pad of the at least two travel limiting pads.
7. The brushless rotary actuator according to claim 6, wherein each of the at least two engaging pads extends perpendicular to a radial arm.
8. The brushless rotary actuator according to claim 7, wherein the radial arm extends to an intermediate annular zone, and is connected by radially extending hairpin bridges.
9. The brushless rotary actuator according to claim 8, wherein the radial arm and the hairpin bridges extend in a first transverse plane, offset with respect to a second plane corresponding to the centering element formed of arms connecting an annular central zone for passage of the shaft, the arms being connected to a junction point between the radial arm and one of the hairpin bridges.
10. The brushless rotary actuator according to claim 9, further comprising an annular magnet in an interior zone between the shaft and the junction point between the radial arm and one of the hairpin bridges.
11. The brushless rotary actuator according to claim 6, wherein each of the at least two travel limiting pads extends perpendicular to a radial arm, in a direction opposite to a direction of the at least two engaging pads.
12. The brushless rotary actuator according to claim 11, wherein each of the at least two travel limiting pads extends perpendicular to an elastically deformable radial arm.
13. The brushless rotary actuator according to claim 12, wherein the elastically deformable radial arm comprises a bracket split by a radial slot.
14. The brushless rotary actuator according to claim 1, wherein the control member is in a form of a coupling fork.
15. The brushless rotary actuator according to claim 1, wherein the first end of the shaft has a knurled configuration for receiving a ring, and a thermoplastic part being overmolded onto the ring to form the control member.
16. The brushless rotary actuator according to claim 1, further comprising a position sensor designed to provide feedback on a position of the rotor in order to determine a state of actuation.
17. A brushless rotary actuator comprising: an actuator housing; a cover configured to cooperate with the actuator, the cover comprising a stop; a shaft having a first end and a second end; a stator surrounding at least a portion of the shaft; a rotor attached to the shaft proximate to the second end of the shaft; and a travel limiter proximate to the rotor, the travel limiter comprising: a central portion; a first arm extending radially away from the central portion; a first engaging pad extending in a first axial direction perpendicularly from an end of the first arm; a second arm extending radially away from the central portion in a direction opposite the first arm; a second engaging pad extending in the first axial direction perpendicularly from an end of the second arm; a first pair of curved bridges extending from the central portion, the first pair of curved bridges connecting the first arm to the central portion; a second pair of curved bridges extending from the central portion, the first pair of curved bridges connecting the second arm to the central portion; a third arm extending radially away from the central portion; a first travel limiting pad extending in a second axial direction perpendicularly from an end of the third arm, the second axial direction opposite the first axial direction; a fourth arm extending radially away from the central portion; and a second travel limiting pad extending in the second axial direction perpendicularly from an end of the fourth arm; wherein the first engaging pad and the second engaging pad are configured to engage with the rotor; and wherein the first pair of curved bridges and the second pair of curved bridges are configured to elastically deform when one or more of the first travel limiting pad and the second travel limiting pad contact the stop of the cover.
18. The rotary actuator of claim 17, further comprising a return spring configured to engage with the travel limiter.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The present invention will be better understood upon reading the detailed description of a non-limiting embodiment of the invention which follows, referring to the accompanying drawings in which:
(2)
(3)
(4)
(5)
(6)
DETAILED DESCRIPTION
(7)
(8) This shaft (7) drives, at its first end, a control member (9), the details of which are shown in
(9) The actuator comprises, in a known manner, a stator formed by a base plate (13) comprising a plate stack of ferromagnetic sheets in which the pole pieces (14, 15) are driven in the form of cylinder portions, each surrounded by a coil (16, 17) of electric wires. In the center of the stator, the actuator has a tube (19) in the central position, which surrounds the shaft (7) and supports at its rear end an axial ball bearing (20) supporting the rotor (21) having, in a known manner, a ferromagnetic yoke carrying permanent magnets used for actuation in combination with the action of the coils (16, 17). This assembly causes the angular displacement of the rotor (21) in a first direction when the wound stator is supplied with electric current. A spring (22) ensures the angular displacement (the return) of the rotor (21) in an opposite angular direction, until it returns to an original position.
(10) A travel limiting part (23) rigidly attached to the rotor (21), and positioned at the second end of the shaft (7), limits its movement between a rest position controlled by the spring (22), and a working position controlled by the current supply of the stator. An annular permanent magnet (24) rigidly attached to the rotor (21) provides a magnetic field detected by a magnetosensitive probe (25) positioned in the extension of the shaft (7). This magnetosensitive probe (25) is mounted on a printed circuit board (26) fixed on the cover (2). It is specified that the position sensor formed by the annular magnet (24) and the magnetosensitive probe (25) is used in order to roughly determine the position of the rotor (for example, to know whether or not the rotor has performed the movement) but that it is not used for closed-loop control of the actuator.
(11)
(12) In
Detailed Description of the Travel Limiting Part
(13) The travel limiting part (23) consists of an injected plastic part as can be observed in
(14) These arms (44, 45) do not join the center of the part (23) but extend from an end corresponding to the radius of the rotor (21) to an intermediate radius (46, 47). Similarly, the arms (32, 33) do not join the center of the part (23) but extend from an end corresponding to the radius of the rotor (21) to an intermediate radius (48, 49). The rear end of an arm (44, 45) supporting the engaging pad (42, 43) is connected to the rear end of an adjacent arm (32, 33) supporting the travel limiting pad (30, 31) by a bridge (50, 51, 52, 53) in the form of a pin (50 to 53).
(15) These bridges (50, 51, 52, 53) extend radially and define a curved end extended by two arms separated by a radial slot (54 to 57). This slot (54 to 57) widens slightly on the side of the angularly closest limiting pad. These bridges (50, 51, 52, 53) forming bending, mechanical beams, thus offer viscoelastic deformation making it possible to absorb the impact and dissipate its energy when the travel limiting pads (30, 31) come into contact with the stop (34, 35 or 36, 37). Preferably, by the combination of the damping properties accumulated between this travel limiting part (23) and the control member (9), the viability and the service life of the actuator in the application are considerably increased.
(16) Inside this part (23) is a configuration having a central passage (58) defined by four split arms (59 to 62) connected to the junction region between a bridge (50, 51, 52, 53) and an arm (32, 33, 44, 45). This configuration is in a plane offset axially with respect to the plane defined by the bridges (50, 51, 52, 53) and the arms (32, 33, 44, 45). To allow optimal adjustment of the spring preload, the stop limiting part has several forks (29, 63 to 66). The movable end of the spring can be engaged in any one of these forks (29, 63 to 66).