1. Field of the Invention
The present invention relates to an actuator, and more particularly, to a pneumatic actuator.
2. Statement of the Problem
An actuator is a device that performs some mechanical action. One actuator is a piston, wherein a plunger of the piston moves in a reciprocating manner. The plunger can therefore be connected to some manner of work piece or other mechanical system.
In some actuator applications, it is desirable to have more than one actuation speed and/or more than one actuation force over the range of motion of the actuator. For example, in a spot welder machine, a pair of welding jaws must be brought together onto a work piece during a welding operation. The jaws must clamp onto the work piece with a desired force. Therefore, at the end of a clamping motion range, a relatively high actuation force must be provided to the welding jaws. However, an actuator that provides a high level of force typically provides a relatively small range of actuation travel. This can be a problem where the jaws of the spot welder machine must open wide in order to be positioned on the work piece. Therefore, a jaw actuator of the spot welder machine needs to move relatively rapidly during a first actuation span and a large force is not required. During the second actuation span, the jaws need to move only a small distance, but must be able to provide a large clamping force.
A pneumatic actuator is provided according to an embodiment of the invention. The actuator comprises an actuator body and a piston rod extending from the actuator body. The piston rod moves over an actuation span. The actuation span comprises a first stroke span that is traversed by the piston rod at a first actuation speed and a second stroke span that is traversed at a second actuation speed that is substantially slower than the first actuation speed.
A pneumatic actuator is provided according to an embodiment of the invention. The actuator comprises an actuator body and a piston rod extending from the actuator body. The piston rod moves over an actuation span. The actuation span comprises a first stroke span that is traversed by the piston rod using a first actuation force and a second stroke span that is traversed using a second actuation force that is substantially greater than the first actuation force.
A pneumatic actuator is provided according to an embodiment of the invention. The actuator comprises an actuator body including an outer shell and an inner shell, a piston slidably located in a piston chamber in the inner shell, and a ram slidably located in the outer shell and configured to move at least partially into the inner shell. The actuator further comprises a movable ring slidably located in a ring chamber located between the inner shell and the outer shell and a hydraulic fluid located in a region between the ram, the piston, and the movable ring. Upward movement of the movable ring forces the piston downward over a first stroke span due to movement of a first volume of the hydraulic fluid from the ring chamber into the piston chamber. Downward movement of the ram forces a second volume of the hydraulic fluid down into the piston chamber, wherein the downward movement of the ram forces the piston downward over a second stroke span.
In one embodiment of the actuator, the second stroke span is substantially smaller in length that the first stroke span.
In another embodiment of the actuator, the first stroke span is traversed by the piston rod at a first actuation speed and the second stroke span is traversed by the piston rod at a second actuation speed that is substantially slower than the first actuation speed.
In yet another embodiment of the actuator, the first stroke span is traversed by the piston rod using a first actuation force and the second stroke span is traversed by the piston rod using a second actuation force that is substantially greater than the first actuation force.
In yet another embodiment of the actuator, the second stroke span occurs at any point along the actuation span.
In yet another embodiment of the actuator, the second stroke span is generated by a force multiplier of the actuator.
In yet another embodiment of the actuator, the actuator further comprises a plurality of pneumatic ports in the actuator body.
In yet another embodiment of the actuator, the actuator further comprises a port A that introduces pressurized gas into the ring chamber below the movable ring.
In yet another embodiment of the actuator, the actuator further comprises a port B that introduces pressurized gas into the ram chamber below the ram.
In yet another embodiment of the actuator, the actuator further comprises a port C that introduces pressurized gas into the ram chamber above the ram.
In yet another embodiment of the actuator, the actuator further comprises a port D that introduces pressurized gas into the piston chamber below the piston.
In yet another embodiment of the actuator, the actuator further comprises a piston ring located in the outer shell and below the piston, with the piston ring slidably located in the outer shell and being configured to sealingly slide on the piston rod, wherein a port E is located below the piston ring and the piston ring moves up and pushes the piston upward when pressurized gas is introduced into port E.
In yet another embodiment of the actuator, the actuator further comprises one or more hydraulic fluid passages extending between the ram throat and the ring chamber.
The same reference number represents the same element on all drawings. It should be understood that the drawings are not necessarily to scale.
The first stroke span can be traversed at a first actuation speed and the second stroke span can be traversed at a second actuation speed. In one embodiment, the second actuation speed is substantially slower than the first actuation speed.
The first stroke span can be traversed using a first actuation force and the second stroke span can be traversed using a second actuation force. In one embodiment, the second actuation force is substantially greater than the first actuation force.
The actuator 100 in one embodiment includes a force amplifier. In one embodiment, the actuator 100 includes a hydro-pneumatic force amplifier. The force amplifier can provide a force greater than a force generated by a supplied pneumatic pressure alone. The actuator 100 in one embodiment can provide a force amplifier at any point in the overall actuation span. The force amplifier can be actuated at a midpoint of the actuation span or can be actuated before or after the midpoint.
Referring again to
The actuator 100 further includes an inner shell 109, a lower inner plug 131, and an upper inner plug 135. The inner shell 109 forms the piston chamber 126. The lower inner plug 131 is located at a bottom region of the piston chamber 126 and the upper inner plug 135 is located at a top region of the piston chamber 126. In addition, the lower inner plug 131 and the upper inner plug 135 hold the inner shell 109 substantially in position within the outer shell 101. In one embodiment, the inner shell 109 is substantially coaxial with the outer shell 101. The upper inner plug 135 includes an upper inner plug seal(s) 136 that substantially seal the upper inner plug 135 to the outer shell 101. In addition, the upper inner plug 135 includes hydraulic fluid passages 137, a ram throat 138, and ram throat seals 139. The ram throat 138 receives a ram 160, with the ram throat seals 139 sealing the ram 138 to the upper inner plug 135. As a consequence, the ram 138 blocks the ram throat 138 and can move reciprocally up and down in the ram throat 138.
The actuator 100 further includes a piston ring 110. The piston ring 110 can include piston ring seals 112. The piston ring 110 can move with respect to the outer shell 101 and can move with respect to the piston rod 108. The piston ring 110 can move under influence of pressurized gas above and below the piston ring 110. The pressurized gas can be introduced and exhausted from above and below the piston ring 110 by port D and port E, respectively.
The actuator 100 further includes a movable ring 140 located in a ring chamber 147 formed between the inner shell 109 and the outer shell 102. The upper side of the movable ring 140 contacts a hydraulic fluid, which is also present in the piston chamber 126 above the piston 120. The movable ring 140 is configured to move reciprocally up and down between the outer shell 101 and the inner shell 109 in response to gas introduced and exhausted by port A. The movable ring 140 can include movable ring seals 144. The movable ring seals 144 substantially seal the movable ring 140 to the outer shell 101. In addition, the movable ring seals 144 substantially seal the movable ring 140 to the inner shell 109.
The actuator 100 further includes the ram 160. The ram 160 moves reciprocally up and down in a ram chamber 161. The ram 160 includes ram seals 163, a ram conduit(s) 163, and a ram filling cavity 166. The ram filling cavity 166 is fed pressurized gas by a pipe 170 that extends from the top plug 103 and that is connected to port B. The gas is transferred to a portion of the ram chamber 161 below the ram 160, with the gas traveling through the ram conduit(s) 163 to the portion of the ram chamber 161. In addition, the ram 160 is in communication with port C. As a result, the ram 160 can be moved down by introduction of pressurized gas into port C and can be moved up by introduction of pressurized gas into port B.
Upward movement of the movable ring 140 forces the piston 120 downward over a first stroke span due to movement of a first volume of the hydraulic fluid from the ring chamber 147 into the piston chamber 126. Downward movement of the ram 160 forces a second volume of the hydraulic fluid down into the piston chamber 126, wherein the downward movement of the ram 160 forces the piston 120 downward over a second stroke span.
The figure shows the actuator 100 in a fully retracted position, where the piston rod 108 is fully retracted within the actuator 100. Pressurized gas can be supplied into port D to move the piston 120 to (and hold the piston 120 in) the fully retracted position. Correspondingly, port A, port B, and port C are released in order to allow the piston 120 and the ram 160 to move to fully retracted upward positions. As the piston 120 is moved upwards, the hydraulic fluid above the piston 120 is moved out of the piston chamber 126 and is forced into the chamber between the outer shell 101 and the inner shell 109, pushing the movable ring 140 fully downward. As a result, gas is forced out of port A. In addition, port C is released and the gas between the ram 160 and the top plug 103 is not held. As a result, the upward movement of the piston 120 causes the ram 160 to move fully upward.
To actuate the force multiplier, port B is released, the pressure at port A is held, and pressurized gas is further supplied to port C. This moves the ram 160 downward in the ram chamber 161, moving the ram 160 fully into the ram throat 138. As a result, the ram 160 blocks off the hydraulic fluid passage(s) 137 and consequently seals the hydraulic fluid in the piston chamber 126. The volume of hydraulic fluid displaced by the ram 160 in the ram throat 138 causes the piston 120 to move additionally downward. The large cross-sectional area of the top of the ram 160, combined with the smaller cross-sectional area of the bottom of the ram 160, provides the force multiplier effect. The ram 160 presses the hydraulic fluid into the piston chamber 126. The force at the end of the ram 160 in one embodiment is about 6 times the force on the upper side of the ram 160. No additional hydraulic fluid needs to be provided to the actuator 100. The ram 160 therefore provides a large second actuation force over the second (small) stroke span.
It should be understood that the force multiplier can be actuated at any point in the first (large) stroke span. As a result, even if the piston rod 108 is only at a midpoint of the first stroke span, the ram 160 can be moved downward and the second (small) stroke span can be traversed by the piston rod 108, in addition to any portion of the first stroke span already traversed.
The retraction operation is essentially the opposite of the extension operation. For retraction, the pressurized gas at port A and port C is released. Subsequently, pressurized gas is supplied to port B, moving the ram 160 upward to a fully retracted position. The retraction of the ram 160 unblocks the hydraulic fluid passage(s) 137, allowing hydraulic fluid to move from the piston chamber 126 to the ring chamber 147. Then, pressurized gas is introduced to port E in order to force the piston ring 110 fully upward, thereby forcing the piston 120 partially upward (see
The pneumatic pressure coupler according to the invention can be employed according to any of the embodiments in order to provide several advantages, if desired. The invention provides an actuation span including first and second stroke spans, where the first and second stroke spans can be of different lengths. The invention provides an actuation span including first and second actuation speeds. The invention provides an actuation span including first and second actuation forces. The invention provides an actuator including a force multiplier. The invention provides an actuator including a hydro-pneumatic force multiplier. The invention provides an actuator including a force multiplier that can be actuated at any point in a first stroke span.
Advantageously, in the actuator according to the invention, no biasing springs are required. In the actuator according to the invention, no hydraulic fluid is supplied to the actuator. In the actuator according to the invention, force amplification is achieved using only pneumatic inputs.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/EP2006/007567 | 7/31/2006 | WO | 00 | 1/16/2009 |
Publishing Document | Publishing Date | Country | Kind |
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WO2008/014799 | 2/7/2008 | WO | A |
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3991661 | Mocha | Nov 1976 | A |
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5381661 | Malina | Jan 1995 | A |
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5943862 | Malina | Aug 1999 | A |
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2505553 | Apr 1976 | DE |
19534380 | Mar 1997 | DE |
4627692 | Sep 1971 | JP |
4995394 | Sep 1974 | JP |
57179404 | Nov 1982 | JP |
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Number | Date | Country | |
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20090282971 A1 | Nov 2009 | US |