The present application relates to sanders and, more particularly, to monopodic sanders and methods for controlling the same.
A known application of a sander is sanding an underwing structure of an aircraft. Underwing sanding poses a number of ergonomic challenges for a person operating a sander. Accordingly, those skilled in the art continue with research and development efforts in the field of sanders for various applications such as sanding an underwing structure of an aircraft.
In one aspect, a monopodic sander is provided for an operator to sand a surface, such as an overhead surface. The monopodic sander comprises a rotary sanding head for contacting the surface and an extendable actuator rod having one end pivotally coupled to the rotary sanding head. The monopodic sander further comprises a controller handle operatively coupled to the one end of the extendable actuator rod to allow the operator to select a pressure applied by the rotary sanding head against the surface.
In another aspect, a monopodic sander is provided for an operator to sand a surface, such as an overhead surface. The monopodic sander comprises a rotary sanding head for contacting the surface and an extendable actuator rod having one end pivotally coupled to the rotary sanding head. The monopodic sander further comprises a dust containment shield surrounding the rotary sanding head and configured to create a suction effect around the rotary sanding head to collect dust particles as the rotary sanding head is moving laterally across the surface and pivoting about the one end of the extendable actuator rod during operation of the monopodic sander.
In yet another aspect, a method for operating a monopodic sander is provided. The method comprises contacting a rotary sanding head of the monopodic sander against a surface, such as an overhead surface, with a substantially constant predetermined pressure. The method further comprises maintaining the rotary sanding head against the surface with the substantially constant predetermined pressure as the rotary sanding head moves laterally across the surface during operation of the monopodic sander.
In still another aspect, a method for operating a monopodic sander is provided. The method comprises contacting a rotary sanding head of the monopodic sander against a surface, such as an overhead surface. The method further comprises creating a suction effect around the rotary sanding head to collect dust particles as the rotary sanding head is moving laterally across the surface during operation of the monopodic sander.
Other aspects will become apparent from the following detailed description, the accompanying drawings and the appended claims.
The present application is directed to monopodic sanders and methods of controlling the same for an aerospace vehicle such as an aircraft. Non-aerospace applications are also contemplated. The specific monopodic sander and method, and the industry in which the monopodic sander and method are implemented may vary. It is to be understood that the disclosure below provides a number of embodiments or examples for implementing different features of various embodiments. Specific examples of components and arrangements are described to simplify the present disclosure. These are merely examples and are not intended to be limiting.
By way of example, the disclosure below describes monopodic sanders and methods of controlling the same for airplanes. More specifically, the disclosure below describes a monopodic sander for sanding an underwing structure of an airplane. The monopodic sander and method for operating the monopodic sander may be implemented by an original equipment manufacturer (OEM) for assembling airplane structures in compliance with military and space regulations.
Referring to
The monopodic sander 100 includes a rotary sanding head 102 for contacting a surface (not shown), such as an overhead surface (e.g., an underwing structure of an airplane). A sanding pad 104 is disposed on the rotary sanding head 102 for contacting a surface to be sanded. A pneumatic motor 106 is operatively coupled to the rotary sanding head 102 in known manner to drive the rotary sanding head 102 to move the sanding pad 104 laterally across the surface to be sanded. Structure and operation of rotary sanding heads and pneumatic motors for driving rotary sanding heads are known and conventional and, therefore, will not be described.
The monopodic sander 100 further includes a gimbal ring 108 that is operatively coupled to an attachment arm 110. The attachment arm 110 is connected to an extendable actuator rod 112 of a counter-balance actuator 114 by using a pair of clamp bars 116 that are fastened together with a pair of bolts 118 and a mating pair of nuts 120. A foot 122 is attached to an end of the actuator 114 to support the monopodic sander 100 on a floor (not shown). The actuator rod 112 is shown in the figures as near fully retracted.
A first end 126 of the extendable actuator rod 112 telescopes in an air chamber 128 of the actuator 114. A second end 130 of the extendable actuator rod 112 is connected through the gimbal mechanism (i.e., the attachment arm 110 and the gimbal ring 108) to the rotary sanding head 102. The gimbal mechanism supports the rotary sanding head 102 for rotation about a first axis “A” (
The monopodic sander 100 also includes an accessory attachment clamp 140 to which a dust collection device 142 and a vacuum device 143 are attached on one side of the clamp 140. A dust collection tube 144 interconnects the vacuum device 143 and a substantially circular-shaped motor shroud 146 that surrounds the pneumatic motor 106 and the rotary sanding head 102. A substantially circular-shaped dust containment shield 148 is concentric with the motor shroud 146, and surrounds the sanding pad 104. The circular-shaped dust containment shield 148 has a diameter that is greater than the diameter of the sanding pad 104. The dust containment shield 148 is configured to create a suction effect around the rotary sanding head 102 to collect dust particles as the rotary sanding head 102 is moving laterally across the surface and pivoting about the second end 130 of the extendable actuator rod 112 during operation of the monopodic sander 100.
A controller handle 150 is attached on an opposite side of the accessory attachment clamp 140. The controller handle 150 is operatively connected via the clamp 140 to the second end 130 of the extendable actuator rod 112. The controller handle 150 allows an operator to select a pressure applied by the rotary sanding head 102 against the surface to sand the surface, as will be described herein.
In the example embodiment shown in
The controller handle 150 includes a hand-operated actuator 160 for allowing the operator to adjust a flow rate of pressurized air to the rotary sanding head 102 and thereby to allow the operator to select the pressure applied by the rotary sanding head 102 against the surface. The hand-operated actuator 160 comprises a pneumatic valve that is slidable between a fully closed position and a fully open position. The pneumatic valve of the hand-operated actuator 160 is positioned on the second arm portion 158 so as to allow the operator to use the other hand to slide the pneumatic valve of the hand-operated actuator 160 between the fully closed position and the fully open position to adjust the pressure applied by the rotary sanding head 102 against the surface. Thus, the rotary sanding head 102 moves towards the surface in response to the operator sliding the pneumatic valve of the hand-operated actuator 160 in a first direction, and moves away from the surface in response to the operator sliding the pneumatic valve of the hand-operated actuator 160 in a second direction which is opposite the first direction. The hand-operated actuator 160 may comprise a lever that is pressed or moved to cause the pneumatic valve to deliver pressurized air to the rotary sanding head 102 for operating the sanding head, and is movable to a fully closed position upon release by the operator's hand to cause the pneumatic valve to close and discontinue delivery of pressurized air, to provide a safety function for turning off the sander.
The monopodic sander 100 further comprises a pressure regulator 162 for maintaining the selected pressure that is applied by the rotary sanding head 102 against the surface substantially constant as the rotary sanding head 102 is moving laterally across the surface and pivoting about the second end 130 of the extendable actuator rod 112 during operation of the monopodic sander 100. The pressure regulator 162 regulates pressure in the air chamber 128 of the actuator 114 by equalizing pressure in the air chamber 128 when the rotary sanding head 102 is contacting the surface during operation of the monopodic sander 100. An example pressure regulator that can be used is model number 41595K21 commercially available from McMaster-Carr of Elmhurst, Ill. Other pressure regulators from other sources are possible.
A compressed air source 170 (
The monopodic sander 100 also comprises an air splitter 164 (shown only in
The second air path in pneumatic line 168 is in fluid communication with the pressure regulator 162. As previously mentioned, the pressure regulator 162 regulates pressure in the air chamber 128 of the actuator 114 by equalizing pressure in the air chamber 128 when the rotary sanding head 102 is contacting the surface (or when the extendable actuator rod 112 has reached its maximum length of extension) during operation of the monopodic sander 100.
In block 420, the rotary sanding head is maintained against the surface with the substantially constant predetermined pressure as the rotary sanding head moves laterally across the surface during operation of the monopodic sander. The process then ends.
In some embodiments, the rotary sanding head is contacted against the surface with a pressure selected by an operator of the monopodic sander.
In some embodiments, the rotary sanding head is contacted against the surface with the selected pressure in response to the operator sliding a pneumatic valve in a first direction. In some embodiments, the rotary sanding head is moved away from the surface in response to the operator sliding the pneumatic valve in a second direction which is opposite the first direction.
In some embodiments, the rotary sanding head is contacted against the surface with a selected pressure sufficient to remove material from the surface.
In block 520, a suction effect around the rotary sanding head is created to collect dust particles as the rotary sanding head is moving laterally across the surface during operation of the monopodic sander. The process then ends.
It should be apparent that an underwing structure of an airplane that is sanded in accordance with the above-described example methods require less time and less labor to achieve. The result is a much quicker turnaround time of the sanding process as compared to known sanding methods that require more time and more labor to achieve.
It should also be apparent that the L-shaped arm of the controller handle 150 of the above-described monopodic sander 100 provides a mechanical advantage that reduces ergonomic risks for a person operating the monopodic sander 100. This is because the person uses one hand to control the first arm portion 156 of the L-shaped arm of the controller handle 150 to raise and lower the rotary sanding head 102, the other hand to control the second arm portion 158 of the L-shaped arm of the controller handle 150 to select the pressure applied by the rotary sanding head 102 against the surface, and both hands to move the rotary sanding head 102 laterally across the surface. The person does not need to look up to move the rotary sanding head 102 either horizontally or vertically, or both, and to select the amount of pressure applied by the rotary sanding head 102 against the surface. Moreover, the dimension ranges of the first and second arm portions 156, 158 of the L-shaped arm of the controller handle 150 allows an average-height person to easily raise and lower the rotary sanding head 102. The dimension ranges of the first and second arm portions 156, 158 are preferably sized to yield a minimum length of the controller handle 150 of about 18 inches, which allows an average-height person to easily move the rotary sanding head 102 several feet laterally across the surface, by holding the second arm portion 158 steady and swinging the first arm portion 156 with minimal back and forth movement of the controller handle, as shown in
It should further be apparent that an integrated vacuum system (i.e., the dust collection device 142, the vacuum device 143, the dust collection tube 144, and the dust containment shield 148) is provided for collecting dust particles in the air. Accordingly, the exposure of the operator to dust particles as a result of the sanding operation is reduced.
It should also be apparent that the above-described monopodic sander 100 occupies a relatively small footprint since it stands on the floor with only the one foot 122 (i.e., a single pod) when the monopodic sander 100 is in operation.
Examples of the disclosure may be described in the context of an aircraft manufacturing and service method 1000, as shown in
Each of the processes of method 1000 may be performed or carried out by a system integrator, a third party, and/or an operator (e.g., a customer). For the purposes of this description, a system integrator may include without limitation any number of aircraft manufacturers and major-system subcontractors; a third party may include without limitation any number of venders, subcontractors, and suppliers; and an operator may be an airline, leasing company, military entity, service organization, and so on.
As shown in
The disclosed monopodic sander and sanding methods may be employed during any one or more of the stages of the aircraft manufacturing and service method 1000. As one example, components or subassemblies corresponding to component/subassembly manufacturing 1008, system integration 1010, and/or maintenance and service 1016 may be assembled using the disclosed monopodic sanders and sanding methods. As another example, the airframe 1018 may be constructed using the disclosed monopodic sanders and sanding methods. Also, one or more apparatus examples, method examples, or a combination thereof may be utilized during component/subassembly manufacturing 1008 and/or system integration 1010, for example, by substantially expediting assembly of or reducing the cost of an aircraft 1002, such as the airframe 1018 and/or the interior 1022. Similarly, one or more of system examples, method examples, or a combination thereof may be utilized while the aircraft 1002 is in service, for example and without limitation, to maintenance and service 1016.
The above-described monopodic sanders and sanding methods are described in the context of an aircraft. However, one of ordinary skill in the art will readily recognize that the disclosed monopodic sanders and sanding methods are suitable for a variety of applications, and the present disclosure is not limited to aircraft manufacturing applications. For example, the disclosed monopodic sanders and sanding methods may be implemented in various types of vehicles including, for example, helicopters, passenger ships, automobiles, marine products (boat, motors, etc.) and the like. Non-vehicle applications are also contemplated.
Although the above description describes a pneumatic-based monopodic sander to sand underwing structures of an aircraft, it is conceivable that a monopodic sander that is other than pneumatic-based may be used.
Also, although the above-description describes monopodic sanders and sanding methods for sanding underwing structures of an airplane in the aviation industry in accordance with military and space regulations, it is contemplated that the monopodic sanders and sanding methods may be implemented to facilitate sanding for any type of large manufacturing assembly in any industry in accordance with the applicable industry standards. The specific monopodic sander and sanding method can be selected and tailored depending upon the particular application.
Further, although various aspects of disclosed embodiments have been shown and described, modifications may occur to those skilled in the art upon reading the specification. The present application includes such modifications and is limited only by the scope of the claims.
Number | Name | Date | Kind |
---|---|---|---|
4204292 | Lester | May 1980 | A |
4399578 | Bordeaux | Aug 1983 | A |
4829719 | Braselton | May 1989 | A |
4870730 | Belknap | Oct 1989 | A |
5289605 | Armbruster | Mar 1994 | A |
6722967 | Oddo | Apr 2004 | B1 |
6793567 | Corkill | Sep 2004 | B1 |
7074111 | Cecil | Jul 2006 | B2 |
7249996 | Volyar | Jul 2007 | B1 |
7549913 | Weiford | Jun 2009 | B2 |
7828631 | Herbert | Nov 2010 | B1 |
8844884 | Bottazzi | Sep 2014 | B2 |
9242365 | Bureau | Jan 2016 | B1 |
9364935 | Fuller | Jun 2016 | B2 |
9534730 | Black et al. | Jan 2017 | B2 |
20020132570 | Berg | Sep 2002 | A1 |
20040072519 | Oddo | Apr 2004 | A1 |
20080201877 | Sengewald | Aug 2008 | A1 |
20100048108 | Stott | Feb 2010 | A1 |
20130074966 | Bottazzi | Mar 2013 | A1 |
20160016300 | Bureau | Jan 2016 | A1 |
20160184954 | Roeck | Jun 2016 | A1 |
20170307132 | Kerestes | Oct 2017 | A1 |
20190160622 | Barth | May 2019 | A1 |
Entry |
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https://www.ergonomicpartners.com/zero-gravity-tool-balancer.aspx. |
Number | Date | Country | |
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20190247972 A1 | Aug 2019 | US |