The invention generally relates to a system for adjusting the pitch of a plurality of rotor blade assemblies and, more particularly, to a system for selectively simultaneously adjusting the pitch of a plurality of rotor blade assemblies in a power trowel.
Ride-on power trowels generally include a plurality of rotor blade assemblies, which comprise a plurality of rotor blades. During operation, it is often desirable to adjust the pitch of the rotor blades within the rotor blade assemblies. Further, it is often desirable to adjust the pitch of rotor blades within the separate rotor blades an essentially equal amount. Accordingly, some ride-on power trowels include systems for simultaneously adjusting the pitch of rotor blades in a pair of rotor blade assemblies. However, these systems involve a number of moving mechanical parts, including miter boxes and connector extensions between one side of the adjustment system and the other. These parts provide hazards to the operator while getting into and getting out of the ride-on power trowel's operator seat. Further, the number of moving parts provides numerous opportunities for a part of the system to become dysfunctional and add to the number of areas that need periodic maintenance.
The present simultaneous twin pitch adjustment system accomplishes selective simultaneous adjustment of the pitch of rotor blades in a plurality of rotor blade assemblies while decreasing the number of parts involved, decreasing the frequency of necessary maintenance, and decreasing the hazard of getting into and out of the operator's seat of a ride-on power trowel. More specifically, the present simultaneous twin pitch adjustment system utilizes a flexible shafting cord to accomplish the connection between a plurality of pitch adjustment subassemblies. Examples of flexible shafting cords are those described by U.S. Pat. No. 2,368,457 to George G. Eisenbeis and assigned to Stow Manufacturing Co., or by U.S. Pat. No. 2,388,129 to George G. Eisenbeis and assigned to Stow Manufacturing Co, the disclosures of which are incorporated herein by reference. The connection between the plurality of pitch adjustment subassemblies can be selectively disengaged so as to allow separate pitch adjustments before reconnecting the subassemblies.
A typical power trowel, with which the simultaneous twin pitch adjustment system would be incorporated, includes a frame that supports two or more rotor blade assemblies. Taking, as an example, the power trowel having two rotor blade assemblies. The twin pitch adjustment system used therewith includes first and second mounting brackets that mount first and second posts to the frame. Atop each post is a coupler, to which is attached a handle. A pitch communicator extends from the coupler through the post to a rotor assembly connector. A flexible shafting cord extends between the two couplers. The system is configured so that when an operator manipulates one handle, the handle communicates via its respective pitch communicator to adjust the pitch of its respective rotor blade assembly and also communicates via the flexible shafting cord to adjust the pitch of the other rotor blade assembly. Accordingly, manipulation of one handle simultaneously adjusts the pitch of both rotor blade assemblies.
In instances where the operator wishes to adjust the pitch of only one rotor blade assembly, one handle is selectively disengaged from the flexible shafting cord, such that manipulation of the handle will adjust the pitch of the associated rotor blade assembly without also adjusting the pitch of the other rotor blade assembly. The handle can then be reengaged with the flexible shafting cord, such that manipulation of the handle thereafter results in simultaneous pitch adjustment of both rotor blade assemblies.
The purpose of the Summary is to enable the public, and especially the scientists, engineers, and practitioners in the art who are not familiar with patent or legal terms or phraseology to determine quickly, from a cursory inspection, the nature and essence of the technical disclosure of the application. The Summary is neither intended to define the invention of the application, which is measured by the claims, nor is it intended to be limiting as to the scope of the invention in any way.
Still other features and advantages of the claimed system will become readily apparent to those skilled in the art from the following detailed description describing preferred embodiments of the system, simply by way of illustration of the best mode contemplated by carrying out the system. As will be realized, the system is capable of modification in various obvious respects all without departing from the invention. Accordingly, the drawings and description of the preferred embodiments are to be regarded as illustrative, and not restrictive.
While the system is susceptible of various modifications and alternative constructions, certain illustrated embodiments thereof have been shown in the drawings and will be described below in detail. It should be understood, however, that there is no intention to limit the invention to the specific form disclosed, but, on the contrary, the invention is to cover all modifications, alternative constructions, and equivalents falling within the spirit and scope of the invention as defined in the claims.
In the following description and in the figures, like elements are identified with like reference numerals. The use of “e.g.,” “etc,” and “or” indicates non-exclusive alternatives without limitation unless otherwise noted. The use of “including” means “including, but not limited to,” unless otherwise noted.
As shown in the figures, for purposes of illustration, depicted is a system for selectively and simultaneously adjusting the pitch of a plurality of rotor blades within separate rotor blade assemblies. The system includes few parts, thereby decreasing the potential for system failure and the frequency of maintenance. The arrangement of the parts further decreases the hazards and risks to an operator getting into and out of the trowel's operator seat.
A first coupler 22 is connected to the first post 24 and is supported thereby. The first coupler 22 is further connected to the first pitch communicator 28. A first handle 20 supported by the first coupler 22 is configured to be manipulated by an operator and further configured so that manipulation of the first handle 20 translates to manipulation of the first pitch communicator 28, and, thereafter, manipulation of the pitch of the first rotor blade within the first rotor blade assembly 42.
Preferably, the first mounting bracket 26 is supported by and mounted to a first rotor assembly connector 27 (
The simultaneous twin pitch adjustment system 10 further includes a second mounting bracket 36 and a second post 34 connected to the second mounting bracket 36. A second pitch communicator 38 extends at least partially through the second post 34. Ideally, the second pitch communicator 38 extends from the top of the second post 34 down past the second mounting bracket 36 and to a point where it communicates to a second rotor blade assembly 44 (shown in
A second coupler 32 is connected to the second post 34 and is supported thereby. The second coupler 32 is further connected to the second pitch communicator 38. A second handle 30 supported by the second coupler 32 is configured to be manipulated by an operator and further configured so that manipulation of the second handle 30 translates to manipulation of the second pitch communicator 38, and, thereafter, manipulation of the pitch of the second rotor blade within the second rotor blade assembly 44.
Preferably, the second mounting bracket 36 is supported by and mounted to a second rotor assembly connector 37 (
The simultaneous twin pitch adjustment system 10 further includes a flexible shafting cord 12 that has a first cord end and a second cord end. As shown in
The flexible shafting cord 12 is further configured such that, selectively, manipulation of the first handle 20 translates through the flexible shafting cord 12 to the second handle 30 and thus while manipulation of the first handle 20 leads to adjustment of the pitch of the first rotor blade within the first rotor blade assembly 42, selectively, via the flexible shafting cord 12, manipulation of the first handle 20 further leads to adjustment of the pitch of the second rotor blade within the second rotor blade assembly 44. Accordingly, the operator may manipulate one handle so as to adjust the pitch of rotor blades within the plurality of rotor blade assemblies of the machine essentially an equal amount. Of course, it is preferred that the simultaneous twin pitch adjustment system 10 is configured such that manipulation of either the first handle 20 or the second handle 30 translates to manipulation of both the first pitch communicator 28 and the second pitch communicator 38 so as to adjust the pitch of both the first and second rotor blades within the first rotor blade assembly 42 and the second rotor blade assembly 44 essentially an equal amount.
According to the one embodiment, shown in
As shown in
Also as shown in
Each handle 20, 30 is further configured so that each can be selectively positioned in a disengaged position, such as by raising the handle away from the coupler to bring the master gear 86 out of operative communication with the slave gear 84. In the disengaged position, manipulation of the handle 20, 30 translates to manipulation of the master gear 86 and manipulation of the associated pitch communicator 28 or 38 so as to adjust the pitch of the blades of only the associated rotor blade assembly 42 or 44. Accordingly, when the first handle 20 is raised or otherwise placed in the disengaged position such that the master gear 86 within the first coupler 22 is taken out of operative connection with the slave gear 84, manipulation of the first handle 20 leads to adjustment of the pitch of the blades of the first rotor blade assembly 42, but not adjustment of the blades of the second rotor blade assembly 44. Alternatively, with the first handle 20 in the disengaged position, manipulation of the second handle 30 leads to adjustment of the pitch of the blades of the second rotor blade assembly 44, but not adjustment of the blades of the first rotor blade assembly 42. Likewise, when the second handle 30 is raised or otherwise placed in the disengaged position such that the master gear 86 within the second coupler 32 is taken out of operative connection with the slave gear 84, manipulation of the second handle 30 leads to adjustment of the pitch of the blades of the second rotor blade assembly 44, but not adjustment of the blades of the first rotor blade assembly 42. Alternatively, with the second handle 30 in the disengaged position, manipulation of the first handle 20 leads to adjustment of the pitch of the blades of the first rotor blade assembly 42, but not adjustment of the blades of the second rotor blade assembly 44. However, transitioning the handles 20, 30 back into the engaged position, such as by lowering the handle, to bring the master gear 86 back into operative connection with the slave gear 84, the simultaneous pitch adjustment is again engaged such that manipulation of one handle 20, 30 leads to adjustment of the blade pitch within both rotor blade assemblies 42, 44.
Preferably, the linkage between the first handle 20 and second handle 30 via the flexible shafting cord 12 is selectively activated by the operator, such as by positioning the first handle 20 and second handle 30 in a lowered position, wherein the handle 20 or 30 is in close proximity to the associated coupler 22 or 32, to put the handles 20, 30 in an engaged position. Accordingly, if and when the operator wants to adjust the pitch in only one of the rotor blade assemblies 42, 44, the twin-pitch adjustment connection via the flexible shafting cord 12 may be selectively disengaged, such as by placing the first handle 20 or second handle 30 in a disengaged position such as by raising either handle 20, 30 to move the handle 20, 30 farther away from the associated coupler 22 or 32. This allows the operator to adjust the desired rotor blade assembly's blade pitch by adjusting the associated handle 20, 30. Following which, when the operator desires to again provide for simultaneous twin pitch adjustment via the flexible shafting cord 12, the connection between the first handle 20 and the second handle 30 may be selectively engaged as by repositioning the first handle 20 and second handle 30 to the engaged position, such as a lowered position.
In other embodiments, however, the connection between the first handle 20 and the second handle 30 via the flexible shafting cord 12 is not selectively disengageable.
As shown in
Likewise, the second rotor blade assembly 44 is supported by the frame 40 and is operatively attached to a second rotor assembly connector 37. Preferably, the second rotor assembly connector 37 also supports the second mounting bracket 36. Accordingly, the frame 40 supports the second post 34 of the simultaneous twin pitch adjustment system 10 via the second rotor assembly connector 37. Preferably, the second pitch communicator 38 is configured to be operatively connected to the second rotor blade assembly 44 through the second rotor assembly connector 37.
As shown in
While there is shown and described the present preferred embodiment of the system, it is to be distinctly understood that this system is not limited thereto but may be variously embodied to practice within the scope of this disclosure. From the foregoing description, it will be apparent that various changes may be made without departing from the spirit and scope of the invention as defined by this disclosure.
Still other features and advantages of the present system will become readily apparent to those skilled in this art from the following detailed description describing preferred embodiment of the simultaneous twin pitch adjustment system, simply by way of illustration of the best mode contemplated by carrying out the system. As will be realized, the system is capable of modification in various obvious respects all without departing from the invention. For example, while the depicted embodiment shows a ride-on power trowel 4 that includes only two rotor blade assemblies, in some embodiments, the system 10 is utilized with more than two rotor blade assemblies. In some such embodiments, each rotor blade assembly is connected to a separate post, mounting bracket, coupler, handle, etc., with the flexible shafting cord 12 being connected between each of the couplers of the system. In any regard, the drawings and description of the preferred embodiments are to be regarded as illustrative in nature, and not as restrictive in nature.
This application claims the priority date of the provisional application entitled “Simultaneous Twin Pitch Adjustment System” invented by Michael Julius and filed on Feb. 2, 2009, with application Ser. No. 61/149,254, the disclosure of which is incorporated herein by reference.
Number | Name | Date | Kind |
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2368457 | Eisenbeis | Jan 1945 | A |
2388129 | Eisenbeis | Oct 1945 | A |
6739799 | Eitzen | May 2004 | B1 |
7039986 | Glenn et al. | May 2006 | B2 |
7044682 | Glenn et al. | May 2006 | B2 |
7690864 | Allen et al. | Apr 2010 | B2 |
8132983 | Lutz et al. | Mar 2012 | B2 |
20110222966 | Allen et al. | Sep 2011 | A1 |
Number | Date | Country | |
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20100196162 A1 | Aug 2010 | US |
Number | Date | Country | |
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61149254 | Feb 2009 | US |