This invention relates generally to a support for a helical flight of an auger, and more particularly, to an auger flight support which results in lower stress concentrations when mounted to an auger shaft, for reducing possible occurrences of fatigue related failure.
A wide variety of supports have been long utilized for supporting an auger flight on an auger shaft. Reference in this regard, Van Arsdell U.S. Pat. No. 701,969 entitled End Support For Spiral Conveyors; Quelms U.S. Pat. No. 1,371,116 entitled Screw Conveyor Drive Clamp; Hartley U.S. Pat. No. 1,643,986 entitled Power Driven Conveyor; and Ryder U.S. Pat. No. 1,761,591 entitled Spiral Conveyor Coupling, all of which disclose manners of affixing a helical auger flight to a shaft, typically utilizing fasteners of some sort. It is evident from a study of the referenced patents, that numerous of these older style auger flight supports have shapes which require bending and other additional manufacturing steps so as to be disadvantageous costwise in a modern context.
Reference also
Thus, what is sought is an auger flight support that overcomes one or more of the problems and disadvantages set forth above.
What is disclosed is an auger flight support which overcomes one or more of the problems and disadvantages set forth above, by providing a weldable member which is easily manufactured, and provides improved load transfer and distribution, for reducing stress concentrations that can lead to fatigue failures.
According to a preferred aspect of the invention, an auger flight support includes a mounting portion having an arcuate concave surface adapted to be fixedly mounted around at least a portion of an outer circumferential surface of an auger shaft adjacent to an auger flight extending along a helical path around the shaft. The flight support includes a support portion in connection with the mounting portion, including an outwardly extending edge positioned and oriented for abutting and affixing to a radially extending edge of a flight of an auger when the mounting portion is mounted around at least a portion of an outer circumferential surface of the auger, for supporting the flight and forming an extension of the flight beyond the edge thereof.
According to another preferred aspect of the invention, the mounting portion is welded to the outer circumferential surface of an auger shaft and is ring shaped so as to distribute loads around a substantial portion of the circumference of the shaft.
According to another preferred aspect, the outwardly extending edge of the support portion is welded to the edge of the flight along substantially the radial length thereof. Still further, the edge of the support portion can include a groove which receives the edge of the auger flight, for facilitating support thereof, and transfer of loads applied against the flight through the support portion to the mounting portion, for distribution about the auger shaft.
According to a still further preferred aspect of the invention, the mounting portion and the support portion of the auger flight support are substantially flat and integrally formed from flat plate or sheet metal material. As a result, the flight support can be stamped or plasma cut from the flat plate or sheet metal material, to facilitate simple and inexpensive manufacture.
Referring now to the drawings, wherein preferred embodiments of the present invention are shown, in
A problem that has been observed as a result of the use of auger flight supports such as support 18 in the manner just described, is concentration of loads along an edge 22 of support 18 in contact with surface 14 of shaft 12, which can result in stress leading to premature fatigue related failures at that location.
Referring also to
Edge 30 preferably includes a recessed radially extending groove 34, which groove 34 is adapted for cooperatively receiving a radially outwardly extending terminal edge of an auger flight, here, represented by radially outwardly extending edge 36 of flight 16 of auger 10. Radially outwardly extending edge 30 of flight support 24 is rigidly affixed to a radially outwardly extending edge of an auger flight, such as edge 36, in a suitable manner, such as by welding, here represented by weld bead 38 shown in
It is desirable for loading conditions resulting from such conditions, as well as normal operation, and applied against an auger flight, to be transferred by support portion 28 radially inwardly to mounting portion 26, so as to be distributed at least partially around an outer circumferential surface of a shaft of an auger, such as surface 14 of auger 12, to both provide support for the auger flight, and reduce stress concentrations resulting from the loads which can result in fatigue failures.
To effect transfer and distribution of loads and stress around the outer circumference surface of an auger shaft, such as surface 14 of shaft 12, an inner circumferential surface 40 of mounting portion 26 of flight support 24 is preferably welded or otherwise suitably rigidly affixed to an underlying portion of the outer circumferential surface of an auger shaft around which flight support 24 is mounted, as illustrated by weld bead 42 in
Referring also to
It will be understood that changes in the details, materials, steps, and arrangements of parts which have been described and illustrated to explain the nature of the invention will occur to and may be made by those skilled in the art upon a reading of this disclosure within the principles and scope of the invention. The foregoing description illustrates the preferred embodiment of the invention; however, concepts, as based upon the description, may be employed in other embodiments without departing from the scope of the invention. Accordingly, the following claims are intended to protect the invention broadly as well as in the specific form shown.
Number | Name | Date | Kind |
---|---|---|---|
289751 | Chivill | Dec 1883 | A |
349390 | Gilbert et al. | Sep 1886 | A |
355124 | Birkholz | Dec 1886 | A |
415604 | Birkholz | Nov 1889 | A |
701969 | Van Arsdell | Jun 1902 | A |
1371116 | Quelms | Mar 1921 | A |
1643986 | Hartley | Oct 1927 | A |
1761591 | Ryder | Jun 1930 | A |
2014636 | Rosendahl | Sep 1935 | A |
3659700 | Tunderman | May 1972 | A |
4429782 | Pierson | Feb 1984 | A |
6093099 | Groff | Jul 2000 | A |
6106390 | Doggrell et al. | Aug 2000 | A |
6688970 | Tanis | Feb 2004 | B1 |