The invention presented herein concerns a mechanical assembly allowing the control of a plurality of concentrically orbiting pendulums which may be made through a series of simple movements to revolve first in coplanar and subsequently in non-coplanar orbits. This mechanism has applications in dynamic physical models of orbital systems, in devices for scientific education, specifically yet not solely, in pendular and gyroscopic motion and in optics, and in devices for physical education, as well as in whirling toys and accessories for artistic performance.
In background art in the field of dynamic physical models of atomic motion there exist no hand-held devices involving two and more pendulums as in the present invention and, as such, none of the background art in this field offers kinesthetic appreciation of the orbital relationships represented. In background art devices in this field the structures representing electrons have revolved in two dimensions or have been attached to spheres, rings, or complex armatures and have not been free to orbit through all positions available within an orbital shell.
In background art in the field of educational devices relating to pendular physics, gyroscopic precession, and orbital systems there exist none employing a plurality of concentric, adjustable, orbiting pendulums and allowing an operator to induce precession and subsequent intersecting non-coplanar orbits of said pendulums.
In background art in the field of whirling toys involving two counter-rotating tethered objects it is intended that the tethers be counter-rotating and non-coplanar from the commencement of operation. Said background art has not relied upon precession of the orbiting tethers for the establishment of non-coplanar orbits. In none of said background art are two or more tethers attached to a shared rotatable structure. In such background art in this field where provision is made for the potential use of more than two whirling objects said objects are attached to the handle of the device in such a way as to specifically prevent precession of the orbiting members and the resultant intersection of orbital planes. In none of said prior art devices do the orbits of three and more independent pendulums or tethers share a common center. There exist no prior art devices employing more than two pendulums in precessing, non-coplanar, concentric orbits.
In background art in the field of whirling toys of the sort comprising a disc suspended on a loop of cord encircling both hands of an operator and incorporating a plurality of light-emitting structures said structures are constrained to coplanar orbits or to parallel orbital planes and their operation does not proceed in the manner of the present invention.
Relevant prior art of which I am aware includes:
In the field of whirling toys:
U.S. Pat. No. 128,239 Morris, 1872
U.S. Pat. No. 139,533 Batchelder, 1873
U.S. Pat. No. 610,600 Davis, 1898
U.S. Pat. No. 1,374,002 Edson, 1921
U.S. Pat. No. 1,858,145 Felardo, 1930
U.S. Pat. No. 1,915,868 Rogers, 1933.
U.S. Pat. No. 1,932,943 Smith, 1933
U.S. Pat. No. 3,325,940 Davis, 1967
U.S. Pat. No. 3,009,285 Brown, 1961
U.S. Pat. No. 3,010,249 Sirks, 1961
U.S. Pat. No. 3,157,962 Bonnely, 1964
U.S. Pat. No. 3,461,603 Rowell, 1966
U.S. Pat. No. 3,608,235 Harton, 1971
U.S. Pat. No. 5,314,369 Gamble, 1994
U.K. Patent GB416853 (A) Butler, 1934
U.K. Patent GB2325174 (B) Tett, 2000
U.K. Patent GB2374554 (A) Zabrana, 2002
In the field of orbital systems dynamics:
U.S. Pat. No. 2,204,952, Wittigschlager, 1940
U.S. Pat. No. 2,601,729 Underwood, 1952
U.S. Pat. No. 5,695,344 Tomasello, 1997
Motifs incorporating concentric circles, interlocking rings, and nesting spheres are common in the histories of artistic, philosophical, religious, and scientific thought. The convergence of these diverse fields upon these shared physical forms has rendered these motifs particularly captivating to people, as evidenced by their widespread current use in commercial art.
It is an object of the present invention to offer a mechanism which incorporates this powerful imagery and can, furthermore, contribute to the understanding and greater appreciation of each of the aforementioned domains of human endeavor.
A second object of the present invention is to provide a simple device capable of presenting, in dynamic, physical form, an orbital system similar to the Bohr model of atomic structure, which is the model most widely employed to introduce the concept to students.
A third object of the invention is to provide a mechanism which can simultaneously provide amusement, develop coordination through physical exercise, and offer an opportunity for discovery through intellectual and kinesthetic exploration of scientific principals.
The present invention resides in a mechanical assembly comprising:
The orbiters of an array may be identical, but for optimum ease of operation, and specifically in arrays intended for beginning operators or involving large numbers of orbiters, the orbiters' lengths, weights, aerodynamic properties or a combination thereof are arranged such that the orbiters will react at different rates and to differing degrees to changes made to the orientation of the axis of rotation of the bail, said changes being effectively the introduction of a secondary axis having for its center the wrist, elbow or shoulder of the operator and on which the entire assembly is made to revolve in a precessing manner in a direction opposite that of the bail's primary rotation. As the revolving orbiters react differently to this stimulus they can be caused, through the inducement of gyroscopic precession, to orbit on non-parallel planes. When this occurs, tertiary axes specific to the individual orbiters are created, having for their centers the points of attachment of the orbiters to the bail.
In order for operation to proceed as in the following two examples and as detailed below in the discussion of the attached figures and in the explanatory section titled Operation, the operator must begin by whirling the array of orbiters in such a way that the most reactive orbiter (if differences exist) precedes the others as they move through space, in order to minimize the likelihood of collision, as will become apparent through examination of the accompanying figures.
The effect created through the basic operation of such a mechanism equipped with a symmetrical bail and with an array of two orbiters of unequal length is the independent non-coplanar revolution of the two orbiters, and the rotation on a secondary, precessing axis, of the ring described by die free end of the shorter, more reactive orbiter within the greater ring described by the free end of the longer and Less reactive orbiter.
The basic effect of such a mechanism equipped with a symmetrical bail and with an array of three orbiters of unequal length is the independent non-coplanar revolution of the three orbiters and the rotation of the ring described by the shortest orbiter within the ring described by the mid-length orbiter, which is itself rotating within that described by the longest orbiter.
Other movements of the operator's body may be employed to speed, to slow, or to halt precession of one or more of the orbiters, or for example to cause the largest of the orbits to rotate around those contained by it, and are explained further in the sections titled Assembly and Operation. The two-orbiter configuration and other arrays of orbiters are included in the accompanying figures and discussion.
Assembly
Bearings:
In the assembly of the present invention any sort of bearing mechanism may be employed, so long as it allows proper rotation of the bail and of an attached array of orbiters.
Bails:
A variety of bails may be employed, which may be flexible or rigid and of any suitable material and manufacture, as long as rotation on the bearing and attachment of the orbiters are provided for. The bail may be symmetrical or asymmetrical. Bail asymmetry may, for example, be used to create the illusion of same-length orbiters, when although the distance from bail axis to orbiter end is identical for all orbiters in the array, the actual length of the free orbiters varies from one to the next, and their behaviors vary accordingly.
Orbiters and Arrays:
A variety of orbiters may be employed. The orbiters may be of any number greater than one, provided that their disposition on the bail and their properties of length, weight, and tendency to precess allow for the proper operation of the device in accordance with the explanations made in the present document.
The orientation of the points of attachment of the orbiters in relation to the axis of rotation of the bail may be parallel, perpendicular or diagonal and the points of attachment may be arranged in a linear or non-linear fashion. Arrangements of orbiters which are diagonal or parallel to the axis of rotation of the bail may be used to similar effect as those of bail asymmetry, as a point of attachment further from the hand of the operator is subject to greater movement with each change made to the attitude of the device than is a point of attachment closer to the hand of the operator, and orbiters attached thereto are affected to a greater degree.
The orbiters may be flexible or rigid. With flexible orbiters constructed of braided cord or like material it is preferable to include a swivel mechanism to minimize twisting and resultant tangling of the orbiters. Swivel mechanisms are not necessary in arrays of rigid orbiters, but they may be included to smooth the operation of the device.
The orbiters may be simple or decorated or shaped along their length for optical effect. They may be equipped internally or externally with a single fixed or movable object or with a plurality of fixed or movable objects. Said objects may be of diverse natures including but not limited to light- or sound-emitting elements and including but not limited to objects capable of exerting an effect on the trajectory of the orbiter, such as movable weights, weights reactive to centripetal force, spinning objects, or airfoils. The orbiters of a given array need not be of the same materials. The orbiters may be of fixed form or may elongate when subjected to centripetal force. The orbiters may be interchangeable. They may be modifiable in length, width, weight, appearance, and function for purposes of creation of novel visual or auditory effect and experimentation by the operator. There is a necessary correlation between the length and weight of the orbiters, and devices intended for use by children must necessarily be both lighter and smaller than devices intended for use by adults. It is possible through variation in these characteristics to produce devices operating effectively at very different rates of rotation.
It is preferable that arrays of more than three orbiters employ rigid orbiters to minimize the likelihood of tangling and to render operation more fluid. A rigid orbiter will not collapse upon itself if sufficient speed is not maintained as will a flexible orbiter, and rigid orbiters are not subject to tangling at each orbiter-to-orbiter collision. However, experienced operators may appreciate the challenge offered by flexible orbiters.
Also, with each additional orbiter in an array there is a corresponding lessening of the maneuverability of the assembly. Arrays of two orbiters are well suited to operation involving pivoting movements of the operator's body, and thus to performance applications, whereas such movements with an array of seven orbiters is likely, if not guaranteed, to provoke collapse of the mechanism.
With arrays incorporating same-length orbiters there is the added difficulty of confusion of the orbiters and these are best suited to arrays of lesser number. In addition, collision of same-length orbiters is more likely to provoke collapse of the mechanism since orbiter end collisions are more direct than collisions along the length of the orbiters, which tend to be more glancing in nature.
Handles:
A variety of integral or non-integral handles may be employed for support of the bearing-bail-orbiter assembly. Certain ergonomic variations to the handle are possible, including, but not limited to changes in the angle of the bearing surface relative to the length of the handle. In configurations where the bail rotates on an axis parallel to the length of the handle changes to the attitude of the rotating bail are made by inclining the assembly. In configurations where the axis of rotation of the bail is misaligned with the length of the handle, such changes in attitude may be made by causing the handle to rotate on an axis parallel to its length. In this way one may minimize the movements necessary to operate the device and may fine-tune attitudinal changes with less effort. Such configurations may also be employed to minimize the likelihood of collision of the whirling orbiters with the back of the operator's hand.
This great variety of components not withstanding, the elementary functional components of the mechanism remain the bearing, bail, and orbiter array, and their interaction based on the principles of pendular and gyroscopic movement as described above and illustrated in the accompanying figures.
The attached figures represent various modes of the present invention and together, with the basic description above and description of best modes following complete the disclosure of the device.
Bail 308 consists of a length of wire shaped at its extremities to form eyelets 310 and 312, and bent into the form shown, having a maximum internal diameter slightly larger than the minimum diameter of channel 306, allowing it to rotate freely around handle 300 when clipped onto it at channel 306.
The form of bail 308 prevents its accidental removal but allows its deliberate removal from handle 300, with orbiters 314 and 316 attached, for replacement with another bail equipped with different orbiters or for the purposes of converting the device from a configuration better suited to operation with the right or left hand to one better suited to operation with the other hand. This latter is accomplished by removing bail 308 and rotating it 180 degrees on a vertical axis so that the positions of extremities 310 and 312 and those of attached orbiters 314 and 316 are reversed as illustrated in
The two orbiters 314 and 316 consist of unequal lengths of braided cord or other suitable flexible material attached at their proximal ends to bail 308 with identical conventional split rings 318L and 318R and identical conventional barrel swivels 320L and 320R to which they may be tied or attached through other appropriate means. Conventional barrel swivels are employed here, but any suitable swivel mechanism may be used. Orbiters 314 and 316 are weighted at their distal ends with conventional beads 322 and 324, which must be of sufficient mass to assure the tension and easy rotation of orbiters 314 and 316, to which they are attached in an appropriate manner.
Referring to
Operation of the same embodiment configured for the left hand proceeds in the same manner, with the sense of rotation and the sequence of movements through the imaginary points reversed. A detailed explanatory text concerning this basic operation and subsequent possibilities of movement is to be found in the section titled Operation below.
Operation—Referring to the Two-Orbiter Configuration of
For the purposes of this explanation, I refer again to
Operation of the mechanism equipped with arrays of a greater number of orbiters is substantially the same as that explained here, but practice with a two-orbiter array is a necessary prerequisite, and an operator skilled in said operation will have no difficulty in extending the principles to more complex arrays.
The manipulations outlined in the discussion of the attached figures and narrated in this section describe everything necessary for an inexperienced operator to learn to perform the basic operation of the present invention, although more time may be necessary for the operator to succeed at any given step than is apparent in the description.
To use the mechanism, the operator holds the handle in a horizontal position with its distal end toward Imaginary Point I (
To cause the orbiters to occupy different planes of rotation the operator now changes the orientation of the handle, pointing the distal end up a few degrees and to the left toward Imaginary Point II and maintaining the whirling motion. This change in orientation causes both of the orbiters to deviate from their initial plane of rotation due to the inducement of gyroscopic precession. However, the shorter orbiter reacts more quickly than does the longer orbiter; its movement is greater, and is perceived by the operator and observers as independent of that of the longer orbiter.
If this orientation is maintained the shorter orbiter may eventually reach a substantially horizontal orbit and may come into contact with the operator's arm, causing the movement of the device to be interrupted or, barring this, the longer orbiter may precess sufficiently to occupy the same plane as the shorter orbiter. To avoid this situation, the operator continually changes the orientation of the handle, moving the distal end in a counter-clockwise circular path, indicating with the distal end of the handle the Imaginary Points II, III, IV, and V in series.
This continual movement must occur at a rate sufficient to avoid orbiter-arm collision and to maintain the two planes of orbit. As indicated above, if the movement through the cycle of imaginary points is too slow the longer orbiter will deviate from its plane of rotation and will move to join the shorter, more reactive orbiter. If the movement is too quick arm-orbiter or orbiter-orbiter collision may occur. In this explanation of basic operation the handle is initially held in a horizontal position, but it important to note that operation may proceed as described regardless of the initial orientation of the handle provided that the sequence of changes in orientation is respected relative to the initial plane of rotation of the orbiters.
As the operator gains proficiency this sequence of movements through the imaginary points will become more natural, more fluid and better controlled. Physical and mental concentration, leading to muscular and intellectual memory, renders the basic movements almost automatic, at which point ease of operation allows other movements to be performed.
Examples of other movements include:
The effect of these alternate movements is particularly interesting, as they may be used to cause rapid changes in orientation to a specific orbit. Movements in line with a specific plane will tend to reduce the precession of the occupying orbiter and it is also possible to pull an orbiter into a different plane of rotation by changing not the attitude of but the location of the axis. It is in this way possible to isolate one or the other orbiter and to concentrate on its movement, the simplest example being to cause the ring described by the object borne by the longer orbiter to become more dynamic and to revolve around the ring described by the object borne by the shorter orbiter. In addition, as the speed of revolution and rate of precession of the orbiters increase, smaller changes in attitude are sufficient to maintain precession or to cause changes in behavior, and it is possible for an experienced operator to use the device with almost no perceptible changes in the attitude of the handle.
The best mode envisioned at the time of this writing is a hand-held device comprising an integral or non-integral handle, a bearing surface, interchangeable rotating structures (bail), and interchangeable arrays of pendulums (orbiters) of different types including pendulums (orbiters) with light-emitting components.
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/US2011/000151 | 1/27/2011 | WO | 00 | 7/19/2012 |
Publishing Document | Publishing Date | Country | Kind |
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WO2011/094007 | 8/4/2011 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
139533 | Batchelder | Jun 1873 | A |
665980 | Roche | Jan 1901 | A |
1331971 | Adler | Feb 1920 | A |
1538720 | Mercer | May 1925 | A |
1858145 | Felardo | May 1932 | A |
1915868 | Rogers | Jun 1933 | A |
2684850 | Williams | Jul 1954 | A |
2991585 | Drees | Jul 1961 | A |
3093376 | Terry | Jun 1963 | A |
3157962 | Bonnelly | Nov 1964 | A |
3325940 | Davis | Jun 1967 | A |
3550312 | East | Dec 1970 | A |
3608235 | Harton | Sep 1971 | A |
3672093 | Meek, Sr. | Jun 1972 | A |
3693285 | Manzo | Sep 1972 | A |
3693286 | Marcotti | Sep 1972 | A |
3834069 | Brown | Sep 1974 | A |
4062542 | Manera | Dec 1977 | A |
4333658 | Giovetti | Jun 1982 | A |
D326484 | Nwoke | May 1992 | S |
D337621 | Wong | Jul 1993 | S |
5314369 | Gamble | May 1994 | A |
5492335 | Videnov | Feb 1996 | A |
6004184 | Piluso | Dec 1999 | A |
6227929 | Nelson et al. | May 2001 | B1 |
6413099 | Rainey | Jul 2002 | B2 |
6776742 | Domenge | Aug 2004 | B2 |
6802758 | Somers | Oct 2004 | B2 |
20010003644 | Rainey | Jun 2001 | A1 |
20040009833 | Selevan | Jan 2004 | A1 |
20120329360 | Edge | Dec 2012 | A1 |
Number | Date | Country |
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2515054 | Apr 1983 | FR |
Entry |
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English-language abstract of French Patent No. FR 2,515,054, downloaded from espacenet.com, Aug. 21, 2015. |
Number | Date | Country | |
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20120329360 A1 | Dec 2012 | US |