This application was prepared with financial support from the Saudi Arabian Cultural Mission (SACM), and in consideration therefore the present inventor has granted The Kingdom of Saudi Arabia a non-exclusive right to practice the present invention.
This disclosure relates to a feather imping pin, and more specifically, to a feather imping pin with a roughened surface.
This disclosure describes a feather imping pin.
A feather imping pin attaches a donor feather to a receiving feather, the feather imping pin includes a shaft that is cylindrical with two ends and a diameter sized to slide within a receiving feather shaft of the receiving feather, and a donor shaft of the donor feather such that the shaft has a roughened surface, and the shaft fits into the receiving feather shaft of the receiving feather on one end and fits into a donor feather shaft of the donor feather on the other end so that the opposing shaft ends of the receiving feather and donor feather oppose one another and interconnect the receiving feather to the donor feather.
According to one embodiment, the feather imping pin is made of materials that have similar density to that of a feather and has similar flexibility to that of a feather.
According to one embodiment, the feather imping pin has a roughened surface.
According to one embodiment, the feather imping pin has a toothed surface. The teeth on the feather imping pin surface protrude outward. According to one embodiment, the teeth are tilted against the pin surface. According to one embodiment, the teeth are tilted in different directions against the pin surface to secure the feather imping pin within a receiving and/or a donor feather, and prevent rotation of the receiving and/or donor feather around the feather imping pin, and/or prevent movement of the receiving and/or donor feather along the feather imping pin.
According to one embodiment, the feather imping pin has a grooved surface. The grooves on the feather imping pin surface may be longitudinal, around an axis of the feather imping pin, or any combination thereof.
According to one embodiment, the feather imping pin has one or more roughened ends. Each roughened end may include a spring attached to that end.
According to one embodiment, the feather imping pin is extendable. The feather imping pin may be extendable via one or more spring-loaded sections along the feather imping pin.
According to one embodiment, there is provided a method of imping feather via a feather imping pin that is light and flexible as a feather and has a roughened surface.
According to one embodiment, glue is applied to the feather imping pin to make the pin more secure and more coherently attached.
According to one embodiment, a kit is provided for quick feather imping. The kit may include any of the disclosed feather imping pin embodiments. The kit may include a feather imping cutter. The kit may include a measurement device to measure the cross-section or other size of the receiving and/or donor feather. The kit may include a marker to mark the receiving and or donor feather before cutting. The kit may include glue for more secure and coherent feather imping.
The disclosed embodiments may be used for imping different types of feather.
A more complete appreciation of the present application and many of the advantages thereof will be readily obtained as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawings, wherein:
Referring now to the drawings,
Feather imping is performed using the feather imping pin 101 that connects the donor feather 202 and the receiving feather 201. The feather imping pin 101 fits inside both the broken shaft 203 of the receiving feather 201 and the newly cut shaft 204 of the donor feather 202. The feather imping pin 101 fits tightly inside both the broken shaft 203 and the newly cut shaft 204. The feather imping pin 101 may be inserted inside the broken shaft 203 and newly cut shaft 204 symmetrically or asymmetrically. For example, a ratio of a length of the feather imping pin 101 that is inserted into the broken shaft 203 to a length of the feather imping pin 101 that is inserted into the newly cut shaft 204 may be 1:1, 0.8:1, 1:0.8, 1:0.5, or 0.5:1. The feather imping pin 101 may include one or more marks to indicate a length to be inserted into the broken shaft 203 and the newly cut shaft 204. The feather imping pin 101 may be further secured/fixed with glue or other adhesive. Examples of glues and adhesives that can be used to further secure the feather imping pin 101 include, but are not limited to, cyanoacrylate, super glue, and epoxy.
The receiving feather 201 is usually attached to an avian but may also be a feather that is detached from an avian. The feather imping process may be performed to fix the feather of the avian as a medical aid. The avian may be sedated while the feather imping is being performed. Alternatively, the feather imping may be performed to only fix a detached feather. The feather imping may be used to connect one or more than one donor feather to the receiving feather or donor feather. For example, feather imping may be performed to connect a second donor feather to a first donor feather that is already connected to the receiving feather.
The feather imping pin 101 may be made of materials having a similar density as of the feather. Additionally, the feather imping pin 101 may be made of materials having a similar flexibility as of the feather. Alternatively, feather imping may be performed using the feather imping pin 100 that is flexible or non-flexible. Examples of materials that the feather imping pin 101 can be made of include, but are not limited to, titanium, aluminum, fiber glass, carbon fiber composite, and/or plastic.
It should be noted that when the feather imping pins 112 and 113 does not have tilted teeth 104, upon pressure to the feather after performing the feather imping, the donor feather 202 may rotate around the feather imping pins 112 and 113 or move along the feather imping pins 112 and 113, causing the feather to break again after the feather imping, which results in a need for re-imping the broken feather. Performing the feather imping with feather imping pins 112 and 113 having the tilted teeth 104 provides an advantage that the feather imping results in a more durable feather imping and a lower likelihood of a re-break of the feather. The feather imping pins, as disclosed in this application, may be made entirely from one material or may be made of a combination of different materials. For example, the tilted teeth 104 of the feather imping pins 112 and 113 may be made of a metal that is assembled on a plastic rod. Additionally, the tilted teeth 104 may cover the surface of the feather imping pins 112 and 113 entirely or partially.
At step S303, the feather imping pin (any of the embodiments disclosed in the present application) is partially inserted into the broken shaft 203 of the receiving feather 201. Glue may be applied to the pin prior to insertion. The feather imping pin may be extended to a desirable length before insertion. The extension may be via releasing one or more spring-loaded extension portions along the shaft of the feather imping pin.
At step S305, the donor feather 202 is attached to the exposed end of the feather imping pin. Glue may be applied (in any embodiment) to the feather imping pin prior to attachment. Alternatively, the feather imping pin may be partially inserted into the newly cut shaft 204 of the donor feather 202, and then, the receiving feather 201 may be attached to the exposed end of the feather imping pin.
The feather imping pin is first partially inserted into the broken shaft 203 of the receiving feather 201. Then, the donor feather 202 can be attached to the exposed end of the feather imping pin, which is inserted into the newly cut shaft 204 of the donor feather 202. Alternatively, the feather imping pin may be first partially inserted into the newly cut shaft 204 of the donor feather 202, and then, the receiving feather 201 can be attached to the exposed end of the feather imping pin, which is inserted into the broken shaft 203 of the receiving feather 201. Glue may be applied to the feather imping pin prior to any of the above-noted insertions or attachments.
It is preferred that the donor feather is selected/cut such that, after attachment, the donor feather 202 and the receiving feather 201, collectively, look like an undamaged/full receiving feather 201. It is preferred that, if the feather imping is performed on an avian that is alive and has many broken feathers that needs to be fixed, the avian being sedated.
According to another embodiment of the present application, a kit may be provided for quick feather imping. The kit may include any embodiment of the disclosed feather imping pins as described in this application. Additionally, the kit may include a plurality of feather imping pins having different sizes and lengths. The kit may further include a feather imping cutter. The kit may further include a measurement device to measure the sizes, for example, a cross-section size of the receiving feather 201 and/or the donor feather 202. The kit may further include a marker to mark the receiving feather 201 and/or the donor feather 202 before cutting. The kit may include glue for more secure and coherent feather imping. The kit may be used to fix avian having broken feathers by imping broken feathers.
The foregoing discussion discloses and describes merely exemplary embodiments of the present application. As will be understood by those skilled in the art, the present disclosure may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. Accordingly, the disclosure of the present disclosure is intended to be illustrative, but not limiting of the scope of the disclosure, as well as other claims. The disclosure, including any readily discernible variants of the teachings herein, defines, in part, the scope of the foregoing claim terminology such that no inventive subject matter is dedicated to the public.
This application is a Divisional of and is based upon and claims the benefit of priority under 35 U.S.C. §120 for U.S. Ser. No. 13/757,348, filed Feb. 1, 2013. The present application contains subject matter related to that described in commonly owned Saudi application No. 110310420, filed May 19, 2012, at the Saudi Arabian General Directorate of Industrial Property Filing and Granting, the entire contents of each which are incorporated herein by reference.
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6719793 | McGee | Apr 2004 | B2 |
20090210006 | Cohen et al. | Aug 2009 | A1 |
Number | Date | Country |
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201350321 | Nov 2009 | CN |
2 754 142 | Apr 1998 | FR |
WO 0149190 | Jul 2001 | WO |
Entry |
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Number | Date | Country | |
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20140215776 A1 | Aug 2014 | US |
Number | Date | Country | |
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Parent | 13757348 | Feb 2013 | US |
Child | 14148179 | US |