The invention relates to a shuttlecock with a crown having a substantially conical shape, wherein the crown is connected to a striking cap in the region of the narrow crown end.
WO 2005/000428 A1 includes a number of terminology definitions which can analogously be adopted for the present invention.
The conventional subject matter disclosed therein is a shuttlecock with a conical crown and a striking cap arranged on the crown. At least one removable ring is arranged on the crown which can be used to alter the flight characteristics. The crown itself has a straight conical surface envelope.
It is an object of the invention to provide a shuttlecock which has improved flight characteristics compared to conventional shuttlecocks and which ensures, more particularly, a stable flight path and a greater range.
The shuttlecock should also retain to the greatest possible extent its dimensional stability even when damaged.
The object is solved with the invention by the features in the characterizing portion of claim 1. Advantageous embodiments of the invention are recited in the dependent claims.
According to the invention, a shuttlecock is provided which has a conically shaped crown that is connected with a striking cap. Unlike the otherwise straight conical envelope in the end region of conventional shuttlecocks, the surface envelope of the crown is here provided with an inwardly curved radius in the region of the crown opening. The surface envelope, which is inwardly curved in the end region of the crown opening with a radius, reduces the air resistance of the shuttlecock, meaning that the shuttlecock experiences less wind resistance along its flight path. This shape of the surface envelope with an inwardly curved radius in the region of the crown opening advantageously also reduces the deviations of the shuttlecock during flight from its intended flight path in crosswind. The shape of the shuttlecock according to the invention also points the shuttlecock much better into the wind on its flight path than a smooth conical shuttlecock with a straight surface envelope. At the same time, the shape of the shuttlecock according to the invention keeps the shuttlecock on its path and extends the range, because the shuttlecock does not rotate in the air along its flight path about its own axis, i.e., around itself.
According to an advantageous embodiment of the invention, the cross rib arranged at the crown opening has a wavelike shape. As a result, the end segments at the crown opening have indentations and protrusions. This also improves the accuracy of the flight path and of the flight trajectory, and the shuttlecock also becomes dimensionally more stable. Consequently, even if continuous use of the shuttlecock causes partially vertically extending cracks, its flight characteristics remain superb.
By only providing the transverse rib disposed at the crown opening with a wavelike shape, the shuttlecock does not rotate about its own axis during flight.
Advantageously, with this embodiment of the shuttlecock, either the wave maximum is located at a longitudinal rib and the wave minimum is located centrally between the longitudinal ribs, or vice a versa.
The flight characteristics can be further improved by arranging the segment ribs in the end segments in the region of the crown opening with mutually different spacing.
The flight stability and range can be further improved by implementing the transition between the striking cap and the press ring without a step.
The invention will now be described in more detail with reference to exemplary embodiments which are at least partially illustrated in the drawings. It is shown in:
As seen in
The segments 7 have segment ribs 8. The segment ribs 8 have different spacings from one another in the end segments 7a proximate to the crown opening 3. For example, the separation between the segment ribs in the end segments 7a can be very narrow on one side and somewhat wider on the other side.
As seen from
Releasable rings 11 can be arranged between the crown 1 and the striking cap 9 for increasing the weight of the shuttlecock and changing the flight characteristics, as illustrated in the Figure and in
The cross-sectional view according to
The invention is not limited to the illustrated embodiments. Additional modified embodiments can be realized by modifying the aforementioned elements and features, without departing from the spirit of the invention.
Number | Date | Country | Kind |
---|---|---|---|
10 2007 041 169.5 | Aug 2007 | DE | national |
This application is a National Phase Patent Application of International Patent Application Number PCT/EP2008/061061, filed on Aug. 25, 2008, which claims priority of German Patent Application Number 10 2007 041 169.5, filed on Aug. 24, 2007.
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/EP08/61061 | 8/25/2008 | WO | 00 | 2/18/2010 |