Note : Les revendications sont présentées dans la langue officielle dans laquelle elles ont été soumises.
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CLAIMS
1° The Shuttlecock Launcher of various uses is a flying object comprises of a
normally elastic body (which may bounce or not and which may adopt multiple
shapes) enabling to couple various directional elements (normally designed,
which influence its flight and are always placed at the rear) varying according
to all the various possible uses with the characteristics of a body (2) (or various
(48) bodies integrated in one body (2)), with an aerodynamic design - Images 1
and 6 of variable sizes according to its use, it may also adopt multiple shapes,as spheric, etc. with a cavity (1) which may cross through if partly or completely
and which may couple in different directional elements (23), (24), (33), (34),
(17), etc. with a support part (8) which may support the various directional
elements (7), (16), (17), (20), (23), (33) which may be cylindric and circled
by projection/s (5) at convenient lengths, supporting the body (2) ( as
directional elements with projection/s) by the pressure performed by the
material of the body (2) when expanded (by its adjusted measures). It is partly
or completely crossed by a cavity (9) (the axles normally fit), its preferable
shape is conic-trunk (it may also be cylindric or with different diameters, etc.and have a support part, etc.) among its possibilities ; according to the cavityshape (9) to the coupling position in the body (2) it is possible to vary ; the
elements to couple and its possible uses.
2° The Shuttlecock Launcher of various uses, according to Claim n° 1 has the
characteristics that when part (8) is coupled in the body (2) the cavity (9) is
conic-trunk, its smaller opening (4) faces the exterior, this cone shape (or theexternal face of the bigger openings (6)) shall work as a top, in order to prevent
the flexible elements (17) from falling out and be supported by a knol (18) etc.,
forming a tuft (17) be launched as a sling, by means of a thread (16) in various
possibilities ; in one of them, an end supports the body (2) by the neck (3); inanother one this thread (16) is joint to the tuft (17) in the cavity (9) they appear
from it ; either together by the opening (4) or separately by (4) and (6). The
end/s of the thread (16) may have a part/s (12) to hold (one), hollow (14) with a
cover (10) or without it and, on the opposite and a central orifice (11) to
introduce the thread (16) etc. which is fix by a knol (15) and sell rotates ( or a
similar part, or ring with an orifice in the edge), only the tuft (17) or the thread
(16).
When the bigger opening (6) of the conic-trunk faces the exterior, the cone may
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be inserted by: a) directional elements (20) which fasten tightly according to abigger penetration and b) directional elements with projection/s (23), (24),
(33),etc.
In this position the cavity (9) may be completely crossed and the external face
of the smaller opening (4) may be used as fastening of the last ring (29) of thedirectional elements with projections; of the knot/s (18), of (17) and/or of (16)
which may be used as described, with the opening (4) facing the exterior.
3° The Shuttlecock Launcher of various uses , according to Claims n° 1 has
the characteristics that the knot/s (18) etc. (of (16) and / or (17), etc.) may also
be fastened to the cavity (9) depending on its use, it may cross the part (8)
completely or partially, have various shapes, as cylinder or conic-trunk,etc. and
have a support part); by its shape ( with different diameters, conic-trunk, etc.);
by the external face of the opening situated inside the body (2); or by the
pressure performed by the material of the part (8) when expanded by this knot
(18).With a possible part with possible orifice/s,etc. wedge like and/or fitted etc.
in (9) and /or (8) fastening (18); by top/s; by an orifice/s; pressing it and the
walls of (9) and / or in (8), (16) and / or (17) etc. as (12) in (9) and / or in (6) or
(4) etc. and also this pressure of the material (9) may support directional
elements with or without projection/s.
This knot/s (18) may also be situated in the cavity (1 ) and be fastened by; thecavity shape (1) with different diameters, etc.; by one or several (48) of the
possible bodies (48) integrated in one body (2) with an orifice/s (46) or by thepressure of the material of the body (2) against this knot (18) and/or against asupport part ( with projection/s , orifice ) as a wedge or without it.
4° The Shuttlecock Launcher of various uses, according to the 1st Claim, has
the characteristics that the various elements were designed (23), (24), (33) in
order to be coupled between them, and once they are coupled they may
couple as directional elements in the body (2), with the possibility of coupling ;
either in the part (8) and in the body (2) or directly in the body (2).
Formed by; a central axle (21) on its external part with side wing/s (22), in anaerodynamic position (41) with possible fissure/s projection/s , etc.; projections
(26) fastening rings with coupling males and females (25) or without them, on
its base (28) on its internal faces (27) ( or their hypothetical extension ) forming
an angle obtained by dividing 360 degrees by the number of coupled
elements, with the possibility of coupling fewer elements ( or elements with anynumber of degrees ), proportionally completing 360 degrees with intervening
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wedges as 1, 2, 3 4, 5, etc. coupled elements, with an angle of 90 degree (31)
it is possible to couple; 4 elements (23), (24), (33) ( similar or not ); or 3 with 3
wedges of 30 degree (30) interposed; or 2 with 2 wedges of 90 degree and
with an angle of 120 degrees (32) it is possible to couple; 3 elements; or 2 with
2 wedges of 60 degree, etc.
With possible rings or similar circling the base (28) as brackets.
These directional elements (23), (24), (33) without the base (28) with the
external part only with a coupler (40) ( with changeable angle(27), males and
females or not etc.) as (38) (39), it is possible to couple the spaces (36) leftbetween some intervening elements (34) (35) which appear from the body (2)
work as a base (28), with projection/s (26), males and females (25) or without
them and/or rings, etc. and they may self couple, the same way (23), (24), (33)
and to couple; in the part (8) and in the body (2) directly in the body (2), So, it
is possible; 4 elements (38) (39) with the coupler (40) with 90 degree (31)
similar or not, coupled in 4 intervening elements (34) (35) with an angle of 90
degree (31); or 3 with 90 degree (31) in 3 intervened elements of 90 degree
(31) and with three intervened wedges of 30 degrees (30), which become
biped in the space (36), or without this biped part with another support part
(43), or without these wedges with an angle of 120 degrees (32) leaving in (36)
the spaces to couple the 3 (38) (39) with coupler (40) of 90 degree or not with
the coupler (40) with 120 degrees; or place 2 with coupler (40) with 180
degrees in 2 intervening elements with 180 degrees, etc...
This coupling and fastening system of the base (28) to the body (2), may be
used for other possible shapes or number of directional elements.
The external part of these directional elements (23), (24), (38), (39) may have
one or several integrated elements and it may adopt various aerodynamic
shapes, with one or several axles (21) or none with only a sort of aerodynamic
membrane (42) with one or several wings (22), etc.
5° The Shuttlecock Launcher of various uses , according to the 1st Claim, has
the characteristics that, these directional elements coupled (24), (23), (38),
(39) etc. or some of them, may be cast by injecting one single piece, as (7),
now with the possibilities of its external face of; a) to place 1,2,3,4, etc.
directional elements; b) adopt various shapes; c) to be joint by its wing (42) or
wings (22) or by its axles (21) etc.; d) to be used or shared one of these parts(42), (22), (21) by one or several elements at once, and they may couple;
either on the exterior of the part (8), or in the cavity (9), with the help of a
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fastening piece, as (44), or not with the base (28) integrated. and this way in
the body (2); or directly in the body (2), with these fastening pieces, as (44),with projection/s (26) etc., if the base (28) is not integrated.
6° The Shuttlecock Launcher of various uses, according to the 1st Claim, has
the characteristics that, the body (2) may be comprised of one body (2) or
various bodies (48) integrated in one body (2) image 53, which may fit into
each other in various shapes ( or various shapes at once ), as concentric
layers, or spherical sectors etc., with possible fissure/s, projection/s, male/sand female/s orifice/s (46), with the possibility of: a) change the volume only by
changing them (48) (2): b) change the external shape only by changing the
shape of the body or bodies (48) (2) or external part/s: c) one or several of
them (48) working as support part, etc, and it may (2) (48) adopt multiple
shapes and sizes in order to reach functional purposes, commercial, or any
sort of advertising messages, but also with the possibility to adopt the shape
and similarity of the product itself or the advertised object, etc....