Toy Flying Disc

1. Field of Invention

This invention is a toy flying disc having a particular construction to result in improved stability of flight and direction in flight.

2. Description of the Prior Art

Whirling or flying discs are a popular toy and a principal object has been the effort to stabilize the flight and thus lengthen the extents of flight.

In reference to U.S. Pat. No. 2,659,178, the disc is denominated to be a saucer and represents an inverted bowl having a substantially flat top portion formed as a dome having a non-rotatable underlying floor having an outwardly extending rudder which retains the floor plate against rotation.

In U.S. Pat. No. 4,209,936 a flying saucer is disclosed with a flexible pivoted tail which tends to oscillate with the saucer in flight and trail in a direction opposite to that of flight.

In U.S. Pat. No. 4,846,749 a saucer like device is disclosed having an overhead centrally mounted propellor having an adjustable pitch of the blades.

Reference is also had to U.S. Pat. No. 5,324,223 disclosing a flying toy comprising a disc having overhead a toy aircraft having an operable fan which in its rotation allegedly aids in the flight of the disc.

A principal object of this invention is to provide a toy flying disc having superior flying qualities which embody superior stability and operating controls.

It is a particular object of this invention to provide a disc particularly configured to cause the passing air currents to impose a stabilizing pressure on the disc.

It is a further object to pivot a fuselage section to said disc having a particularly devised pivot to connect the two, said pivot having an enlarged washer between said fuselage and disc to stabilize the same and with the fuselage having a tail section directionally adjustable to cause said disc to pursue a particular course such as a circular course.

It is another object to transversely configure the disc and particularly the rim portion thereof whereby the air streams passing therethrough engage the upper and lower facing surfaces of said rim portion to cause the same to be stabilized to insure a longer flight and cause the disc to be responsive to the directional control of the tail piece.

These and other objects and advantages of the invention will be set forth in the following description made in connection with the accompanying drawings in which like reference characters refer to similar parts throughout the several views.

FIG. 1 is a view in side elevation;

FIG. 2 is a top plan view;

FIG. 3 is a view in cross section taken on line 3--3 of FIG. 1 as indicated;

FIG. 4 is a vertical longitudinal section taken on line 4--4 of FIG. 2 as indicated;

FIG. 5 is a view in cross section taken on line 5--5 of FIG. 4 as indicated; and

FIG. 6 is an enlarged expanded view of a pivot structure.

With particular reference to FIGS. 1 and 2, the device comprising the invention herein is indicated by the reference numeral 10 and includes a disc 12 having a tail section or fuselage 14 pivoted thereto by a pivot 16.

Referring now particularly to FIG. 4, the disc 12 is saucer like in form and is shown in an inverted or upside down position having a concave bowl 12a forming a convex upwardly facing top portion 12b and having formed thereabout a circular upturned perimeter or edge portion 12c having formed between it and said convex top portion a concave circular passage or rim flange 12d.

Extending outwardly of said disc 12 and pivoted thereto, as will be described, is a fuselage or tail section 14. Said fuselage as shown in plan in FIG. 2, is plate like in form having a front end nose section 14a here shown as being rounded and said fuselage extends rearwardly widening transversely having rearward transversely spaced end portions or tail sections 14b and 14c having a V-shaped separation 14d therebetween. Forwardly of said V-shaped separation 14d is a V-shaped opening 14e.

Upstanding centrally longitudinally from each of said end portions or tail sections are substantially triangular upstanding rudder members 17 and 18, said tail sections being respectively slotted at 14f and 14g to receive therein said rudders, the rudders being secured as with a suitable adhesive not shown. Carried by said rudders and extending thereacross horizontally is an elevating member 19 which is shown being triangular in plan. Said elevating member is slotted as at 19a and 19b being disposed to respectively receive in said slots said rudders 17 and 18. The slots are tightly fit said rudders but permit vertical movement or tilted movement of said elevating member thereon as indicated in FIG. 3. The tilting of said elevating member causes the device to define a particular flight pattern.

Referring now to the pivot 16 which connects said fuselage and said disc, said pivot as shown in FIGS. 5 and 6 is disposed through a front end central vertical opening or hole 14h in said fuselage and through the central opening 12e in said dics. Said pivot comprises a stem 16a having an enlarged circular flange like head portion 16b and a split tapered bottom end portion 16c having a slightly enlarged collar 16d and an upward extending slot 16e from said bottom end portion, the same being somewhat yielding to be compressible. Said stem is disposed through said slot 14h in said fuselage and placed onto said stem underlying said fuselage is a collar 16f which is oversized to provide a supporting surface for said fuselage, said stem is then disposed through the hole 12e into the base of said pivot which comprises a bottom collar 16g having upstanding therefrom a stub sleeve 16h having therethrough a hole 16i through which is disposed the bottom portion 16c of said stem 16a, said collar 16f being compressed in being squeezed through said hole 16i and through the collar 16g to expand thereunder for a secure hold as shown in FIG. 5.

Referring to the drawings, the device 12 is contoured having a concave underside resulting in a convex upper facing side and adjacent to the perimeter of the upper facing side is a concave passage. The effect thereof upon an airstream thereover with the device in flight is to stabilize the device for flying horizontally for a greater distance than otherwise.

The pivot 16 connecting said disc and the fuselage (FIGS. 4 and 5) has a fairly substantial washer 16f disposed therebetween to maintain the fuselage in a horizontal position relative to the general plane of the disc.

The fuselage has a unique function whereby it pivots very readily to always be trailing said disc in flight and it affects the direction of the flight of the disc.

At the tail end section of the fuselage is the elevating means 19 which is carried by the pair of spaced rudders 17 and 18 and is attached to said rudders to be tiltable as indicated in FIG. 3. The tilt causes the device when launched by a forward thrust to pursue a circular course.

The fuselage being formed to be platelike and flared in width rearwardly has significant influence in causing said device to have an extended horizontal flight.

The underlying concavity and the overlying convexity of the disc appear to reduce air friction to a nominal amount causing considerable improvement in extending flight movement.

It will of course be understood that various changes may be made in the form, details and arrangement of the device comprising the invention such as discussed and defined in the appended claims.