The invention relates to an electric power, paper airplane, conversion kit and conversion unit.
A common paper glider/sailplane, folded from standard A4 or letter paper by following the steps shown in
The invention concerns an electrical power conversion kit/unit which can be mounted on such common airplane design to provide adequate propulsion to transform the paper sailplane into a free flight, soaring paper airplane.
A prior electric power conversion unit, disclosed in my prior patent publication 2008/0125002, published May 29, 2008, and comprising a battery housing nose-piece connected by a wire receiving conduit to a rear electric motor driving a propellor is secured to the leading edges of the paper aiplane wings on each side of a central (fuselage) crease by a nose-piece clip portion. The clip portion has a pair of leaf springs extending rearwardly in spaced-apart, coplanar, side-by-side relation below the battery holding housing portion. A vertical fold/paper (fuselage) crease is received between the leaf springs which exert a vertical clamping force on leading edge portions of the horizontal wings on each side of the crease.
A disadvantage of my prior approach is that the clip exerts only a vertical clamping force on the paper wings which can be insufficient for reliable retention during powered flight and does not reliably prevent yaw of the power unit relative to the paper plane when under power, as torque is applied to the power unit as a result of the rotation of the propellor.
It is an object of the invention to provide a power unit which reliably mounts to a paper airplane throughout powered flight without significant yaw and to improve the power to weight relation by obviating the requirement for a relatively heavy battery to be the power source.
According to one aspect of the invention, a toy airplane comprises paper wings extending horizontally from respective opposite longitudinal free edges of a vertical, fuselage forming crease and an electric power conversion unit operably mounted thereon, the electric power conversion unit comprising:
a nose piece molded in one piece of plastic and comprising a combination capacitor mounting portion and nose clip;
a rear propulsion unit including an electric motor mount and motor driving a pusher propellor and,
an electrical lead connecting the capacitor to the electric motor and contained in a conduit extending rearwardly (above the crease) to the tail; wherein:
the conduit is of square cross-section and keys into a complementary socket of the motor mount maintaining the rear propulsion unit tilted upward at a predetermined angle relative to the nose-piece as required for flight stability; and,
the nose clip comprising a pair of cantilever spring arms extending rearwardly in spaced-apart, coplanar, side-by-side relation under the capacitor mounting portion and having converging portions adjacent their rear free ends and,
a stubby, paper spreading fin depending from the nose-piece rearward of free ends of the springs and stuffed into the vertical paper crease, maintaining the paper walls of the crease spread apart with the vertical paper crease received between the leaf springs and the converging portions of the spring arms in horizontal, inward clamping engagement with the vertical walls of the paper crease which are urged horizontally apart by the spreading action of the fin and with leading edge portions of the horizontal wings on each side of the crease clamped vertically between respective cantilever arms and the capacitor mounting portion.
The weight of the conversion kit in the center of the airplane will tend to raise the dihedral angle, (the wings), thus reducing lift properties. The crease spreading action of the fin will tend to reduce the dihedral angle, forcing the wing tip downward at least partly compensating for the weight effect of the conversion kit.
In order that the invention may be readily understood, a specific embodiment thereof will now be described with reference to the accompanying drawings in which:
As shown particularly in
The propulsion unit is a rear pusher propeller which will, in operation, tend to demount the module from the paper airplane nose. In order to retain the nose-piece firmly and accurately in place, the nose-clip has three special friction gripping interfaces including a pair of rearwardly convergent leaf springs 11 in cooperation with a rearwardly adjacent, crease spreading fin 12.
The first is achieved by the cantilever arm springs pressing upwards so that the horizontally extending paper 13 is gripped between the springs 11 and opposed, spaced apart limbs 14 of a rectangular portion of the frame, together with the tube 8.
The second friction interface is on the sides of the vertical V-shape fuselage forming crease 5. The cantilever spring arms of the clip portion clamp vertical walls of the crease horizontally together (
The third friction element is the crease spreading/stuffing fin 12, depending rearwardly of the frame member of the nose-piece, and positioned to protrude into the crease. The counter-reacting forces between the springs 11 and the outer surfaces of the paper forming the V-groove, the fin and the inner sides of the paper V-groove and bottom horizontal surface of the clip frame and the top surface above the V-groove, provide a strong gripping action creating the required fastening and accurate solution needed.
The capacitor 7 is securely mounted to the nose-piece housing against an upstanding rear abutment portion 15, by reversely bending the capacitor leads 16 into front opening wire retaining grooves 17, preformed on opposite sides of outwardly extending lip flanges of an annular frame portion 19 and then bending the wires downward behind those flanges, as best seen in
The power unit is balanced/weighted to be slightly nose-heavy so that, when installed on the common, neutrally balanced paper airplane, the center of gravity of the assembly is shifted slightly towards the front/nose, intentionally providing additional stability during flight. Control of the direction of flight is achieved by forming elevators and a rudder by severing and bending the trailing edges of the paper stock prior to launch, as indicated in
The nose of the conversion kit/power unit protrudes beyond the paper airplane front to provide extra protection in case of crash.
The weight of the conversion kit in the center of the airplane will tend to raise the dihedral angle (wings) thus reducing lift properties. The crease spreading action of the fin will tend to reduce the dihedral angle, forcing the wing tip downward (
This special clip design can be incorporated in a conversion kit that has radio control capability controlling the thrust and pitch by increasing propeller speed and yaw by a rear controllable rudder.
This is a continuation of application Ser. No. 13/848,151 filed Mar. 21, 2013, the disclosure of which is incorporated by reference. Priority is claimed from my provisional application 61/614,390 filed Mar. 22, 2012, the disclosure of which is incorporated herein by reference. The disclosure of my design patent application Ser. No. 29/416,487 also filed Mar. 22, 2012, is also incorporated herein by reference.
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Number | Date | Country | |
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61614390 | Mar 2012 | US |
Number | Date | Country | |
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Parent | 13848151 | Mar 2013 | US |
Child | 15186711 | US |