|Publication number||US3408767 A|
|Publication date||Nov 5, 1968|
|Filing date||Dec 21, 1965|
|Priority date||Dec 21, 1965|
|Publication number||US 3408767 A, US 3408767A, US-A-3408767, US3408767 A, US3408767A|
|Inventors||Anderson Gordon H|
|Original Assignee||Lakeside Ind Inc|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (4), Referenced by (28), Classifications (5)|
|External Links: USPTO, USPTO Assignment, Espacenet|
Nov. 5, 1968 G, H. ANDERSON TOY AIRPLANE WITH FOLDING WINGS HAVING TABS 2 Sheets-Sheet 1 Filed Dec. 21, 1965 INVENTOR. GOPDON ANDERSON BY u M 5M! 1 A TTUQN YS Nov. 5, 1968 G. H. ANDERSON TOY AIRPLANE WITH FOLDING WINGS HAVING TABS 2 Sheets-Sheet 2 Filed Dec. 21, 196
INVENTOR. GORDON Ll ANDERSON v/1 UM; mum
ATTORNEYS- United States Patent-O 3,408,767 TOY AIRPLANE WITH FOLDING WINGS HAVING TABS Gordon H. Anderson, Palos Verdes Estates, Calif., as-
signor to Lakeside Industries, Inc., a corporation of Delaware Filed Dec. 21, 1965, Ser. No. 515,350 10 Claims. (CI. 46-80) ABSTRACT OF THE DISCLOSURE .The device is a toy airplane made of light weight ma-v The present invention relates to a toy airplane and more particularly to a toy airplane having rearwardly folding wings which enable the plane to be launched like a rocket with the wingsfolded rearwardly, and thereafter flown and landed like a glider after the wings'have opened in flight at a predetermined time after launching.
While, many toy airplane constructions have been utilized, which have incorporated foldable wings for the purpose of enabling the plane to be launched with the wings in a retracted position, many of these have not.
been entirely satisfactory for various reasons. Some of the more common disadvantages of previous constructions have included:
(1) Difliculty in maintaining the wings in a retracted position prior to and during launching, and during initial flight of the arplane;
(2) A fragile construction which resulted'in damage to the airplane during folding of the wings, launching or landing;
(3) The provision of a complicated locking mechanism for maintaining the wings in a retracted position during launching which was unreliable in operation and costly and diflicult to assemble or replace;
(4) A wing construction which necessitated that the wings first be rotated before they could be folded back against the tail end of the airplane, with a consequent difliculty in the retracting of the wings prior to launching; and
(5) An airplane construction that was complicated and comprised a large number of parts, thereby being difficult and expensive to manufacture and assemble, and frequently impossible to repair.
The general purpose of the present invention is to provide a toy airplane having foldable wings which embraces substantially all of the advantages of prior and similarly employed toy airplanes, and which possesses none of the above-mentioned disadvantages.
It is an object of the present invention, therefore, to
provide a toy airplane which is so constructed that it can be launched like a rocket with a minimum ofair resistance, and then flown and landed like a glider without requiring further control by the operator.
An additional object of the present invention is the provision of a toy airplane having wings which may be folded rearwardly toward the tail end of the body or fuselage and which may be maintained in a retracted 3,408,767 Patented Nov. 5, 196 8 2 position during launching and initial flight of the airplane. I I
Another object of the present invention is to provide. a toy airplane having foldable wings which are normally. biased to, an open position and which may be 'easily manually retracted and maintained in a retracted posi tion during launching and initial flight of the airplane.
A further object is to provide a toy airplane having rearwardly foldable wings which are so constructed as to be maintainable in a retracted position during launch ing and the initial flight of the airplane, after which the wings will open to sustain flight ofthe airplane 'in a glider-like manner. V Still another object is to provide a toy airplane having rearwardly foldable wingswith tab means thereon, the tab means being so constructed and positioned as to' be easily gripped by the operator to maintain thewirlgsin a retracted position during launching of the airplane, to
maintain the wings in said retracted position during the":
initial flight of the airplane, and to serve as air. brakes to reduce the glide velocity of the airplane when its wings are open and it is descending.
A still further object is the provision of a toy airplane of the foldable'wing type which is durable, simple in construction, inexpensive to manufacture and assemble, easily repairable, and reliable in operation.
An additional object is to provide such a toy airplane which is so constructed that the components thereof may be easily formed or molded from a suitable plastic material so as to provide a durable, light-weight and economical construction.
According to the present invention, the toy airplane comprises a pair of wings which are pivotally mounted on the body so as to be foldable rearwardly into an abutting relation with the tail end of the body. Each of the wings is normally retained in an open positionby suitable resilient means secured to the body and to the wings. A small upright tab is provided on the outer trailing edge of each of the wings and is so constructed as to serve a three-fold purpose: (1) It can be easily gripped by the operator to hold its respective wing in a retracted position against the tail end of the body during launching of the airplane; (2) It prevents its respective wing fromunfolding to an open position during the faster initial flight of the airplane; and (3) It serves as an air brake when the wing is open to reduce the glide velocity of the plane when it is descending to thereby prevent a hardlanding and damage resulting therefrom. In operation,
increased air pressure against the surface of each of the tabs during the initial flight of the airplane prevents the wings from unfolding to an open position until the maximum height of the airplane is attained. Thereafter,
owing to reduce air pressure against the tabs, the resilient means secured to the wings and'the body causes the wings to unfold to a fully open position to thus sustain the flight of the airplane in a glider-type manner and enable it to be smoothly landed.
The present invention, both as to its organization and manner of operation, together with further objects and FIGURE 1 is a perspective view of a toy airplane constructed in accordance with the principles of the instant invention, showing the wings in a fully opened position;' FIGURE 2 is a perspective view of the airplane shown in FIGURE 1 as it is about to be launched, showing the wings held back in a retracted position against the tail end of the airplane by one hand of the operator, with the nose of the airplane being engaged by the flexiblev member of a slingshot held in the other hand of the operator;
FIGURE 3 is a bottom plan view of the toy airplane shown in FIGURES l and 2, showing one wing in an open position and the other wing in a retracted position; and
FIGURE 4 is a diagrammatic view in perspective show-' ing the intended flight path of the instant toy airplane after launching. 4
As an exemplary embodiment of the instant invention,
7 FIGURES 1 through 3 illustrate a toy airplane 10 comprising an elongated body or fuselage 12, a pair of wings 14 movably mounted on the body 12, a pair of stabilizers 16 formed integral with the body 12, and a tail fin 18 removably secured to the rear portion of the body. Each of these components of the toy airplane 10 preferably is formed or molded from a suitable flexible resilient plastic material, such as polyethylene or polypropylene. It is to be understood, however, that the airplane may be formed of any other suitable material, without departing from the principles or scope of the instant invention.
The elongated body 12 is generally U-shaped in crosssection to define a longitudinally extending, upwardly facing groove 20 therein (see FIGURE 1). In order to impart a desired amount of rigidity to the body 12, one or more cross members 22 are provided in the groove 20, preferably near the front or nose portion 24 of the body. A bumper or shock absorbing member 26 is removably mounted in any suitable manner on the nose portion 24 of the body 12, and is formed of any suitable flexible and resilient material, such as rubber or a synthetic equivalent thereof. Rearwardly of the bumper 26, the body 12 is provided with a depending projection 28 on the underside thereof, which defines a notch 3ll-that is adapted to receive the flexible member 32 of a slingshot 34 for launching (see FIGURES 1 and 2).
The airplane body 12 further comprises a pair of generally laterally extending, wing-supporting extensions or projections 36 formed integral therewith and disposed on opposite sides thereof. As illustrated in FIGURE 3, each of the wing-supporting projections 36 is provided with a depending flange 38 at its leading edge, a depending and generally laterally extending rib 40 which intersects at its outer end with the rear portion of the flange 38, and a depending pivot member 42 which is generally circular in cross-section and disposed rearwardly of the rib 40. The wings 14 have circular openings 44 near the inner ends thereof through which the pivot members 42 extend to thus pivotally support the wings on the lateral projections 36 of the airplane body 12. An elongated spring member 46, formed of any suitable flexible and resilient material, extends through aligned apertures in the pivot members 42, the body 12 and transverse ribs 48 formed on the undersurface of the wings 14. The spring member 46 serves to bias each of the wings 14 into an open position, wherein the inner leading edge of each wing engages the adjacent rib 40 on the undersurface of one of the body projections 36 (see FIGURE 3), the ribs 40 serving as means for limiting the opening movement of the wings. Each end of the spring member 46 is provided with a curl or enlargement 50 to prevent the spring mem ber from sliding out of the openings in the transverse wing ribs 48. It will be apparent, therefore, that the spring member 46 and rearwardly extending beads 52 formed on the ribs 40 of the wing-supporting projections 37, serve to retain the wings 14 on the pivot members 42.
A tab 54 is provided on the outer trailing edge of each of the wings 14 and, preferably, is formed integral therewith. Each of the tabs 54 extends both upwardly and downwardly in substantially equal distances from its respective wing 14 at substantially right angles to the upper and lower wing surfaces, and is provided with a straight outer wall '56 and laterally inwardly tapered, upper and lower, inner wall portions 58, as shown in FIGURES l and 2. The wings 14 are so pivotally mounted on the supporting body projections 36 as to be foldable rearwardly into a position wherein their trailing edges abut or are disposed closely adjacent to the body 12 of the airplane (see FIGURES 2 and 3). In this retracted position, the wings 14 are disposed beneath the stabilizers 16, and the tabs 54 are disposed in abutting relation or closely adjacent to the tail fin18. As shown in FIGURE 1, the tail fin 18 is provided with a lower portion 60 which extends beneath the body 12, so that both the upper and lower portion of the wing tabs 54 are disposed closely adjacent to a portion of the tail fin when the wings 14 are in a retracted position.
In the operation of the instant toy airplane, it is launched preferably in a vertical or near vertical direction, by engaging the flexible member 32 of the slingshot 34 in the notch 30 provided on the undersurface of the forward body portion 24 as shown in FIGURE 2. The wings 14 are pivoted rearwardly against the force of the spring member 46 to their retracted positions wherein the tabs 54 are' disposed closely adjacent to the tail fin 18. Both the upper and lower portions of the tabs are of sufficient size so that the operator may grasp either of them between his fingers and hold them against the tail fin 18 to maintain the wings 14 in a retracted position during launching of the airplane with the slingshot 34, as illustrated in FIGURE 2. With the wings in this retracted position, and because of the rearwardly tapered leading edge of the wing-supporting projections 36, the airplane presents a streamlined shape which offers minimum resistance to the passage of air during launching and initial flight.
After the tabs 54 and tail fin 18 are released from the grip of the operator, during substantially vertical launching of the airplane under the force of the slingshot member 32, the tabs 54 serve to maintain the wings *14 in retracted position against the force of the spring 46', owing to increased air pressure acting on the outer tab surfaces during the initial flight of the airplane. It is to be understood that the tabs 54 are of a predetermined size, which is relative to the strength of the spring member 46, so that the air pressure on the frontal or outer area of the tabs during initial flight of the airplane will overcome the resilient force of the spring member, thus preventing the wings from unfolding until substantially the maximum height of projected flight is attained, whereupon the air pressure is substantially reduced to allow the wings to unfold.
Referring to FIGURE 4, as the airplane nears or reaches its maximum height and is decelerating, the air pressure against thesurfaces of the tabs 54 decreases to a point where the force of the spring member 46 is sufficient to overcome the diminishing air resistance against the tabs and to open the wings 14. Thereafter, with the wings in an open position, the flight of the airplane is sustained in a glider-like manner, and it is adapted to land in a gradual and smooth flight path, owing to the air braking elfect of the tabs as the plane is descending. The forward portion 24 of the body 12 is curved slightly downwardly, as shown in FIGURE 1, so that the flexiblebumper 26 will initially strike the ground during landing to absorb the shock and prevent damage to other parts of the airplane. In addition, because the instant airplane preferably is formed substantially entirely of a flexible plastic material, it is resistant to damage from normal or even abnormal use.
From the foregoing description, it will be readily understood that the instant toy airplane is so constructed that it can be launched like a rocket to provide a minimum of frontal area which in turn reduces air resistance, and then down and landed like a glider, without requiring further control by the operator or a complicated timing mechanism. The wing tabs of the instant airplane serve the three-fold purpose of enabling the wings to be conveniently manually retained in a retracted position during launching, preventing the wings from opening during the launching and initial flight of the airplane, and reducing the glide velocity as the plane is descending. As an additional advantage, the simple construction and small number of parts of the instant airplane, and the simple manner of removably securing them, enables the airplane to be easily and cheaply assembled, and the parts thereof to be easily removed 'for repair or replacement.
It is obvious that many modifications could be made to the instant toy airplane construction without departing from the principles of this invention. For example, the wings could be so' pivotally mounted on the body that, in a. retracted position, they would be disposed over, rather than under the stabilizers of the airplane; the tabs 54 could be of any suitable shape and relative size other than those specifically disclosed herein, and the tabs need not necessarily extend in equal distances both upwardly and downwardly from the wings 14; moreover, the wings 14 could be pivotally mounted on the body 12 in any suitable or conventional manner other than the pivotal mounting specifically disclosed herein, and various types of resilient means other than the spring member 46 could be utilized to bias the wings to an open position.
It will be understood that the foregoing description and examples are only illustrative of the present invention, and it is not intended that the invention be limited thereto. All substitutions, alterations and modifications of the present invention which come within the scope of the following claims or to which the present invention is readily susceptible, without departing from the spirit and scope of this disclosure, are considered part of the present invention.
What is claimed is:
1. A toy airplane comprising:
a body having a front end and a tail end,
a pair of wings movably mounted on said body for movement between an open position wherein said wings extend laterally outwardly from said body and a closed position wherein said wings extend substantially parallel to and are disposed closely adjacent to said body, and
resilient means for urging said wings to said open position,
each of said wings having a vertical tab on the outer trailing edge thereof, said tabs being disposed closely adjacent the tail end of said body and adjacent each other when said wings are in said closed position whereby to be easily manually gripped to retain said wings in said closed position against the force of said resilient means during launching of said airplane.
2. The toy airplane of claim 1 wherein said tabs are of a size suflicient to resist opening of said wings after launching and during initial flight of said airplane, owing to increased air pressure acting on said tabs during the initial flight of said airplane.
3. The toy airplane of claim 1 wherein said tabs are rigidly secured to the trailing edges of said wings and extend both upwardly and downwardly therefrom substantially at right angles to the upper and lower wing surfaces.
4. The toy airplane of claim 1 wherein a tail fin is secured to the tail end of said body and extends both rearwardly and downardly therefrom, and wherein said tabs are disposed closely adjacent both sides of said tail fin when said wings are in said closed position.
5. The toy airplane of claim 1 wherein said body comprises lateral extensions on both sides thereof, said extensions having pivot members on which said wings are pivotally mounted.
6. The toy airplane of claim 5 wherein said resilient means comprises an elongated spring member secured to said pivot members and said wings, and wherein said lateral extensions are provided with means for limiting the opening movement of said Wings.
7. The toy airplane of claim 6 wherein said front end of said airplane is adapted to receive the flexible member of a slingshot for launching of said airplane, and wherein a flexible bumper member is removably mounted on the front end of said body.
8. A toy glider-type airplane comprising:
an elongated body having a front end and a tail end,
a pair of wings pivotally mounted near the front end of said body for movement between an open position wherein the wings extend laterally outwardly from said body and a closed position wherein said Wings extend substantially parallel to and the trailing edges thereof are disposed closely adjacent to said body, and
resilient means secured to said wings and said body for urging said wings to said open position,
each of said wings having a vertical tab formed integral there-with and disposed on the outer trailing edge thereof, said tabs being disposed closely adjacent the tail end of said body and adjacent each other when said wings are in said closed position whereby to be easily manually gripped to maintain said wings in said closed position against the force of said resilient means during launching of said airplane.
9. The toy airplane of claim 8 wherein a tail fin is provided on the tail end of said body and extends rearwardly and downwardly therefrom, and wherein said tabs extend both upwardly and downwardly from the trailing edges of said Wings and are adapted to be positioned closely adjacent both the rear and bottom portion of said tail fin when said wings are in said closed position.
10. The toy airplane of claim 8 wherein said body comprises lateral extensions on both sides thereof which are formed integral therewith, said lateral extensions having depending pivot members on which said wings are pivotally mounted for movement in a substantially common plane, and wherein said resilient means comprises an elongated spring member' extending through said depending pivot members and said body and being secured to said wings.
References Cited UNITED STATES PATENTS 2,158,377 5/1939 OHare 4680 2,417,267 3/1947 Porter 46-80 2,746,207 5/ 1956 Starkey 46--75 3,222,817 12/ 1965 Brandstetter 46-80 LOUIS G. MANCENE, Primary Examiner.
R. F. CUTTING, Assistant Examiner.
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|International Classification||A63H27/00, A63H27/01|