Semi-scale toy plane

Information

  • Patent Grant
  • 6688937
  • Patent Number
    6,688,937
  • Date Filed
    Friday, June 30, 2000
    24 years ago
  • Date Issued
    Tuesday, February 10, 2004
    21 years ago
  • Inventors
  • Examiners
    • Banks; Derris H.
    • Miller; Bena B.
Abstract
A semi-scale toy plane is disclosed. The fuselage is made of tetrahedral folding plates. Fuselage has a front and a rear parts. The front fuselage is an enhanced straight tube, the rear fuselage is a tetrahedral cone. Front and rear fuselages are joined by joint members. Rear fuselage and tail plane are integrally formed with a crease divided therebetween. Wing is secured to fuselage by engaging buttons to button holes. V-shaped dihedral frames are secured between wing and dihedral holders of fuselage. This invention is capable of finishing assembly in about 10 seconds without requiring a user having any glue, tool, skill or aerodynamics knowledge.
Description




FIELD OF THE INVENTION




The present invention relates to toys and more particularly to a semi-scale toy plane having the characteristics of easy assembly.




BACKGROUND OF THE INVENTION




Model planes have been popular for a long time. In the past, model plane is made of lightweight wood. Recently, model plane is mostly made of plastic material. However, the conventional design suffered from a disadvantage. For example, it usually requires a person have some aerodynamics knowledge and skill in order to assemble the components of model plane. As such, an ordinary person, especially a child, may not able to assemble a model plane in a quick and correct way. This often frustrates many people. In conclusion, the conventional model plane is a hobby not that a toy.




SUMMARY OF THE INVENTION




It is therefore an object of the present invention to provide a novel lightweight semi-scale toy plane having the advantage of quick assembly without requiring a user having any skill or aerodynamics knowledge.




To achieve the above and other objects, the present invention provides a semi-scale toy plane wherein the fuselage is made of tetrahedral folding plates, fuselage has a front and rear parts, the front fuselage is a tetrahedral straight tube for receiving rubber band, the rear fuselage is a tetrahedral cone, front and rear fuselages are joined by joint members, rear fuselage and tail plane are integrally formed with a crease divided therebetween, wing is installed to fuselage by engaging buttons to button holes, and V-shaped dihedral frames are secured between wing and fuselage.











The above and other objects, features and advantages of the present invention will become apparent from the following detailed description taken with the accompanying drawings.




BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is an exploded view of the flat fuselage plates of the invention;





FIG. 2

is a front view of the basic form of the joined flat fuselage by

FIG. 1

;





FIG. 2A

is a front view of the basic form of tetrahedral fuselage folding plates by

FIG. 1

;





FIG. 3

is an exploded view of the fuselage components with the member parts according to the invention;





FIG. 4

is a longitudinal-sectional view of the assembled fuselage of

FIG. 3

;





FIG. 4A

is a perspective view of a joint member of front fuselage of

FIG. 4

;





FIG. 4B

is a plan view of a joint member of rear fuselage of

FIG. 4

;





FIG. 5

is an enlarged longitudinal section view of the disengage form of

FIG. 4

;





FIG. 5A

is a schematic plan view of a joint member of rear fuselage of

FIG. 4

;





FIG. 6

is a perspective view of the assembled tail plane of

FIG. 3

;





FIG. 6A

is a cross-sectional view taken along line A—A of

FIG. 6

showing the assembly of tail plane folding plate;





FIG. 7

is a perspective view schematically showing the assembly of wing to the fuselage of the invention;





FIG. 8

is a perspective view showing the assembly of V-shaped dihedral frame of the invention;





FIG. 9

is a perspective view showing the assembly of bowed dihedral by six support points; and





FIG. 10

is a perspective view showing the features of four trilateral structures between fuselage and wing of the invention.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS




The semi-scale toy plane of the invention is made of a lightweight polystyrene paper (PSP) in replacement of conventional Balsa wood. The specific gravity of PSP is lower than that of Balsa wood, it is possible making a wing loading of 6g/dm


2


, also it is possible that the PSP material printed with a color pattern prior to being cut into fuselage plates of the invention, and has the advantages of low cost and thus are widely used in manufacturing toys. The only drawback of PSP is that it is loose. As such, it is necessary to enhance the strength of PSP by adding a few molding members and steel wires into it. As a result, a desired semi-scale PSP plate is obtained by the invention.




Above semi-scale idea means that fuselage is made as a tetrahedral tube shape or conic shape after two fuselage plates are joined. The tetrahedral shape used herein means that it consists of regular tetragon or rhomb and two diagonals which are normally crossed. The profile area of the tetrahedron is subject to design requirements. The maximum torsion of tetrahedral plate is determined by the diagonals, PSP foam density, and the thickness of plate. In an experimental data, a tetrahedral tube having a specific gravity 0.1, thickness 2 mm, and side length 20 mm can withstand


250


complete rotations of four 1.5mm


2


rubber bands without breaking or contorting.




The fuselage of the invention is joined by two parts. The front fuselage is generally an enhanced straight tube for receiving rubber band. The rear fuselage is generally a tetrahedral cone.




The invention adopts a button hole design of installing wing and implements a V-shaped dihedral frame design. This is an improvement to prior art which typically glues components together.




Referring to

FIG. 1

, there is shown four fuselage plates (e.g., left and right front fuselage plates


11


and left and right rear fuselage plates


12


) constructed in accordance with the invention. Each fuselage plate


11


has two outer creases


111


and an inner crease


112


. Similarly, each fuselage plate


12


has two outer creases


121


and an inner crease


122


. In front fuselage


11


, inner crease


112


is parallel to outer creases


111


such that a generally straight tube is formed. In rear fuselage


12


, inner and outer creases


122


and


121


are tapered toward rear to form a cone. Rear fuselage


12


and tail plane


13


are integrally formed. Only a crease


131


is seen between tail plane


13


and rear fuselage


12


.




Referring to

FIG. 2

, the diagrammatic number


21


is a basic form by joining left and right side of fuselage plates


11


(or


12


) before folding work, while outer creases


111


(or


121


) and inner crease


112


(or


122


) of left fuselage plate are direct towards outer creases


111


(or


121


) and inner crease


112


(or


122


) of right fuselage plate, and the area out of outer creases


111


(or


121


) is adhered together.




Referring to

FIG. 2A

, the diagrammatic number


22


is a basic form of tetrahedral fuselage folding plate by FIG.


2


. Note that this tetragon consists of regular tetragon or rhomb in consideration of the vertical diagonal


221


is normally crossed the horizontal diagonal


222


.




Referring to

FIG. 3

, an assembly of fuselages


11


,


12


is detailed below. Incident shelf


34


has a leading edge button


341


and a trailing edge button


342


, and two button necks


343


each abutted to buttons


341


,


342


. Buttons


341


,


342


are made different for avoiding the inversion of wing during installation. Dihedral frame holder


35


comprises a neck


351


and a landing gear socket


352


, wherein dihedral frame holder


35


and neck


351


are exposed. Tail member


36


comprises a movable tail plane holder


361


and a tail skid


362


adhered to fuselage. Head member


37


is then assembled with front fuselage


11


after folding work of fuselage has been completed. Head member


37


comprises a propeller journal bearing


371


and a front landing gear socket


372


. Joint member


31


is mounted in rear of front fuselage


11


. Joint member


32


is mounted in front of rear fuselage


12


. These two joint members


31


,


32


are detachably joined together so as to join or detach front and rear fuselages


11


,


12


in a quick manner. As to tail fin


38


, it is a single plate stuck between two rear fuselage plates


12


. The construction of tail fin


38


is not the subject of the invention.




Referring to

FIG. 4

, there is shown an assembled fuselage with propeller, rubber bands and rubber hook


41


in the joint member


31


. Referring to

FIGS. 4A and 4B

, two joint hooks


42


are provided on the top and bottom of joint member


31


respectively. Joint hooks


42


cooperate with escapement


43


in the joint member wherein the wedge portions of joint hooks


42


extend beyond escapement


43


so as to flexibly-secure together.




Referring to

FIGS. 5 and 5A

, a description of disassembly of the two-part fuselage is detailed below. A thin arcuate escapement


43


is connected between top and bottom corners of joint member


32


of rear fuselage. In disassembly, press the left and right sides


51


of joint member


32


toward each other as indicated by arrows. This will increase the distance between the top and bottom corners, i.e., increase the distance between escapement


43


. As a result, two joint hooks


42


disengage from escapement


43


.




Referring to

FIGS. 6 and 6A

, tail planes


13


are formed by unfolding from crease


131


. Tail plane holder


361


is hooked to tail plane hook


363


, this completes a horizontal stabilizer.




Referring to

FIG. 7

, wing


71


has a crease


72


along its length to fold up an aerofoil profile for lift. A leading edge button hole


73


and a trailing edge button hole


74


formed on the center of wing


71


for permitting leading edge button


341


and trailing edge button


342


to insert and secure therein respectively. Button slits


75


of button holes


73


and


74


cling into button necks


343


of buttons


341


and


342


. This wing and fuselage joining is stable in the longitudinal direction, while not stable in the lateral direction.




Referring to

FIG. 8

, a pair of V-shaped dihedral frames


81


are provided to enhance the stability of wing


71


in the lateral direction. V-shaped dihedral frame


81


is formed of a thin metal wire comprising two sticking pieces


82


each having a groove


821


, and a dihedral framing ring


83


formed at the bottom of the dihedral frame


81


, four sticking pieces


82


are adhered to the wing


71


.




Referring to

FIGS. 9 and 10

, dihedral framing rings


83


is clung to neck


351


of dihedral frame holders


35


. As such, wing


71


are supported in six points


92


A to


92


F and secured to bowed dihedral


91


of fuselage (FIG.


9


). As shown in

FIG. 10

, four trilateral structures


101


W,


101


X,


101


Y, and


101


Z are formed, provide a competent strength of structure.




The invention is capable of finishing assembly in about


10


seconds without requiring any glue, tool, skill or aerodynamics knowledge. This is also true for detaching the same.




While the invention herein disclosed has been described by means of specific embodiments, numerous modifications and variations could be made thereto by those skilled in the art without departing from the scope and spirit of the invention set forth in the claims.



Claims
  • 1. A semi-scale toy plane comprising:(a) a fuselage including a front fuselage and a rear fuselage each formed of regular tetragonal or rhombic folding plates; (b) a tail plane integrally formed with the rear fuselage which are spaced into a plurality of different sections by a plurality of creases; (c) a wing secured to the front fuselage through six supporting points; said wing being a bowed dihedral framing; and (d) four trilateral structures; each having a V shaped dihedral frame and being installed between the front fuselage and the wing; each side of the fuselage having two trilateral structure.
  • 2. The semi-scale toy plane of claim 1, wherein said fuselages is formed by a plurality of tetrahedral folding plates.
  • 3. The semi-scale toy plane of claim 2, wherein each of said tetrahedral folding plate of the front fuselage is formed as a straight tube, each of the tetrahedral folding plates of the rear fuselage is tapered toward the rear as a cone, the front and the rear fuselages are detachably secured by a pair of joint members with joint.
  • 4. The semi-scale toy plane of claim 1, wherein both sides of the tail plane are integrally formed with the rear fuselage, and each divided by a tail crease such that the expanded tail planes are secured by a movable tail plane holder for forming a horizontal stabilizer.
  • 5. The semi-scale toy plane of claim 1, wherein the V-shaped dihedral frame is formed of a thin metal wire, a dihedral framing ring formed at a bottom the V-shaped dihedral frame and a movable sticking piece positioned at a tip point of The V-shaped dihedral frame.
US Referenced Citations (5)
Number Name Date Kind
1883651 Ensley Oct 1932 A
2251090 West Jul 1941 A
2864613 Porter Dec 1958 A
4895541 Miller Jan 1990 A
5482489 Stone Jan 1996 A