US2397364A

US2397364A - Toy airplane

Info

Publication number: US2397364A
Application number: US536594A
Authority: US
Inventors: Fred D Myers
Original assignee: General Mills Inc
Current assignee: General Mills Inc
Priority date: 1944-05-20
Filing date: 1944-05-20
Publication date: 1946-03-26
Anticipated expiration: 1963-03-26

Description

March 26, 1946. F. D. MYERS TOY AIRPLANE Filed May 20, 1944 1N VEN 7' 01? FEED "D. M YER? 5r TTY March 26, 1946.. F. D. MYERS 2,397,364

T TOY AIRPLANE Filed May 20, 1944 3 Sheets-Sheet 2 INVENTOIE March 26, 1946.

TOY AIRPLANE Filed May 20, 19:44

' 3Sheets-Shee 3 d. YEES ATTY Patented Mar. 26, 1946 TOY AIRPLANE Fred D. Myers, Minneapolis, Minn, assignor: to General Mills, Inc., a corporation of Delaware" Application May 20, 1944, Serial No. 536,594:

16 Claims. (Cl. 46

This invention relates to improvements in cutouts for constructing a model airplane from sheet material such as paper.

Numerous attempts have been made to produce toy airplanes capable of sustained flight over appreciable distances. These attempts have met with varying degrees of success. Largely, the toys thus produced have, however, been'a disappoint ment in that they are incapable of any pro-, longed flight and/or have been unduly cumbersome to construct.

It has now been discovered that toy airplanes, which may, if desired, be quite accurate replicas of full-sized planes, may be constructed with great ease and facility even by young children. Moreover, such toy airplanes are capable of sustained flight over appreciable distances, especially under outdoor flight conditions. These results have been achieved by means of the present inventors designs of the respective arts and the method of assembly. The parts may be supplied in the form of a sheet having the parts illustrated thereon or in the form of the parts al-' ready cut out from the sheet material.

It is, therefore, a primary object of the invention to provide illustrations of the respective parts of a toy airplane, capable of being assembled with ease to form a toy airplane capable of sustained flight over appreciable distances.

Another object of the present invention is to provide a novel design of airplane cut-outs.

Another object of this invention is to form a part ofthe fuselage of a model airplane in such a manner that the application of a wing cut-out thereon will automatically position the end portions thereof on a predetermined dihedral angle.

A further object of this invention is to form a part of the fuselage of a model airplane in such a manner that the application of a wing cut-out thereon will automatically position the wing at right angles transversely of the fuselage.

Other objects of this invention will be apparent from the following description, reference being had to the drawings, in which:

Figs. 1 to 9, inclusive, illustrate cut-outs from a sheet of paper. These cut-outs when folded, glued and assembled according to instructions, will form a model airplane that is a replica of an airplane.

Figure 1 illustrates the fuselage cut-out;

Figs. 2 and 3 illustrate the inner and outer nose cone cut-outs, respectively;

Fig. 4 illustrates the cockpit cover cut-out;

Fig. 5 illustrates the rudder cut-out;

Fig. 6 illustrates the stabilizer. cut-out;

Fig. '7 illustrates the ventilator cut-out;

Fig. 8 illustrates the weight holder cut-out;

Fig, 9 illustrates the wing cut-out;

Fig. 10 is a view principally in side elevation of a model airplane constructed from the cut-outs shown in Figs. 1 to 9, inclusive;

Fig. 11 is a fragmentary detail view in horizontal section. taken on the line ofFig.

Fig. 1215 a view in transverse vertical section taken on theline |2|2 of Fig. 10;

Fig. 13 is a viewin longitudinal vertical section taken centrally through the fuselage, the cockpit cover and. the wing'of the model airplane shown in Fig. 10; i

Fig. '14 is a view partly in edge elevation and partly in transverse vertical section taken on the line |4-|4 of Fig. 10;

Fig. 15 is a fragmentary detail view partly in side elevation and partly in section taken on the irregular line |5-| 5 of Fig. l6;'

Fig. 16 is a 'view partly in edge elevation and partly in transverse vertical'section'taken on the line |6|6 of Fig. 15;

Fig. 1'? is a detail view in section taken on the line |'|-l'| of Fig. 10;

Fig. 18 is a detail-view partly in plan and partly in section takenon' the line |8--|8 of Fig.10; y A

Fig. 19 is a front "elevation of the model airplane shown in Fig. 10 and Fig. 201s a fragmentaryplan view of thesame.

The model airplane includes the following cutouts, to wit: thefuselage 2|, the inner cone 22, the outer cone 23, the cockpit cover 24, the rudder 25, the stabilizer 26, the ventilator .21, the weight holder 28 and the wing2 9. These cut-outs shown in Figs/1 to 9, inclusive, are just as they appear after having been cut from one or more sheets of paper on which theyare printed- Fuselage The fuselage 2| is formed from a single piece of paper and when folded and certain of the parts thereof connected by glue, is a replica of the fuselage of an airplane of which it is a model. The broken line 30 is at the transverse center of the fuselage 2|. On each side of the line 30 are front, intermediate and rear broken lines 3|, 32 and 33, respectively. Primarily the lines 3| are in forwardly converging relation and the

lines

32 and 33 of each pair are in forwardly diverging relation. For the sake of brevit the prefix cut-out" will not be used when referring to the illustrations in Figs. 1 to 9, inclusive.

Front and rear pairs of V-shaped notches 34 extend inwardly from the longitudinal edges of the fuselage 2|. The apeXes of the notches "34 are at the adjacent ends of the broken lines 3| and 32 and 32 and 33. These notches 3llfdividef' the bottom of the fuselage 2|, outwardlyof the rear two-

part sections

35, 36 and 31. When the fuselage 2| is folded, the

bottom sections

35,

and 31 are inoverlappingrelation and form a two-plybottom'for the fuselageji and thereby reinforce the same. The purpose of the notches 34 is to permit the bottom'of'the fuselage 2| to be'bent to position the several sections thereof relative to each othenas shown in Fig. 10. The perimeter of each member of. the bottom sectionsi. 35 and 3B is rectangular and the perimeter of each member of each bottom section 31 is wedge-shaped and the, taper thereof is toward the rear of the fuselage 2|. I

A deep-.V-shapednotch;38 extends longitudinallyginto the fuselage 2i from-the front end thereof and its apex is substantially on the line 30. At the inner end of the notch 38 is a second notch 39. This notch 39is in the form of an equilateral triangle, with its apex at the apex of the notch 38 and forms a. continuation of the notch 38 on the line 30. The purpose of the notch 39 is to permitthe edge portions 40 of the fuselage 2| at the notch'3 8 to be brought into overlapping relation and without overlapping the main body of said fuselage. The edge portions 40 of the fuselage 2|, when brought into overlapping arrangement, lowers the height of said fuselage at its front end portion. V

Qutwardly projectingtabs 4| are formed on the longitudinal edges of one of the-members of the

bottom sections

35, 36 and 31, and slits-42 therefor are formed on the broken lines 3|,;32 and 33 on the other members of said bottom sections. The insertion of thetabs 41 into the slits 42 .Drings the membersof each pair of bottom sections'35, 36 and 3'! into coincident relation, atj-the time said bottom members are being folded into overlapping positions. A pair of tabs 43 is formed in notches in one'of the edge portions 43 and s1its44 therefor are formed in the other of said edge portions. Formed in the front end portion of the fuselage 2|, on each side-of the notch 33, is a notch 45 having parallel sides. The notches 45 are'p'rovlded for receiving the end portions of the weight holder 28 andassist in holding the same within the fuselage (2|, as will presently appear. Also formed on the front end of the fuselage 24 is a plurality of forwardly projecting prongs 46- W I shaping the cut-out shown in Fig. 1, to form the fuselage 2|, glue is directly applied to one of the edgeportions 40 and thereafter .saidedge portionsare brought into overlapping relation and the tabs -43 inserted through the slits 44, which brings'sald edge portions into coincident relation. .Saidedge portions 4|! are then pressed together with the-glue therebetween and thus bottom sections.

5 T overlapping relation,

held until the glue is set. Glue, wherever shown in the drawings, is indicated by the numeral 41. A further step in shaping the fuselage is to fold slightly the members of the bottom section 36 downwardly on broken lines 48. These broken lines 48 extend the full length of the members of the bottom section 36, and at the transverse centers thereof. Next, the members of the

bottom sections

35, 36 and 31 are folded downwardly onthe

lines

31, 32 and 33 and, thereafter glue is applied .to one of the members of each of said Finally,.the members of the

bottom sections

35, 36 and 31 are broughtinto the tabs 4| inserted through the slits 42 and said members pressed 'together'withthe'glue therebetween. This completes the formation of the fuselage 2|. broken lines 3|, 32 and 33, into'front, central and Y I I I Weight holder A further step in forming the model airplane isto apply two spots of glue to the weight holder 28, as-shown-in Fig. 8., Aweight 49, seel ig. 11, is placed on one of the spots of glue and the weightholder iii is folded upon itself, on the broken lines 5ll,fwith the weight 49 therebetween and held by'the two spots of glue. The end portions of theweight holder 28 are next folded outward'ly on the broken lines 5|. The weight holderI28 at its end portions is contracted on the brokenlines 52 and then expanded to form disklike members 53. To apply-the weight holder 28 to the fuselage 2|, the same is inserted into said fuselageat the open front end thereof and the contracted end portions of said holder inserted into the two notches '45 and the disk-like members 53.,folded on the .broken' lines 52 and glued to the sides of the fuselage 2|, see Fig. 11. This weight holder 28 supports the weight 49 in a vertical'position at the exact transverse cente r of the fuselage 2|.

' Cones Formed in, the

cones

22 and 23 are V-shaped notches 54 and 55, respectively. These notches 54 and 55 extend from the perimeters of the

cones

22, and 23 to'holes in the centers thereof; A tab 56 on the cone 221primari1y extends into the notch 54 and, a tab'. 5'| ,on' thecone '23 primarily extends into the notch 55. slits 58 and 59 for the tabs .53 and, 5'| are formed in the respective cones .22 and 23. The

cones

22 and 23 are formed by bringing the portions thereof, at the notches 54 and 55, into (overlapping relation and insert-c ing the tabs 56 and 51 into the respective slits 58 and 59. The .insertionof the tabsr5llflan'd 51 into the slits I58 and 59 brings the'cu't-o'uts 22 and 23 ,'into the ,iorms of cones. Prior to the 'sha'pinigiof the

cones

22 and 23,. glue is applied to' the cut,-.outs,' as shown. At' the completion 'of the formationof the .con'es'22 and 23, glue is applied to the prongs 46 andlthe cone .22 inserted over said prongsf. This application of the inner cone 2 2 overthe. prongs liilaen'dssaid prongs inwardly so that-thesurfaces, thereof to which glue has been applied, are pressed onto, theinner surface of the cone 22 and'thereby connect said cone to the fuselage zl. Next,- glue is applied to the interior of the -cone'23 and-said cone placed I on the cone 22 for reinforcing the same.

..Ve1 fi lator Y a The ventilator 21 isiheldsuspended frointhe fuselage 2| at the under side of its bottomfsection 35. In ahplyingithe ventilator 27 to thefu'selage 2|, thesame-is' folded upon itselfio'n a transverse curve at its forward portion'and then folded, at its rear portion, on'the broken lines 60. Next, the tabs 6|, on the upturned ends of the ventilator 21, are inserted in slits 52 in the side of the fuselage 2| above its bottom section 35 and the end portions of the ventilator 21 secured to the fuselage 2| by glue.

Cockpit cover The cockpit cover 24' has formed therein a pair of aligned slits 63 which extend transversely into said cover from the side edges thereof. These slits 63 divide the cockpit cover 24 into front and rear sections. The front and rear sections of the cockpit cover 24 are each provided at the notches 63 with a pair of outwardly projecting

tabs

64 and 65, respectively. In forming the cockpit cover 25 from the cut-out shown in Fig. 4,

said cut-out is bent to permit the tabs 5 to be 1 the adjacent end of the rear end portion of said fuselage. The top of the rear end portion of the fuselage 2| is rearwardly and downwardly inclined. It is at thejunction of the front and rear sections of the top of the fusela e 2| that the cockpit cover 24 is applied. The cockpit cover is outlined to represent transparent panes.

Rudder and stabilizer The rudder 25 and the stabilizer 28 are inter-' locked by inserting the stabilizer into a deep and narrow V-shaped notch 61 in said rudder. A notch 58 in the stabilizer 25 limits the movement of said stabilizer into the rudder 25. On the front end of the stabilizer 26 is a tab 59, provided to direct stabilizer into the fuselage 2| at the rear E .A long slit NJ on the line end portion thereof. is provided for receiving the rudder 25 and positioning the same at the transverse center of the fuselage 2|. Formed in the rudder 25 above the slit 10 is a small notch II which limits the movement of the rudder 25 into the fuselage 2|. The stabilizer 25 extends into a pair of slits 12 in the side of the fuselage. The several prongs on the rear end portion of the fuselage 2| formed by the slits 10 and I2 are glued to the rudder 25 and the stabilizer 26 and thereby securely hold the rudder 25 and stabilizer 26 at right angles to each other and also secure said rudder and stabilizer in their proper position on the fuselage 2 5.

Wing

The final operation in assembling the several cut-outs of the model airplane is the attachment of the wing 29 to the fuselage 2|. The folding of the bottom section of the fuselage 2| on the inset broken lines t8 forms, on each side of the fuselage 2|, a pair of stop shoulders 73, see Figs. 15 and 16. In folding the members of the bottom section 36 on the broken lines 43, said section is shaped so that it upwardly and outwardly diverges from the transverse center of the fuselage 2| and affords a seat for the Wing 29.

To mount the wing 29 on the fuselage 2|, its end portions are first upwardly folded on the broken line 14 and thereafter glue is applied thereto, asshown. .The Wing 29 is. thenplaced in its seat between the shoulders 13 and which shoulders automatically position the wing 29 at right angles to the center 1ine,30-of the fuselage and securely hold the same against angular m ve ment relative to the fuselage. Next, thewing 29 is pressed against the bottom section 36 and its contact with the upwardly diverging surfaces thereof automatically positions the end portion of the wing 29 at a predetermined dihedral angle which is'absolutely necessary for the correct flying of the model airplane.

It will'be understood that .the invention described is capable of various modifications within thescope of the invention herein disclosed'and claimed- I claim as my invention:

a l. A fuselage fora model airplane formed from sheet material and having a wing-positioning seat, said seat having two surfaces that diverge upwardly and outwardly from thetransverse cen-. ter of the fuselage, and a cut-out wing folded at its longitudinal center, mounted in said seat and positioned thereby with its, end portions at a predetermined dihedral angle.

2. The structure defined in claim 1 in whichthe seat is provided with stop shoulders that positionthe axis of the wing at right angles to the longitudinal center of the fuselage.

3. The structure defined in claim 1 in whichthe seat is provided with stop shoulders that position the axis of the wing at right angles to the longitudinal center of the fuselage and hold the same against angular movement in the planes of the end portions of the wing.

4. A fuselage cut out for a model airplane formed of sheet material and foldable upon itself to form the top, the sides and the bottom of the fuselage, said cut-out having a deep-notch extending inwardly from its front end and also being transversely cut at the inner end of the notch, whereby the portions of the cut-out, at the notch, may be drawn together, overlapped and connected to lower the height of the fuselage at its front end portion relative to its rear end po-r-,

tion.

5. A fuselage cut-out for a model airplane formed of sheet material and foldable upon itself to form the top, the sides and the bottom of the fuselage, said cut out having a deep V-shaped notch, extending inwardly from its front end, and a substantially. equilateral notch formin a continuation of the first noted notch, the two notches being joined at their 'apexes, whereby the portions of the cut-out at the notches may be drawn together, overlapped and connected to lower the height of the fuselage at its front end portion, relative to its rear end portion.

6. The structure defined in claim 5, further including tabs on one of the edges of the cutout formed by the V-shaped notch and slits therefor in the cut-out on the opposite side of said notch.

7. A fuselage cut-out fora model airplane formed from sheet material and foldable to form the fuselage, notches extending transversely into the cut-out from its longitudinal edges and having their inner ends at the adjacent ends of the front and the center folding lines and at the adjacent ends of the rear andthe center folding lines, these notches dividing thecut-outoutwardly'of the folding lines into front, center and rear sections which, when folded on said lines, overlapped and connected form atwo-ply bottom for the fuselage.

8. The structure defined in claim 7 in which the folding lines for the members of the center section of the bottom of the fuselage are inset from the adjacent ends of the front and rear folding lines, each member of the center bottom section having a longitudinal central folding line, the members of the center bottom section, when folded on the respective folding lines, diverging upwardly and outwardly from the transverse center of the fuselage and affording 2. Wing seat and exposing the adjacent ends of the front and the rear bottom sections, and which ends afford stop shoulders for a Wing cut-out, said seat when the wing cut-out is placed therein and pressed thereagainst, automatically positioning the end portions of the wing at a predetermined dihedral angle and said stop shoulders automatically positioning the axis of the wing at right angles to the longitudinal center of the fuselage.

9. The structure defined in claim 7 further including outwardly projecting tabs on the outer longitudinal edges of one of the members of each bottom section and slits in the cut-out for the.

tabs. a x

10. The structure defined in claim 7 in which the members of the front bottom section are in forwardly converging relation and the members of the center and rear bottom section are in forwardly diverging relation.

11. A fuselage cut-out for a model airplane formed from sheet material and foldable upon itself to form the top, the sides and the bottom of the fuselage, said cut-out having a plurality of forwardly projecting prongs, and a paper cone cut-out that'is severed from its outer edge to its center whereby the severed portions of the cone cut-out may be drawn together, into overlapped relation and connected to shape the cone, said cone being applicable over the prongs on the fu- A selage and thereby contacting and pressing the same into outwardly converging relation and secured to the cone by glue previously appliedto the prongs. V

1'2. The structure defined in claim 11 further including a second cone, similar to the first noted cone, applicable over the'ifirst noted cone and glued thereto to reinforce the same. I r

' 13. A fuselage for a model airplane formed from sheet material, a sheet material cockpit cover cut-out having a pair of slits extending transversely fromopposite edges thereof and dividing the cut-out into front and rear sections, a tab on the cut-out on each side of'said slit, said cockpit cover cut-out being formable into a cockpit cover by moving the tabs on said front section under the tabs on the rear section, whereby the cut-out is transversely curved and the front section thereof drawn downwardly, the formed cockpit cover being mounted on the fuselage by placing the same transversely thereover and inserting the tabs into slits in the fuselage.

14. A fuselage for a model airplane formed from sheet material and having in the top of its rear end portion a long slit at the transverse center of the fuselage, said fuselage also having in'its sides underv said slit a pair of slits, a rudder cut-out, and a stabilizer cut-out, said rudder cutout havinga notch into which the stabilizer extends, said rudder extending into said top slit and the stabilizer extending into the side slits, the end portions of the fuselage formed by the slits therein being glued to the rudder and the stabilizer.

15. A fuselage for a model airplane formed from sheet material and having in its sides at the front end thereof a pair of notches, a weight, a holder cut-out for the weight within the fuselage, said holder cut-out being folded upon itself with the weight held therein, tabs on the outer ends of the weight holder, opposing notches in the cut-out between the weight holder and its tabs, said tabs being turned outwardly and backwardly with the notchedportions of the weight holder in said first noted notches, said tabs being glued to the sides of the fuselage on the outside thereof.

16. A fuselage for a model airplane formed from sheet material, and a ventilator cut-out having tabs on its ends, said cut-out being folded upon itself and extending transversely under the fuselage with its tabs extending into slits in the sides of the fuselage, said ventilator being glued to the fuselage.

FRED D. MYERS.