US1798358A - Advertising device - Google Patents

Advertising device Download PDF

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Publication number
US1798358A
US1798358A US427555A US42755530A US1798358A US 1798358 A US1798358 A US 1798358A US 427555 A US427555 A US 427555A US 42755530 A US42755530 A US 42755530A US 1798358 A US1798358 A US 1798358A
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Prior art keywords
aeroplane
motor
secured
shaft
body plate
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Expired - Lifetime
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US427555A
Inventor
James H Slachter
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DILMUS L JARRETT
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DILMUS L JARRETT
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Priority to US427555A priority Critical patent/US1798358A/en
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    • GPHYSICS
    • G09EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09FDISPLAYING; ADVERTISING; SIGNS; LABELS OR NAME-PLATES; SEALS
    • G09F21/00Mobile visual advertising
    • G09F21/06Mobile visual advertising by aeroplanes, airships, balloons, or kites
    • GPHYSICS
    • G09EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09FDISPLAYING; ADVERTISING; SIGNS; LABELS OR NAME-PLATES; SEALS
    • G09F19/00Advertising or display means not otherwise provided for
    • G09F19/02Advertising or display means not otherwise provided for incorporating moving display members

Description

March 31, 1931. J s c 1,798,358
ADVERTI SING DEVI CE 2 Sheets-Sheet 1 Filed Feb. 11, 1930 3M \IAMES 51/) CH TEA March 31, 1931.
J. H. SLACHTER ADVERTISING DEVICE Filed Feb. 11, 1930 2 Sheets-Sheet 2 atented Mar. 31, 1931 UNITED STATES PATENT QFFEE JAMES H. SLACHTER, OF MINERAL, VIRGINIA, ASSIGNOR 0F ONE-HALF T0 DILMUS L. JARRETT, OF BUCKNER, VIRGINIA ADVERTISING DEVICE Application filed February 11, 1930. Serial No. 427,555.
This invention appertains to advertising devices and more particularly to a novel window or store display for attracting the attention of prospective buyers.
One of the primary objects of my invention is to provide a miniature aeroplane exhibit in which the aeroplane is supported for rotary movement and is provided with an electric motor for driving the propeller, whereby the aeroplane will be caused to maintain a circular path when the motor is in operation, the plane being of such a character as to carry a suitable advertising sign or the like.
Another salient object of my invention is the provision of a novel bearing for rotatably supporting the aeroplane either from an overhead ceiling bracket or floor standard, the bearing having associated therewith in a novel manner the radially extending arm carrying the aeroplane and the non-conducting disc for supporting the annular contact rings for conducting the current to the motor of the aeroplane, the rings being adapted to be engaged by the roller contacts of the stationary supporting bracket.
A further important object of my invention is the provislon of a novel means for forming the inner and outer contact rings, one of,
the rings being provided with a depressed groove or track for receiving one contact roller and the other ring having an upstanding guard flan e for engaging the other contact roller, the ange acting as means for holding the rollers accurately positioned relative to the contact rings.
A further salient object of my invention is the provision of means for forming the body plate or fuselage of the aeroplane, the body plate being provided with a cut out portion adjacent to its forward end for receiving the electric motor, the motor being provided with a holding strap provided with ears for engaging the opposite faces of the body plate, the strap forming an efficient means for holding the motor in place and accurately disposed relative to the longitudinal axis of the plate, whereby the propeller driven directly from the armature shaft of the motor will be correctly centered, the strap also allowing the qiliick assembling of the motor with the aeroane.
A still further object of my invention is the provision of an improved miniature aeroplane advertising device of the above character, which will be durable and efficient in use, one that will be simple and easy to manufacture, and one which can be placed upon the market at a reasonable cost.
With these and other objects in view, the invention consists in the novel construction, arrangement and formation of parts as will be hereinafter more specifically described, claimed and illustrated in the accompanying drawings, in which drawings Figure 1 is a side elevation of my improved device, showing the aeroplane in front elevation and partly broken away.
Figure 2 is a section taken on the line 2-2 of Figure 1 looking in the direction of the arrows showing the aeroplane in side elevation, the rear end'of the aeroplane being broken away.
Figure 3 is a transverse section through the aeroplane taken on the line 33 of Figure 2 looking in the direction of the arrows illustrating the novel means for associating the electric drive motor for the propeller with the aeroplane.
Figure 4 is a top plan view of the ceiling bracket and novel bearings for supporting the aeroplane.
Figure 5 is an enlarged vertical section through the supporting bracket and novel bearings taken on the line 55 of Figure 4 looking in the direction of the arrows.
Figure 6 is a horizontal section taken on the line 66 of Figure 5 looking in the direction of the arrows illustrating the novel contact rings.
Figure 7 is a horizontal section taken on the line 7 7 of Figure 5 looking in the direction of the arrows, illustrating the novel means of securing the arm to the bearings, and
Figure 8 is a vertical section taken on the line 8-8 of Figure 5 looking in the direction of the arrows illustrating one of the contact rollers and its contact ring.
Referring to the drawings in detail, wherein similar reference means for pre nting the slipping of the rollresponcung certs en "*2 end 32) in cut of engagement With views, the etter A i flie 8323,1101 33 are Q o improved do 1-29. which ing shaft or pest W21 ycrted In vertical'pier .7 stated and are by iesf springs 34, eted or otherwise secured to 31. 'lheleaf springs cennected thereto the and 85 which can *ihie source 05 electrical \flill the hub 18 I use a ra supporting arm for the med the reference characfil he later described. The
be-iorined solider or" ahol- The cei 11g bracket L ly disgosed central hos tending l3 legs Us the upper with g i e1 in lie can the shaft is 17 and the heft ogpcsite ends i 19 and 20 to secured t, fitted between th feces of cu? 18 is supported site ends .d is free 5; with minimum an lower (la 21 rests is; the upper i:- boss l z of 23 can he shaft in the boss 12 V. assembled n end of the hub supper dially extending flan extreme upper end 25 formed of The upper ce L concentrically Q1 of chine; arms gtwhich are placed in 1; 5 genient' with the upper face of A uh flange Qand ing eleinei'itSS. The outer ends Iii; 9 iperts the connecting links I ne and the outer end 01 can provided With an eye 40 an eye 41 formed on theupper d link or red 39. The arm 36 is I u; by a diagonally extending in l is riveted or otherwise secured in; 5i as at adjacent to the outer f. The inner end of the brace bar vy secured to a collar l-EL placed uh 18, preferably in clese proxlevrer hearing cup thereof.
u it? formed fi-cm asingle piece of "l I v ll V l suitenly carved or shaped to reprev ii G the'upper and lower planes Q8. The lower plate'lS may carry the ale landing gear such as Wheels 429. In ith my invention the body plate '5 out pee-Lion which is shaped to coming throe-"hwhich extends the ache-i to or'forlning a part c shaft of the motor 51.
of the body plate lh is reinemetel strep Which 8X- e'ning'i cr the shaft 52, and suitable bearing re; led with 1. 1e said shaft.
secured th '3 "1e motor Ellis secured within the cut out spring pie portion the 'iody plstefi in a novel contact employ a split band for enring 29:, wlii and the ends of the hand er 33 is is U d wi h attaching feet which I the opposite sides of -43 below the cut out portion 7l8 L olt fi'ris extended through oplene 45 preferably includes va selage of en'aeroplzifne' and the 1113- 7 edges of the body plate 456 has 1 to its forward end is provided cie'ctric motor 51. 'The forward :1 body plate e6 is provided with a;
ct the nerepsine propeller 53, the
this arm is secured I 0 in any desired Way such'as by a suitten the body plate 46 and the attaching feet 56 and serve the dual function of tightening the band about the motor and holding the motor on the body plate. By this construction I am enabled to easily and quickly connect the motor with the body plate and at the same time centralize the same relative to the longitudinal axis of the aeroplane.
Connected with the inner and outer contact rings 26 and 27 and imbedded in the plate of insulation 25 are the feed and return wires 58 and 59 which may or may not be led through the hollow supporting arm 36. These wires extend down over the connecting rod 39 and terminate in a suitable plug 60, which is detachably connected with a suitable socket 61 connected with the feed and return wire 62 of the motor 51. By this arrangement the feed wires can be readily disconnected from one another when it is desired to detach the aeroplane from the connecting rod 39.
In order to connect the rod 39 with the aeroplane 45 I employ an eye bolt 63 which extends through a suitable opening formed in the body plate 46, which opening communicates with the cut out portion 50. The rod 39 which can be formed of metal is bent through the eye 63 as at G l and a thimble (35 is slid down over the rod and the bent back portion 64: thereof In use of my improved device the var ous parts are assembled as shown and described and when the current is turned on through the motor 51 the propeller 53 will be revolved thereby which will draw the aeroplane through the air in a circular path due to the connection of the aeroplane with the shaft 10. As the aeroplane gains speed the centrifugal force tends to swing the links 39 outward on the pivot 40 the speed of the aeroplane and the sizes of the propeller determining the amount of outward swing of the aeroplane. The opposite sides of the body plate 46 of the aeroplane can be provided with suitable advertising matter and as the aeroplane revolves the same will attract the attention of passers by and to the advertising matter carried thereby.
I lay partricular stress on the formation of the hub 18 and the means of attaching the supporting arm 36 and the insulating disc 35 as well as the formation of the contact rings 26 and 27 and the contact rollers 32 and 33. Likewise I lay stress on the arrangement and the means of connecting the drive motor with the body plate of the aeroplane 45.
Changes in details may be made without departing from the spirit or the scope of this invention, but
\Vhat I claim as new is:
1. In a device of the class described, a supporting shaft, a hub rotatably mounted upon the shaft and having supporting bearings at its opposite ends, an outwardly extending flange formed adjacent to one end of the hub, a disc of insulation secured to the mentioned end of the hub above said flange, a radially extending arm having its inner end bifurcated and secured to the flange, a brace arm connected to the outer end of the supporting arm, a collar secured to the hub adjacent to its lower end, the brace rod being secured to said collar, a rod carried by the outer end of the arm, an aeroplane connected to the rod, an electric drive motor secured to the aeroplane, a propeller driven by said motor, in ner and outer contact rings secured to the upper face of the disc of insulation, current conducting wires secured to the inner and outer contact rings and leading to said motor, and contact rollers frictionally engaging the inner and outer contact rings.
2. In a device of the class described, a supporting shaft, a hub rotatably mounted upon the shaft and having supporting bearings at its opposite ends, an outwardly extending flange formed adjacent to one end of the hub, a disc of insulation secured. to the mentioned end of the hub above said flange, a radially extending arm having its inner end bifurcated and secured to the flange, a brace arm connected to the outer end of the supporting arm, a collar secured to the hub adjacent to its lower end, the brace rod being secured to said collar, a rod carried by the outer end of the arm, an aeroplane connected to the rod, an electric drive motor secured to the aeroplane, a propeller driven by said motor, inner and outer contact rings secured to the upper face of the disc of insulation, current conducting wires secured to the inner and outer contact rings and leading to said motor, contact rollers frictionally engaging the inner and outer contact rings, one of said contact rings being formed relatively wide and provided with a centrally located depressed groove and the other of said rings being provided with an upstanding guard flange.
3. In a device of the class described, a wall bracket including a centrally disposed apertured boss, a shaft having a head on its lower end extended through the boss, a hub rotatably mounted upon the shaft provided with bearings cups at its opposite ends, cones fitted on said shaft engaging respectively the head on the shaft and the lower end of the boss, a nut threaded on the upper end of the shaft engaging the upper end of the boss, a flange formed on the upper bearing cup, a supporting arm rigidly connected to said flange, and an aeroplane carried by the outer end of the arm.
4. In a device of the class described, an aeroplane comprising an elongated flat body plate, wings connected to the body plate, the forward end of the body plate being provided with a cut out portion, openings leading into said out out portion, a motor fitted in said out out portion, the armature shaft of the motor being extended through the opening, a propellet secured to said armature shaft, and a split band encircling said motor having attaching feet engaging the opposite sides of the body plate, and a tightening bolt extending through the attaching feet and the body plate.
In testimony whereof I afilx my signature.
JAMES H. SLACHTER.
US427555A 1930-02-11 1930-02-11 Advertising device Expired - Lifetime US1798358A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3022070A (en) * 1959-02-26 1962-02-20 Strombeck Becker Mfg Co Tethered toy and pylon therefor
US3055660A (en) * 1960-02-23 1962-09-25 Nolan Y Alexander Apparatus for flying model airplanes
US4261657A (en) * 1978-08-09 1981-04-14 Reiback Earl M Optical display device
US5802751A (en) * 1996-04-03 1998-09-08 Schwieterman; Vernon V. Ornamental aircraft having multiple moving parts

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3022070A (en) * 1959-02-26 1962-02-20 Strombeck Becker Mfg Co Tethered toy and pylon therefor
US3055660A (en) * 1960-02-23 1962-09-25 Nolan Y Alexander Apparatus for flying model airplanes
US4261657A (en) * 1978-08-09 1981-04-14 Reiback Earl M Optical display device
US5802751A (en) * 1996-04-03 1998-09-08 Schwieterman; Vernon V. Ornamental aircraft having multiple moving parts

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