US1828819A - Flying machine - Google Patents

Description

Oct. 27, 1931.

s. ROSENBERG ET AL 1,828,819

FLYING MACHINE Filed Feb. 25. 1950 3 Sheets-Sheet 1 Och 1931. s. ROSENBERG ET AL ,8

FLYING MACHINE Filed Feb. 25, 1950 3 Sheets-Sheet 2 gwvcnfozsz I janc/ar foo-e/vex g. .Taco f/acmaa.

duozucq 1931- s. ROSENBERG ET AL 1,323,819

FLYING MACHINE Filed Feb. 25 1 0 3 Sheets-Sheet 3 IHW II Patented Oct. 27, 1931 I it i I UNITED STATES PATENT OFFICE SANDOR ROSENBERG, OF NEW YORK, AND JACOB HOCHMAN, OF BROOKLYN, NEW YORK FLYING MACHINE Application filed February 25, 1930. Serial No. 431,247.

This invention relates to flying machines proceeds, the invention resides in the novel and the improvements are directed to a novel formation, combination and arrangement of form of helicopter, embodying means whereparts, all as will be described more fully by the machine. may rise and descend in a hereinafter, illustrated in the drawings, and

" substantially vertical plane: v particularly pointed out in the claims.

As'will presently appear 1t is proposed to In said drawings: provide means, conveniently termed a con- Figure 1 is a central vertical sectional view denser o'r compressor, adapted to be rotated of the means carrying the series of condensers, and to condense or compress the air passing and also of the supporting means for the 10 therethrough and to discharge said comfirst-named means, the condensers being pressed air onto a blade positioned rearwardshown in elevation. 'ly thereof to facilitate the rise of the ma- Fig. 2 is a horizontal sectional View taken chine and to retard the descent thereof, both on the line 2-2 of Fig. 1, the condensers and I 4 rise and descent taking place in a substanintervening blades being shown in plan. l5 tially vertical plane. Fig. 3 is a plan view, slightly enlarged, of

Another object of the invention is toprothe means carrying the series of condensers vide means for carrying a plurality of conand blades. densers or compressors, said means'embody- Fig. 4 is an elevation thereof. I ing a single casting and being adapted to Fig. 5 is a detail view, in plan, of the base 20 also supportya plurality of blades, disposed member showing the ball race for the bear- 6.;

between and parallel with the horizontal ings. axes of said condensers. Fig'. 6 is an inverted plan view of the Still another object is to provide supportflanged coupling, also illustrating a portion "ing means adapted to be carried by the of the ball race.

.5 5 fuselage of a flying machine, said means em- Fig. 7 is a sectional view of a condenser bracing a rotatable element aflixed to sand and a companion blade, illustrating diameans for carrymg sa1d condensers. grammatically the course of air currents A further object of the invention resides through the former and their impingement v in the production of a novel form of conon the latter in a compressed or condensed 39 denser or compressor having a forward edge condition. greater in width than the retreating edge Fig. 8 is an elevation of a flying machine thereofyand further having a forward edge with our invention applied thereto. greaterin length than the retreating edge Fig. 9 is a View like unto Fig. 2, but show- 7 thereof,said dimensional arrangements tending a modified form of condenser. 35 ing to condense or compress the air passing Fig, 10 i a tional i t k o th through the condenser or compressor in order line 1010 of Fig. 9. that the compressed air may be discharged Referring now more in detail to the acwith great velocity from said retreating edge. companving drawings wherein like charac- A still further object is to provide novel ters of reference denote similar parts 40 means whereby the Width 0f retreating throughout the several views, let 11 indicate ge of a c en r may be var ed wi h r generally a flying machine having the usual spect to the Of the forward 01 leading propeller 12 and the fuselage 13, the latter edge of a condenser. being adapted to support our invention, as

Wi h th s 'o j in V w, g h i h will presently appear. It will, of course, be 5 others. which Will appear as the description understood that the howing of the flying machine in Fig. 8 is illustrative, rather than restrictive, as obvious the particular form of flying machine does not per se limit the application of our invent-ion.

As previously ointed out it is proposed to provide a com ination of parts whereby the flying machine will rise, with its burden, vertically in its ascent and descend to the earth vertically and landing thereon without a shock of importance enough to notice, the aforesaid actions operating somewhat in the nature of an auger entering wood.

To this end we propose to provide a plurality of compressors orcondensers 14, each having an open front and rear, as shown, a flat bottom 15, sides 16 and a top portion 17. Upon inspection of Figs. 1 and 2, it will be observed that the sides 16 converge from the forward edge to .the retreating edge of the condenser, and further that the top portion 17 slopes downwardly from the forward edge to the retreating edge, this arrangement producing a structure wherein the width and length of the forward edge is greater than the retreating edge as to Width and length. In short, each condenser presents an open front of a greater area'than its open rear. As shown in Fig. 2, we provide four of these condensers, though, of course, no restriction as to number is contemplated, and between each pair of condensers we position a plurality of blades which are inclined at an acute angle to the horizontal plane of said condensers, the leading edge of the bladesbeing adjacent the retreating edge of said condensers.

The means for carrying said condensers 14 and blades 18 comprises the element 19, shown in Figs. 3 and 4, and embodies a plurality'of outwardly directed flanges 20, to each of which a condenser is secured by means of fasteners 21, (see Fig. 2). Said element 19 is further provided with spaced lugs 22 for the reception of the end portions 23 of said. blades,'suitable fasteners 24 being used for this purpose, as clearly shown in said Fig. 2. As shown in Fig. 1, the bore 25, in said element 19, receives a sleeve 26, the latter fitting around shaft 27, the latter, the sleeve 26 and the element 19 being bound together by means of a pin 28, or the like. The lower portion of said shaft 27 is reduced in diameter, as shown at 29, for the reception of a coupling 30 and a base member 31, the latter being suitably affixed to the fuselage 13 of a flying machine. As' shown in Fig. 1, the end of the shaft portion 29 carries a bevel gear 32 meshing with a similar gear 33, af-

fixed to shaft 34 extending from any con-.

venient source of power, (not shown). Obviously, the rotation of said shaft 27 and the parts carried thereby, is imparted from said shaft 34, and in order to reduce friction to a minimum we propose to provide a thrust collar -,35 ,which is interposed between the fuselage 13 and the gear 32, and further it will be noted upon inspection of Figs. 5 and 6, that said base member 31 is provided'with a ball race 36 which cooperates with a ball race 37 in said coupling 30 to define a continuous groove for the reception of ball bearings 38, Said coupling 30 is afixed to the shaft portion 29, by means of screws 39, or the like, and naturally rotates with the shaft together with the parts just described.

As shown in Fig. 1, said sleeve 26 also supports a propeller arrangement 40, which includes a suitable casting 41, having a knob portion 42 at one end and a threaded stud 43 at its other end, the latter being provided with left-hand threads and adapted to threadedly engage the upper portion of said sleeve 26 as shown. In view-of this arrangement it is obvious that the propeller 4O rotates with the shaft 27.

After the flying machine has been equipped with our invention and it is deslred to ascend, the usual motor, with which the machine is equipped, is started, the power being transmitted to the shaft 27 and its connected parts, through the bevel gearing 32-33 and shaft 34, all parts rotating simultaneously;

supplied a continuous solid air force, the 'machine rises upwardly. Hence the chief lifting power is to be considered primarily as present in the plane and secondly, by the converging top portion of said condensers. Obviously, as the speed of rotation of the condensers increases a like increase takes place in the velocity of air passing through said condensers. When the machine descends under the law of gravitation, its drop is retarded by regulating the rotation of the condensers, which will permit said machine to descend so graddally and lightly as not to cause a single shock to its occupants.

An inspection of Fig. 7 will instantly reveal the actions hereinbefore described in detail. It will also become apparent that the converging or sloping top portions of the condensers have a certain hfting power in themselves as they cut through the air in operation'and olfer but a very little resistance to the'air when in operation. As the length and width at the leading'edge of the condensers is greater than the length and width at the retreating or rear edge, it follows the aforesaid convergence, air currents of great force leave the retreating edge of the condensers and impact the blades 18 which are pitched at an angle to cause a lifting action in-said machine.

As shown in Figs. 9 and 10, the condensers 14 may be made box-like in formation, hinged vanes 44 being internallyv arranged adjacent the sides of said condensers as shown. These vanes may be swung outwardly to the positions, indicated and locked in that position by means of pins 45 arranged in one of the apertures 46. This arrangement permits a certain amount of adjustment to regulate the quantity of air. passing through the .condensers. In this instance, and in our preferred form, the condensers rotate in the direction of the. full-line arrows, while the discharged air moves in the direction of the dot-and-das h arrows.

,While the present is a disclosure of the like compressors having a forward edge of preferred embodiments of the invention, it

is to be understood that the same is not limited .thereto, as various changes in the minor details of construction, proportion and arrangement of parts may be resorted to without departing from the spirit of the invention as defined in the appended claims.

We claim:

1. In a flying machine, with supporting means, arotatable shaft, a plurality of box-like compressors adapted to compress air as the same are rotated, and a plurality of angularlyarranged'blades disposed parallel with the horizontal plane of said compressors and arranged to receive the air discharged from said compressors.

2. In a flying machine, the-combination with supporting means, a rotatable shaft, a plurality of box-like compressors adapted to compress air as the same are rotated, each of said compressors having a forward edge of a width greater than the retreating edge and a plurality of angularly disposed blades arranged between said compressors and adapted to receive the compressed air discharged from said compressors.

3. In' a flying machine, the combination the combination pressor borne by said support, said compressor having a forward edge of greater width and length-than the retreating edge and an angularly' disposed blade positioned behind said retreating edge.

A 7 A device of the character described comprising a rotatable support, means for compressing air currents and borne b said support, said means including a senes of boxgreater width than the retreating cdge there- A of and a plurality of angularly arranged blades disposed between said compressors and adapted to receive the discharged currents of air from said compressors. 8. In a device of the character described the combination with a rotatable support, of a series of box-like compressors borne by said support, each of said compressors having a forward edge of greater width and length than the retreating edge thereof and a plurality of an ularly arranged blades disposed between sai compressors and adapted to receive the discharged compressed currents of air from said compressors.

, In testimony whereofwe afiix our signatures. SANDOR ROSENBERG.

JACOB HOCHMAN.

with supporting means, a rotatable shaft, a

plurality of box-like compressors adapted to compress air as the same are rotated,-eaoh of said compressors having a forward edge of a width and length greater than the retreating edge thereof and a series of angularly disposed blades arranged behind the retreating-edge of an adjacent compressor and adapted to receive the compressed air discharged therefrom. v

4. In a flyin machine, the combination with supporting mean's,.a rotatable shaft, a plurality of box-like compressors adapted to compress air as the same'are rotated, means for regulating the degree of compression of the-air anda series of angularly disposed blades arranged parallel with the horizontal lot

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