US1010443A - Flying-machine. - Google Patents

Flying-machine. Download PDF

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US1010443A
US1010443A US51551609A US1909515516A US1010443A US 1010443 A US1010443 A US 1010443A US 51551609 A US51551609 A US 51551609A US 1909515516 A US1909515516 A US 1909515516A US 1010443 A US1010443 A US 1010443A
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machine
propellers
shaft
propeller
propel
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US51551609A
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Simon B Minnich
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/003Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage
    • B64C39/005Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage about a horizontal transversal axis

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  • My invention relates to aerial navigation and has for its object to provide a flyingmachine, of that class known as heavier than air or aeroplane, and to so construct i and equip the same with a plurality of sepalifting means that in case all but one' of said power plantsbecome defective and cease to operate, the machine will still havesulfxcient power to sustain-itself from falling 'andthus will vconstitute 'a safety flying machine.
  • Another object is to provide propellers of such a novel form and construction that they may be instantly adjusted to raise, propel and steer the machinel without Ythe use ofV a rudder, although a rudder may .housed if required.
  • Fig. 2 is a plan view of the same, with part oft-he .aeroplane removed.
  • Fig. 3 is a -vertical cross section taken on the line X-X of Fig. 1,'looking. toward the rear.
  • Fig. ⁇ 4 is a detail sectional view of .the controllin hand-levers.
  • Fig. 5,- isl a detail side -view o the same.
  • Fig. 6, is a detail top plan view ofthe sidepropellers, shown in Fi 1 FigL, is aside elevation of the same.
  • yFig 8,' is a detail top plan view of another form of propeller.
  • Fig.9 is a detail side view of the same.
  • Fig. 10 is a detail View of one ofthe cylindrical popellers with part of the side removed.
  • Fig. ll.- is a further detail view of the same, 'showing the operating mechanism.
  • the machine comprises a rectangular aeroplane 1, from' which is .suspended a platform 2, bythe supporting rods 3, and the truss-wires 4, the platform being further braced by the trussrods 5, and provided with ⁇ the wheels 6, which are for the purpose of supporting the machine when resting upon the ground. ⁇
  • vframe 7 At a suitable distance below the aeroplane 1, and attached to the supporting rods 3, is a vframe 7, in which are journaled the propellerfshafts 8, onl the-ends of whlch are mounted the propellers which will hereinafter be described.
  • each of said motors is independently supplied froml an independent fuel tank 10, situated at a convenient place above the motors and a water-cooling tank 11, placed under the platform; or if air-cooled motors are employed the fuel tanks may be placed below the platform and pumps 'be used to raise the fuel to the motors.
  • the propellers are independently or jointly controlled by a setl oflevers and connecting-rods (which will hereinafter be fully described) .inl such a way that the operator will have perfect control of eachpropeller, for the-.purpose of .timing their action and ⁇ changing their direction to raise, propel and guide the machine. f
  • the propellers comprise the blades or shutter frames'12, which are placed at' right angles to each other and which are rigidly secured upon the shafts 8, and within which are journaled the radial Jshutter-shafts f13, upon which are secured the shutters 14, which may be of fabric or other suitable material, such asY sheet aluminum; the outer ends of said shafts being journaled in the frames 12, and the inner ends j'ournaled in and extending through the cross-barV 23, and having secured thereon the cranks 24, which are joined together by a connecting-rod 15; while slidably mounted in suitable bearings 16, in the frame 12, and parallel with the shaft 8, is a reciprocating rod 17, which is connected at a suitable point to said connecting-rod 15, by a link 18, in such a manner that by the reciprocation of the rod 17, the shutters will be given a quarter turn, thus presenting a fiat or an edge surface to the air in
  • I pro- Videla-sleeve 19 mounted upon the shaft 8, between the propeller frame 12, and the Amain frame 7, whichis formed with a camrace 20, in the face thereof, within which runs a roller 21, attached to the end of the reciprocating rod 17; the'cam-sleeve 1g), be.- ing retained in position and from revolving upon the shaft 8, by the'levers 22, attached thereto and the operating-rods 25, (hereafter more fully described) ;the rollers 21, running in the cam-race 20, will recipro- ⁇ v cate the'rods 17, forcing them in and out duringnevery revolution of the propeller about the shaft 8; the timing of said action and the opening and shutting of the shutters being controlled by the positlon of said camsleeve 19, as controlled by thelevers 22, in such a manner that the shutters 14:, close on the forward and down stroke of the propel'- ler blades for the purpose of elevating the machine
  • the machine can be so timed as to propel the machine in any direction or at any angle, and by setting the propeller-s upon one side of the machine Vto propel the machine forward and upon the other side of the machine to propel rearwardly, the machine maybeI steered and turned around in a short space; whileby setting the propellers to elevate the machine, it will rise vertically upward from the ound and require no starting or launchmg apparatus, thus enabling the operator to rise upward amidst trees or buildings and.
  • the propeller-shafts 8 are operated by a sprocket wheel 26, secured thereon and driven by a sprocket chain 27, from one of the motors (or may be driven by shafts and bevel gears), each motor being connected to enoughpf the propellers placed at suitable i places to effect the balance of the machine for propelling and guiding the same.
  • each lever may be'operated independently from each other; one lever being supplied for each cam-sleeve 19, and one lever operating each of the end propel- 1ers; one the center cam-sleeves and one the intermediate pair, as shown in the drawings.
  • the shaft 28, being divided in the center and each half supplied with a' master lever 31, secured to the shaft and engaging a notched segment secured to the central bearing 32, so that all of the levers 56, upon either half of the shaft 28,.
  • the end or corner propellers are of different form and are illustrated in detail in Figs 10and 11, and comprise a cylinder 57, open at both ends, andwithin which is secured the screw-propeller blade 33; while through the center thereof and in axial relation thereto, is the shaft 34, which has secured thereon the flanged collar 35, to which are secured the radial stay-rods 36, which help to support thecylinder 57; and it may here be stated that the cylinder and stayprovided with the levers 22, and rods 25,
  • . 50 is mounted in bearings 51, in the and 7, except that the shutters 45, are slightly concavo-convex in form and are pivoted in a parallel relation to the shaft 8, with their shafts 46, extended through the -frame 47, and ⁇ supplied with the cranks 48,
  • a sleeve provided with a cam mounted upon said shaft ⁇ for opening and closing said blades, lever connected to said sleeve, hand operatingl levers mounted upon said frame,
  • a supporting frame provided with-a transversely Aextending propeller shafts lsuitably mounted on said frame, propellers provided with radial shutters at right angles to each other forming blades, a cam sleeve mounted' upon said propeller shaft and pro vided with a cam-race way, means for holding said cam sleeve fromrotating on Said shaft, a reciprocating rod having a roller suitably secured thereto, said roller adapted to move in said race-way of the cam, sleeve cranks secured to said Shutters, connecting rods between said-cranks and reciprocating rods, hand operating levers mounted upon said frame for the purpose of operating said cam sleeve and timing the opening and shutting of said shutters, substantially as described.

Description

s'. B. MINNIGH. -mmm MACHINE. APPLICATION PILBDAUG. 31, 1909.
Patented Deo. 5, 1911.
S. B. MINNICH.
y FLYING MACHINE.
:APPLIOATION FILED AUG. a1, 1909.
Patented Deo. 5,V 1911.
WH NESSES:
S. B. MINNIGH. FLYING MACHINE. APPLICATION 111.1111 111111.31, 1909.
Patented 1180.5, 1911.
6 SHEETS-SHEET 3.
iNvENToR Simon .B Mnnch',
WITNESS-s:
f ATTORNEY s. B. MINN'IGH. FLYING MACHINE. APPLICATION FILED AUG.31, 1909.
Patented Dec. 5, 1911..
6 SHEETS-SHBET 4.
S. B. MINNIGH.
` FLYING MACHINE.
APPLICATION FILED AUG. 31, 1909.
PatentedA Dec. 5, 1911.
.0 I7 TnS/EBT 5- INVENTOR s. B. MINNIGH.y FLYING MACHINE. l
` v APPLICATION FILED AUG/.31, 190.9.
Patented 1560.5; 1911.
6 SHEETS-SHEET 6.
* I wlNEssEs:
srMoN n, MINNIGH. or LANnIsvILLE, PENNSYLVANIA..
ELvINMAoHINE. I
To allwhom 'it may concern:
Be it known thatI,` SIMON B. MINNIGH, a citizen of the United States, residing at Landisville, in the county'of'Lancast-er and 5 State of. Pennsylvania, have invented certain new anduseful Improvements in Flying-Machines, of which the following is a y specification, reference being had therein to the accompanying drawing.
My invention relates to aerial navigation and has for its object to provide a flyingmachine, of that class known as heavier than air or aeroplane, and to so construct i and equip the same with a plurality of sepalifting means that in case all but one' of said power plantsbecome defective and cease to operate, the machine will still havesulfxcient power to sustain-itself from falling 'andthus will vconstitute 'a safety flying machine.
Another object is to provide propellers of such a novel form and construction that they may be instantly adjusted to raise, propel and steer the machinel without Ythe use ofV a rudder, although a rudder may .housed if required. p
It may also be noted thatl while I employ the use ofA one or more aeroplanes for .the purpose of floating or helping top sustain 80 the machine inthe air, I do notdepend upon them for entirely sustaining the machine, as
this is effected by my novel form of propeller.' And further, it may be noted, that while in the accompanying drawings I have illustrated my machineas having an aeroplane in the center with a row of propellers placed on either side thereof, that I am not `confined to this, construction, as a single or double row of propellers 'maybe placed in 40 the center with an aeroplane ,on either side without departing from the spirit' ofthe invent-ion. A e
lVith these and other objects in view my inventionconsists in certain construction and combination of parts as will hereinafter be fully described and claimed and illustrated in the accompanying drawings, which form a part of this application, and in which like figures of referenceA refer to corresponding parts in all of the views; but it is fully understood, that while I have described my invention as herewith shown, that I do not confine myself to the exact-design as shown,
asslight changes may be made in the con- 55 struction and" arrangement of the several`-V Specication of Letters Patent.
` Application led August 31, 1909. Serial No. 515,516.
rate power plants .and propelling and upratend Dec. 5, 1911.
parts without'departing from the spirit-of the invention'.
In the drawings :-'-Figure l, is a side elevation ofthe flying-machine, showing the propellers set to'raise and propel forward.
Fig. 2, is a plan view of the same, with part oft-he .aeroplane removed. Fig. 3, is a -vertical cross section taken on the line X-X of Fig. 1,'looking. toward the rear.
Fig.` 4, is a detail sectional view of .the controllin hand-levers.. Fig. 5,- isl a detail side -view o the same. Fig. 6, is a detail top plan view ofthe sidepropellers, shown in Fi 1 FigL, is aside elevation of the same. yFig 8,' is a detail top plan view of another form of propeller. Fig.9, is a detail side view of the same. Fig. 10, is a detail View of one ofthe cylindrical popellers with part of the side removed. Fig. ll.- is a further detail view of the same, 'showing the operating mechanism.
Referring to thedr'awings, the machine comprises a rectangular aeroplane 1, from' which is .suspended a platform 2, bythe supporting rods 3, and the truss-wires 4, the platform being further braced by the trussrods 5, and provided with `the wheels 6, which are for the purpose of supporting the machine when resting upon the ground.`
At a suitable distance below the aeroplane 1, and attached to the supporting rods 3, is a vframe 7, in which are journaled the propellerfshafts 8, onl the-ends of whlch are mounted the propellers which will hereinafter be described. v
Upon the platform 2, are mounted a series of motorsf9, whichiare each independentlyA connected to a sufficient number of propellers to balance and sustain the machine in the air; while each of said motors is independently supplied froml an independent fuel tank 10, situated at a convenient place above the motors and a water-cooling tank 11, placed under the platform; or if air-cooled motors are employed the fuel tanks may be placed below the platform and pumps 'be used to raise the fuel to the motors.
The propellers are independently or jointly controlled by a setl oflevers and connecting-rods (which will hereinafter be fully described) .inl such a way that the operator will have perfect control of eachpropeller, for the-.purpose of .timing their action and `changing their direction to raise, propel and guide the machine. f
ico Y While in the accompanying -drawings l have shown three forms of propellers, I, prefer to use one form on the corners. of the machine and another form on the sides, but the machine will operate e ually as well with all of the propellers o either form,
as their action 1s controlled in the same manner, which will be later fully described.-
Referring to the Figs. 6, and 7, of the drawings which illustrate'the form of propeller shown in Fig. 1, the propellers comprise the blades or shutter frames'12, which are placed at' right angles to each other and which are rigidly secured upon the shafts 8, and within which are journaled the radial Jshutter-shafts f13, upon which are secured the shutters 14, which may be of fabric or other suitable material, such asY sheet aluminum; the outer ends of said shafts being journaled in the frames 12, and the inner ends j'ournaled in and extending through the cross-barV 23, and having secured thereon the cranks 24, which are joined together by a connecting-rod 15; while slidably mounted in suitable bearings 16, in the frame 12, and parallel with the shaft 8, is a reciprocating rod 17, which is connected at a suitable point to said connecting-rod 15, by a link 18, in such a manner that by the reciprocation of the rod 17, the shutters will be given a quarter turn, thus presenting a fiat or an edge surface to the air in the direction of their stroke as .the propeller is revolved by the shaft 8.
For automatically operating said shutters 14, and opening and closing them once in every revolution of the propeller, I pro- Videla-sleeve 19, mounted upon the shaft 8, between the propeller frame 12, and the Amain frame 7, whichis formed with a camrace 20, in the face thereof, within which runs a roller 21, attached to the end of the reciprocating rod 17; the'cam-sleeve 1g), be.- ing retained in position and from revolving upon the shaft 8, by the'levers 22, attached thereto and the operating-rods 25, (hereafter more fully described) ;the rollers 21, running in the cam-race 20, will recipro-`v cate the'rods 17, forcing them in and out duringnevery revolution of the propeller about the shaft 8; the timing of said action and the opening and shutting of the shutters being controlled by the positlon of said camsleeve 19, as controlled by thelevers 22, in such a manner that the shutters 14:, close on the forward and down stroke of the propel'- ler blades for the purpose of elevating the machine, as shown in F ig. 7, or close at a quarter of a revolution later or on the down and backward stroke to propel the machine forward, or as still changed by the position of the cam-sleeve 19, to propel the machine rearwardly; the action of the Ashutters 14, being the same as the feathers of a bird, which feather on the upward stroke thus presenting no resistance to the air and on thedownward stroke present a `iat surface v and having their full elfect; and it will thus. be seenthat by this novel construction the opening and closing ofthe shutters 14,
can be so timed as to propel the machine in any direction or at any angle, and by setting the propeller-s upon one side of the machine Vto propel the machine forward and upon the other side of the machine to propel rearwardly, the machine maybeI steered and turned around in a short space; whileby setting the propellers to elevate the machine, it will rise vertically upward from the ound and require no starting or launchmg apparatus, thus enabling the operator to rise upward amidst trees or buildings and.
descend in the same manner. Also by setting-some of the propellers toward the front of the machine to propel forward and upward, and some of ,the propellers near the rear to, propel rearwardly and upward, or Vin other words, counteract each other, the machine 'may be made to hover above a certain object like a humming-bird; the end propellers being set to 'overcome any drift caused by thev wind. u
The propeller-shafts 8, are operated by a sprocket wheel 26, secured thereon and driven by a sprocket chain 27, from one of the motors (or may be driven by shafts and bevel gears), each motor being connected to enoughpf the propellers placed at suitable i places to effect the balance of the machine for propelling and guiding the same. As here shown, I have used three motors, the central one driving the end and central propellers on each side, one side motor driving the next propellers on either side of the central pair andthe other motor driving the remaining ones, so that if either one or two motors stop, the machine can still be operated with the remaining one, the stoppage causing a loss ,of power and rendering some 4of the propellers idle, but still keeping the machine aoat and under control.
The control and operation of the camsleeves 19, is effected by the rods 25, which V are attached at one end tothe levers 22;
and at the otherl end to the hand-levers 56, which are mounted on the cross-shaft 28, which-is in a convenient -location for the operator; said shaft 28, having rigidly secured thereon, adjacent t0 eachhand-lever,
56, a notched segment 29, to which the handlever can be lockedvby the dog 30, in such amanner that each lever may be'operated independently from each other; one lever being supplied for each cam-sleeve 19, and one lever operating each of the end propel- 1ers; one the center cam-sleeves and one the intermediate pair, as shown in the drawings. The shaft 28, being divided in the center and each half supplied with a' master lever 31, secured to the shaft and engaging a notched segment secured to the central bearing 32, so that all of the levers 56, upon either half of the shaft 28,. and the connected cam-sleeves upon that side of the machine may be shifted by the master lever 31,*and thus the end propellers may be readily set to guide the machine l while the other propellers are set to propel it inthe desired direction. The motor control is elected in the usual way, any variation in the speed of the various motors being corrected by the timing of the opening andshutting of the shutters.
The end or corner propellers are of different form and are illustrated in detail in Figs 10and 11, and comprise a cylinder 57, open at both ends, andwithin which is secured the screw-propeller blade 33; while through the center thereof and in axial relation thereto, is the shaft 34, which has secured thereon the flanged collar 35, to which are secured the radial stay-rods 36, which help to support thecylinder 57; and it may here be stated that the cylinder and stayprovided with the levers 22, and rods 25,
I ings, I show another form .of propeller 44,
thus inclining the axis-of the propeller for- Ward or backward, as may be deslred. The propeller being driven by the bevel gears 43,
' which is secured upon vthe shaft 8 and in mesh with the gear 39; while the shaft 8, is rotated in the before mentioned manner as used 'with'the other style of propeller.
Referring to Figs.`^8, and 9,0f the drawwhich is similar to that shown in Figs'. 6,
. 50, is mounted in bearings 51, in the and 7, except that the shutters 45, are slightly concavo-convex in form and are pivoted in a parallel relation to the shaft 8, with their shafts 46, extended through the -frame 47, and`supplied with the cranks 48,
which -are connected together by the connecting-rod 49 while the reciprocatin rod ame 47, and is connected to the rod 49, byfther plied. with a roller 53, which runs in a'. camrace 54, in ,the face of a cam 55, which is mounted on the shaft 8, and operated by the levers 22, in the same Way as thatform shown in Figs. 6, and 7. The advantage of this style of shutter being that the curve of the shutter being struck with a radius equal to the distance bet-Ween the shutter and the center of the shaft- 8; as the propeller'is revolved and the shutter is opened, it presents no resistance to the air, while in a closed position its cup-shaped form presents the greatest resistance to the air.
Having' thus described my invention what I claim as new and desire to secure by Letters Patent .is:-
1. In a {iying machine of the class decribed, incombination with a main frame, a platform having brace rods and provided with ground wheels suitably suspended from said frame, transverse parallel propellershafts mounted upon said frame,l propellers provided with a series of blades adapted to open and close placed at right angles to each:
other, suitably secured upon said shafts, a sleeve provided with a cam mounted upon said shaft `for opening and closing said blades, lever connected to said sleeve, hand operatingl levers mounted upon said frame,
and rods connecting said sleeve ,operating lever to said hand levers for timing the vopeningfand shutting of said blades.
2. In a flying machine of the class described, a supporting frame provided with-a transversely Aextending propeller shafts lsuitably mounted on said frame, propellers provided with radial shutters at right angles to each other forming blades, a cam sleeve mounted' upon said propeller shaft and pro vided with a cam-race way, means for holding said cam sleeve fromrotating on Said shaft, a reciprocating rod having a roller suitably secured thereto, said roller adapted to move in said race-way of the cam, sleeve cranks secured to said Shutters, connecting rods between said-cranks and reciprocating rods, hand operating levers mounted upon said frame for the purpose of operating said cam sleeve and timing the opening and shutting of said shutters, substantially as described.
In testimony whereof I aix my signature in presence of two witnesses- SIMON B. MINNICH. llVitriesse's:V
' WM. J. COULTER,
MABEL L. LEFEVRE.
US51551609A 1909-08-31 1909-08-31 Flying-machine. Expired - Lifetime US1010443A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2436113A (en) * 1942-10-05 1948-02-17 David W Main Airplane propeller
US2449531A (en) * 1942-06-02 1948-09-14 Lee Nixon Impeller

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2449531A (en) * 1942-06-02 1948-09-14 Lee Nixon Impeller
US2436113A (en) * 1942-10-05 1948-02-17 David W Main Airplane propeller

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