US1043004A - Airship. - Google Patents

Description

1). A. FLANIGAN.

AIRSHIP.

- APPLICATION FILED 513.14, 1911.

04 9 1 9 2 f C 0 d 8 b H m a P 1 T E E H S S T B E H s 2 IN VENT OR WITNESSES D. A. PLANIGAN.

AIR-SHIP. urmcnmn FILED FEB. 14, 1911.

, 1,043,004. Patented 001129, 1912.

- 2 SHEETS-$113111. 2.

[1V VEN TOR WITNESSES @130 n. M I

"UNITED STATES PATENT onnron DAVID ALMA'FLANIGAN, or srnmevinnn; UTAH, Ass renon 'r'o UTAH 1min. nnvren'rron AND rowan COMPANY, or srnINevILLn, UTAH. I

Ainsmr.

1,043,004. Specification 01 Letters Iatent. p t t t 29, 9

Application filed February 14, 1911. Serial No. 608,624.

the braces 4 which support the bearings 5 having rotatably mounted therein the hollow shaft or sleeve 6 which extends the width of the bodyof the car, said sleeve having an enlarged central portion? having a slot 8 in the lower or under side thereof. On the ends of the sleeve arethe heads to which are secured the brackets 9, while connecting the brackets is a brace bar 10.

J ournaled in the sleeve 6 is a shaft 7 having a sprocket wheel 11 located in the enlarged portion 7 of the sleeve, while mounted on each end of the shaft is a beveled gear wheel 12, said gear being in mesh with the beveled gear wheel 13 of the tubular shaft 14 and thegear 15 of the solid shaft 16, the shaft 14 passing throu h an gpening in the end of the bar 10.an held Y while the shaft 16 is journaled in the tubular shaft 14 and has its lower -end supported by the bracket 9. correct position, I mount upon each shaft 16 the loose sleeve/18 held in positionv upon the shaft by the collars 19, said sleeves being connected by the brace rod 20 which serves in connection with the shafts and bar 10 to form a strong rectangular frame.

It will be observedthat I have mounted upon the upper end of each of the shafts the blades or vanes 21, while leading from the sprocket wheel 11 to a power supplying-device 22 is the chain 23 which serves to revolve the shaft 7 which shaft through the medium of the beveled gears causes the tubular shaft and solid shaft journaled therein to revolve in opposite directions and thus create through the blades a strong lifting force for operating the flying machine, as will be readily understood by reference to the drawings.

To all whom it may concern:

Be it known that I, DAVID A. FLANIGAN, a citiz'enof the United States, residing at Springville, in the county of Utah and State of Utah, have invented certain new and useful Improvements in Airships, of which the following is a specification.

My invention relates to improvements in mechanical movements, and the leading object of my invention is the provision of im proved mechanism for the transmission of power which shall be particularly adapted for use in driving flying machines of the helicopter type.

A further object of my invention is the revision of ine of this character a mach which shall be adapted either for use in elevating weights as a helicopter of for the production of power'through the medium of air or other fluid currents impacting against the vanes or blades carried by the shafts.

Another object of the invention is the provision of strong, simple and durable mechanism of a light but efficient type which may be interchangeably employed for use in lift ing a flying machine and sustaining the same or for a power motor.

To attain the desired objects, my invention comprises mechanism for attaining certain mechanical movements, said mechanism comprising a'tubula: shaft having asecon shaft j'ournaled therein, each of said shafts being provided with vanes or blades, and a shaft connected by gearing to the other end of said pair. of shafts in such manner that the tube and shaft journaled therein revolve in opposite directions while the other shaft revolvesin a constant direction and serve either to drive the pair of shafts or be driven thereby, the invention further residing in the novel features of construction and combination and arrangement of parts for service substantially as described and as illustrated in the accompanying drawings.

Figure 1 represents a side elevation of complete machine. Fig. 2 represents a front view thereof. Fig. 3 re resents a sectional View of the hearings or the shafts, the tubular shaft being shown in section, and, Fig. 4 represents a detailed view of-the shaft adjusting mechanism.

In the drawings, the numeral 1 designates the body of the car havin located at the rear the rudder 2 operated the handle 3, and rising from the body f. t e machine are To aid in con scent of my air ship when equipped with the above described lifting fans, sleeve 6 the rock arm 2 1 having pivotally secured to its outer at its other end to the lever 26 pivoted to the bracket 27 carried by the base of the body, said bracket being a segment 28 adapted to be engaged by a dog 29 carried by the lever to lock the same in adjusted position. In operation, the adjustmen-t of the lever 26 serves to swing the sleeve 6. and thus the brackets and shafts at an angle to the car, the direction in which end the link 25 pivoted a collar 17 bearing against the said bar,

To retain the shafts in I trolling the ascent and de-- y I secure to the i i 3 said impact will combination with the bask said shafts are swung 0f the flying machine varying the movement as will be readily understood.

be apparent to all It will that I have vided an improved mechanism for the transblades and thelr shafts and that in this I clalm: 1. In power transmission mechanism, the et, rudder and supports, of a shaft mounted therein, and its outer ends metrically opposite points, respectively, upon tubular shafts having journaled therein solid shafts, the said'pairs of shafts being adapted to be either revolved "in opposite dimain shaft in a' constant direction, said pairs of shafts same in adjusted position. n

the bod belng connected at their upper and lower extremities, respectively, by a pair of brace rods secured thereto, blades d upon said pairs of shafts, and means usting the angle of the pairs of shafts dy of .the machine, a rock arm having one end fastened to a sleeve mounted on the {min shaft and pivotally secured to having its other end a link, said link being pivoted adapted an a1r-sh1p, the combination with rudder and supports, of a main shaft rotatably 'journaled in a sleeve carried by said supports, means for rotating said shaft, gears secured u on the outer extremities of said shaft and meshing with gears secured upon the lower ends pper en s whereby a lifting impact is iven the machine, brace rods connecting 'sai tubular s hafts at'their upper and lower portions and forming a, fr 7, ,ar.

cause the revolution of the cured to its outer end,

- basket, of supports brackets, bevel ved in opposite dit l In a constant "dlrection, tmd'lbl means for adjusting the angle of the pairs of shafts with respect to the body of the machine.

3. In an airship, the combination with the car body and rudder, of a plurality of braces rising therefrom, a sleeve supported by the braces, said sleeve having an enlarged slotted central portion and a drive shaft, brackets secured upon each end of the sleeve, a brace bar connecting said brackets, a sprocket wheel journaled in the enlarged portion of the sleeve, :1 gear mounted at each end of the shaft, a pair of tubular shafts supported by the brackets and brace bar at right angles to the drive shaft, gears carried thereby meshing with the gears on the drive shaft, solid shafts journaled in the tubular shafts, gears carried by said solid shafts meshing with said drive shaft gears, loose sleeves carried at the upper ends of the solid shafts, a brace rod connecting the two shafts and forming with the lower brace rod a substantiallyreetangular frame, vanes upon the upper ends of each of the tubular and solid shafts, driving means connected to the sprocket wheel on the sleeve, and means for controlling the ascent and descent of the airship, said means comprising a rock arm mounted upon the sleeve, a link pivotally sean operating lever pivoted and a Segmental rack carried thereby and adapted to engaged by a dog upon the lever, the arrangement of the drive and driven shafts being such that the tubular and solid shafts are revolved in opposite directions or that revolved by the the drive shaft may be when desired.

driven shafts In an airship, the combination with a rising therefrom, bearings carried by said supports, a sleeve journaled therein, a horizontally disposed shaft in said sleeve, brackets secured to said sleeves, a connecting brace rod for said brackets,-a bevel gear mounted on each end of said shaft, vertical shafts rising from said gears carried thereby meshing with said gears on the horizontal shaft, a brace rod connecting the upper ends'of said vertical shafts, blades secured upon said vertical shafts. and means for adjusting the angle of said shafts with respect to the body 0 the-airship.

5. In an airship,--the combination with a basket, of supports rising'therefrom, a horizontally disposed shaft journaled' thereon, gear wheels carried by said shaft, pairs of tubular and solid shafts arranged adjacent said horizontal shaft, gear wheels carried b said tubular and solid shafts meshing wi said gears on the horizontal shaft, horizona brace rods connectin the upper and lower extremities of the vertical shafts, ades carried by said shafts,-and means for ed therein and formed with an enlarged centively connected with the horizontal shaft,

ed therein and formed with an enlarged central portion, a horizontally disposed shaft 'ournaled therein, as rocket carried by said adjusting the angle of saidshafts with respect to the body of the machine.

(5. In an airship, the combination with a platform, driving means thereon, supports rising from the platform, bearings on the upper ends of said supports, a sleeve mountsleeve, and connected with the driving means by a sprocket chain, brackets secured to said sleeve, a horizontally disposed brace rod .setral portion, a horizontally disposed shaft journaled therein, a sprocket carried by said shaft within the enlarged portion of the sleeve and connected with the driving means by a sprocket chain, brackets'secured to said sleeve, a horizontally disposed brace rod secured to said brackets, a brace rod thereabove, collars on said brace rods, vertically disposed solid and tubular shafts o-peraabove, collars on said brace rods, vertically disposed solid and tubular shafts operatively connected with the horizontal shaft, sleeves on the solid shafts engaged by the collars'on the upper horizontal brace rod, the lower ends of the tubular shafts being engaged by the collars on the lower brace rod, blades carried by said vertical shafts, a rock armsecured to the sleeve of the horizontal sleeves on the solid shafts engaged by the shaft and arranged parallel to the sprocket collars on the upper horizontal brace rod, the lower ends of the tubular shafts being engaged by the collars on the lower brace means, and means connected therewith for adjusting the angle of the vertical shafts. rod, and blades carried by said vertical In testimony whereof I afiix my signature shafts. in presence of two witnesses.

7. In anairship, the combination with. a DAVID ALMA FLAN-IGAN.

platform, driving means thereon, supports Witnesses:

rising from the platform,'bearings on the w W. B. MoPHERsoN, upper ends of said supports, a sleeve mount- J. D. BAGLEY.

shaft within the en arged portion of the cured to said brackets, a brace rod there-' 'chain connecting said shaft and the driving

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