US996547A - Propeller for aerial vehicles. - Google Patents

Propeller for aerial vehicles. Download PDF

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Publication number
US996547A
US996547A US58279710A US1910582797A US996547A US 996547 A US996547 A US 996547A US 58279710 A US58279710 A US 58279710A US 1910582797 A US1910582797 A US 1910582797A US 996547 A US996547 A US 996547A
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Prior art keywords
propeller
aerial vehicles
ropes
blade
axis
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US58279710A
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Richard Wilcke
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/38—Blades
    • F04D29/384—Blades characterised by form

Definitions

  • the driving planes may be made practically as large as may be desired.
  • the operative surface is located farther from .the axis of the propeller than in the case of well-known propellers the speed may be less.
  • the driving planes are pivoted on their supports they can be adjusted, preferably by means of ropes, in such manner that they drivebackward or forward or not at all.
  • each driving plane or blade '0 is pivotally mounted on an arm a of a spoke a carried by the propeller shaft 6.: These planes are inclined both relatively to the pro eller shaft and the spokes and can be rocke on the hinges e by means of the ropes. d or the like. The ropes also serve for anchoring the planes in their adjusted positions. Now by swinging each plane or blade 0 about its appertaining pivot f I can adjust the inclination of the planes radially inwardly or outwardly and relatively to the spokes or to an imaginary cylinder around the axis of the propeller before starting the journey. The adjustment by means of the ropes d can also be made while traveling. v
  • the ropes may be led along outside or through the hollow propeller shaft to adjusting devices.
  • I may attach the ropes to a ring 9 which participates in the rotation of the propeller shaft and is displaceable longitudinally of the shaft. This ring can beshiftedby a non-rotatable fork or ring it which engages in the former ring, whereby the ropes can be adjusted.
  • An aerial propeller comprising in combination, a propeller shaft, propeller arms radiating from said shaft, a blade arm pivotally mounted on one of said propeller arms and having its free end inclined with res ect to the longitudinal axis of said propel er arm, a blade hinged to swing on the lnclined free end of said blade arm, and

Description

R. WILCKE.
PROPELLER FOR AERIAL VEHICLES.
APPLICATION FILED SEPT. 19, 1910.
996,547, Patented June 27, 1911,
Qflifmoaes; 1 f flawmtazi RICHARD WILCKE, 0F FRIE DENAU, NEAR BERLIN, GERMANY.
PROPELLER'FOR AERIAL VEHICLES.
Specification of Lettersl'atent.
Patented June 27, 1911.
Application filed September 19, 1910. Serial No. 582 ,797.
To all whom it may concern:
Be it known that I, RICHARD WILoKE, a
subject-of the German Emperor, and residefiiciency, and one in which the propelling action can be varied and reversed. To this end I impart to the driving planes or blades of the propeller, in addition to the Wellknown inclination relatively to the plane at rightangles to its axis, an inclination relatively to an imaginary cylindrical surface around the axis, in such manner that the planes exercise an inwardly-directed pressure. In consequence of this inwardly-directed component the .air is not thrown to the rear in the form of a cone as when the well-known propellers are used, but in the form of a cylinder parallel to the axis of the propeller. Besides increasing the efiioiency this has the additionahadvantage that disturbing currents of air are not caused laterally of the propeller. When the propeller is arranged in-this noyel manner the driving planes may be made practically as large as may be desired. As the operative surface is located farther from .the axis of the propeller than in the case of well-known propellers the speed may be less. When the driving planes are pivoted on their supports they can be adjusted, preferably by means of ropes, in such manner that they drivebackward or forward or not at all.
One constructional form of my invention is represented by way of example in the accompanying drawing, wherein I Q Figure l is a side elevation showing my propeller, and Fig. 2 is' a cross-section through the same. I
Referring to the drawing, each driving plane or blade '0 is pivotally mounted on an arm a of a spoke a carried by the propeller shaft 6.: These planes are inclined both relatively to the pro eller shaft and the spokes and can be rocke on the hinges e by means of the ropes. d or the like. The ropes also serve for anchoring the planes in their adjusted positions. Now by swinging each plane or blade 0 about its appertaining pivot f I can adjust the inclination of the planes radially inwardly or outwardly and relatively to the spokes or to an imaginary cylinder around the axis of the propeller before starting the journey. The adjustment by means of the ropes d can also be made while traveling. v
The ropes may be led along outside or through the hollow propeller shaft to adjusting devices. For example,in order to prevent the ropes being twisted by the motion of the propeller shaft, I may attach the ropes to a ring 9 which participates in the rotation of the propeller shaft and is displaceable longitudinally of the shaft. This ring can beshiftedby a non-rotatable fork or ring it which engages in the former ring, whereby the ropes can be adjusted.
I claim:-
1. In an aerial propeller of the character described, the combination of a spoke having a slanting arm pivoted thereto, a blade or plane pivoted on said arm, and means attached to the blade or planefor inclining the same relatively to a plane at right angles to the axis of the propeller and relatively to an imaginary cylinder around the same axis for the purpose of acting radially inwardly on the air.
2. An aerial propeller comprising in combination, a propeller shaft, propeller arms radiating from said shaft, a blade arm pivotally mounted on one of said propeller arms and having its free end inclined with res ect to the longitudinal axis of said propel er arm, a blade hinged to swing on the lnclined free end of said blade arm, and
means for adjusting said blade on its hinged mounting to impart a radial inward move ment to the air.
In testimony whereof I aifix my signature in presence of two witnesses.
RICHARD wILoKn.
- Witnesses:
ROLLEN KUHN, WOLDEMAR HAUPT.
US58279710A 1910-09-19 1910-09-19 Propeller for aerial vehicles. Expired - Lifetime US996547A (en)

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US58279710A US996547A (en) 1910-09-19 1910-09-19 Propeller for aerial vehicles.

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US58279710A US996547A (en) 1910-09-19 1910-09-19 Propeller for aerial vehicles.

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