US187633A - Improvement in screw-propellers - Google Patents

Improvement in screw-propellers Download PDF

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US187633A
US187633A US187633DA US187633A US 187633 A US187633 A US 187633A US 187633D A US187633D A US 187633DA US 187633 A US187633 A US 187633A
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Prior art keywords
blades
shaft
propellers
improvement
screw
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/06Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00Fluid reaction surfaces, i.e. impellers
    • Y10S416/03Sheet metal

Definitions

  • Figure 1 is a Vside View
  • Fig. 2 an end view.
  • My invention relates to a novel construction of propeller, designed to secure a greater driving capacity with a smaller Aexpenditure I of power, and adapted to operate either upon the air or water as a fulcrum.
  • the invention consists in a set of rightangled triangular vanes, blades, or fans, one side of each of which blades is attached to the propeller-shaft at right angles thereto,
  • the laterally projecting tapering blades thus constructed and arranged serving to distribute the work in ratio corresponding to the leverage throughout the length of the blades
  • A represents a portion of the propeller-shaft, to which the4 blades are attached, which shaft is to be located in bearings, and rotated by connection with any suitable driving mechanism.
  • B B B are the right-angled triangular blades,
  • the blades I find, however, work well for a variation of fifteen degrees upon either side of the angle thus formed, and I therefore do Inot limit myself in this particular.
  • the face of the@ blades which operates upon the fluid shouldbe straight, or nearly so, in order to reduce as far as possible the friction incident to the ⁇ curves of propellers, as heretofore constructed, and any number of blades may be employed in the construction of the propeller Propellers as heretofore constructed have generally their widest faces and largest propelling-surfaces at the extremity or long end ot' the lever, the effect of which is seen in the great expenditure of power required to propel, a large portion of which power expended is lost in carrying dead-water.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Description

I k, 'di' WILLIAM S. HULL, or IIINDS COUNTY, MISSISSIPPI.
, IMPROVEMENT In scnEwfPRoPELLERs.
Specilication' forming part of Letters Patent N o. 187,633-,` dated February 20,1871; application filed November 7, 1876.`
To all whom it may concern :v
Be it known that I, WILLIAM S. HULL, of the county of Hinds and State of Mississippi, have invented a new and Improved Propeller; and I do hereby declare that the following .is a full, clear, and exact description of the same,
' reference being had to the accompanying drawing, forming part of this specication, in which.-
Figure 1 is a Vside View, and Fig. 2 an end view.
My invention relates to a novel construction of propeller, designed to secure a greater driving capacity with a smaller Aexpenditure I of power, and adapted to operate either upon the air or water as a fulcrum.
The invention consists in a set of rightangled triangular vanes, blades, or fans, one side of each of which blades is attached to the propeller-shaft at right angles thereto,
while the rear and less acute apices are deflected away from the said shaft, the laterally projecting tapering blades thus constructed and arranged serving to distribute the work in ratio corresponding to the leverage throughout the length of the blades, and
thus securing a greater motive effect from a smaller expenditure of power.
In the accompanying drawing, A represents a portion of the propeller-shaft, to which the4 blades are attached, which shaft is to be located in bearings, and rotated by connection with any suitable driving mechanism. B B B are the right-angled triangular blades,
which are attached at their right angles to light material, attached at their front sides' to stiff laterally-projecting radial arms D D D, and at their rear deflected apices to corresponding radial arms G G C, or, when used to operate upon water as a fulcrum, may be cast in one piece, stiff enough to dispense with said arms C and D, and provided with a coupling at their right angles for direct atlengthiof the larger side at right angles to the shaft.
The blades I find, however, work well for a variation of fifteen degrees upon either side of the angle thus formed, and I therefore do Inot limit myself in this particular. The face of the@ blades which operates upon the fluid shouldbe straight, or nearly so, in order to reduce as far as possible the friction incident to the `curves of propellers, as heretofore constructed, and any number of blades may be employed in the construction of the propeller Propellers as heretofore constructed have generally their widest faces and largest propelling-surfaces at the extremity or long end ot' the lever, the effect of which is seen in the great expenditure of power required to propel, a large portion of which power expended is lost in carrying dead-water.
By means of the propeller blades constructed as described, it will be seen that the resisting surface is distributed throughout the length of the blade in proper ratio to the leverage; and I am thus enabled to secure the maximum effect of the propelling power with the smallest amount lof resistance.
By the Same construction of blade, also, when arranged as described, I am enabled'to employ the full width of the blade near the shaft, without the cbjection of a lack Vof clearance for the fluid operated upon, the ldeflection of,` the rear apex of the bladefrom the shaft permitting a free and easy passage of the iiuid to the rear.
Having thus described my invention, what I claim as new isrIheeornbination, with the propeller-shaft, of a series of right-angled triangular blades, having their front sides attached to said shaft at right angles, and their rear apices deiiected away from thesame, substantially as and for the purpose described.
i WILLIAM S.. HULL.
Witnesses:
`W. S. HAMILTON, JNO. T. HALL.
US187633D Improvement in screw-propellers Expired - Lifetime US187633A (en)

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