US954053A - Propeller. - Google Patents

Propeller. Download PDF

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Publication number
US954053A
US954053A US43535808A US1908435358A US954053A US 954053 A US954053 A US 954053A US 43535808 A US43535808 A US 43535808A US 1908435358 A US1908435358 A US 1908435358A US 954053 A US954053 A US 954053A
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Prior art keywords
propeller
lines
cone
blades
water
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US43535808A
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Henry F Shaw
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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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H1/00—Propulsive elements directly acting on water
    • B63H1/02—Propulsive elements directly acting on water of rotary type
    • B63H1/12—Propulsive elements directly acting on water of rotary type with rotation axis substantially in propulsive direction
    • B63H1/14—Propellers
    • B63H1/26—Blades

Definitions

  • the object is to construct 'a propeller for boats that will admit of a high speed of rota tion and still retain a firm and steady .hold upon the water in its field of action. I attain this advantage by the construction illus- ,trated ,in the-accompanying drawings, in
  • Figure l is a rear end View of one of the propeller wheels.
  • Fig. 9 is a plan view of one of my propellers and its ⁇ shaft, also lines a method of determining the required surface form of the blades.
  • Figs?) is a side view showing one of the blades in full and one in section, also indicating by dotted lines a method of determining the required surface of form of It is Well known that the propellers now in use if madeto rotate above a certain velo'city' will break up the water and thus lose; the ig hold upon the water and consequently their efliciency.
  • the cause of this breaking up the water is that the propeller blades have heretofore been so shaped that when made to rotate with a velocity of rotation above a certain fixed ratethey throw the water that is in their field of action out-
  • My propeller has blades the working surfacesof which are so formed that all of the water that comes within their field of action is'thrown inwardly as well as rearwardly; thus the water is kept within the working the blades of the propeller, thus e propeller a body of water to act upon.
  • the hub A A which may be shaped in the form approximating that of a frustum of a cone or pyramid, the larger end being indicated by A and the smaller by A
  • the bladesB and C have working surfaces that are generated by the movement of a line one end of which is always at the point B and the other end directed by a circle, theplane of which is at right angles to a line that passes through the point B and the center of said circle.
  • the working surfaces of the blades lie in the surface of a right cone the axis of which will be at an angle with the propeller shaft and the apex of the cone will be in front of the propeller and at a distance from the shaft, as shown in Figs. 2 and 3.
  • the distance that'the apexof the cone, that is, the point B, is from the propeller and from the shaft must depend upon circumstances. 'I have found by theory and experiment that the distance of the said distance that the said apex is in front of the rear edge of the hub is about two and a quarter times the width-of the blade.
  • the dotted lines refer to a device that I have used laying out the surface of the working side. of the blade, and consists in an adjustable sliding piece N, which may be held at any desired position by the set screw N an arm P extends laterally from the said sliding piece N and has a ball and socket joint at R., The radial wire S swings on this joint as indicated; in the drawing Figs. 2-and 3.
  • the moving end of the wire is directed by a circle the diameter of which and the distance of its plane from the point B will determine the angle or pitch of the blade.
  • the above suggested location of the apex of the cone is not to be considered as exact but only approximate.
  • I will term the boundary lines of the propeller blades as followsqThe lines L L L of Fig.
  • the end A of the hub is the aft end, and the end A is the fore end.
  • The' lines L L L indicate aft boundary lines and lie approximately in the surface ofan imaginary cone the axis of which coincides with that of the axis of rotation of the propeller; that is, if the propeller is rotated in sand the pit left 1n the apex from the center of the shaft is, about one-half of the width of the blade, and the said sand will be shaped as a frustum of a cone.
  • a propeller having a its fore end than on its coned hub lar er on aft end, and lades surface tangent to hub and continuing therefrom constituting coned surfaces, s'aid coned surfaces of each blade bein a part of the surface of a cone the axis of which isinclined to the axis of rotation of the propeller as described; the aft boundary lines, that is the aft edge lines of the propeller blades, lie approximately in the surface of a cone the axis of which coincides with that of the rotation" of the propeller; substantially as and for the purose set forth.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Ocean & Marine Engineering (AREA)
  • Toys (AREA)

Description

H. F. SHAW.
V PROPELLER. APPLIOATION FILED .MAY 27, 1908.
Patented Apr. 5, 1910.
"esaoaa.
HENRY r. sHAw, or BOSTON, messnonu'snmsf PrELLnn.
lwhile-in rotation to cause the water in its field of action to flow inwardly. as well as rearwardly, thus always furnishing a steady and evemresistance for the propeller to react upon.
The object is to construct 'a propeller for boats that will admit of a high speed of rota tion and still retain a firm and steady .hold upon the water in its field of action. I attain this advantage by the construction illus- ,trated ,in the-accompanying drawings, in
3 the blades.
' space of giving th showing f in dotted ,wardly and then break it up.
Figure l is a rear end View of one of the propeller wheels. Fig. 9 is a plan view of one of my propellers and its \shaft, also lines a method of determining the required surface form of the blades. Figs?) is a side view showing one of the blades in full and one in section, also indicating by dotted lines a method of determining the required surface of form of It is Well known that the propellers now in use if madeto rotate above a certain velo'city' will break up the water and thus lose; the ig hold upon the water and consequently their efliciency. The cause of this breaking up the water is that the propeller blades have heretofore been so shaped that when made to rotate with a velocity of rotation above a certain fixed ratethey throw the water that is in their field of action out- My propeller has blades the working surfacesof which are so formed that all of the water that comes within their field of action is'thrown inwardly as well as rearwardly; thus the water is kept within the working the blades of the propeller, thus e propeller a body of water to act upon.
i In Fig. 1 of the drawings the propeller is Specification of Letters Patent. f- I Application filed May 27, 1908. Serial No. 435,858.
Patented Apr.5,i19il.
shown in elevation; the hub A, A which may be shaped in the form approximating that of a frustum of a cone or pyramid, the larger end being indicated by A and the smaller by A The bladesB and C have working surfaces that are generated by the movement of a line one end of which is always at the point B and the other end directed by a circle, theplane of which is at right angles to a line that passes through the point B and the center of said circle. In other words, the working surfaces of the blades lie in the surface of a right cone the axis of which will be at an angle with the propeller shaft and the apex of the cone will be in front of the propeller and at a distance from the shaft, as shown in Figs. 2 and 3. The distance that'the apexof the cone, that is, the point B, is from the propeller and from the shaft must depend upon circumstances. 'I have found by theory and experiment that the distance of the said distance that the said apex is in front of the rear edge of the hub is about two and a quarter times the width-of the blade.
The dotted lines refer to a device that I have used laying out the surface of the working side. of the blade, and consists in an adjustable sliding piece N, which may be held at any desired position by the set screw N an arm P extends laterally from the said sliding piece N and has a ball and socket joint at R., The radial wire S swings on this joint as indicated; in the drawing Figs. 2-and 3. The moving end of the wire is directed by a circle the diameter of which and the distance of its plane from the point B will determine the angle or pitch of the blade. The above suggested location of the apex of the cone is not to be considered as exact but only approximate. I For convenience and ease of description I will term the boundary lines of the propeller blades as followsqThe lines L L L of Fig. 2 1 call the aft lines and the lines T T T, Fig. 2,-the fore lines. The end A of the hub is the aft end, and the end A is the fore end. The' lines L L L indicate aft boundary lines and lie approximately in the surface ofan imaginary cone the axis of which coincides with that of the axis of rotation of the propeller; that is, if the propeller is rotated in sand the pit left 1n the apex from the center of the shaft is, about one-half of the width of the blade, and the said sand will be shaped as a frustum of a cone.
Claim. A propeller having a its fore end than on its coned hub lar er on aft end, and lades surface tangent to hub and continuing therefrom constituting coned surfaces, s'aid coned surfaces of each blade bein a part of the surface of a cone the axis of which isinclined to the axis of rotation of the propeller as described; the aft boundary lines, that is the aft edge lines of the propeller blades, lie approximately in the surface of a cone the axis of which coincides with that of the rotation" of the propeller; substantially as and for the purose set forth.
In testimony whereof, I have signed my name to this specification in the presence of 20 two subscribing witnesses, on this sixth day of May A. D. 1908.
HENRY F. SHAW.
Witnesses:
WILLIAM Enson, JAMES MACLEAN.
US43535808A 1908-05-27 1908-05-27 Propeller. Expired - Lifetime US954053A (en)

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US43535808A US954053A (en) 1908-05-27 1908-05-27 Propeller.

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