US1427307A - Propeller - Google Patents

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US1427307A
US1427307A US264050A US26405018A US1427307A US 1427307 A US1427307 A US 1427307A US 264050 A US264050 A US 264050A US 26405018 A US26405018 A US 26405018A US 1427307 A US1427307 A US 1427307A
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pitch
propeller
blade
inner part
outer part
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US264050A
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Roy C Makenney
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H1/00Propulsive elements directly acting on water
    • B63H1/02Propulsive elements directly acting on water of rotary type
    • B63H1/12Propulsive elements directly acting on water of rotary type with rotation axis substantially in propulsive direction
    • B63H1/14Propellers
    • B63H1/26Blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/16Blades

Definitions

  • This invention relates to improvements in propellers and the objects of the invention are to secure greater efficiency from the propeller and avoid waste of power near the hub thereof.
  • Fig. 2 is a top View.
  • Fig. 3 is an end view showing the opposlte side of Fig. 1. s
  • Fig. i is a perspective in detail also showing a helical twist of the inner part.
  • Fig. 5 is a section on the line 2-2 of Figure 4. s 1
  • Fig. 6 is a side elevation of one of the blades showing the pitch lines thereon.
  • A represents the hub of the propeller and B the blades, of which any number desired may be provided.
  • the propeller illustrated has three blades and is designed to turn in clockwise direction, which is known as right hand.”
  • Aleft hand propeller would have the inclinations reversed.
  • Each blade is formed with an inner part 10 and an outer part 11, the outer part being considerably wider than the inner part and set at a greater pitch thereto.
  • the object for designing the bladein two parts namely an inner vpart l0, and an outer part 11, is the following.
  • the inner part 10 is given less pitch than the outer parts pitch base line L (which Wlll be described hereafter), so that when revolving through the water the inner part will not push or interfere in any way, and will thus save considerable power.
  • This power, in the true-screw propeller, is wasted Specification of Letters Patent. Fata [ted Afig, 29, 1922,
  • the inner part has a helical twist on the driving side and the'edges are curved'in opposite direc tions both fore and aft and sideways,salso the innerpart is set at approximately 20 to 35 per cent less pitchthan the outer part 11 pitch base line L. In this way when theproits entire width and depth, and consequently there is less friction and backpressure than with a concaved true-screw or other deslgned blade, which will exert a difierentpressure on water at different points of its blade surface both radial and axial. I l.
  • the driving blade face of my propeller being set at right angles to shaft forces the water in a straight line parallel to shaft with the result that there is no waste of. powerby exerting force 1n an indlrect manner.
  • the outer part 11 is rounded off nicely on the edges to form a pleasing shape, and is not limited to this particular style in the attached drawings as to shape of blade.
  • V I do not choose any particular portion of the diameter of a propeller to set the pitch llne base L on, as in pract ce, raising or lowering.
  • the pitch base line L may be proved more efiicient.
  • the pitch base line L is vplacedat two-thirds the diameter of propellerand find it very satisfactory.
  • the proper angle at which to set the outer part 11 is calculated at this pitch baseline and is governed by the diameterofthe propeller,
  • the outer part 11 has a flat driving face, therefore it has the same angle throughout its length and width, and this will cause the pitch to increase radially outward to the end of blade, till at its highest point above the pitch base line L it would be 50% more than at the pitch base line.
  • pitch base line was lowered to one-half the diameter instead of two thirds the pitch would be 100% more at the top, or if base line was raised above the 2/3 diameter the pitch would decrease accordingly.
  • the space between the pitch line basis L and the line 0 drawn at the top of the inner part 10 is the slip portion of the driving blade or outer part 11. That is :the driving blade being flat the angle is the same throughout and this portion being below the pitch base line L will decrease in pitch, till if propeller is slipping, say, 20 per cent. The lowest part of the driving blade '11 will cease to push when it is 20 per cent of the distance below pitch base line L to the axis of the propeller.
  • the curved line 0 shown on. the blade illustrated in Figure 6 shows the portion between the inner portion 10 and the blade or outer part 11.
  • the helical twist of the inner part starts from this line.
  • the inner part 10 from its top (that is from line 0) to the hub has helical twist on its back face, and its edges curving in opposite directions sideways (to strengthen same) and fore and aft, so that the front portion 12 of the inner part 10 is constructed at as muchslant aft as possible. This is the reason for giving the inner part 10 a helical twist; so that when the boat is mov ing ahead the water will strike against the front portion 12 opposing very little resistance, and whatever resistance there is is utilized to turn the propeller over, similar to a windmill, and thereby aid at pushing the boat ahead by transmitting power.
  • the front portion 15 011 the outer part 11 as well as the front portion 12 on the inner part 10 are rounded off tapering to a sharp cutting edge 1'7, which cuts through the water with less resistance than a blunt or wedge-shaped cutting edge.
  • a propeller blade comprising an inner and outer part, the inner part being set with a helical twist at 25 to 30 per cent less pitch than the outer part pitch basis, the driving side of the outer part being flat and at right angles to the axis of the hub of the propeller, thereby causing the pitch to expand as it nears the top of the blade, and the front face of the blade being convex and tapering of]? to a sharp cutting edge.

Description

R. C. MAKENNEY.
PROPELLER.
APPLICATION FILED NOV.25, 191a.
Patented Aug. 29, 1922.
JMVEAITDR' RWL'iMnKENI/EY ROY C. MAKENNEY, OF ST. JOHN, NEVV' BRUNSWICK, CANADA.
rnor nnrinn.
earner.
Application filed November 25, 1918. Serial No. 264,050.
T 0 all whom it may concern:
Be it known that 1, Box C. MAKnnNnY, a subject of the King of Great Britaln, and resident of the city of St. John, in the Province of New Brunswick, Dominion of Canada, have invented certain new and useful Improvements in Propellers, of which the following is a specification.
This invention relates to improvements in propellers and the objects of the invention are to secure greater efficiency from the propeller and avoid waste of power near the hub thereof.
Further objects are to provide an unproved desi n of blade by which a greater propulsive force may be obtained from the same amount of power, and it consists essentially of the improved construction hereinafter described in detail in the accompanying specification and drawings In the drawings Fig. l is an end view of propeller.
Fig. 2 is a top View.
Fig. 3 is an end view showing the opposlte side of Fig. 1. s
Fig. i is a perspective in detail also showing a helical twist of the inner part.
Fig. 5 is a section on the line 2-2 of Figure 4. s 1
Fig. 6 is a side elevation of one of the blades showing the pitch lines thereon.
In the drawings like characters of reference indicate corresponding parts in all the figures.
Referring to the drawings, A represents the hub of the propeller and B the blades, of which any number desired may be provided. The propeller illustrated has three blades and is designed to turn in clockwise direction, which is known as right hand." Aleft hand propeller would have the inclinations reversed.
Each blade is formed with an inner part 10 and an outer part 11, the outer part being considerably wider than the inner part and set at a greater pitch thereto.
The object for designing the bladein two parts namely an inner vpart l0, and an outer part 11, is the following.
The inner part 10 is given less pitch than the outer parts pitch base line L (which Wlll be described hereafter), so that when revolving through the water the inner part will not push or interfere in any way, and will thus save considerable power. This power, in the true-screw propeller, is wasted Specification of Letters Patent. Fata [ted Afig, 29, 1922,
on account of the low angle with reference to direction of the boat on the inner part of the true-screw propeller blade, which push the water more sideways than astern. Themore the water is pushed astern the easier the boat moves ahead. 1
In the embodiment illustrated the inner part has a helical twist on the driving side and the'edges are curved'in opposite direc tions both fore and aft and sideways,salso the innerpart is set at approximately 20 to 35 per cent less pitchthan the outer part 11 pitch base line L. In this way when theproits entire width and depth, and consequently there is less friction and backpressure than with a concaved true-screw or other deslgned blade, which will exert a difierentpressure on water at different points of its blade surface both radial and axial. I l.
The driving blade face of my propeller being set at right angles to shaft forces the water in a straight line parallel to shaft with the result that there is no waste of. powerby exerting force 1n an indlrect manner. The outer part 11 is rounded off nicely on the edges to form a pleasing shape, and is not limited to this particular style in the attached drawings as to shape of blade.
V I do not choose any particular portion of the diameter of a propeller to set the pitch llne base L on, as in pract ce, raising or lowering. the pitch base line L, may be proved more efiicient.
As at present designed the pitch base line L is vplacedat two-thirds the diameter of propellerand find it very satisfactory. The proper angle at which to set the outer part 11 is calculated at this pitch baseline and is governed by the diameterofthe propeller,
type of boat and purpose it is to be used for,
horsepower, revolution and type of engine. Any width of blade may be used as further experiment will prove the most suitable.
As already stated the outer part 11 has a flat driving face, therefore it has the same angle throughout its length and width, and this will cause the pitch to increase radially outward to the end of blade, till at its highest point above the pitch base line L it would be 50% more than at the pitch base line.
This is owing to the longer circumference line at the edge of the blades over that at the pitch line and this increase averages 25% more pitch than a true screw propeller at the outer one-third diameter.
In other words, on account of the outer part 11 having a flat face the angle is the sameithrough any cross sections therefore causing-the pitch to be greater the further thecross section turns off from the hub because the line of circumference gets larger.
Therefore it will be noted that by the saving of power on the inner part 10 it is possible to use a flat driving blade on the outer part 11, and this driving blade being fiat eX- pands the pitch radially outward, which, in the case of the above figured examples, averages 25% more pitch (which practically means push) than a true screw propeller,
on this outer portion of the blades where the water ofiers more resistance.
This gives my propeller the same advantage a long oar over ashort one, and in consequence of this gain in pitch a gain in speed is secured over a true screw propeller of equal pitch and diameter.
It is obvious that if pitch base line was lowered to one-half the diameter instead of two thirds the pitch would be 100% more at the top, or if base line was raised above the 2/3 diameter the pitch would decrease accordingly.
The space between the pitch line basis L and the line 0 drawn at the top of the inner part 10 is the slip portion of the driving blade or outer part 11. That is :the driving blade being flat the angle is the same throughout and this portion being below the pitch base line L will decrease in pitch, till if propeller is slipping, say, 20 per cent. The lowest part of the driving blade '11 will cease to push when it is 20 per cent of the distance below pitch base line L to the axis of the propeller.
The curved line 0 shown on. the blade illustrated in Figure 6 shows the portion between the inner portion 10 and the blade or outer part 11. The helical twist of the inner part starts from this line.
The inner part 10 from its top (that is from line 0) to the hub has helical twist on its back face, and its edges curving in opposite directions sideways (to strengthen same) and fore and aft, so that the front portion 12 of the inner part 10 is constructed at as muchslant aft as possible. This is the reason for giving the inner part 10 a helical twist; so that when the boat is mov ing ahead the water will strike against the front portion 12 opposing very little resistance, and whatever resistance there is is utilized to turn the propeller over, similar to a windmill, and thereby aid at pushing the boat ahead by transmitting power.
The front portion 15 011 the outer part 11 as well as the front portion 12 on the inner part 10 are rounded off tapering to a sharp cutting edge 1'7, which cuts through the water with less resistance than a blunt or wedge-shaped cutting edge.
Qn my improved blade,the circumference on the outer part being obviously longer than it is on the inner part, it is not necessary to set the blades at such a sharp angle as near the hub to secure the same number or more inches pitch ahead at each revolution. In this way a greater push is secured by my propeli'er, as the angle of pressure is less while the pitch averages more. The whole propeller blade is designed to eliminate all possible angle of pressure, and this is accomplished by the above described combination, which will -Force the boat or aircraft ahead at a greater speed.
As many changes could be made in the above construction and many apparently widely different embodiments of my inven tion within the scope of the claims constructed without departing from the spirit or scope thereof, it is intended that all matter contained in the accompanying specification and drawings shall be interpreted as illustrative and not in a limiting sense.
What I claim as my invention is:
A propeller blade comprising an inner and outer part, the inner part being set with a helical twist at 25 to 30 per cent less pitch than the outer part pitch basis, the driving side of the outer part being flat and at right angles to the axis of the hub of the propeller, thereby causing the pitch to expand as it nears the top of the blade, and the front face of the blade being convex and tapering of]? to a sharp cutting edge.
In witness whereof I have hereunto set my hand in the presence of two witnesses.
ROY C. MAKENNEY.
lVitnesses TRUEMAN E. Eisner, STEPHEN W. PALMER.
US264050A 1918-11-25 1918-11-25 Propeller Expired - Lifetime US1427307A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2758658A (en) * 1954-07-09 1956-08-14 Guy L Dakin Propeller blade shank
US3044557A (en) * 1959-01-08 1962-07-17 American Metal Prod Variable pitch fan blade
US3053325A (en) * 1961-10-25 1962-09-11 Paul F Ferreira Aeronautical propeller
US3066742A (en) * 1957-01-11 1962-12-04 Georgia Tech Res Inst Rotor blade

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2758658A (en) * 1954-07-09 1956-08-14 Guy L Dakin Propeller blade shank
US3066742A (en) * 1957-01-11 1962-12-04 Georgia Tech Res Inst Rotor blade
US3044557A (en) * 1959-01-08 1962-07-17 American Metal Prod Variable pitch fan blade
US3053325A (en) * 1961-10-25 1962-09-11 Paul F Ferreira Aeronautical propeller

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