US187633A - Improvement in screw-propellers - Google Patents
Improvement in screw-propellers Download PDFInfo
- Publication number
- 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
- Authority
- US
- United States
- Prior art keywords
- blades
- shaft
- propellers
- improvement
- screw
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000010276 construction Methods 0.000 description 6
- 230000000694 effects Effects 0.000 description 6
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 6
- 230000000875 corresponding Effects 0.000 description 4
- 239000012530 fluid Substances 0.000 description 4
- 230000037250 Clearance Effects 0.000 description 2
- 210000003414 Extremities Anatomy 0.000 description 2
- 230000001154 acute Effects 0.000 description 2
- 230000035512 clearance Effects 0.000 description 2
- 230000001808 coupling Effects 0.000 description 2
- 238000010168 coupling process Methods 0.000 description 2
- 238000005859 coupling reaction Methods 0.000 description 2
- JVTAAEKCZFNVCJ-UHFFFAOYSA-N lactic acid Chemical compound CC(O)C(O)=O JVTAAEKCZFNVCJ-UHFFFAOYSA-N 0.000 description 2
- 239000000463 material Substances 0.000 description 2
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S416/00—Fluid reaction surfaces, i.e. impellers
- Y10S416/03—Sheet 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.
Landscapes
- 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.
Publications (1)
Publication Number | Publication Date |
---|---|
US187633A true US187633A (en) | 1877-02-20 |
Family
ID=2257040
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US187633D Expired - Lifetime US187633A (en) | Improvement in screw-propellers |
Country Status (1)
Country | Link |
---|---|
US (1) | US187633A (en) |
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0
- US US187633D patent/US187633A/en not_active Expired - Lifetime
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