US141871A - Improvement in screw-propellers - Google Patents
Improvement in screw-propellers Download PDFInfo
- Publication number
- US141871A US141871A US141871DA US141871A US 141871 A US141871 A US 141871A US 141871D A US141871D A US 141871DA US 141871 A US141871 A US 141871A
- Authority
- US
- United States
- Prior art keywords
- blades
- propellers
- improvement
- screw
- angles
- 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
- 230000000875 corresponding Effects 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 210000003746 Feathers Anatomy 0.000 description 2
- 241000272168 Laridae Species 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000005755 formation reaction Methods 0.000 description 2
Images
Classifications
-
- 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
- This invention relates to an improvement on that class of rotary stern propellers having angular blades feathered around a hub.
- My object is to increase the efficiency of such wheels by so constructing the outer edges or peripheries of the blades that the surfaces at these points will not allow the water to glance oft laterally from the blades, but will catch the outwardly-flarin g currents and direct them backward nearly in a line coinciding with the length of the vessel, as wil be hereinafter explained.
- a A represent the blades of the propeller, which are usually four in number, and which are secured into or cast with a hub, 0, at regular intervals around the same. These blades are feathered in the usual well-known manner, and may be of the usual well-known angular shape represented in the drawings. The circumferential edges of the blades are arcs of a circle-which is concentric to the axis of the wheel. Looking at the back face of the wheel,
- angular furrows B are seen, and on the front or opposite side of the wheel corresponding ridges are presented.
- the furrows present two angular surfaces, at b, the outer one, s a, of which will catch the currents of water which are impelled obliquely outwardly and change their direetionthat is to say, the surfaces a will direct the currents backward in the wake of the Vessel, or nearly at right angles to the .plane of the wheels.
- angles B have the same feather as the plain faces of the blades
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
UNITED- STATES DAVID EEEED, oE PHILADELPHIA, PENNSYLVANIA.
PATENT OFFICE.
IMPROVEMENT IN scREw-PRoPeLLERs.
Specification forming part of Letters Patent No. 141,871, dated August 19; 1873; application filed J une 11, 1873.
To all whom it may concern:
Be it known that I, DAVID FREED, of the city and county of Philadelphia and State of Pennsylvania, have invented a new and Improved Propeller; and I do hereby declare that the following is a full, clear, and exact description thereof, reference being had to the accompanying drawings, in which- Figure 1 is 'a face View of the propeller. Fig. 2 is an edge View of the same. Fig. 3 is a section through one of the blades.
Similar letters of reference indicate corresponding parts in the several figures.
This invention relates to an improvement on that class of rotary stern propellers having angular blades feathered around a hub. My object is to increase the efficiency of such wheels by so constructing the outer edges or peripheries of the blades that the surfaces at these points will not allow the water to glance oft laterally from the blades, but will catch the outwardly-flarin g currents and direct them backward nearly in a line coinciding with the length of the vessel, as wil be hereinafter explained. I
The following description of my invention will enable others skilled in the art to understand it.
In the accompanying drawings, A A represent the blades of the propeller, which are usually four in number, and which are secured into or cast with a hub, 0, at regular intervals around the same. These blades are feathered in the usual well-known manner, and may be of the usual well-known angular shape represented in the drawings. The circumferential edges of the blades are arcs of a circle-which is concentric to the axis of the wheel. Looking at the back face of the wheel,
angular furrows B are seen, and on the front or opposite side of the wheel corresponding ridges are presented. The furrows present two angular surfaces, at b, the outer one, s a, of which will catch the currents of water which are impelled obliquely outwardly and change their direetionthat is to say, the surfaces a will direct the currents backward in the wake of the Vessel, or nearly at right angles to the .plane of the wheels.
When the rotation of the wheel is reversed for backing the vessel the rear faces 11 of the angles B will operate to change the direction of the outwardly-fiarin g currents, as described for front faces a of the angles B.
It will be seen that the angles B have the same feather as the plain faces of the blades;
also, that the faces a b of the angles are concentric with the axis of the wheel.
I not only augment the propelling capacity of the blades by the formation of the angles B on them, but by means of such blades a vessel is kept more steady in its course.
Having described my invention, what I claim as new is-- The concavo-convex angular furrow circu- Witnesses:
J. N. CAMPBELL, EDM. F. BROWN.
Publications (1)
Publication Number | Publication Date |
---|---|
US141871A true US141871A (en) | 1873-08-19 |
Family
ID=2211284
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US141871D Expired - Lifetime US141871A (en) | Improvement in screw-propellers |
Country Status (1)
Country | Link |
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US (1) | US141871A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2965180A (en) * | 1954-12-20 | 1960-12-20 | American Radiator & Standard | Propeller fan wheel |
US20050281676A1 (en) * | 2004-06-16 | 2005-12-22 | Egolf Thomas A | Multi-hedral rotary wing |
-
0
- US US141871D patent/US141871A/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2965180A (en) * | 1954-12-20 | 1960-12-20 | American Radiator & Standard | Propeller fan wheel |
US20050281676A1 (en) * | 2004-06-16 | 2005-12-22 | Egolf Thomas A | Multi-hedral rotary wing |
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