US183373A - Improvement in sgrew-propellers - Google Patents
Improvement in sgrew-propellers Download PDFInfo
- Publication number
- US183373A US183373A US183373DA US183373A US 183373 A US183373 A US 183373A US 183373D A US183373D A US 183373DA US 183373 A US183373 A US 183373A
- Authority
- US
- United States
- Prior art keywords
- blades
- blade
- edge
- propellers
- sgrew
- 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
- 239000011295 pitch Substances 0.000 description 7
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 7
- 238000010276 construction Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
Images
Classifications
-
- 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
-
- 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
- B64C11/46—Arrangements of, or constructional features peculiar to, multiple propellers
- B64C11/48—Units of two or more coaxial propellers
Definitions
- This invention consists in a screw-propeller the blades whereof are formed with concave faces and correspondingly convex backs, corrugated, crimped, fluted, or not, as desired, to-
- Figure 1 is a perspective view.
- Fig. 2 is a front view;
- Fig. 3 a rear view.
- Figs. 4, 5, and 6 are central longitudinal sections of the several forms of the blades.
- a B indicate blades of a screw-propeller having in common a concave face, correspondingly-convex back, and reversely-curved'ends or tips, and securedto the hub D in the same plane and at the same pitch or angle, or alternately in different planes and pitches or angles, for a purpose hereinafter referred/r0.
- blade A its edge from a to bis straight and thickened to afford better and greater resistance in backing. Its edge from a to a is somewhat parabolic and sharp, so as to afford the least resistance in entering the water. Its face 0 is concave, but extending to the edge a b on a level.
- Its back 01 is of a convexity corresponding to the concavity of the face, and its outer end or tip 0 is curved reversely to the face and back curves from the points 1 to 2, or front to, or nearly to, rear edges, so as to gather the water and throw it outwardly from the stern on opposite sides of a longitudinal line parallel with the wheel or propeller shaft, whereby the vessel is made to reversely or diagonally across the blades, as is best suited for the vessel to which they are to be applied relatively to its destined speed.
- the concavity and convexity are not uniform or regular throughout the blades.
- the edges a b and a a" are in the same plane, and the edge a b is in the same plane with thecenter of the concavity, while edge a a is in a higher plane.
- the back is convex both longitudinally and transversely, and this construction will be found best adapted for advantageous action in entering and leaving the water.
- edge a b is curved but slightly, its center being beyond the blade, and its edge a a is elliptical, or nearly so, both'edges being sharpened.
- Its concavity c has its surrounding edges or limits convexly formed, so as to most readily shed the water.
- Its back d is perfectly convex, except at its end or tip 0, which is reversely curved from points 1 to 2, or from front to, or nearly to, rear edges.
- a blade of the shape of blade A should be set on the hub at a less pitch or greater angle than such a one as B, in order to obtain the best results in motiona necessity arising from the shape of such blades.
- the blade 0 In the blade 0 is shown a feature-namely, the corrugations, flutes, or furrows fwhich may be employed in either of the other blades.
- corrugations constitutes a concavity in which the water is gathered, and is deepest at its end g, where the most power is to be gained, and gradually decreases rearwardly to such extent that that edge of the blade is almost straight, whereby the water is readily shed.
- a blade thus grooved, fluted, or-otherwise furrowed will present the entire tip or outer end from front to rear in a shape corresponding to that marked 6 in the other blades, and thus obtain the advantages inherent therein.
- the blades should be alternately set on the hub in difl'erent planes. If three blades be used, two should be set at the same'angleor pitch forward, and the other rearward and atan increased pitch or less angle. The varying resistance thus aiforded gives the result.
- a propeller-blade having one edge straight, or nearly so, and the other parabolic or elliptical, a concave face, convex back, and a reversely-curved tip or edge, substantially as and for the purpose specified.
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Earth Drilling (AREA)
Description
UNITED STATES omen HARRY A. OROSSLEY Awesome-w. FRENCH, or cnEvEnAivD, onto.
IMP'RQVEMEN'T m"s'eREwm'nomLms;,
I Specification formingpart of Letters Patent Biol 183,373, dated October 17 1876, application filed Septemberfll, 1876.
To allwhom itmay concerm, v.
Be it known that we, HARRY A. H RossLEY and GEORGE W. FRENCH, of Cleveland, in the county of Ouyahoga and State of Ohio, have invented certain new and useful Improvements in Screw-Propellers, of which the following is a full, clear, and exact descrip tion.
This invention consists in a screw-propeller the blades whereof are formed with concave faces and correspondingly convex backs, corrugated, crimped, fluted, or not, as desired, to-
augment the resisting surface, having their outer ends reversely curved, and set on the hub inthe same or different planes, and at the same or different angles or pitch, whereby the resistance is so increased that as the vessel progresses its motion is accelerated without increasing the proportionate number of revolutions of the wheels, and whereby, when the vessel is to be backed, the blades act to throw the water outwardly from the sides, instead of against the stern, of the vessel, substantially as hereinafter specified.-
In the drawings illustrating this invention, Figure 1 is a perspective view. Fig. 2 is a front view; Fig. 3, a rear view. Figs. 4, 5, and 6 are central longitudinal sections of the several forms of the blades.
A B indicate blades of a screw-propeller having in common a concave face, correspondingly-convex back, and reversely-curved'ends or tips, and securedto the hub D in the same plane and at the same pitch or angle, or alternately in different planes and pitches or angles, for a purpose hereinafter referred/r0. In blade A its edge from a to bis straight and thickened to afford better and greater resistance in backing. Its edge from a to a is somewhat parabolic and sharp, so as to afford the least resistance in entering the water. Its face 0 is concave, but extending to the edge a b on a level. Its back 01 is of a convexity corresponding to the concavity of the face, and its outer end or tip 0 is curved reversely to the face and back curves from the points 1 to 2, or front to, or nearly to, rear edges, so as to gather the water and throw it outwardly from the stern on opposite sides of a longitudinal line parallel with the wheel or propeller shaft, whereby the vessel is made to reversely or diagonally across the blades, as is best suited for the vessel to which they are to be applied relatively to its destined speed.
It will be noticed that the concavity and convexity are not uniform or regular throughout the blades. For illustration, the edges a b and a a" are in the same plane, and the edge a b is in the same plane with thecenter of the concavity, while edge a a is in a higher plane. The back is convex both longitudinally and transversely, and this construction will be found best adapted for advantageous action in entering and leaving the water.
In the blade B the edge a b is curved but slightly, its center being beyond the blade, and its edge a a is elliptical, or nearly so, both'edges being sharpened. Its concavity c has its surrounding edges or limits convexly formed, so as to most readily shed the water. Its back d is perfectly convex, except at its end or tip 0, which is reversely curved from points 1 to 2, or from front to, or nearly to, rear edges. A blade of the shape of blade A should be set on the hub at a less pitch or greater angle than such a one as B, in order to obtain the best results in motiona necessity arising from the shape of such blades.
In the blade 0 is shown a feature-namely, the corrugations, flutes, or furrows fwhich may be employed in either of the other blades.
They are shown ina blade of ordinary form,
in order to illustrate the manner in which better results may be obtained in forward or backward motion with such blades. corrugations constitutes a concavity in which the water is gathered, and is deepest at its end g, where the most power is to be gained, and gradually decreases rearwardly to such extent that that edge of the blade is almost straight, whereby the water is readily shed. A blade thus grooved, fluted, or-otherwise furrowed will present the entire tip or outer end from front to rear in a shape corresponding to that marked 6 in the other blades, and thus obtain the advantages inherent therein.
Each of such After a vessel has got under way, could the pitch or angle of the blade be changed, greater speed might be obtained without increasing the number of revolutions of the propeller. In a measure to accomplish this the blades should be alternately set on the hub in difl'erent planes. If three blades be used, two should be set at the same'angleor pitch forward, and the other rearward and atan increased pitch or less angle. The varying resistance thus aiforded gives the result.
What we claim is-- 1. A propeller-blade having one edge straight, or nearly so, and the other parabolic or elliptical, a concave face, convex back, and a reversely-curved tip or edge, substantially as and for the purpose specified.
2. The blades of a screw-propeller, having 4. A propeller-blade having corrugations,
flutes, or grooves, decreasing gradually in depth rearwardly, and its tip or edge curved backwardly, substantially as shown and described. HARRY A. GROSSLEY. GEORGE W. FRENCH. Witnesses:
J OHN '1. DRAM, EDMOND F. ATIIERTON.
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US183373A true US183373A (en) | 1876-10-17 |
Family
ID=2252778
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US183373D Expired - Lifetime US183373A (en) | Improvement in sgrew-propellers |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US183373A (en) |
-
0
- US US183373D patent/US183373A/en not_active Expired - Lifetime
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