US559890A - Screw-propeller - Google Patents
Screw-propeller Download PDFInfo
- Publication number
- US559890A US559890A US559890DA US559890A US 559890 A US559890 A US 559890A US 559890D A US559890D A US 559890DA US 559890 A US559890 A US 559890A
- Authority
- US
- United States
- Prior art keywords
- blades
- screw
- sleeve
- propeller
- shaft
- 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
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 12
- 210000001699 lower leg Anatomy 0.000 description 4
- 239000000835 fiber Substances 0.000 description 2
- 230000002441 reversible Effects 0.000 description 2
Images
Classifications
-
- 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
- B64C11/30—Blade pitch-changing mechanisms
- B64C11/32—Blade pitch-changing mechanisms mechanical
- B64C11/36—Blade pitch-changing mechanisms mechanical non-automatic
Definitions
- My invention relates to improvements in screw-propellers, and more particularly to that class of propellers having reversible blades, whereby the action of the same is reversed without reversing the driving mechanism, and its object is to provide the same with certain new and useful features hereinafter more fully described, and particularly pointed out in the claims, reference being had to the accompanying drawings, in which- Figure 1 is a section on the line 1 1 of Fig. 2 of a device embodying my invention; Fig. 2, a section of the same on the line 2 20f Fig. 1; Fig. 3, a section on the line 3 3 of Fig. 2, and Fig. 4: a side elevation.
- A is a drivin -shaft, adapted to be moved longitudinally from inside the boat in any suitable manner and having the reduced portions A A" near its end, one of said reducti ens, A, having flattened sides A'.
- Secured to said shanks by means of splines D are sectors D, which sectors engage with racks formed by cutting away portions of the sides of the sleeve F and forming teeth on the lower edges of the openings thus made through said sleeve.
- Said sleeve F engages the reduced portion A of said shaft, which has the flattened sides A and has an inner surface to conform to that of the shaft, thus preventing said sleeve from turning bn said shaft, but allowing a free longitudinal movement of said shaft, said sleeve being prevented from moving longitudinally by a flange F on its inner end, which engages a casing II, said casing being adapted to receive a screw-threaded follower G, which is attached, by means of bolts, to the boat, and interposed between said flange and casing and flange and follower are rings of fiber I to prevent friction and wearing.
- a sleeve J on said shaft engages a screw-threaded opening in said follower, and, extending through the boat, has a stuffing-box K on its inner end to prevent the water from entering the boat.
- the blades 0 are so constructed that theline of each axis does not pass through the centerof the blade, but is farthest from the lead side, thus making an unbalanced blade.
- the shaft A is moved inward, carrying with it the hol low hub B and blades O, and as said blades are connected with said sleeve by means of the racks and sectors said blades will be retated to the position shown in dotted lines in Figs. 1 and a as said hub B slides over said sleeve, moving said sectors along said racks until the end of said sleeve comes in contact with the end of the cavity in said hub.
- said shaft is moved outward until the shoulder formed by the reduction A strikes the inner end of the sleeve F, determining the throw of the blades.
- said propeller is revolved in the direction indicated by the arrows in Fig. 3, with said blades in their maximum positions for forward motion, there being a greater amount of surface to be contacted by the water on the lead side of the axial line of said blades, the force of said water will tend to throw said blades farther in that direction, and thus the same are held in said maximum position, and when said blades are reversed and said sides pass said axial lines the action of the water throws said blades into their maximum positions in the other direction and holds them there the same as before.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Hydraulic Turbines (AREA)
Description
(No Model.) v G. H. GERE. SCREW PROPELLER.
No. 559,890. Patented May 12, 1896.
' h m ll 11 il l MIIIIIIIIIIA whim eases CQQYCYZ e en @513 a iko'wvma 7 Am WW ANDREW I GHAMMA PKDTD-UMQWASHINGIQNJC UNITED STATES PATENT EEicE.
GEORGE H. GERE, OF GRAND RAPIDS, MICHIGAN.
SCREW-PROPELLER.
SPECIFICATION forming part of Letters Patent No. 559,890, dated May 12, 1896.
Application filed September 18, 1895. Serial No. 562,834. (No model.)
zen of the United States, residing at Grand Rapids, in the county of Kent and State of Michigan, have invented certain new and useful Improvements in Screw-Propellers; and 1 do hereby declare the following to be a full, clear, and exact description of the invent-ion, such as will enable others skilled in the art to which it appertains to make and use the same.
My invention relates to improvements in screw-propellers, and more particularly to that class of propellers having reversible blades, whereby the action of the same is reversed without reversing the driving mechanism, and its object is to provide the same with certain new and useful features hereinafter more fully described, and particularly pointed out in the claims, reference being had to the accompanying drawings, in which- Figure 1 is a section on the line 1 1 of Fig. 2 of a device embodying my invention; Fig. 2, a section of the same on the line 2 20f Fig. 1; Fig. 3, a section on the line 3 3 of Fig. 2, and Fig. 4: a side elevation.
Like letters refer to like parts in all of the figures.
A is a drivin -shaft, adapted to be moved longitudinally from inside the boat in any suitable manner and having the reduced portions A A" near its end, one of said reducti ens, A, having flattened sides A'. Firmly secured on said reduced portion A, by means of a nut in the end of said shaft, is the hollow hub B, on which are journaled, in bearings B, the blades 0, which blades are provided with shanks 0, held in said bearings 13 by means of nuts and washers. Secured to said shanks by means of splines D are sectors D, which sectors engage with racks formed by cutting away portions of the sides of the sleeve F and forming teeth on the lower edges of the openings thus made through said sleeve. Said sleeve F engages the reduced portion A of said shaft, which has the flattened sides A and has an inner surface to conform to that of the shaft, thus preventing said sleeve from turning bn said shaft, but allowing a free longitudinal movement of said shaft, said sleeve being prevented from moving longitudinally by a flange F on its inner end, which engages a casing II, said casing being adapted to receive a screw-threaded follower G, which is attached, by means of bolts, to the boat, and interposed between said flange and casing and flange and follower are rings of fiber I to prevent friction and wearing. A sleeve J on said shaft engages a screw-threaded opening in said follower, and, extending through the boat, has a stuffing-box K on its inner end to prevent the water from entering the boat. The blades 0 are so constructed that theline of each axis does not pass through the centerof the blade, but is farthest from the lead side, thus making an unbalanced blade.
To reverse the motion of the boat, the shaft A is moved inward, carrying with it the hol low hub B and blades O, and as said blades are connected with said sleeve by means of the racks and sectors said blades will be retated to the position shown in dotted lines in Figs. 1 and a as said hub B slides over said sleeve, moving said sectors along said racks until the end of said sleeve comes in contact with the end of the cavity in said hub. To again give the boat a forward motion, said shaft is moved outward until the shoulder formed by the reduction A strikes the inner end of the sleeve F, determining the throw of the blades.
lVhen said propeller is revolved in the direction indicated by the arrows in Fig. 3, with said blades in their maximum positions for forward motion, there being a greater amount of surface to be contacted by the water on the lead side of the axial line of said blades, the force of said water will tend to throw said blades farther in that direction, and thus the same are held in said maximum position, and when said blades are reversed and said sides pass said axial lines the action of the water throws said blades into their maximum positions in the other direction and holds them there the same as before. I thus secure a screw propeller having reversing blades, which blades are thrown to their maximum pitch or position by the action of the water after passing the center of throw, the water then tending to hold the blades when the wheel is rotated at the maximum pitch or position.
It will be observed that by employing a
Publications (1)
Publication Number | Publication Date |
---|---|
US559890A true US559890A (en) | 1896-05-12 |
Family
ID=2628614
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US559890D Expired - Lifetime US559890A (en) | Screw-propeller |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20080230652A1 (en) * | 2004-04-06 | 2008-09-25 | Biornstad Robert D | Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections |
US20100083504A1 (en) * | 2004-04-06 | 2010-04-08 | The Boeing Company | Methods of manufacturing structural panels |
-
0
- US US559890D patent/US559890A/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20080230652A1 (en) * | 2004-04-06 | 2008-09-25 | Biornstad Robert D | Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections |
US20100083504A1 (en) * | 2004-04-06 | 2010-04-08 | The Boeing Company | Methods of manufacturing structural panels |
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