US1341653A - Fan, propeller, &c. - Google Patents
Fan, propeller, &c. Download PDFInfo
- Publication number
- US1341653A US1341653A US115165A US11516516A US1341653A US 1341653 A US1341653 A US 1341653A US 115165 A US115165 A US 115165A US 11516516 A US11516516 A US 11516516A US 1341653 A US1341653 A US 1341653A
- Authority
- US
- United States
- Prior art keywords
- blades
- propeller
- hub portion
- water
- conoidal
- 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
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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
- B63H1/14—Propellers
- B63H1/26—Blades
-
- 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
- B63H1/14—Propellers
- B63H1/16—Propellers having a shrouding ring attached to blades
-
- 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
- B63H1/14—Propellers
- B63H1/20—Hubs; Blade connections
-
- 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
- B63H1/14—Propellers
- B63H2001/145—Propellers comprising blades of two or more different types, e.g. different lengths
Definitions
- the present invention relates to screw propellers, meaning thereby such helix-carrying devices as are used to propel submarine and other vessels, or to circulate air for ventilating purposes and the like; andv its object is, generally, to provide an improved device of that character; and, more particularly, a more economically constructed device of that character; and further, such a device whereby the propeller.
- such a device having bracing rods which shall minimize the water displacement and water friction thereon; and further, such a device which shall have a plurality of sets of blades, one set being disposed farther from the axis of the propellers rotation than another set; and further, such a devicewherein the water acted on by the propeller shall be deflected in such a way as to offer less resistance to the passage of the vessel through the water, than heretofore.
- Fig. 2 is a side view thereof
- Fig. 3' is an end view of a modified con struction
- Fig. 4 is a side View of the same.
- Fig. 5 is a side view of the bow portion of. a submarine vessel furnished with such screw propeller.
- the screw propeller 1 has a central or hub pdrtion 2 ooaxial with and rotated by the Shaft a.
- This hub portion is conoidal in formas shown, with an apex 4:.
- Helically disposed propeller blades 5 are carried by the hub portion, and may be formed by press-diem the same from a suitable sheet metal blan so blades.
- rods 8 extend between the hub portion and the parts of the blades remote from the hub portion, thus to secure the blades from deflection by the water, etc.
- rods In order to minimize the water displacement by these .rods and the water friction thereon, such rods have their greatest cross-sectional extension in the direction the water acted on by the propeller passes thereby or therethrough; the'rods cross-sectional extension at right angles to the Waters direction of movement being the least. This is particularly shown in the cross-section of one.
- This member.9 is spaced from, and is parallelly disposed relatively to, the surface of the hub portion.
- Braces 8' extend from the surface of the hub portion to points on said member 9 midway between the vanes 11. Said member thus acts as a brace for the Furthermore, inasmuch as the water passing back between the hub portion and this member 9 is held by said member against the same degree of centrifugal or radial motion the rotation of the blades would otherwise give to it, it is manifest that the thrust of the propeller on the water is more nearly in the direction opposite toy that of the vessels motion, which is a very desirable end.
- the conoidal hub portion effects a further advantage especially when the propelleris applied to the bow of a vessel, as the submarine vessel 10 shown in Fig. 5. It will be seen that the conoidal hub portion deflects the water laterally' from the vessels sides, whereby the friction of the water thereon is lessened; and in fact a slight air space near the vessels stein, between vessel and water, may be created, the tendency of which is to draw the vessel forward; the annular member 9 all the while directing the water rearwardly and preventing it from too great a diver gence' under the action of the conoidal hub portion and the centrifugal motion imparted by the blades themselves.
- the propeller blades 5 are mounted upon the outer surface of the conoidal hub member, and it is preferable that the blades, or at least the major parts of the blades, be within the limits of the axially projected area of the base of said hub member.
- the surface of the conoidal hub member is also preferably disposed at an angle of degrees with respect to the axis of said member so that the fluid upon which the propeller is acting is deflected from its course at an angle of approximately 45 degrees.
- I claim A In a screw propeller, a conoidal hub portion, propeller blades carried by the hub portion, and a continuous annular member of unitary character spaced from and parallelly disposed relatively to the surface of the hub portion, and connecting the blades at medial points remote from the hub por tion, whereby substantially two sets of blades are formed, one set within said member and another set outside it.
- a device of the character described comprising a rotary hub of conoidal shape, a plurality of blades disposed spirally there on, the outer and inner edges of said blades being substantially parallel, an annular band of conoidal shape mounted on the outer edge of said blades, and a plurality of 1 posed substantially to describe a common cylindricalsurface when the device rotates.
- a device of the character described comprising a plurality of spaced concentrically arranged conoidal members of like angularity with respect to their common axis, in combination with a plurality of sets of vanes arranged peripherally of said members respectively and standing outward thereon, and adjacent members beingheld in rigid relation to each other by the corresponding intermediately positioned vanes.
- a device of "the character described comprising a pair of concentric conoidal members suitably spaced apart, a plurality of spirally disposel vanes arranged peripherally between said members in spaced mutual relation, and braces arranged alternately with respect to said vanes for rigidly securing said members with respect to each other.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
C. M. LEE.
FAN, PROPELLER, &c. APPLICATION FILED AUG-16,1916.
1,341,653 r Patented June 1, 1920,
3 SHEETSSHEET 1- WITNESSES: g! glVE/VTOR. 73 7 1 D By I A TTORNE YS.
c. M. LEE.
Patented June 1, 1920.
3 SHEETS$HEET 2'- ma sa.
C. M. LEE.
FAN, PROPELLER, &c. APPLICATION FILED AUG-16,1916.
Patented June 1,1920.
3 SHEETS-SHEET 3- CHARLES M. LEE, 0F FALLS CITY, NEBRASKA.
ran, raornntnn, 8w.
menses.
Specification of Letters Patent.
Patented June 1, 1920.
Application filed August 16, 1916. Serial No. 115,165.
To all whom it may concern:
Be it known that I, CHARLES M. LEE, a citizen of the United States of America, and a resident of Falls City, county of Richardson, and State of Nebraska, have invented certain new and useful Improvements in Fans, Propellers, &c., of which the following is a specification.
The present invention relates to screw propellers, meaning thereby such helix-carrying devices as are used to propel submarine and other vessels, or to circulate air for ventilating purposes and the like; andv its object is, generally, to provide an improved device of that character; and, more particularly, a more economically constructed device of that character; and further, such a device whereby the propeller.
' blades shall be firmly braced; and further,
such a device having bracing rods which shall minimize the water displacement and water friction thereon; and further, such a device which shall have a plurality of sets of blades, one set being disposed farther from the axis of the propellers rotation than another set; and further, such a devicewherein the water acted on by the propeller shall be deflected in such a way as to offer less resistance to the passage of the vessel through the water, than heretofore.
These and any other objects appearinghereinafter are attained by, and the invention finds preferable embodiment in, the structure hereinafter described and illustrated by the accompanying drawings, in
' which- Figure 1 is an end view of a screw propeller;
Fig. 2 is a side view thereof;
Fig. 3'is an end view of a modified con struction;
' Fig. 4 is a side View of the same; and
Fig. 5 is a side view of the bow portion of. a submarine vessel furnished with such screw propeller.
In the embodiment of themvention chosen for illustration by the drawings and for detailed description herein, the screw propeller 1 has a central or hub pdrtion 2 ooaxial with and rotated by the Shaft a. This hub portion is conoidal in formas shown, with an apex 4:. Helically disposed propeller blades 5 are carried by the hub portion, and may be formed by press-diem the same from a suitable sheet metal blan so blades.
of the rods as seen in Fig. 2.
In .the modification shown in Figs. 3 and 4, there is provided a thin annular member 9, as of sheet metal, connecting the blades at points remote from the hub portion. This member.9 is spaced from, and is parallelly disposed relatively to, the surface of the hub portion. Braces 8' extend from the surface of the hub portion to points on said member 9 midway between the vanes 11. Said member thus acts as a brace for the Furthermore, inasmuch as the water passing back between the hub portion and this member 9 is held by said member against the same degree of centrifugal or radial motion the rotation of the blades would otherwise give to it, it is manifest that the thrust of the propeller on the water is more nearly in the direction opposite toy that of the vessels motion, which is a very desirable end.
The conoidal hub portion, assisted by the combination therewith of the annular member 9, effects a further advantage especially when the propelleris applied to the bow of a vessel, as the submarine vessel 10 shown in Fig. 5. It will be seen that the conoidal hub portion deflects the water laterally' from the vessels sides, whereby the friction of the water thereon is lessened; and in fact a slight air space near the vessels stein, between vessel and water, may be created, the tendency of which is to draw the vessel forward; the annular member 9 all the while directing the water rearwardly and preventing it from too great a diver gence' under the action of the conoidal hub portion and the centrifugal motion imparted by the blades themselves.
It will be seen that by connecting the annular member 9 to the blades at their middle portions, or by securing member 9 between inner blades 11 and outer blades 12 (which is essentially the same), two sets of blades are provided, one set being farther from the propellers axis than the other set.
The propeller blades 5 are mounted upon the outer surface of the conoidal hub member, and it is preferable that the blades, or at least the major parts of the blades, be within the limits of the axially projected area of the base of said hub member. The surface of the conoidal hub member is also preferably disposed at an angle of degrees with respect to the axis of said member so that the fluid upon which the propeller is acting is deflected from its course at an angle of approximately 45 degrees.
The invention being intended to be defined solely by the claims, is not to be limited to or by details of construction shown or described.
I claim A 1. In a screw propeller, a conoidal hub portion, propeller blades carried by the hub portion, and a continuous annular member of unitary character spaced from and parallelly disposed relatively to the surface of the hub portion, and connecting the blades at medial points remote from the hub por tion, whereby substantially two sets of blades are formed, one set within said member and another set outside it.
2. A device of the character described, comprising a rotary hub of conoidal shape, a plurality of blades disposed spirally there on, the outer and inner edges of said blades being substantially parallel, an annular band of conoidal shape mounted on the outer edge of said blades, and a plurality of 1 posed substantially to describe a common cylindricalsurface when the device rotates.
4. A device of the character described, comprising a plurality of spaced concentrically arranged conoidal members of like angularity with respect to their common axis, in combination with a plurality of sets of vanes arranged peripherally of said members respectively and standing outward thereon, and adjacent members beingheld in rigid relation to each other by the corresponding intermediately positioned vanes.
5. A device of "the character described, comprising a pair of concentric conoidal members suitably spaced apart, a plurality of spirally disposel vanes arranged peripherally between said members in spaced mutual relation, and braces arranged alternately with respect to said vanes for rigidly securing said members with respect to each other.
Signed at Falls City this 11th day of August 1916.
CHARLES M. LEE.
Witnesses C. 'F. PHILLIPS, F. A. HEBENsTREET.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US115165A US1341653A (en) | 1916-08-16 | 1916-08-16 | Fan, propeller, &c. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US115165A US1341653A (en) | 1916-08-16 | 1916-08-16 | Fan, propeller, &c. |
Publications (1)
Publication Number | Publication Date |
---|---|
US1341653A true US1341653A (en) | 1920-06-01 |
Family
ID=22359666
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US115165A Expired - Lifetime US1341653A (en) | 1916-08-16 | 1916-08-16 | Fan, propeller, &c. |
Country Status (1)
Country | Link |
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US (1) | US1341653A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2649921A (en) * | 1949-05-10 | 1953-08-25 | Guy S Faber | Propeller for fluid |
US2913055A (en) * | 1950-09-01 | 1959-11-17 | Thomas E Quick | Propulsion device |
US3228475A (en) * | 1961-11-30 | 1966-01-11 | Worthmann Wilhelm | Windmill |
US4057915A (en) * | 1974-03-30 | 1977-11-15 | Firma Ing. Alfred Schmidt Gmbh | Ring structure for preventing blade damage |
US4060337A (en) * | 1976-10-01 | 1977-11-29 | General Motors Corporation | Centrifugal compressor with a splitter shroud in flow path |
US20060213074A1 (en) * | 2005-03-25 | 2006-09-28 | Matsushita Electric Works, Ltd. | Hair dryer |
US20070036642A1 (en) * | 2005-08-10 | 2007-02-15 | The Boeing Company | Bridged inducer |
US11053950B2 (en) * | 2018-03-14 | 2021-07-06 | Carrier Corporation | Centrifugal compressor open impeller |
-
1916
- 1916-08-16 US US115165A patent/US1341653A/en not_active Expired - Lifetime
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2649921A (en) * | 1949-05-10 | 1953-08-25 | Guy S Faber | Propeller for fluid |
US2913055A (en) * | 1950-09-01 | 1959-11-17 | Thomas E Quick | Propulsion device |
US3228475A (en) * | 1961-11-30 | 1966-01-11 | Worthmann Wilhelm | Windmill |
US4057915A (en) * | 1974-03-30 | 1977-11-15 | Firma Ing. Alfred Schmidt Gmbh | Ring structure for preventing blade damage |
US4060337A (en) * | 1976-10-01 | 1977-11-29 | General Motors Corporation | Centrifugal compressor with a splitter shroud in flow path |
US20060213074A1 (en) * | 2005-03-25 | 2006-09-28 | Matsushita Electric Works, Ltd. | Hair dryer |
US20070036642A1 (en) * | 2005-08-10 | 2007-02-15 | The Boeing Company | Bridged inducer |
US11053950B2 (en) * | 2018-03-14 | 2021-07-06 | Carrier Corporation | Centrifugal compressor open impeller |
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