GB1576818A - Scot jubilee jet propeller - Google Patents
Scot jubilee jet propeller Download PDFInfo
- Publication number
- GB1576818A GB1576818A GB5033976A GB5033976A GB1576818A GB 1576818 A GB1576818 A GB 1576818A GB 5033976 A GB5033976 A GB 5033976A GB 5033976 A GB5033976 A GB 5033976A GB 1576818 A GB1576818 A GB 1576818A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shroud
- hub
- propeller
- blades
- diameter
- 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
Links
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
- B63H1/16—Propellers having a shrouding ring attached to blades
Landscapes
- 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
(54) SCOT JUBILEE JET PROPELLER
(71) I, JAMES BOWMAN, "Hermione" 11 Milton Place, Pittenweem, Fife, British, do hereby declare the invention, for which I pray that a patent may be granted to me, and the method by which it is to be performed, to be particularly described in and by the following statement:- This invention relates to improvements in propellers mainly for marine purposes although the invention may be applied to aircraft, hovercraft or large volume, low pressure pumping of fluids and in the latter case high pressure can be obtained by having one propeller after another.
According to the present invention, a propeller has a frusto-conical shroud with conical inner and outer surfaces fixed to the blades of the propeller, a hub which in that region where the blades are attached increases in diameter in the direction in which the shroud decreases in diameter, and a boss attached to the hub which projects beyond the shroud at its low diameter end.
A ship makes considerable aeration immediately forward of the propeller which the cone by squeezing turns this soft water into more solid water. Further into the cone the blades and hub squeeze the water firmer still and thrust it aft. However in the region of the blades, a vacuum factor develops on conventional propellers which is overcome in the present invention by the increasing diameter of the hub together with the decreasing diameter of the shroud so that the vacuum area becomes a pressure area. The boss extending clear of the shroud may be constructed and streamlined as is most suitable. The boss in a large deep-drafted ship may be fitted with a non-return air pressure valve.
The invention is more particularly described with reference to the accompanying drawing of a sectional elevation through the propeller.
In the drawing a propeller with a hub 1 has blades 2 which are connected to a shroud 3 which is of frusto-conical shape with conical inner and outer surfaces. The hub 1 is extended outside of the shroud by a boss 4. It can be seen that the radius of the hub increases continuously in the region denoted by lines AA where the blades are connected to the hub by an amount "d" and in the direction in which the diameter of the shroud is decreasing. The maximum and minimum diameters of the shroud are 28 and 25 inches respectively. The length is 7 inches making an angle of 18 which is considered to give maximum efficiency.
The boss is hollow and defines with its walls and sealing plate 5 a chamber 6 wherein air can be pressurised by way of a nonreturn air pressure valve 7.
WHAT I CLAIM IS:
1. A propeller comprising a frustoconical shroud with conical inner and outer surfaces fixed to the blades of the propeller, a hub which in that region where the blades are attached increases in diameter in the direction in which the shroud decreases in diameter and a boss attached to the hub which projects beyond the shroud at its low diameter end.
**WARNING** end of DESC field may overlap start of CLMS **.
Claims (1)
- **WARNING** start of CLMS field may overlap end of DESC **.(54) SCOT JUBILEE JET PROPELLER (71) I, JAMES BOWMAN, "Hermione" 11 Milton Place, Pittenweem, Fife, British, do hereby declare the invention, for which I pray that a patent may be granted to me, and the method by which it is to be performed, to be particularly described in and by the following statement:- This invention relates to improvements in propellers mainly for marine purposes although the invention may be applied to aircraft, hovercraft or large volume, low pressure pumping of fluids and in the latter case high pressure can be obtained by having one propeller after another.According to the present invention, a propeller has a frusto-conical shroud with conical inner and outer surfaces fixed to the blades of the propeller, a hub which in that region where the blades are attached increases in diameter in the direction in which the shroud decreases in diameter, and a boss attached to the hub which projects beyond the shroud at its low diameter end.A ship makes considerable aeration immediately forward of the propeller which the cone by squeezing turns this soft water into more solid water. Further into the cone the blades and hub squeeze the water firmer still and thrust it aft. However in the region of the blades, a vacuum factor develops on conventional propellers which is overcome in the present invention by the increasing diameter of the hub together with the decreasing diameter of the shroud so that the vacuum area becomes a pressure area. The boss extending clear of the shroud may be constructed and streamlined as is most suitable. The boss in a large deep-drafted ship may be fitted with a non-return air pressure valve.The invention is more particularly described with reference to the accompanying drawing of a sectional elevation through the propeller.In the drawing a propeller with a hub 1 has blades 2 which are connected to a shroud 3 which is of frusto-conical shape with conical inner and outer surfaces. The hub 1 is extended outside of the shroud by a boss 4. It can be seen that the radius of the hub increases continuously in the region denoted by lines AA where the blades are connected to the hub by an amount "d" and in the direction in which the diameter of the shroud is decreasing. The maximum and minimum diameters of the shroud are 28 and 25 inches respectively. The length is 7 inches making an angle of 18 which is considered to give maximum efficiency.The boss is hollow and defines with its walls and sealing plate 5 a chamber 6 wherein air can be pressurised by way of a nonreturn air pressure valve 7.WHAT I CLAIM IS:1. A propeller comprising a frustoconical shroud with conical inner and outer surfaces fixed to the blades of the propeller, a hub which in that region where the blades are attached increases in diameter in the direction in which the shroud decreases in diameter and a boss attached to the hub which projects beyond the shroud at its low diameter end.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5033976A GB1576818A (en) | 1977-11-28 | 1977-11-28 | Scot jubilee jet propeller |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5033976A GB1576818A (en) | 1977-11-28 | 1977-11-28 | Scot jubilee jet propeller |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1576818A true GB1576818A (en) | 1980-10-15 |
Family
ID=10455548
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5033976A Expired GB1576818A (en) | 1977-11-28 | 1977-11-28 | Scot jubilee jet propeller |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1576818A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4413947A (en) * | 1980-10-24 | 1983-11-08 | Nissan Motor Company, Limited | Fan arrangement |
WO2004020278A1 (en) * | 2002-08-30 | 2004-03-11 | Romero Vazquez Juan Jose | Propeller, propeller propulsion system and vessel comprising propulsion system |
-
1977
- 1977-11-28 GB GB5033976A patent/GB1576818A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4413947A (en) * | 1980-10-24 | 1983-11-08 | Nissan Motor Company, Limited | Fan arrangement |
WO2004020278A1 (en) * | 2002-08-30 | 2004-03-11 | Romero Vazquez Juan Jose | Propeller, propeller propulsion system and vessel comprising propulsion system |
WO2004020280A1 (en) * | 2002-08-30 | 2004-03-11 | Romero Vazquez Juan Jose | Propeller, propeller propulsion system and vessel comprising propulsion system |
ES2249072A1 (en) * | 2002-08-30 | 2006-03-16 | Juan Jose Romero Vazquez | Propeller, propeller propulsion system and vessel comprising propulsion system |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |