GB417232A - Improvements in and relating to the construction of air propellers and blades therefor - Google Patents
Improvements in and relating to the construction of air propellers and blades thereforInfo
- Publication number
- GB417232A GB417232A GB978334A GB978334A GB417232A GB 417232 A GB417232 A GB 417232A GB 978334 A GB978334 A GB 978334A GB 978334 A GB978334 A GB 978334A GB 417232 A GB417232 A GB 417232A
- Authority
- GB
- United Kingdom
- Prior art keywords
- relating
- construction
- impeller
- blades
- air propellers
- 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
-
- 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
- F04D29/388—Blades characterised by construction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
417,232. Screw fans. MATHER, C., 353, The Cliff, Higher Broughton, Salford, Lancashire. March 29, 1934, No. 9783. [Class 110 (i).] A hollow bladed impeller is strengthened by rods 10 held between the plates 5 forming the blades. The rods 10 are contained within slots 9 in the plate and ribs 7 in the members 5. A flange 6 may be cut away to provide an impeller of any required size. Additional strength is afforded by a plate 8 and the hub of the impeller is composed of the superposed plates 5 and 8.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB978334A GB417232A (en) | 1934-03-29 | 1934-03-29 | Improvements in and relating to the construction of air propellers and blades therefor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB978334A GB417232A (en) | 1934-03-29 | 1934-03-29 | Improvements in and relating to the construction of air propellers and blades therefor |
Publications (1)
Publication Number | Publication Date |
---|---|
GB417232A true GB417232A (en) | 1934-10-01 |
Family
ID=9878666
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB978334A Expired GB417232A (en) | 1934-03-29 | 1934-03-29 | Improvements in and relating to the construction of air propellers and blades therefor |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB417232A (en) |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2440127A (en) * | 1944-07-31 | 1948-04-20 | Curtiss Wright Corp | Art of producing propeller blades |
US2514525A (en) * | 1944-03-09 | 1950-07-11 | Curtiss Wright Corp | Method of producing blade constructions and propeller blades |
US2535917A (en) * | 1945-08-04 | 1950-12-26 | Smith Corp A O | Propeller blade with a tubular backbone |
US2647586A (en) * | 1945-07-30 | 1953-08-04 | Smith Corp A O | Wide hollow steel propeller blade and method of making the same |
US2823889A (en) * | 1950-04-05 | 1958-02-18 | Stalker Dev Company | Rotor construction and fabrication |
US2887957A (en) * | 1953-05-29 | 1959-05-26 | Stalker Corp | Bladed axial flow pump construction |
US3947939A (en) * | 1974-07-18 | 1976-04-06 | Foster Wheeler Energy Corporation | Method for the manufacture of turbulators |
US4053260A (en) * | 1975-02-18 | 1977-10-11 | Wallace Murray Corporation | Double spider stiffening assembly for fan blades |
US4172691A (en) * | 1975-10-21 | 1979-10-30 | Wallace Murray Corporation | Sheet metal fan assembly |
US4174924A (en) * | 1975-10-21 | 1979-11-20 | Wallace Murray Corporation | Sheet metal fan assembly |
GB2289089A (en) * | 1994-04-28 | 1995-11-08 | Tygar Co Ltd | Fan blade |
GB2296743A (en) * | 1995-01-06 | 1996-07-10 | Huang Yung Chung | Fan |
-
1934
- 1934-03-29 GB GB978334A patent/GB417232A/en not_active Expired
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2514525A (en) * | 1944-03-09 | 1950-07-11 | Curtiss Wright Corp | Method of producing blade constructions and propeller blades |
US2440127A (en) * | 1944-07-31 | 1948-04-20 | Curtiss Wright Corp | Art of producing propeller blades |
US2647586A (en) * | 1945-07-30 | 1953-08-04 | Smith Corp A O | Wide hollow steel propeller blade and method of making the same |
US2535917A (en) * | 1945-08-04 | 1950-12-26 | Smith Corp A O | Propeller blade with a tubular backbone |
US2823889A (en) * | 1950-04-05 | 1958-02-18 | Stalker Dev Company | Rotor construction and fabrication |
US2887957A (en) * | 1953-05-29 | 1959-05-26 | Stalker Corp | Bladed axial flow pump construction |
US3947939A (en) * | 1974-07-18 | 1976-04-06 | Foster Wheeler Energy Corporation | Method for the manufacture of turbulators |
US4053260A (en) * | 1975-02-18 | 1977-10-11 | Wallace Murray Corporation | Double spider stiffening assembly for fan blades |
US4172691A (en) * | 1975-10-21 | 1979-10-30 | Wallace Murray Corporation | Sheet metal fan assembly |
US4174924A (en) * | 1975-10-21 | 1979-11-20 | Wallace Murray Corporation | Sheet metal fan assembly |
GB2289089A (en) * | 1994-04-28 | 1995-11-08 | Tygar Co Ltd | Fan blade |
GB2289089B (en) * | 1994-04-28 | 1997-10-08 | Tygar Co Ltd | Fan blade |
GB2296743A (en) * | 1995-01-06 | 1996-07-10 | Huang Yung Chung | Fan |
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