US3759630A - Flexible bladed fan with improved reinforcing - Google Patents
Flexible bladed fan with improved reinforcing Download PDFInfo
- Publication number
- US3759630A US3759630A US00246540A US3759630DA US3759630A US 3759630 A US3759630 A US 3759630A US 00246540 A US00246540 A US 00246540A US 3759630D A US3759630D A US 3759630DA US 3759630 A US3759630 A US 3759630A
- Authority
- US
- United States
- Prior art keywords
- sheet
- trailing
- reinforcing strip
- decamber
- curved
- 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
-
- 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
- F04D29/382—Flexible blades
Definitions
- ABSTRACT A fan having curved flexible resilient blades which decamber with an increase in rotational speed and aerodynamic forces.
- Each of the blades has an overlying reinforcing strip in partial contact with a trailing sheet, which decambers as the rotational speed increases.
- the reinforcing strip and trailing sheet which is of significantly thinner cross-section, are joined to each other and to a supporting arm extending from a central hub.
- the reinforcing strip preferably has a curved trailing decamber limiting portion and a curved bending limiting portion disposed along the inner side edge of the reinforcing strip and its decamber limiting portion.
- FIG. 1 is a plan view of the upstream side of an engine cooling fan embodying the present invention.
- FIG. 2 is an enlarged end view of an arm and blade of the fan viewed as indicated by line 2-2 of FIG. 1.
- FIG. 3 is an enlarged sectional view of the same arm and blade taken along line 3-3 of FIG. 1.
- FIG. 4 is a partial enlarged sectional view of the arm and blade taken along line 4-4 ofFIG. 2.
- FIG. 5 is a partial enlarged sectional view of another arm and blade of thesame fan taken along line 5-5 of FIG. 1.
- FIG. 5a is a view similar to FIG. 5 showing a portion of a blade in a supported position.
- FIG. I there is illustrated a cooling fan generally designated by the numeral 10 composed of a spider 12 having a hub portion 13 and a plurality of spider arms 14. These arms are oriented perpendicularly to the axis of rotation of the fan. Joined to the spider arms are a plurality of fan blade constructions generally designated as 16.
- each blade iti i'i'r''frafiiy constructed of a reinforcing hub plate 18 trailing flexible sheet 20 joined together by rivets 22 and also to the spider arm 14 by rivets 24.
- the trailing portion 26 of the reinforcing strip 18 is curved away from the trailing sheet 20 to act as a deflection limit stop for the sheet 20 as the sheet decambers during rotation of thegfan.
- radius arrow R It distributes stresses in the trailing sheet 20 more evenly than-would otherwise occur if the reinforcing sheet contained a sharp bend.
- the trailing sheet 20 will progressively engage the inner surface of the curved portion 26 as the blade decambers during rotation. This will provide all the advantages hitherto recognized for flexible bladed fans in that less noise and a significant power saving will occur in the decambered position.
- the feature which has not previously been recognized and which is now encompassed in the present invention is that as the blade decambered in prior art constructions the inner side edge, shown here as 28, would engage the trailing edge 27 of the reinforcing portion thus creating a high stress concentration point at the intersection of the two edges.
- the present invention overcomes this problem by curving the inner edge portion 30 of the reinforcing portion upwardly from the trailing sheet.
- the curvature of the reinforcing portion has a radius R which is the same as the curvature shown in FIG. 4. These two radii, however, need not always be equal.
- a fan having curved flexible resilient blades which decamber with an increase in rotational speed and aerodynamic forces,'each of said blades comprising a reinforcing strip overlying and in partial contact with a trailing sheet, which decambers as rotational speed increases, joined to each other and to a supporting arm extending outwardly from a central hub portion, said trailing sheet being of significantly thinner cross-section than said reinforcing strip, said reinforcing strip comprising,
- a trailing decamber-limiting portion extending partially coextensively with a portion of said trailing sheet and at an acute angle to said sheet
Abstract
A fan having curved flexible resilient blades which decamber with an increase in rotational speed and aerodynamic forces. Each of the blades has an overlying reinforcing strip in partial contact with a trailing sheet, which decambers as the rotational speed increases. The reinforcing strip and trailing sheet, which is of significantly thinner cross-section, are joined to each other and to a supporting arm extending from a central hub. The reinforcing strip preferably has a curved trailing decamber limiting portion and a curved bending limiting portion disposed along the inner side edge of the reinforcing strip and its decamber limiting portion. As the trailing sheet decambers it also makes progressive contact with the reinforcing strip in a direction toward the inner side edge of the sheet, thus reducing stress concentration at the intersection of the inner side edge of the sheet and the decamber limiting portion of the reinforcing strip.
Description
ilnited States Patent [1 1 Freeman et al.
[ Sept. 18, 1973 1' FLEXIBLE BLADED FAN WITH IMPROVED REINFORCING [75] Inventors: Willard Anton Freeman; Donald Jean Hartley, both of Indianapolis,
Ind.
[73] Assignee: Wallace Murray Corporation, New
-' York, NY.
[22] Filed: Apr. 24, 1972 [21] Appl; No.: 246,540
[52] U.S. Cl. 416/132, 416/240 Primary Examiner-Everette A. Powell, Jr. Attorney-Herman Foster [57] ABSTRACT A fan having curved flexible resilient blades which decamber with an increase in rotational speed and aerodynamic forces. Each of the blades has an overlying reinforcing strip in partial contact with a trailing sheet, which decambers as the rotational speed increases. The reinforcing strip and trailing sheet, which is of significantly thinner cross-section, are joined to each other and to a supporting arm extending from a central hub. The reinforcing strip preferably has a curved trailing decamber limiting portion and a curved bending limiting portion disposed along the inner side edge of the reinforcing strip and its decamber limiting portion. As the trailing sheet decambers it also makes progressive contact with the reinforcing strip in a direction toward the inner side edge of the sheet, thus reducing stress concentration at the intersection of the inner side edge of the sheet and the decamber limiting portion of the reinforcing strip.
3 Claims, 6 Drawing Figures FLEXIBLE BLADE!) FAN WITH IMPROVED REINFORCING BACKGROUND OF THE INVENTION I means to prevent undue weakness in the fan structure As has been noted in U.S. Pat. Ne.3,s94,09s, ui' decamber rate may be controlled by utilizing a weighted trailing edge of each blade. Another approach to achieving the same results is to make the flexible portion of the blade as thin as possible so that decambering can result with a minimum of resistance.
Unfortunately, when a blade is made very thin it be- 2 comes prone to tearing at high stress concentration points, One such point is at the intersection of the inner edge of the flexible portion of the blade and the rein forcing strip used to limit the amount of decambering flexure. Because of the necessity for preventing tearing at this point, the flexing blades were normally made of a thicker cross section than would be used if this problem could otherwise be solved. The present invention offers a solution to thisproblem, thus resulting in an economic savings.
BRIEF DESCRIPTION OF THE DRAWING FIG. 1 is a plan view of the upstream side of an engine cooling fan embodying the present invention.
FIG. 2 is an enlarged end view of an arm and blade of the fan viewed as indicated by line 2-2 of FIG. 1.
FIG. 3 is an enlarged sectional view of the same arm and blade taken along line 3-3 of FIG. 1.
FIG. 4 is a partial enlarged sectional view of the arm and blade taken along line 4-4 ofFIG. 2.
FIG. 5 is a partial enlarged sectional view of another arm and blade of thesame fan taken along line 5-5 of FIG. 1. l
FIG. 5a is a view similar to FIG. 5 showing a portion of a blade in a supported position.
DESCRIPTION oE T iiE PREFERRED EMBODIMENTS Referring initially to FIG. I there is illustrated a cooling fan generally designated by the numeral 10 composed of a spider 12 having a hub portion 13 and a plurality of spider arms 14. These arms are oriented perpendicularly to the axis of rotation of the fan. Joined to the spider arms are a plurality of fan blade constructions generally designated as 16.
As seen in FIGS. 1 and 2 each blade iti i'i'r''frafiiy constructed of a reinforcing hub plate 18 trailing flexible sheet 20 joined together by rivets 22 and also to the spider arm 14 by rivets 24. The trailing portion 26 of the reinforcing strip 18 is curved away from the trailing sheet 20 to act as a deflection limit stop for the sheet 20 as the sheet decambers during rotation of thegfan.
bend, is indicated by radius arrow R. It distributes stresses in the trailing sheet 20 more evenly than-would otherwise occur if the reinforcing sheet contained a sharp bend.
As will be seen in FIG. 2 the trailing sheet 20 will progressively engage the inner surface of the curved portion 26 as the blade decambers during rotation. This will provide all the advantages hitherto recognized for flexible bladed fans in that less noise and a significant power saving will occur in the decambered position.
The feature which has not previously been recognized and which is now encompassed in the present invention is that as the blade decambered in prior art constructions the inner side edge, shown here as 28, would engage the trailing edge 27 of the reinforcing portion thus creating a high stress concentration point at the intersection of the two edges. The present invention overcomes this problem by curving the inner edge portion 30 of the reinforcing portion upwardly from the trailing sheet. In the particular embodiment shown in FIGS. 5 and 5a the curvature of the reinforcing portion has a radius R which is the same as the curvature shown in FIG. 4. These two radii, however, need not always be equal. The advantage of this type of formation is that 5 as the trailing portion 20 decambers to position 20a it the sheet, precluding a sharp engagement of the intersecting edges previously describedTherefore the stress concentration will be less than would otherwise occur, thus permitting the use of thinner sheet stock for the trailing edge portion 20. As previously indicated, the use of thinner stock will create a more efficiently operating flexible bladed fan.
We claim:
1. In a fan having curved flexible resilient blades which decamber with an increase in rotational speed and aerodynamic forces,'each of said blades comprising a reinforcing strip overlying and in partial contact with a trailing sheet, which decambers as rotational speed increases, joined to each other and to a supporting arm extending outwardly from a central hub portion, said trailing sheet being of significantly thinner cross-section than said reinforcing strip, said reinforcing strip comprising,
a. a trailing decamber-limiting portion extending partially coextensively with a portion of said trailing sheet and at an acute angle to said sheet, and
b. a bending limiting curved portion disposed along the inner side edge of said reinforcing strip and decamber-limiting portion whereby, as said trailing sheet decambers, progressive contact is made by said sheet with said reinforcing strip in a direction toward the inner side edge of said sheet, thus reducing stress concentration at the intersection of said inner side edge of said sheet and said decamberlimiting portion.
2. A fan as called for in claim 1 wherein said (a) trailing decamber-limiting portion and said (b) bending limiting curved portion are both curved in a direction away from the surface of said trailing sheet which is in contact with said reinforcing strip.
3. A fan as called for in claim 2 wherein said (a) trailing decamber-limiting portion and said (b) bending limiting curved portion are both curved, with equal
Claims (3)
1. In a fan having curved flexible resilient blades which decamber with an increase in rotational speed and aerodynamic forces, each of said blades comprising a reinforcing strip overlying and in partial contact with a trailing sheet, which decambers as rotational speed increases, joined to each other and to a supporting arm extending outwardly from a central hub portion, said trailing sheet being of significantly thinner cross-section than said reinforcing strip, said reinforcing strip comprising, a. a trailing decamber-limiting portion extending partially coextensively with a portion of said trailing sheet and at an acute angle to said sheet, and b. a bending limiting curved portion disposed along the inner side edge of said reinforcing strip and decamber-limiting portion whereby, as said trailing sheet decambers, progressive contact is made by said sheet with said reinforcing strip in a direction toward the inner side edge of said sheet, thus reducing stress concentration at the intersection of said inner side edge of said sheet and said decamber-limiting portion.
2. A fan as called for in claim 1 wherein said (a) trailing decamber-limiting portion and said (b) bending limiting curved portion are both curved in a direction away from the surface of said trailing sheet which is in contact with said reinforcing strip.
3. A fan as cAlled for in claim 2 wherein said (a) trailing decamber-limiting portion and said (b) bending limiting curved portion are both curved, with equal radii of curvature.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US24654072A | 1972-04-24 | 1972-04-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3759630A true US3759630A (en) | 1973-09-18 |
Family
ID=22931124
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US00246540A Expired - Lifetime US3759630A (en) | 1972-04-24 | 1972-04-24 | Flexible bladed fan with improved reinforcing |
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US (1) | US3759630A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3860362A (en) * | 1973-12-14 | 1975-01-14 | Ford Motor Co | Flexible bladed fan |
US3914069A (en) * | 1973-06-06 | 1975-10-21 | Fort Worth Pressed Steel Corp | Axial flow fan having fully streamlining flexible blades |
US4012168A (en) * | 1975-05-12 | 1977-03-15 | Wallace-Murray Corporation | Twisted flex fan |
USD246794S (en) * | 1976-04-02 | 1977-12-27 | Flex-A-Lite Corporation | Fan for internal combustion engines |
US4547126A (en) * | 1983-12-08 | 1985-10-15 | Jackson Samuel G | Fan impeller with flexible blades |
US4755105A (en) * | 1986-10-27 | 1988-07-05 | Chemcut Corporation | Impeller improvement |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3044557A (en) * | 1959-01-08 | 1962-07-17 | American Metal Prod | Variable pitch fan blade |
US3406760A (en) * | 1967-09-18 | 1968-10-22 | Wallace Murray Corp | Flexible blade fan |
US3639078A (en) * | 1970-11-04 | 1972-02-01 | Shrinivas V Pratinidhi | Flexible-bladed fan with extended blade structure |
US3679321A (en) * | 1971-04-26 | 1972-07-25 | Fran Corp | Prestressed flexible bladed fan |
US3698835A (en) * | 1971-02-01 | 1972-10-17 | John C Kelly | Fan construction |
-
1972
- 1972-04-24 US US00246540A patent/US3759630A/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3044557A (en) * | 1959-01-08 | 1962-07-17 | American Metal Prod | Variable pitch fan blade |
US3406760A (en) * | 1967-09-18 | 1968-10-22 | Wallace Murray Corp | Flexible blade fan |
US3639078A (en) * | 1970-11-04 | 1972-02-01 | Shrinivas V Pratinidhi | Flexible-bladed fan with extended blade structure |
US3698835A (en) * | 1971-02-01 | 1972-10-17 | John C Kelly | Fan construction |
US3679321A (en) * | 1971-04-26 | 1972-07-25 | Fran Corp | Prestressed flexible bladed fan |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3914069A (en) * | 1973-06-06 | 1975-10-21 | Fort Worth Pressed Steel Corp | Axial flow fan having fully streamlining flexible blades |
US3860362A (en) * | 1973-12-14 | 1975-01-14 | Ford Motor Co | Flexible bladed fan |
US4012168A (en) * | 1975-05-12 | 1977-03-15 | Wallace-Murray Corporation | Twisted flex fan |
US4105366A (en) * | 1975-05-12 | 1978-08-08 | Wallace Murray Corporation | Twisted flex fan |
USD246794S (en) * | 1976-04-02 | 1977-12-27 | Flex-A-Lite Corporation | Fan for internal combustion engines |
US4547126A (en) * | 1983-12-08 | 1985-10-15 | Jackson Samuel G | Fan impeller with flexible blades |
US4755105A (en) * | 1986-10-27 | 1988-07-05 | Chemcut Corporation | Impeller improvement |
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