US3827826A - Flexible bladed fan with strengthened leading edge - Google Patents

Flexible bladed fan with strengthened leading edge Download PDF

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Publication number
US3827826A
US3827826A US00390010A US39001073A US3827826A US 3827826 A US3827826 A US 3827826A US 00390010 A US00390010 A US 00390010A US 39001073 A US39001073 A US 39001073A US 3827826 A US3827826 A US 3827826A
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Prior art keywords
blade
reinforcing member
leading edge
adjacent
reversely bent
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US00390010A
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K Strick
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Siemens Bendix Automotive Electronics Ltd
Bendix Engine Components Ltd
Foram Corp
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Foram Corp
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Priority to US00390010A priority Critical patent/US3827826A/en
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Publication of US3827826A publication Critical patent/US3827826A/en
Priority to CA206,596A priority patent/CA998028A/en
Assigned to BENDIX ELECTRONICS LIMITED reassignment BENDIX ELECTRONICS LIMITED CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). EFFECTIVE DATE: 06/02/86 Assignors: BENDIX ENGINE COMPONENTS LIMITED
Assigned to BENDIX ENGINE COMPONENTS LIMITED reassignment BENDIX ENGINE COMPONENTS LIMITED CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). EFFECTIVE 10-01-85 Assignors: CANADIAN FRAM LIMITED
Assigned to SIEMENS-BENDIX AUTOMOTIVE ELECTRONICS LIMITED reassignment SIEMENS-BENDIX AUTOMOTIVE ELECTRONICS LIMITED MERGER (SEE DOCUMENT FOR DETAILS). EFFECTIVE DATE: OCT. 1, 1988 Assignors: 67393 ONTARIO LIMITED, BENDIX ELECTRONICS LIMITED, SBAE CANADA HOLDINGS LIMITED
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    • 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

  • the reinforcing member comprised one or two reverse folds of the blade upon itself extending along the entire leading edge of the blade and having a substantial transverse width for supporting and reinforcing the blade during decambering.
  • the reinforcing member extending substantially along the entire length of the blade leading edge contributes materially to overall fan 3 SUMMARY OF THE INVENTION
  • the present invention features a reinforcing member overlying the fan blade and extending from the radially inner edge of the blade to a position spaced from the radially outer edge or tip of the blade a distance in the range of about 25-50 percent of the radial extent of the blade.
  • the leading edge of the blade is reversely bent along substantially its entire length and overlies the reinforcing member thereadjacent.
  • the reverse bend of the blade leading edge provides inherently increased strength and rigidity to the leading edge of both the blade and the reinforcing member. Additionally, since the reverse bend overlies the reinforcing member, additional strength and resistance to bending stresses is provided to the blade leading edge outwardly of the reinforcing member by the transmission of forces to the reinforcing member. This in turn permits the use of the short reinforcing member which reduces the weight of the fan. Since the reverse bend is not used for supporting the blade as it decambers, it need not extend rearwardly any substantial distance and terminates forward of fasteners connecting the blade and the reinforcing member. The reduction of material in the reinforcing member exceeds the additional blade material employed in the reverse bend.
  • the reinforcing member comprises a member separate from the supporting arm. Also in a preferred embodiment the outer portion of the blade leading edge is more tightly folded outwardly of the reinforcing member.
  • the fold of the blade leading edge provides strength to improve durability in handling of the fan and contributes to personal safety by turning back a relatively sharp blade edge.
  • the elimination of a tip rivet, employed in certain prior art fans, eliminates weight and eliminates, as well, a stress riser at the blade tip.
  • the folded leading edge also protects against the accumulation of foreign matter between the blade and the reinforcing members, another potential source of stress risers.
  • FIG. 1 is a fragmentary plan view of a fan embodying the invention
  • FIG. 2 is an enlarged sectional view taken along the line 2-2 of FIG. 1;
  • FIG. 3 is an enlarged fragmentary end view taken along the line 3--3 of FIG. 1.
  • the fan embodying the invention comprises a central hub 10 having a plurality of arms 12, integral with hub 10 and extending generally radially outwardly from the hub 10.
  • each arm 12 Overlying each arm 12, on the upstream side thereof, defined by the direction of airflow as indicated by arrows in FIG. 2, is mounted a blade 14 of thin flexible resilient material, AISI 301 stainless steel 0.020 inch thick in the illustrated preferred embodiment.
  • the blade 14 has generally radially extending leading and trailing edges l6, 18, respectively defined by the direction of fan rotation indicated by arrows in FIG. I.
  • the blade 14 is curved between the transversely spaced leading and trailing edges 16, 18 thereof, presenting a convex side on the upstream side of the blade 14 and a concave side on the downstream side thereof.
  • the leading edge 16 is positioned forward of arm 12 and the trailing edge 18 is positioned behind the arm 12.
  • a relatively rigid reinforcing member 26 Overlying blade 14, on the upstream side thereof, is a relatively rigid reinforcing member 26.
  • Member 26 has a leading edge 28 adjacent blade leading edge 16 and extends transversely to a trailing edge 30 intermediate the blade leading and trailing edges l6, l8.
  • Member 26 extends radially along blade 14 from adjacent the inner edge 20 of blade 14 to a position inwardly spaced from blade tip 22 a distance in the range of about 25-50 percent, about 30 percent in the illustrated preferred embodiment, of the radial extent of the blade 14.
  • a radially extending strengthening rib 32 is provided along member 26 rearwardly of its leading edge 28.
  • Rivet fasteners 34 extend through and fasten together arm 12, blade 14 and reinforcing member 26. Fasteners 34 are positioned rearwardly of blade and reinforcing member leading edges 16, 28 and rearwardly of rib 32.
  • the blade 14 is reversely bent at its leading edge to provide a reversely bent portion 24 on the upstream side thereof.
  • Reversely bent portion 24 extends continuously along substantially the entire length of blade leading edge 16, the radially inner portion thereof overlying reinforcing member 26 and the outer portion thereof overlying the upstream side of blade 14.
  • the reversely bent portion 24 of blade 14 extends rearwardly from blade leading edge 16 a limited extent to a position forward of fasteners 34 and forward of reinforcing member rib 32. As illustrated in FIG.
  • the outer portion of reversely bent portion 24 is bent to a position more closely adjacent the underlying portion of blade 14 thereadjacent than is possible at the inner portion of reversely bent portion 24 overlying reinforcing member 26, thus assuring tight contact of the inner portion with reinforcing member 26.
  • the continuous reverse bend at the leading edge of blade 14 inherently strengthens the blade leading edge to resist vibration.
  • Overlying reinforcing member 26, additional resistance to vibration in use is imparted to blade 14 beyond member 26.
  • the reversely bent portion 24 overlying reinforcing member 26 also rigidities and mutually strengthens member 26.
  • a shorter reinforcing member 26 may be employed without inadmissably shortening fatigue life of the blade and, additionally lighter material may be employed in the reinforcing member 26 than heretofore customary, 0.060 inch thick aluminum being used in the illustrated preferred embodiment. The result is a strenghtened leading edge in the fan blade assembly and a desirably lighter fan.
  • the reinforcing member may comprise an integral portion of the arm.
  • an automotive cooling fan having a hub, arms radially projecting from said hub and blade structures connected to said arms, said blade structures each comprising:
  • a resilient blade having generally radially extending
  • said blade extending from its inner edge adjacent said hub to a blade tip remote from said hub, said blade having one side facing upstream of the direction of airflow and the other side facing downstream thereof, the portion of said blade adjacent said trailing edge thereof decambering in an upstream direction as fan rotational speed increases;
  • a blade reinforcing member positioned against the upstream side of said blade and having a leading edge adjacent said blade leading edge, said reinforcing member extending transversely from adjacent said blade leading edge in the direction of said blade trailing edge and extending generally radially from adjacent said inner edge of said blade toward said tip thereof;
  • said reinforcing member extends generally radially from adjacent said inner edge of said blade to a position spaced radially inwardly from said tip of said blade a distance in the range of about 25-50 percent of the radial extent of said blade;
  • said blade is continuously reversely bent along substantially the length of its said leading edge providing a radially inner reversely bent portion thereof bent around said reinforcing member leading edge and transversely extending along the upstream side of said reinforcing member a limited extent to a position intermediate said reinforcing member leading edge and said fasteners and providing a radially outer reversely bent portion thereof extending radially outwardly of said reinforcing member substantially to said blade tip, said inner and outer reversely bent portions integral with said blade and with each other.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

A flexible bladed automotive cooling fan having a reinforcing member on the upstream side of the blade, the reinforcing member radially spaced inwardly from the tip of the blade a distance in the range of 25-50 percent of the radial extent of the blade and the blade reversely bent continuously along its leading edge overlying the reinforcing member at an inner portion of the reverse bend.

Description

nited States Patent [191 Strick Aug. 6, 1974 FLEXIBLE BLADED FAN WITH 3,664,165 5/1972 Harvill et al. 416/240 UX STRENGTHENED LEADING EDGE Inventor! Karl Chatham, Ontario, Primary Examine rEverette A. Powell, Jr.
Canada [73] Assignee: Foram Corporation, East Providence, RI. [57] ABSTRACT [22] Wed: 1973 A flexible bladed automotive cooling fan having a re- [21] Appl. No.: 390,010 inforcing member on the upstream side of the blade, the reinforcing member radially spaced inwardly from g the tip of the blade a distance in the range of 25-50 g 1 6 3 percent of the radial extent of the blade and the blade [58] Fieid 136 A 240 reversely bent continuously along its leading edge v overlying the reinforcing member at an inner portion [56] References Cited of the reverse bend.
UNITED STATES PATENTS Weir 416/132 4 Claims, 3 Drawing Figures FLEXIBLE BLADED FAN WITH STRENGTHENED LEADING EDGE BACKGROUND OF THE INVENTION 1. Field Of The Invention This invention relates to automotive fans and particularly to automotive fans employing resilient blades which decamber as rotational fan speed increases.
2 Description Of The Prior Art Strength at the leading edge of a fan blade assembly, to prevent vibration, and minimal fan weight are basic design parameters with any automotive fan. Weight is important as, typically, the fan is mounted as a cantilevered load on the end of an engine water pump shaft and unnecessary weight is deleterious to water pump shaft and bearing life. Vibration is a matter of concern particularly at the outer tip of the fan blade as unnecessary vibration can lead to metal fatigue and premature blade failure. Vibration transmitted from the blade to an overlying reinforcing member can also lead to fatigue and failure of the reinforcing member.
Heretofore, to deal with blade tip vibration, a reinforcing member of heavier material than the blade was, in some fans, wrapped around the blade leading edge and extended along substantially the entire leading edge thereof, as in US. Pat. No. 3,594,098. In other fans, a reinforcing member was simply placed on the upstream side of the blade extending along substantially the entire leading edge thereof and was secured thereto by rivets including a rivet adjacent the blade tip, as in US. Pat. No. 3,594,098. In yet another design, as in US. Pat. No. 3,406,760, the reinforcing member comprised one or two reverse folds of the blade upon itself extending along the entire leading edge of the blade and having a substantial transverse width for supporting and reinforcing the blade during decambering. In each of the foregoing fans, the reinforcing member extending substantially along the entire length of the blade leading edge contributes materially to overall fan 3 SUMMARY OF THE INVENTION In general the present invention features a reinforcing member overlying the fan blade and extending from the radially inner edge of the blade to a position spaced from the radially outer edge or tip of the blade a distance in the range of about 25-50 percent of the radial extent of the blade. The leading edge of the blade is reversely bent along substantially its entire length and overlies the reinforcing member thereadjacent. The reverse bend of the blade leading edge provides inherently increased strength and rigidity to the leading edge of both the blade and the reinforcing member. Additionally, since the reverse bend overlies the reinforcing member, additional strength and resistance to bending stresses is provided to the blade leading edge outwardly of the reinforcing member by the transmission of forces to the reinforcing member. This in turn permits the use of the short reinforcing member which reduces the weight of the fan. Since the reverse bend is not used for supporting the blade as it decambers, it need not extend rearwardly any substantial distance and terminates forward of fasteners connecting the blade and the reinforcing member. The reduction of material in the reinforcing member exceeds the additional blade material employed in the reverse bend.
In a preferred embodiment, the reinforcing member comprises a member separate from the supporting arm. Also in a preferred embodiment the outer portion of the blade leading edge is more tightly folded outwardly of the reinforcing member.
Advantageously, the fold of the blade leading edge provides strength to improve durability in handling of the fan and contributes to personal safety by turning back a relatively sharp blade edge. The elimination of a tip rivet, employed in certain prior art fans, eliminates weight and eliminates, as well, a stress riser at the blade tip. The folded leading edge also protects against the accumulation of foreign matter between the blade and the reinforcing members, another potential source of stress risers.
BRIEF DESCRIPTION OF THE DRAWING Other objects, features and advantages of this invention will be apparent to those skilled in the art from the following detailed description of a preferred embodiment thereof taken together with the accompanying drawing, in which:
FIG. 1 is a fragmentary plan view of a fan embodying the invention;
FIG. 2 is an enlarged sectional view taken along the line 2-2 of FIG. 1; and
FIG. 3 is an enlarged fragmentary end view taken along the line 3--3 of FIG. 1.
DESCRIPTION OF THE PREFERRED EMBODIMENT As illustrated in FIG. 1, the fan embodying the invention comprises a central hub 10 having a plurality of arms 12, integral with hub 10 and extending generally radially outwardly from the hub 10.
Overlying each arm 12, on the upstream side thereof, defined by the direction of airflow as indicated by arrows in FIG. 2, is mounted a blade 14 of thin flexible resilient material, AISI 301 stainless steel 0.020 inch thick in the illustrated preferred embodiment. The blade 14 has generally radially extending leading and trailing edges l6, 18, respectively defined by the direction of fan rotation indicated by arrows in FIG. I. The blade 14 is curved between the transversely spaced leading and trailing edges 16, 18 thereof, presenting a convex side on the upstream side of the blade 14 and a concave side on the downstream side thereof. The leading edge 16 is positioned forward of arm 12 and the trailing edge 18 is positioned behind the arm 12.
Overlying blade 14, on the upstream side thereof, is a relatively rigid reinforcing member 26. Member 26 has a leading edge 28 adjacent blade leading edge 16 and extends transversely to a trailing edge 30 intermediate the blade leading and trailing edges l6, l8. Member 26 extends radially along blade 14 from adjacent the inner edge 20 of blade 14 to a position inwardly spaced from blade tip 22 a distance in the range of about 25-50 percent, about 30 percent in the illustrated preferred embodiment, of the radial extent of the blade 14. A radially extending strengthening rib 32 is provided along member 26 rearwardly of its leading edge 28.
Rivet fasteners 34 extend through and fasten together arm 12, blade 14 and reinforcing member 26. Fasteners 34 are positioned rearwardly of blade and reinforcing member leading edges 16, 28 and rearwardly of rib 32.
The blade 14 is reversely bent at its leading edge to provide a reversely bent portion 24 on the upstream side thereof. Reversely bent portion 24 extends continuously along substantially the entire length of blade leading edge 16, the radially inner portion thereof overlying reinforcing member 26 and the outer portion thereof overlying the upstream side of blade 14. The reversely bent portion 24 of blade 14 extends rearwardly from blade leading edge 16 a limited extent to a position forward of fasteners 34 and forward of reinforcing member rib 32. As illustrated in FIG. 3, the outer portion of reversely bent portion 24 is bent to a position more closely adjacent the underlying portion of blade 14 thereadjacent than is possible at the inner portion of reversely bent portion 24 overlying reinforcing member 26, thus assuring tight contact of the inner portion with reinforcing member 26.
In operation, the continuous reverse bend at the leading edge of blade 14 inherently strengthens the blade leading edge to resist vibration. Overlying reinforcing member 26, additional resistance to vibration in use is imparted to blade 14 beyond member 26. Advantageously, the reversely bent portion 24 overlying reinforcing member 26 also rigidities and mutually strengthens member 26. Thus, a shorter reinforcing member 26 may be employed without inadmissably shortening fatigue life of the blade and, additionally lighter material may be employed in the reinforcing member 26 than heretofore customary, 0.060 inch thick aluminum being used in the illustrated preferred embodiment. The result is a strenghtened leading edge in the fan blade assembly and a desirably lighter fan.
Other embodiments of this invention will occur to those skilled in the art which are within the scope of the following claims. ln one such modification, the reinforcing member may comprise an integral portion of the arm.
What is claimed is:
1. In an automotive cooling fan having a hub, arms radially projecting from said hub and blade structures connected to said arms, said blade structures each comprising:
a resilient blade having generally radially extending,
transversely spaced leading and trailing edges, said blade extending from its inner edge adjacent said hub to a blade tip remote from said hub, said blade having one side facing upstream of the direction of airflow and the other side facing downstream thereof, the portion of said blade adjacent said trailing edge thereof decambering in an upstream direction as fan rotational speed increases;
a blade reinforcing member positioned against the upstream side of said blade and having a leading edge adjacent said blade leading edge, said reinforcing member extending transversely from adjacent said blade leading edge in the direction of said blade trailing edge and extending generally radially from adjacent said inner edge of said blade toward said tip thereof; and
a plurality of fasteners connecting said blade and said reinforcing member, said fasteners spaced rearwardly from said blade and reinforcing member leading edges;
the improvement in said blade structure in which said reinforcing member extends generally radially from adjacent said inner edge of said blade to a position spaced radially inwardly from said tip of said blade a distance in the range of about 25-50 percent of the radial extent of said blade; and
said blade is continuously reversely bent along substantially the length of its said leading edge providing a radially inner reversely bent portion thereof bent around said reinforcing member leading edge and transversely extending along the upstream side of said reinforcing member a limited extent to a position intermediate said reinforcing member leading edge and said fasteners and providing a radially outer reversely bent portion thereof extending radially outwardly of said reinforcing member substantially to said blade tip, said inner and outer reversely bent portions integral with said blade and with each other.
2. The improvement claimed in claim 1 in which said outer reversely bent portion is bent to a position more closely adjacent the portion of said blade which it overlies than said inner reversely bent portion.
3. The improvement claimed in claim 1 in which said blade and reinforcing member are positioned on the upstream side of one said arm and are connected thereto by said fasteners.
4. The improvement claimed in claim 3 in which said outer reversely bent portion is bent to a position more closely adjacent the portion of said blade which it overlies than said inner reversely bent portion.
UNITED STATES PATENT GFFICE CERTIFIECATE OF CGRREQTION Patent No. 3,827 ,826 I Dated August 6, 1974 Inventofls) Karl H. Strick v I It is certified that error appears in the above-identified patent and that said Letters Patent are hereby corrected as shown below:
Change the Ass ignee from "Foram Corporation" to "Pram Corporation- Signed and sealed this 3rd day of December 1974.
(SEAL) Attest:
McCOY M.. GIBSON JR'. 0. MARSHALL DANN Attesting Officer Commissioner of Patents mm b mum; Hil 15)

Claims (4)

1. In an automotive cooling fan having a hub, arms radially projecting from said hub and blade structures connected to said arms, said blade structures each comprising: a resilient blade having generally radially extending, transversely spaced leading and trailing edges, said blade extending from its inner edge adjacent said hub to a blade tip remote from said hub, said blade having one side facing upstream of the direction of airflow and the other side facing downstream thereof, the portion of said blade adjacent said trailing edge thereof decambering in an upstream direction as fan rotational speed increases; a blade reinforcing member positioned against the upstream side of said blade and having a leading edge adjacent said blade leading edge, said reinforcing member extending transversely from adjacent said blade leading edge in the direction of said blade trailing edge and extending generally radially from adjacent said inner edge of said blade toward said tip thereof; and a plurality of fasteners connecting said blade and said reinforcing member, said fasteners spaced rearwardly from said blade and reinforcing member leading edges; the improvement in said blade structure in which said reinforcing member extends generally radially from adjacent said inner edge of said blade to a position spaced radially inwardly from said tip of said blade a distance in the range of about 25-50 percent of the radial extent of said blade; and said blade is continuously reversely bent along substantially the length of its said leading edge providing a radially inner reversely bent portion thereof bent around said reinforcing member leading edge and transversely extending along the upstream side of said reinforcing member a limited extent to a position intermediate said reinforcing member leading edge and said fasteners and providing a radially outer reversely bent portion thereof extending radially outwardly of said reinforcing member substantially to said blade tip, said inner and outer reversely bent portions integral with said blade and with each other.
2. The improvement claimed in claim 1 in which said outer reversely bent portion is bent to a position more closely adjacent the portion of said blade which it overlies than said inner reversely bent portion.
3. The improvement claimed in claim 1 in which said blade and reinforcing member are positioned on the upstream side of one said arm and are connected thereto by said fasteners.
4. The improvement claimed in claim 3 in which said outer reversely bent portion is bent to a position more closely adjacent the portion of said blade which it overlies than said inner reversely bent portion.
US00390010A 1973-08-20 1973-08-20 Flexible bladed fan with strengthened leading edge Expired - Lifetime US3827826A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4012168A (en) * 1975-05-12 1977-03-15 Wallace-Murray Corporation Twisted flex fan
US4037987A (en) * 1975-06-30 1977-07-26 Fram Corporation Flexible bladed fan with increased natural frequency
WO2016012456A1 (en) * 2014-07-23 2016-01-28 Ebm-Papst Mulfingen Gmbh & Co. Kg Blade for an impeller
US20230081223A1 (en) * 2021-09-16 2023-03-16 Vornado Air, Llc Space Heater

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111911458B (en) * 2020-09-22 2021-10-26 江西艾斯欧匹精密智造科技有限公司 Blade for fan

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3406760A (en) * 1967-09-18 1968-10-22 Wallace Murray Corp Flexible blade fan
US3664165A (en) * 1969-08-04 1972-05-23 Wallace Murray Corp Method and die construction for fan blade

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3406760A (en) * 1967-09-18 1968-10-22 Wallace Murray Corp Flexible blade fan
US3664165A (en) * 1969-08-04 1972-05-23 Wallace Murray Corp Method and die construction for fan blade

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US4037987A (en) * 1975-06-30 1977-07-26 Fram Corporation Flexible bladed fan with increased natural frequency
WO2016012456A1 (en) * 2014-07-23 2016-01-28 Ebm-Papst Mulfingen Gmbh & Co. Kg Blade for an impeller
US20230081223A1 (en) * 2021-09-16 2023-03-16 Vornado Air, Llc Space Heater

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