US3639078A

US3639078A - Flexible-bladed fan with extended blade structure

Info

Publication number: US3639078A
Application number: US86750A
Authority: US
Inventors: Shrinivas V Pratinidhi
Original assignee: Shrinivas V Pratinidhi
Current assignee: Siemens Bendix Automotive Electronics Ltd; Bendix Engine Components Ltd
Priority date: 1970-11-04
Filing date: 1970-11-04
Publication date: 1972-02-01
Anticipated expiration: 1989-02-01

Abstract

A fan having a hub, a plurality of arms each extending radially outwardly of the hub and at an acute angle to the rotational plane of the fan, and blade structures, one secured to each arm, each blade structure having a flexible, resilient trailing airfoil portion, comprising the major portion of the blade structure, which decambers as rotational speed increases, and a less flexible leading airfoil portion comprising a slat extending forward of the respective arm and disposed at an angle thereto lying within the above specified acute angle, with the trailing and leading portions mutually constructed to have the leading and trailing edges of the blade define therebetween a chord disposed at a predetermined chord angle to the rotational plane of the fan.

Description

United States Patent Pratinidhi 1 Feb. i 1972 [54] FLEXlBLE-BLADED FAN WITH 3,356,154 12/1967 Cassidy ..4l6/240 X EXTENDED BLADE STRUCTURE 3,373,930 31968 Rom "416/240 3,406,760 10 1968 Weir ..416 132 UX [72] Inventor: Shrinivas V. Pratinidhi, Chatham, On-

tam) Canada Primary Examiner Everette A. Powell, Jr. 22 Filed: Nov.4, 1970 Hulbefl 21 Appl. No.: 86,750 57 ABSTRACT Related US. Application Data A fan having a hub, a plurality of arms ea-ch extending radially I outwardly of the hub and at an acute angle to the rotational [63] f; 6 g of plane of the fan, and blade structures, one secured to each an one arm, each blade structure having a flexible, resilient trailing airfoil portion, comprising the major portion of the blade 416/132 176 structure, which decambers as rotational speed increases, and 58] Fie'ld 240 237 a less flexible leading airfoil portion comprising a slat extending forward of the respective arm and disposed at an angle thereto lying within the above specified acute angle, with the [56] References cued trailing and leading portions mutually constructed to have the UNITED STATES PATENTS leading and trailing edges of the blade define therebetween a l 799 745 4/1931 G 416/237 chord disposed at a predetermined chord angle to the rotaunn tiona] lane fth f 2,132,133 10/1938 Smith... ..4l6/132 p 3,289,924 12/1966 Weir ..416/24O X 12 Claims, 5 Drawing Figures FLEXIBLE-BLADE) FAN WITH EXTENDED BLADE STRUCTURE This application is a continuation-in-part of my copending US. application, Ser. No. 18,855, filed Mar. I2, 1970, now abandoned.

This invention relates to fans having flexible blades which decamber as rotational speed increases.

The principal object of this invention is to increase the pumping, and hence the cooling capacities of flexible bladed fans without increasing the number of blades or substantially altering the space requirements for the fan. Other objects are to provide improved cooling capacity in such fans without increasing fan vibration, noise, weight, or size to unacceptable levels, and while maintaining the advantages of flexible blades.

The invention features, in a fan having a hub, a plurality of arms extending radially outwardly of the hub, and blade structures secured to these arms, the blade structures each com prising a flexible, resilient trailing portion, defining an air foil surface terminating in the trailing edge of the blade structure, which decambers as rotational speed increases, the improvement wherein each arm is disposed at an acute angle to the rotational plane of said fan, and wherein each blade structure also comprises a leading portion, less flexible than the trailing portion, extending forward of the arm to which it is secured, and effectively disposed at an angle thereto lying within the aforementioned acute angle, each leading portion comprising a slat defining an extended airfoil surface terminating in the leading edge of its corresponding blade structure, the trailing portion comprising the major portion of the blade structure and the leading edge of the leading portion and trailing edge of the trailing portion defining between them a chord disposed at a predetermined chord angle to the rotational plane of the fan.

In a preferred embodiment, the chord angle (with the blade structure in an unbiased condition) is between about 25 and 35, most preferably about 32, and the chord lies in a plane defined by the substantially parallel leading and trailing edges of the fan; the respective leading portion is effectively disposed at an angle (preferably less than about most preferably about 15) to the arm, the leading and trailing edges are located on opposite sides of the rotational plane of the hub; the leading portion is composed of a more rigid material than the trailing portion; and the blade structure comprises separate trailing and leading members, including the trailing and leading portions, respectively, which are arranged to overlap and are secured between a separate reinforcing cap and the arm, with the trailing member, between the cap and the overlapping portion of the leading member, extending somewhat forward of the arm but still behind the leading member and the reinforcing cap secured to the blade structure at a point radially outward of the arm.

Other objects, features and advantages will be apparent to one skilled in the art from the following description of a preferredembodiment of the invention, taken together with the attached drawings thereof, in which:

FIG. 1 is a plan view of the upstream side of an engine-cooling fan embodying the present invention;

FIG. 2 is a side elevational view of the fan of FIG. 1;

FIG. 3 is an enlarged sectional view of an arm and blade structure of the fan taken along the line 3-3 of FIG. 2;

FIG. 4 is a sectional view of an arm and blade structure of the fan taken along the line 4-4 of FIG. 3; and,

FIG. 5 is an enlarged partial view similar to FIG. 3 taken along the line 5-5 ofFIG. 3.

There is shown in the figures generally at 11 an engine-cooling fan adapted for use on a motor vehicle. The fan has a central planar hub I2, with asymmetrically disposed arms 13 extending therefrom. As best shown in FIGS. 2 and 4, each arm has a twisted section 14 joining it to the hub so that the plane of each arm is at an acute angle e (FIG. 3) to the plane 12a of the hub I2.

A blade structure I5 is secured to the upstream side of each arm I3, and has an air-moving or airfoil surface formed, as illustrated, on two separate pieces, a leading member 16 and a trailing member I8. The leading blade member I6, here constructed as a separate slat formed of a relatively rigid steel (SAE 950, prepainted, 0.024 inch thick), defines an extended air-moving or airfoil surface I60, terminating in the leading blade edge I7. The curved trailing blade member I3 is formed of a resilient, more flexible steel (AISI 301 stainless steel, 0.018 inch thick), and defines an air-moving or airfoil surface 18a, terminating in the trailing blade edge 19, which is sub stantially parallel to leading edge I7. The trailing member 18, extending rearwardly from arm 13 a greater distance than the forward extension of leading member I6, forms the major portion of the blade structure.

Provided at the trailing edge of each trailing blade member 18 is a weight 20. As illustrated the weight 20 is an integral portion of blade member I8 folded upon itself at the trailing edge so as to engage the convex side of the blade member and has a mass of about 15 percent of the total mass of the blade member I8. Such weights are fully described in my copending US. Pat. application Ser. No. 857,849, filed Sept. 15, 1969, entitled Fan with Weighted Flexible Blades."

As shown in greater detail in FIGS. 3 and 4, each blade member 16, I8 overlies the arm 13 to which it is mounted on the upstream side of the arm, and is secured to the arm by a reinforcing cap 24, which overlies the convex side of the blade member I8, and rivets 25. The flat portion 26 of leading member I6 is overlapped by the flat portion 28 of trailing member 18, and the

flat portion

26, 28 are secured between reinforcing cap 24 and The upstream side of arm I3 by the rivets 25 therethrough. The reinforcing cap also is radially coextensive with the leading member 16 which lies against arm 13, and is secured to the members I6, 18, past the end of arm 13 by the rivet 29 to reduce flutter of the

blade members

16, 18. The trailing portion of trailing member 18 is curved through the plane of arm I3 toward the downstream side of the fan, convexly, as viewed in FIG. I, away from the plane of hub I2, whereas the leading portion of leading member 16 is bent toward the plane of hub 12. The angle a of the chord plane 0 (FIG. 2) between the leading edge I7 and the trailing edge I9 with the rotational plane of the fan (which, in the illustrated embodiment, is also the plane 12a of hub I2) is about 32 as illustrated and preferably between about 25 and about 35, when, as in the illustrated embodiment, the fan is idle and the trailing member 18 is not otherwise biased or sup ported between the arm 13 and the trailing edge I9. To provide this chord angle, the airfoil surface is effectively disposed at an angle at to the arm 13, which is within the acute angle e of the arm 13 to the plane 12a (FIG. 3) of hub 12. As illustrated, the angle dis about l5 (preferably less than about 200). Although as shown, a separate, a separate slat I6 is provided to form this leading airfoil surface, otherportions of the fan structure, such as the trailing member 18 or even the reinforcing cap 24 should be extended forward to form the slat.

The reinforcing cap 24 is also bent away from the plane of arm 13 at its trailing edge (FIG. 3) and has reinforcing

lips

30 and 32 which are integrally formed by turning up the edges of cap 24 (about one-eighth inch) extending along its inner and outer edges, respectively, to render the reinforcing cap (0.048 inch SAE 950A steel) both strong and light weight.

The arms 13 are arranged for balance of the fan, and the arcuate distances between the

reference lines

40, 41, 42, 43, 44 (drawn radially of hub 12 and parallel to the edges 17, I9) are as follows:

In operation, as the fan rotates clockwise, in the direction indicated by the arrow in FIG. 1, air is moved from upstream to downstream as indicated by the arrows in FIG. 2, by the

airfoil surfaces

16a and 180. As fan speed increases, air pressure and centrifugal force cause only the trailing blade members I8 to decamber-in general, to move toward the plane of hub 12. The addition of the leading airfoil surfaces 16a permit a fivebladed fan, as shown, to move as much air as a seven-bladed fan without any increase in noise, or any substantial increase in size or weight. Furthermore, as illustrated, the more corrodible trailing blade member 18 is protected by being secured between a prepainted cap 24 and a prepainted leading blade member or slat 16. Where blade structure is a single flexible element, of which portions extend on both sides of arm 13, similar to the illustrated

separate members

16 and 18, the forward member being shorter and hence relatively less flexible than the trailing member, the underlying surface of arm 13 is preferably prepainted.

Other embodiments will occur to those skilled in the art from the foregoing nonlimiting description of a preferred embodiment thereof.

What is claimed is:

1. In a fan having a hub, a plurality of arms projecting radially outwardly of said hub, and blade structures secured to said arms, said blade structures each comprising a flexible, resilient trailing portion, defining an airfoil surface terminating in the trailing edge of said blade structure, which decambets as rotational speed increases, the plane of each said arm being disposed at an acute angle to the rotational plane of said fan,

the improvement wherein each said blade structure also comprises a leading portion, less flexible than said trailing portion, extending forward of the arm to which it is secured and effectively disposed at an angle to the plane thereof lying within said acute angle, said leading portion comprising a slat defining an extended airfoil surface terminating in the leading edge of said blade structure, said trailing portion comprising the major portion of said blade structure and said leading edge and said trailing edge defining therebetween a chord disposed at a predetermined chord angle to the rotational plane of said fan. 7

2. The fan of claim 1 wherein said predetermined chord angle is between about 25 and about 35 when said blade structure is in an unbiased position.

3. The fan of claim 2 wherein said chord angle is about 32.

4. The fan of claim 2 wherein said leading edge and said trailing edge are substantially parallel to one another to define therebetween a plane disposed at said chord angle to the rotational plane of said fan.

5. The fan of claim 1 wherein said leading portion is composed of a more rigid material than said trailing portion.

6; The fan of claim 1 wherein said leading edge and said trailing edge are located, respectively, on opposite sides of the rotational plane of the hub of said fan.

7. The fan of claim 1 wherein saidangle between said leading portion and the plane of said arm is less than about 20.

8. The fan of claim 7 wherein said angle between said leading portion and the plane of said arm is about [5".

9. The fan of claim 1 wherein each said blade structure comprises a flexible, resilient trailing member including said trailing portion and a separate leading member including said leading portion, and said members are arranged to overlap one another where secured to said arm.

10. The fan of claim 9 including a separate reinforcing cap overlaying the convex side of each said blade structure, and wherein said members overlap between said reinforcing cap and said arm, and are secured therebetween with said trailing rnember sandwiched between said reinforcing cap and the overlapping portion of said leading member.

11. The fan of claim 10 wherein said members extend radially beyond said arm and said reinforcing can extends radially coextensively with the one of said members sandwiched against said arm and is secured to said blade structure at a point radially outwardly of said arm adjacent the end of said one of said members.

12. The fan of claim 9 wherein said trailing member extends forward of said arm and is disposed adjacent said leading member, and said leading member extends forward of said trailing member.

UNITED STATES PATENT OFFICE v CETIFICATE 0F CTION Patent No. 3 639 ,078

Dated February 1, 1972 Shrinivas V Pratinidhi Inventor(s) It is certified that error appears in the above-identified patent and that said Letters Patent are hereby corrected as shown below:

Col. 2, line 29, change "The" to -the--;

Col. 2, line 50, change "200" to -20--;

Col. 2 line 50,, delete f'a separateflo Signed and sealed this 13th day of June 1972,

(SEAL) Attest:

EDWARD M.FLETCHER, JRo ROBERT GOTTSCHALK Commissioner of Patents Attesting Officer FORM PC4050 (0459) uscoMM-Dc 60376-P59 U-S. GOVERNMENY PRINTING OFFICE: 959 0-356-334

Claims

1. In a fan having a hub, a plurality of arms projecting radially outwardly of said hub, and blade structures secured to said arms, said blade structures each comprising a flexible, resilient trailing portion, defining an airfoil surface terminating in the trailing edge of said blade structure, which decambers as rotational speed increases, the plane of each said arm being disposed at an acute angle to the rotational plane of said fan, the improvement wherein each said blade structure also comprises a leading portion, less flexible than said trailing portion, extending forward of the arm to which it is secured and effectively disposed at an angle to the plane thereof lying within said acute angle, said leading portion comprising a slat defining an extended airfoil surface terminating in the leading edge of said blade structure, said trailing portion comprising the major portion of said blade structure and said leading edge and said trailing edge defining therebetween a chord disposed at a predetermined chord angle to the rotational plane of said fan.

2. The fan of claim 1 wherein said predetermined chord angle is between about 25* and about 35* when said blade structure is in an unbiased position.

3. The fan of claim 2 wherein said chord angle is about 32* .

6. The fan of claim 1 wherein said leading edge and said trailing edge are located, respectively, on opposite sides of the rotational plane of the hub of said fan.

7. The fan of claim 1 wherein said angle between said leading portion and the plane of said arm is less than about 20* .

8. The fan of claim 7 wherein said angle between said leading portion and the plane of said arm is about 15* .

10. The fan of claim 9 including a separate reinforcing cap overlaying the convex side of each said blade structure, and wherein said members overlap between said reinforcing cap and said arm, and are secured therebetween with said trailing member sandwiched between said reinforcing cap and the overlapping portion of said leading member.