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US2609058A - Propeller fan construction - Google Patents

Propeller fan construction Download PDF

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Publication number
US2609058A
US2609058A US83702A US8370249A US2609058A US 2609058 A US2609058 A US 2609058A US 83702 A US83702 A US 83702A US 8370249 A US8370249 A US 8370249A US 2609058 A US2609058 A US 2609058A
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blade
hub
blades
stud
studs
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US83702A
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Charles I Place
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/34Blade mountings
    • F04D29/36Blade mountings adjustable

Definitions

  • This invention relates to axial flow or propeller type fans, and has reference more particularly,
  • Another object is to provide a propeller blade and hub structure of simple and sturdy construction, which may be readily shipped or transported in dis-assembled or so-called knockeddown condition such as to afford marked'savings in packaging and shipping costs, and which thereafter may be assembled in the field readily and easily by any one possessed of ordinary skill.
  • a further object is to provide a fan blade and hub structure of the character indicated, wherein the hub and blade parts are formed and adapted for assembly selectively such as to condition the'fan for either clockwise or counterclockwise operation, and "further, in which the blades may be readily reversed in assembly to the hub such that the normal leading edges thereof become the trailing edges in fan operation.
  • Fig. 1 is a view in front elevation, of an axial fiow fan constructed in accordance with the present invention
  • Fig. 2 is an on-edge view of the fan, showing one blade in assembly position, and indicating in broken lines an alternate position of the blade;
  • Fig. 3 is a plan view of a blade before assembly
  • Fig. 4 is an edge view of the blade of Fig. 3';
  • Fig. 5 is a detail view of one of the blade supporting and shaping elements or studs, showing a modification in the manner of blade support thereby; V v
  • Fig. 6 illustrates a modified form of blade-supporting stud
  • Fig. 7 illustrates in front elevation, an axial r fiowfan of a modified construction within the scope of the present invention
  • Fig. 8 is an on-edge view of the fan according to Fig. 7, showing but one blade assembled to the hub;
  • Fig. 9 is afragmentary sectional view transversely of the hub, asta'ken from line 9-9 in Fig. 8; I
  • Fig. 10 is an exploded view of the three-part 2 hub, with each part shown in longitudinal section;
  • Fig. 11 is a fragmentary longitudinal section of the hub in the embodiment of Fig. 8, showing one form of blade pitch adjustment device;
  • Fig. 12 illustrates in plan, a fan blade before assembly thereof in the structure of Fig. 7, and V Fig. 13 shows in plan greatly reduced, a pair of interconnected blades suitable for application to the fan embodiment of Fig. '7.
  • a blade-mounting hub i8 is provided of suitable rigid material, and is cast, pressed or otherwise formed such as to present a central or axial shaft-hub portion H, an annular flange or web [2 on portion H, and a cylindrical wall or rim portion It.
  • the least number of studs or finger elements necessary for effecting the desired blade pitch and shape is three studs for each blade, or a total of twelve for the present four-bladefan. These are relatively arranged about rim M such that in respect to eachblade (Fig. 2), one stud lid is centered longitudinally on the'rim, while a second stud I51) is near the end margin IQ of the rim and angularly. spaced from stud l5a by approximately degrees (circularly of the rim), and a third stud l5c is similarly spaced from stud 5a but on the opposite side thereof and near the opposite .endmargin 20 of the hub.
  • each set of studs each comprised -of studs l5a, I51: and I50, wherein the center studs 1.5a are relatively spaced about the rim H by ninety degrees or a right angle. Consequently, since in each set the studs I51) and 15a are spaced angularly by forty five degrees from and on oplongitudinally of the rim, with the stud I 0f the next adjacent set (Fig. 2). Moreover, in each set the studs I5b and I50 preferably project at least at a slight angle to the radial, outwardly in the direction of the adjacent end of the hub rim I4.
  • the blades I 8 are provided preferably in flat or planar form as illustrated by Figs 3 and 4, and are stamped, out or otherwise produced from suitable sheet material characterized by flexibility and a degree of resiliency affording in the blade, an appreciable spring-back tendency when the blade is flexed out of its planar form.
  • each blade has a relatively straight or rectilinear trailing edge or margin 22, and an arcuate or curved leading edge or margin 23 continuing smoothly into the blade peripheral edge 24.
  • the inner ends of the trailing and leading edges are rounded to mergence with the root edge 26 of the blade, the latter being arcuate or curved on a radius which may correspond substantially to the radius of the peripheral surface of hub rim I4.
  • Notch 2'Ia- is located substantially centrally intermediate the blade trailing and leading margins, while notch 21b is located relatively adjacent the blade trailing edge 22, and notch 21c relatively near the nose portion of the blade leading edge 23.
  • the shape of the notch in each instance is such as to accommodate and snugly receive therein a projecting portion of the head I6 on the associated stud in blade assembly to the hub.
  • the blade as thus formed presents opposite faces 28 and 30, one of which is the leading or fluid impelling face of the blade depending on the position of the blade in assembly, as will hereinafter appear.
  • each blade is flexed and disposed to seat its root margin 26 in edge-abutment with the surface of hub rim I4 in an angular course thereover as shown in Fig. 2, and such as to engage the blade in its root area, against the studs l5a, I5b and I50 in the alternate manner indicated.
  • blade-mounting is such as to locate root areas of the blade on its face 30, against the studs I5b and I5c, with portions of the heads I6 of the latter received in and through the blade notches 21b and 210 respectively, while a root portion of the blade on its opposite face 28, is engaged with the center stud I5a, with a portion of the head I6 thereof through the center notch 21a of the blade.
  • the blades as thus positioned present the faces 28 thereof for fluid displacement.
  • blade faces 28 are the leading faces, While the faces 30 constitute the trailing'faces.
  • Each blade being flexed into alternately opposed engagement with the studs as now described, is retained against the studs through the springback tension obtaining in the flexed condition of the blade. Further, the blade is held against shifting over the surface of rim I4 and also, against displacement outwardly or away from rim I4 as under the action of centrifugal force,
  • the pitch angle of each blade is determined in consequence of the extent of axial off-set of the studs I5b and I5c relative to the center stud I5a.
  • the studs of each set are positioned such that a curved line intersecting the axes of the studs I5b, I5a and IE0, intersects a transverse plane of the hub I0 containing the radial axis of stud I5a, at an angle approximating 30 degrees. Accordingly, the studs as so positioned, pitch the blade at about the same angle.
  • each blade may be determined as desired, by axially off-setting the studs I5b and I50 to a greater or less extent relative to the center stud I 511. It is to be noted additionally, that various blade shapes and pitch angles may be obtained by constructing the hub to have the studs of each set, particularly the studs I5b and I5c thereof, variously inclined from the radial in the same or opposite directions therefrom. Further, while blade mounting is here shown on a cylindrical surface (rim I4), it will be appreciated that the manner of blade mounting according to the present invention, may be applied effectively to hub surfaces of other forms, as full or semispherical surfaces, conical surfaces, arcuate or curved surfaces, and the like.
  • a more positive stud connection of the blades may be efiected in the manner illustrated in Fig. 5.
  • the stud head I6 may have the free terminal 3
  • any one or more of the studs I5a, I51) and I50 in each blade set may be so treated.
  • peening-over of the blade-engaging portions of the stud heads I6 affords a means for retaining pre-formed blades in assembly to the hub.
  • blades pre-formed to have a set pitch and shape in a normal unstressed condition may be applied and held by peening over the stud heads.
  • Fig. 6 illustrates a modification of the center stud I5a of each set in the hub structure according to Figs. -1 and 2.
  • a stud 32 having a center slot 34 to receive the blade.
  • the center notch, as 2711 may be eliminated in each of the blades.
  • the fan as noW described affords a greatly improved and simplified structure, having parts which may be readily and economically manufactured, and assembled easily-and quickly-withoutany necessity for blade shaping and other special assembling tools, the latter because the blades are pitched and shaped in consequence of their mounting on the hub against the studs. Further, by reason of the present improvements in the form and manner of assembly of the fan parts, these parts may be transported or shipped in so-called knocked-down condition, thereby permitting marked savings in packaging and shipping costs.
  • the blades v may be disposed selectively for clockwise or'counterclockwise rotation, or such as to secure various displacement characteristics.
  • the blades as shown by Figs. 1 and 2 are arranged for clockwise rotation.
  • To adapt the fanfor the reverse or counterclockwise rotation it is only necessary to turn each blade end-for-end, as from the blade position shown in Fig. v2, and then apply each such that it will appear according to the blade shown in broken lines in Fig. 2. Again, the normal leading edge of each blade may be made the trailing edge in fan rotation.
  • the fan structure includes a three-part hub assembly comprising a center section ii) and r oppositeend sections 4! and 52.
  • the center section ill is constituted by a tubular, shaft moune ting portion id having an axial bore 55 to receive the fan drive shaft (not shown), and providing centrally intermediate the ends of the portion 64, a plurality of radially outstanding fingers it which are the countereparts of the center fingers or studs its in the first described embodiment of Fig. 1.
  • the present example is in respect to a four-blade fan, hence the fingers is are four in number, equally spaced about the section 50.
  • Portion id is formed further, to provide splines ll externally over one end, and similar splines ls externally over the other. end on the opposite side of fingers it.
  • Hub end section fill is of cup-shape generally
  • the section further, has four fingers 52 equally spaced and inclined in outward projection therefrom, substantially as shown in Fig. 8. In the splined mounting of the section on the center section, it is so disposed as tolocate its fingers 52 intermediate the fingers 46 (Fig. '7) as at approximately 45 degrees to the latter. Fingers 52 are the counterparts of the studs. l5b in th structure of Fig. 1.
  • the remaining hub end section 42 is tubular in form, and like section M has internal splines 54 engaging the splines :38 on the center section 46, the end section further providing four equally spaced'fingers E5 inclined in outward projection therefrom.
  • Fingers 55 have an inclinationopp'o site tothat of the fingers 52, and in assembly of this section to the center section, are disposed intermediate the fingers 4d and such that they are in registry longitudinally of the hub, with the fingers 52.
  • Fingers 55 are the counterparts of the studs We in the embodiment of Fig. l.
  • the four blades 55 are identical, and are provided preferably in flat or planar form, each in accordance with the simple blade shownin plan View in Fig. 12, and in general outline, similar to the blade of Fig. 4, the blades further being produced from flexible, resilient sheet stool-z having a spring-back characteristic as before described in connection with the blades of Figs. land 3.
  • the blade shown has a relatively straight trailing margin 58, an arcuate or curved leading margin 59 and a relatively short arcuate root area 60, the latter having formed integrally therewith a hub mounting projection 52 providing a splined opening 63 for reception of the splined end 48 of the center hub section id in blade-hub assembly.
  • is engaged on the splined end 41 of the center section (it) such as to locate the fingers 52 inter: mediate the fingers 3.5.
  • a blade 58 is applied with its splined opening over the splined end 48 of the center section 48, and such that the blade centrally abuts a finger 46 and engages near its trailing end, against a finger 52 on the side of the latter facing the cup end 50 of the end section at (Fig. 8).
  • Each of the remaining blades is applied in the same manner, in equally spaced relation about the hub.
  • the other hub end section 42 is applied on the splined end 43 of the center section, and is pushed against the stacked blade hub elements or projections 62, with the fingers 55 in axial alignment with fingers s2 and individually engaging the blades near the leading edges thereof (Fig. 8).
  • the end section 42 is secured to the center section as as by a pin or set screw 64, it being noted that the set screw may project through the wall of the tubular portion M (Fig. 9) for fan securernent contact with the drive shaft (not shown) when the latter is received in the hub bore45.
  • each blade has a finger 46 against its central portion on the leading face so of the blade (as appears in Fig. 8), a finger 52 against the trailing blade face 61 near the trailing edge 58, and a finger 55 against the trailing blade face 6! near the leading edge 59.
  • the blade and fingers therefore, bear the same relationship as obtains with the blade and studs shown in Fig. 2. Accordingly, the blades are stressed into shape by the fingers, such as to have the desired pitch angle, determined by the relative axial spacing of the three fingers engaging each blade.
  • the splined end 41 of the center hub section id is formed to provide an end wall 10 having a threaded axial opening H therein. Threaded through opening H is the threaded end 12 of a stud 14, the stud presenting a washer-like flange 15 located between the end wall 10 and the end wall 59 of the hub section M.
  • the head end 78 of the stud is exposed through an opening 18 in end wall 50, and is provided with a slot '59 therein to receive a screwdriver orsimilar tool, for turning the stud.
  • Rotation of the stud in one direction will produce relative separating displacement of the hub sections 63 and 4
  • Such displacement in the separating direction thus increases the axial offset relation of the fingers 46 and 52, which thereby increases the curvature and pitch of the blades.
  • reverse rotation of the stud will have the opposite effect.
  • Fig'. 13 illustrates a pair of connected blades 82 and 83 which, with a like pair, may be employed in the modified embodiment instead of the four separate blades 56.
  • Each blade of the pair has a hub mounting extension 84 which is riveted or otherwise secured at its free end 86, to a root portion 81 of the opposite blade, the extensions of both blades being in overlying contact as indicated, and having the splined openings 88 thereof in registry.
  • Application of the paired blades to the hub structure is accomplished in the same manner as described for the single blades 56. It is to be noted that one advantage possessed by the paired blades over the single blade, is that the interconnection thereof in the root region, materially strengthens the blades against torsional stresses attending hub drive of the blades.
  • each of the three hub sections may be readily and economically produced, as by casting or pressing processes and the like.
  • a propeller fan shaft-mounting hub means, a plurality of fan blades each having leading and trailing margins, and blade-shaping elements for each blade, carried by and extending from said hub means, one of said elements engaging the blade on its trailing face adjacent the trailing margin'thereof, another element engaging the blade on its trailing face adjacent the leading margin thereof, and a third'element engaging the blade on its leading face intermediate the leading and trailing margins of the blade.
  • shaft-mounting hub means a plurality of fan blades each having leading and trailing margins, and blade-shaping elements for each blade, projecting from the hub means and relatively off-set axially of the hub, one of said elements engaging the blade on its trailing face adjacent the trailing margin thereof, another element engaging the trailing face of the blade adjacent the leading margin thereof, and a third element engaging the blade on its leading face intermediate the leading and trailing margins of the blade.
  • a propeller fan shaft-mounting hub means, a plurality of fan blades each having leading and trailing margins, blade-shaping elements carried by and extending outwardly from said hub means, said elements being' arranged in groups one for each blade, and the elements of each group being relatively off-set axially of the hub means such as to determine the pitch of the associated blade, one element of each group engaging its blade on the trailing face adjacent the trailing margin thereof, another element of each group engaging its blade on the trailing face adjacent the leading margin thereof, and a third element of each group engaging its blade on the leading face of the blade substantially centrally between the ends of the blade.
  • a hub assembly comprising hub-forming members in relative engagement, each having a plurality of blade-shaping finger elements projecting therefrom, and flexible blades arranged about the hub assembly in bladeshaping engagement with said finger elements such that the elements of one hub-forming member engage the blades near the trailing margins thereof, the elements of another of the hub-forming members engage the blades near the leading margins thereof, and the elements of a third one of the hub-forming members engage the blades substantially in the central portions thereof, the blades as so engaged by the shaping finger elements, being constrained by the elements to a curved configuration characterized by an effective pitch angle.
  • a hub assembly comprising coaxially related hub-forming members each having a plurality of blade-shaping finger elements projecting therefrom, said members being related in assembly such that one member thereof is capable of adjustment axially relative to the other members, fiexible blades carried by the hub assembly and arranged thereabout for bladeshaping engagement with said finger elements such that the elements of one hub-forming member engage the trailing faces of the blades near the trailing margins thereof, the elements of another of the hub-forming members engage the trailing faces of the blades near the leading margins thereof, and the elements of a third hubforming member engage the leading faces of the blades substantially in the central portions thereof, the blades as so.

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  • General Engineering & Computer Science (AREA)
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Description

Sept. 2, 1952 c, PLACE 2,609,058
PROPELLER FAN CONSTRUCTION Filed March 26, 1949 2 SHEETS-SHEET 1 INVENTOR CHARLES I. PLACE ATTORNEY p 1952 c. 1. PLACE I 2,609,058
PROPELLER FAN CONSTRUCTION Filed March 26, 1949 2 SHEETS-SHEET 2 INVENTOR 7 CHARLES 1. PLACE FIG. [3. ATTORNEY Patented Sept. 2, 1952 UNITED STATES PATENT @FFECE,
f PnornLLEn FAN oon'srnno'rion 7 Charles 1. Place, Norfolk, Conn. lipplicationldarch 26, 1949, Serial No. 83,702
' 6 Claims.
This invention relates to axial flow or propeller type fans, and has reference more particularly,
to improvements in the construction and manner of assembly of such fans.
The principal object of the present invention,
is to provide an axial flow type fan blade and hub structure which is characterized by a relatively simple construction affording economical manufacture of the blade and hub parts, and
wherein the parts are adapted for ready and quick assembly without requiring blade-shaping and other special assembling tools.
Another object is to provide a propeller blade and hub structure of simple and sturdy construction, which may be readily shipped or transported in dis-assembled or so-called knockeddown condition such as to afford marked'savings in packaging and shipping costs, and which thereafter may be assembled in the field readily and easily by any one possessed of ordinary skill.
A further object is to provide a fan blade and hub structure of the character indicated, wherein the hub and blade parts are formed and adapted for assembly selectively such as to condition the'fan for either clockwise or counterclockwise operation, and "further, in which the blades may be readily reversed in assembly to the hub such that the normal leading edges thereof become the trailing edges in fan operation.
These and numerous other objects and advantages of the present invention will appear from the following description of presently preferred embodiments thereof, as such are illustrated in the accompanying drawings, wherein:
i Fig. 1 is a view in front elevation, of an axial fiow fan constructed in accordance with the present invention; I
Fig. 2 is an on-edge view of the fan, showing one blade in assembly position, and indicating in broken lines an alternate position of the blade;
Fig. 3 is a plan view of a blade before assembly;
Fig. 4 is an edge view of the blade of Fig. 3';
Fig. 5 is a detail view of one of the blade supporting and shaping elements or studs, showing a modification in the manner of blade support thereby; V v
Fig. 6 illustrates a modified form of blade-supporting stud;
Fig. 7 illustrates in front elevation, an axial r fiowfan of a modified construction within the scope of the present invention;
i Fig. 8 is an on-edge view of the fan according to Fig. 7, showing but one blade assembled to the hub;
Fig. 9 is afragmentary sectional view transversely of the hub, asta'ken from line 9-9 in Fig. 8; I
Fig. 10 is an exploded view of the three-part 2 hub, with each part shown in longitudinal section;
Fig. 11 is a fragmentary longitudinal section of the hub in the embodiment of Fig. 8, showing one form of blade pitch adjustment device;
Fig. 12 illustrates in plan, a fan blade before assembly thereof in the structure of Fig. 7, and V Fig. 13 shows in plan greatly reduced, a pair of interconnected blades suitable for application to the fan embodiment of Fig. '7. With reference now to the form of the invention shownby Figs. 1 to 4, a blade-mounting hub i8 is provided of suitable rigid material, and is cast, pressed or otherwise formed such as to present a central or axial shaft-hub portion H, an annular flange or web [2 on portion H, and a cylindrical wall or rim portion It. Extending 'from the periphery of rim; l'are a plurality of to the rimi l in any suitable manner, as by threading or press-fitting in rim openings, or by welding to the rim. In the instance of a die-cast hub, these studs may be provided as integral portions, if desired. According to the present example, four blades 13 are shown, each by preference and for greater aerodynamic efficiency, being of a width approximatingor greater thanits radial dimension, such as to afford blade-overlap as appears in Fig. 1. The invention is applicable,
however, to fans of a greater or lesser number of blades, with or without blade-overlap.
In accordance with the present invention, the least number of studs or finger elements necessary for effecting the desired blade pitch and shape, is three studs for each blade, or a total of twelve for the present four-bladefan. These are relatively arranged about rim M such that in respect to eachblade (Fig. 2), one stud lid is centered longitudinally on the'rim, while a second stud I51) is near the end margin IQ of the rim and angularly. spaced from stud l5a by approximately degrees (circularly of the rim), and a third stud l5c is similarly spaced from stud 5a but on the opposite side thereof and near the opposite .endmargin 20 of the hub. Thus there are four sets of studs each comprised -of studs l5a, I51: and I50, wherein the center studs 1.5a are relatively spaced about the rim H by ninety degrees or a right angle. Consequently, since in each set the studs I51) and 15a are spaced angularly by forty five degrees from and on oplongitudinally of the rim, with the stud I 0f the next adjacent set (Fig. 2). Moreover, in each set the studs I5b and I50 preferably project at least at a slight angle to the radial, outwardly in the direction of the adjacent end of the hub rim I4.
The blades I 8 are provided preferably in flat or planar form as illustrated by Figs 3 and 4, and are stamped, out or otherwise produced from suitable sheet material characterized by flexibility and a degree of resiliency affording in the blade, an appreciable spring-back tendency when the blade is flexed out of its planar form. Preferably, each blade has a relatively straight or rectilinear trailing edge or margin 22, and an arcuate or curved leading edge or margin 23 continuing smoothly into the blade peripheral edge 24. The inner ends of the trailing and leading edges are rounded to mergence with the root edge 26 of the blade, the latter being arcuate or curved on a radius which may correspond substantially to the radius of the peripheral surface of hub rim I4. In the root region of the blade and spaced from the blade root edge 26 a distance equivalent to the height of the studs I5 on the rim I4, are a plurality of similar shaped openings or notches 27a, 21b and 210. Notch 2'Ia-is located substantially centrally intermediate the blade trailing and leading margins, while notch 21b is located relatively adjacent the blade trailing edge 22, and notch 21c relatively near the nose portion of the blade leading edge 23. The shape of the notch in each instance is such as to accommodate and snugly receive therein a projecting portion of the head I6 on the associated stud in blade assembly to the hub. The blade as thus formed, presents opposite faces 28 and 30, one of which is the leading or fluid impelling face of the blade depending on the position of the blade in assembly, as will hereinafter appear.
In assembling the blades to the hub I0, each blade is flexed and disposed to seat its root margin 26 in edge-abutment with the surface of hub rim I4 in an angular course thereover as shown in Fig. 2, and such as to engage the blade in its root area, against the studs l5a, I5b and I50 in the alternate manner indicated. More particularly, blade-mounting is such as to locate root areas of the blade on its face 30, against the studs I5b and I5c, with portions of the heads I6 of the latter received in and through the blade notches 21b and 210 respectively, while a root portion of the blade on its opposite face 28, is engaged with the center stud I5a, with a portion of the head I6 thereof through the center notch 21a of the blade. The blades as thus positioned, present the faces 28 thereof for fluid displacement. Hence, blade faces 28 are the leading faces, While the faces 30 constitute the trailing'faces. Each blade being flexed into alternately opposed engagement with the studs as now described, is retained against the studs through the springback tension obtaining in the flexed condition of the blade. Further, the blade is held against shifting over the surface of rim I4 and also, against displacement outwardly or away from rim I4 as under the action of centrifugal force,
- by the stud heads I6 engaged through the blade notches. Thus the blades are supported and shaped by the studs for effective'fluid displacement in fan operation.
In stud-shaping of the blades, the pitch angle of each blade is determined in consequence of the extent of axial off-set of the studs I5b and I5c relative to the center stud I5a. Forexample, in the-present embodiment the studs of each set are positioned such that a curved line intersecting the axes of the studs I5b, I5a and IE0, intersects a transverse plane of the hub I0 containing the radial axis of stud I5a, at an angle approximating 30 degrees. Accordingly, the studs as so positioned, pitch the blade at about the same angle. From the foregoing, it will appear then that the pitch angle and shaping of each blade may be determined as desired, by axially off-setting the studs I5b and I50 to a greater or less extent relative to the center stud I 511. It is to be noted additionally, that various blade shapes and pitch angles may be obtained by constructing the hub to have the studs of each set, particularly the studs I5b and I5c thereof, variously inclined from the radial in the same or opposite directions therefrom. Further, while blade mounting is here shown on a cylindrical surface (rim I4), it will be appreciated that the manner of blade mounting according to the present invention, may be applied effectively to hub surfaces of other forms, as full or semispherical surfaces, conical surfaces, arcuate or curved surfaces, and the like.
Although resilient blades having an appreciable spring-back force when flexed from the normal unstressed conditions thereof, will remain in stud-efiected assembly to the hub under normal fan usage, a more positive stud connection of the blades may be efiected in the manner illustrated in Fig. 5. As there shown, the stud head I6 may have the free terminal 3| of the portion projecting through a notch of the associated blade, turned or peened-over against the blade such as to clamp the blade against the stud. Thus, any one or more of the studs I5a, I51) and I50 in each blade set, may be so treated. Moreover and importantly to the present improvements, peening-over of the blade-engaging portions of the stud heads I6 affords a means for retaining pre-formed blades in assembly to the hub. Thus, in place of the flat blades stressed by flexure into position against the studs and held thereagainst by the pring-back force of the flexed blades, blades pre-formed to have a set pitch and shape in a normal unstressed condition, may be applied and held by peening over the stud heads.
Fig. 6 illustrates a modification of the center stud I5a of each set in the hub structure according to Figs. -1 and 2. Instead of the headed stud I5a, there may be employed a stud 32 having a center slot 34 to receive the blade. By use of the slotted stud, the center notch, as 2711 may be eliminated in each of the blades.
The fan as noW described, affords a greatly improved and simplified structure, having parts which may be readily and economically manufactured, and assembled easily-and quickly-withoutany necessity for blade shaping and other special assembling tools, the latter because the blades are pitched and shaped in consequence of their mounting on the hub against the studs. Further, by reason of the present improvements in the form and manner of assembly of the fan parts, these parts may be transported or shipped in so-called knocked-down condition, thereby permitting marked savings in packaging and shipping costs. Moreover, it will appear now that by reason of the regular order of stud disposition about the hub rim I4, and the manner of blade assembly by blade-flexure into supporting and shaping engagement with the studs, the blades vmay be disposed selectively for clockwise or'counterclockwise rotation, or such as to secure various displacement characteristics. The blades as shown by Figs. 1 and 2, are arranged for clockwise rotation. To adapt the fanfor the reverse or counterclockwise rotation, it is only necessary to turn each blade end-for-end, as from the blade position shown in Fig. v2, and then apply each such that it will appear according to the blade shown in broken lines in Fig. 2. Again, the normal leading edge of each blade may be made the trailing edge in fan rotation. For example and considering the blade shown in solid lines in Fig. 2, this may be accomplished by end-for-end reversal of the blade shown, and then applying it to the same studs, so'that the blade slot or notch Zlc (at the normal leading end of the blade) receives the head of stud 552:, while the blade notch 2% receives the head of stud l5c, and the center notch 27a receives the head of center stud lea. exactly as before. In clockwise rotation of the fan then, the normal trailing edge of the blade becomes the leading edge, with consequent alteration of the fan displacement characteristic. Still other dispositions of the blades are apparent, so that it will be now appreciated that the present fan structure is readily and easily adaptable to different assembly relationships of the hub and blades, usingthe same parts in each case.
Another embodiment of the present invention is illustrated by Figs. 7 through 12. As therein appears, the fan structure includes a three-part hub assembly comprising a center section ii) and r oppositeend sections 4! and 52. The center section ill is constituted by a tubular, shaft moune ting portion id having an axial bore 55 to receive the fan drive shaft (not shown), and providing centrally intermediate the ends of the portion 64, a plurality of radially outstanding fingers it which are the countereparts of the center fingers or studs its in the first described embodiment of Fig. 1. The present example is in respect to a four-blade fan, hence the fingers is are four in number, equally spaced about the section 50. Portion id is formed further, to provide splines ll externally over one end, and similar splines ls externally over the other. end on the opposite side of fingers it.
Hub end section fill is of cup-shape generally,
providing an end wall so and having internal splines 5! for relative engagement with splines Lil of the central section, in reception of the section it thereon. The section further, has four fingers 52 equally spaced and inclined in outward projection therefrom, substantially as shown in Fig. 8. In the splined mounting of the section on the center section, it is so disposed as tolocate its fingers 52 intermediate the fingers 46 (Fig. '7) as at approximately 45 degrees to the latter. Fingers 52 are the counterparts of the studs. l5b in th structure of Fig. 1.
The remaining hub end section 42 is tubular in form, and like section M has internal splines 54 engaging the splines :38 on the center section 46, the end section further providing four equally spaced'fingers E5 inclined in outward projection therefrom. Fingers 55 have an inclinationopp'o site tothat of the fingers 52, and in assembly of this section to the center section, are disposed intermediate the fingers 4d and such that they are in registry longitudinally of the hub, with the fingers 52. Fingers 55 are the counterparts of the studs We in the embodiment of Fig. l.
The four blades 55 are identical, and are provided preferably in flat or planar form, each in accordance with the simple blade shownin plan View in Fig. 12, and in general outline, similar to the blade of Fig. 4, the blades further being produced from flexible, resilient sheet stool-z having a spring-back characteristic as before described in connection with the blades of Figs. land 3. The blade shown has a relatively straight trailing margin 58, an arcuate or curved leading margin 59 and a relatively short arcuate root area 60, the latter having formed integrally therewith a hub mounting projection 52 providing a splined opening 63 for reception of the splined end 48 of the center hub section id in blade-hub assembly.
Assembly of the hub and blade parts of the modified structure, is readily accomplished in the following manner: The hub end section 4| is engaged on the splined end 41 of the center section (it) such as to locate the fingers 52 inter: mediate the fingers 3.5. Then a blade 58 is applied with its splined opening over the splined end 48 of the center section 48, and such that the blade centrally abuts a finger 46 and engages near its trailing end, against a finger 52 on the side of the latter facing the cup end 50 of the end section at (Fig. 8). Each of the remaining blades is applied in the same manner, in equally spaced relation about the hub. Whereupon, the other hub end section 42 is applied on the splined end 43 of the center section, and is pushed against the stacked blade hub elements or projections 62, with the fingers 55 in axial alignment with fingers s2 and individually engaging the blades near the leading edges thereof (Fig. 8). In final assembly, the end section 42 is secured to the center section as as by a pin or set screw 64, it being noted that the set screw may project through the wall of the tubular portion M (Fig. 9) for fan securernent contact with the drive shaft (not shown) when the latter is received in the hub bore45.
In fan assembly as thus described, each blade has a finger 46 against its central portion on the leading face so of the blade (as appears in Fig. 8), a finger 52 against the trailing blade face 61 near the trailing edge 58, and a finger 55 against the trailing blade face 6! near the leading edge 59. The blade and fingers therefore, bear the same relationship as obtains with the blade and studs shown in Fig. 2. Accordingly, the blades are stressed into shape by the fingers, such as to have the desired pitch angle, determined by the relative axial spacing of the three fingers engaging each blade.
Provision is here made as shown in Fig. 8, for permitting adjustment of blade form and pitch after assembly of the parts. The splined end 41 of the center hub section id is formed to provide an end wall 10 having a threaded axial opening H therein. Threaded through opening H is the threaded end 12 of a stud 14, the stud presenting a washer-like flange 15 located between the end wall 10 and the end wall 59 of the hub section M. The head end 78 of the stud is exposed through an opening 18 in end wall 50, and is provided with a slot '59 therein to receive a screwdriver orsimilar tool, for turning the stud. Rotation of the stud in one direction will produce relative separating displacement of the hub sections 63 and 4|, this because the sections are splined together and hence, cannot have relative rotation. Such displacement in the separating direction thus increases the axial offset relation of the fingers 46 and 52, which thereby increases the curvature and pitch of the blades. On the other hand, reverse rotation of the stud will have the opposite effect.
Although the above described provision for selective adjustment of blade shape and pitch is presently preferred, it will be appreciated that adjustments may be made by the use of one or more spacer elements between the sections 40 and M, as the elements or discs 80 shown in Fig. 11. I
Fig'. 13 illustrates a pair of connected blades 82 and 83 which, with a like pair, may be employed in the modified embodiment instead of the four separate blades 56. Each blade of the pair has a hub mounting extension 84 which is riveted or otherwise secured at its free end 86, to a root portion 81 of the opposite blade, the extensions of both blades being in overlying contact as indicated, and having the splined openings 88 thereof in registry. Application of the paired blades to the hub structure is accomplished in the same manner as described for the single blades 56. It is to be noted that one advantage possessed by the paired blades over the single blade, is that the interconnection thereof in the root region, materially strengthens the blades against torsional stresses attending hub drive of the blades.
The now described modified embodiment of the invention is subject to the selectivity of blade mounting and other advantages as hereinbefore expressed in connection with the embodiment of Fig. 1, it being noted further, that each of the three hub sections may be readily and economically produced, as by casting or pressing processes and the like.
Having now described and illustrated presently preferred embodiments of the invention, it is to be understood that various alterations and modifications in addition to those herein expressed, may be made without departing from the spirit and full intended scope of the invention as defined by the appended claims.
I claim:
1. In a propeller fan, shaft-mounting hub means, a plurality of fan blades each having leading and trailing margins, and blade-shaping elements for each blade, carried by and extending from said hub means, one of said elements engaging the blade on its trailing face adjacent the trailing margin'thereof, another element engaging the blade on its trailing face adjacent the leading margin thereof, and a third'element engaging the blade on its leading face intermediate the leading and trailing margins of the blade.
2. In a propeller fan, shaft-mounting hub means, a plurality of fan blades each having leading and trailing margins, and blade-shaping elements for each blade, projecting from the hub means and relatively off-set axially of the hub, one of said elements engaging the blade on its trailing face adjacent the trailing margin thereof, another element engaging the trailing face of the blade adjacent the leading margin thereof, and a third element engaging the blade on its leading face intermediate the leading and trailing margins of the blade.
3. In a propeller fan, shaft-mounting hub means, a plurality of fan blades each having leading and trailing margins, blade-shaping elements carried by and extending outwardly from said hub means, said elements being' arranged in groups one for each blade, and the elements of each group being relatively off-set axially of the hub means such as to determine the pitch of the associated blade, one element of each group engaging its blade on the trailing face adjacent the trailing margin thereof, another element of each group engaging its blade on the trailing face adjacent the leading margin thereof, and a third element of each group engaging its blade on the leading face of the blade substantially centrally between the ends of the blade.
4. In a propeller fan, a hub assembly comprising hub-forming members in relative engagement, each having a plurality of blade-shaping finger elements projecting therefrom, and flexible blades arranged about the hub assembly in bladeshaping engagement with said finger elements such that the elements of one hub-forming member engage the blades near the trailing margins thereof, the elements of another of the hub-forming members engage the blades near the leading margins thereof, and the elements of a third one of the hub-forming members engage the blades substantially in the central portions thereof, the blades as so engaged by the shaping finger elements, being constrained by the elements to a curved configuration characterized by an effective pitch angle.
5. A propeller fan according to claim 4 wherein said flexible blades include hub portions integral therewith, in driven connection with at least one of the hub-forming members.
6. In a propeller fan, a hub assembly comprising coaxially related hub-forming members each having a plurality of blade-shaping finger elements projecting therefrom, said members being related in assembly such that one member thereof is capable of adjustment axially relative to the other members, fiexible blades carried by the hub assembly and arranged thereabout for bladeshaping engagement with said finger elements such that the elements of one hub-forming member engage the trailing faces of the blades near the trailing margins thereof, the elements of another of the hub-forming members engage the trailing faces of the blades near the leading margins thereof, and the elements of a third hubforming member engage the leading faces of the blades substantially in the central portions thereof, the blades as so. engaged by the finger elements, being constrained by the elements to a curved configuration, and means disposed between and operatively interconnecting the said axially adjustable hub-forming member and one of the other said hub-forming members for effecting axial adjustment of said adjustable member relative to the other members, whereby to vary the curved configuration of the blades.
CHARLES I. PLACE.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 157,742 Dowler Dec. 15, 1874 559,775 French May 5, 1896 705,046 Davidson July 22, 1902 1,096,079 Viall May 12, 1914 1,260,562 McIntosh Mar. 26, 1918 1,307,106 Armstrong June 17, 1919 1,411,644 Schmidt Apr. 4, 1922 2,234,319 Preston Mar. 11, 1941 2,270,575 Bahr Jan. 20, 1942 2,292,115 Frisbie Aug. 4, 1942 2,321,143 Horton June 8, 1943 FOREIGN PATENTS Number Country Date 823,447 France Oct. 18, 1937
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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE930340C (en) * 1953-06-06 1955-07-14 Siemens Ag Impeller for table fans u. like
US4474534A (en) * 1982-05-17 1984-10-02 General Dynamics Corp. Axial flow fan
US4515511A (en) * 1982-12-31 1985-05-07 Siemens Aktiengesellschaft Axial fan with blades that automatically adjust to the direction of rotation
US4545728A (en) * 1983-08-30 1985-10-08 Cheney Jr Marvin C Wind turbine generator with improved operating subassemblies
US20080210102A1 (en) * 2006-08-02 2008-09-04 Jiri Rabas Removable blower for convection oven
US8402680B2 (en) 2010-10-29 2013-03-26 Briggs & Stratton Corporation Snow thrower impeller
US9279222B2 (en) 2010-10-29 2016-03-08 Briggs & Stratton Corporation Snow thrower impeller

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US1411644A (en) * 1920-04-29 1922-04-04 Rudolph F Schmidt Adjustable metallic air propeller
FR823447A (en) * 1936-10-02 1938-01-20 Sev Marchal Improvements to blower fans on windshield glass
US2234319A (en) * 1936-10-03 1941-03-11 Chicago Electric Mfg Co Fan blade and hub assembly
US2270575A (en) * 1938-05-25 1942-01-20 Casco Products Corp Fan
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US157742A (en) * 1874-12-15 Improvement in propeller-wheels
US559775A (en) * 1896-05-05 Propeller
US1307106A (en) * 1919-06-17 Strong
US705046A (en) * 1901-04-06 1902-07-22 Samuel Cleland Davidson Rotary propeller-fan and propeller for ships.
US1096079A (en) * 1912-03-18 1914-05-12 William G Viall Fan-wheel.
US1260562A (en) * 1917-04-07 1918-03-26 John G Heal Fan construction.
US1411644A (en) * 1920-04-29 1922-04-04 Rudolph F Schmidt Adjustable metallic air propeller
FR823447A (en) * 1936-10-02 1938-01-20 Sev Marchal Improvements to blower fans on windshield glass
US2234319A (en) * 1936-10-03 1941-03-11 Chicago Electric Mfg Co Fan blade and hub assembly
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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE930340C (en) * 1953-06-06 1955-07-14 Siemens Ag Impeller for table fans u. like
US4474534A (en) * 1982-05-17 1984-10-02 General Dynamics Corp. Axial flow fan
US4515511A (en) * 1982-12-31 1985-05-07 Siemens Aktiengesellschaft Axial fan with blades that automatically adjust to the direction of rotation
US4545728A (en) * 1983-08-30 1985-10-08 Cheney Jr Marvin C Wind turbine generator with improved operating subassemblies
US20080210102A1 (en) * 2006-08-02 2008-09-04 Jiri Rabas Removable blower for convection oven
US7793586B2 (en) * 2006-08-02 2010-09-14 G.S. Blodgett Corp. Removable blower for convection oven
US8402680B2 (en) 2010-10-29 2013-03-26 Briggs & Stratton Corporation Snow thrower impeller
US9279222B2 (en) 2010-10-29 2016-03-08 Briggs & Stratton Corporation Snow thrower impeller

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