US2022417A - Air impeller - Google Patents

Description

Nov. 26, 1935. A. c; GILBERT ET'YAL 2,022,417

AIR IMPELISER Filed Feb. 12, 1935 2 Sheets-Sheet 1 I OV- 3 A. GILBERT- r AL 7 12,022,417

AIR 'IMPELLER Filed Feb. 12, 1935 2 Sheets-Sheet 2 Patented Nov. 26, 1935 PATENT OFFICE Am' IMPELLER,

Alfred 0. Gilbert, Hamden,

Haven, Conn., assignors to The A. 0. Gilbert Company, New Haven, Conn,

Maryland RElSSUED All, 7 1940 and John Lanz, New

a corporation of Application'February 12, 1935, Serial No. 6,156

22 Claims. (.01. 230-259) This invention relates to fan rotors including air impelling blades and to methods of forming and constructing the same.

One object of the invention is to provide an air impeller, with blades of a type adapted to be carried by a dome shaped hub of relatively large a diameter in proportion to the overall size of the impeller.

Another object is to provide a geometrical scheme forconstructing fan blades ina variety of sizes, each size characterized by common principles of outline and surface curvature which curvature may conform advantageously to the surface of a cone.

A further object is to mount a blade or blades of substantially conical curvature in such relation to a hub of dome, or bullet-nose, shape that the air impeller thus formed may efficiently generate a stream of air for ventilating purposes or the like with minimum vibration and noise and with maximum displacement of air at relatively low rotative speeds.

A further object isto' so shape the fan blade in outline that its edges-shall cooperate with the surface curvature to produce the above results.

A further object is to provide a fan blade of thin sheet-like material so flexed and conformed that such material shall oifer a maximum resistance to accidental disturbance or distortion of its designed surface curvature during fabrication and use, without resort to external stiffening expedients. A related object is to provide a blade of this nature and having a large area of working surface with such geometrical curvature that it shall vibrate to a minimum extent in response to forces acting against it when it is rapidly revolved for displacing air.

'A still further object is to so correlate the shape and position of the entering edge of one fan blade to the shape and position of the trailing edge of an adjacent blade that the two blades may cooperate in their combined effect upon the air to producethe desired results when operated as a fan.

A still further object is to so shape and mount sheet-metal fan blades in relation to a hollow hub that a projecting portion of the blade may extend through a perforation in the wall of the hub to assist in g on the hub or to act upon the air inside the hub in a way to agitate or displace the same. The last mentioned action may serve to cool an electric motor if located partial'y or fully within the hub to serve as power unit for driving the impeller.

Further objects will appear from the following description and appended drawings, wherein:-

Fig. 1 is a view of our improved air impeller in rear elevation looking at the open end of its hollow hub. The hubis shown as carrying four fan blades shaped and mounted thereon in accordance with the principles, of these improvements.

Fig. 2 is a view of the impeller in side elevation looking from the right at Fig. 1.

Fig. 3 is another view of the impeller in side elevation looking at Fig. 1 in the direction of the arrow 3 in Fig. 1.

Fig. 4 is a perspective at the front of the impeller of Fig. 1.

Fig. 5 shows suitable shapes for blanks of different sizes from which fan blades for impellers of respectively different overall diameters may be constructed in accordance with the principles of these improvements.

Fig. 6 indicates diagrammatically the side elevation of a cone to respectively different portions of whose curved surface the blanks of Fig. 5 are shown to be conformed.

Fig. '7 indicates diagrammatically the relationvlew looking diagonally ship in which the large and small blades of Fig. 6

may be assembled to their respective hubs.

Fig. 8 is a view taken on the section plane 8-8 through the larger blade of Fig. '7 looking in the direction of the arrows and showing the hub for the larger blade partly in section on a central vertical plane better to expose the interior parts.

Fig. 9 is an enlarged view of the construction by which the interior mounting nipple is se- 'cured to the nose of the hub.

Fig. 10 is a fragmentary section on the plane l0--l0 in Fig. 3 showingan edgewise view of the interior air impelling fin.

Because of the complex action and reaction of eddies, vacuum effects and other unpredictable characteristics of air behavior when air is forcibly displaced by revolving impeller blades, the determination of the actual effect upon the air which will result from varying the shape, size, contour, and positional disposition:of such blades relative to their axis of rotation is usually empirical. But there are certain structural characteristics which we have discovered a fan blade should possess for purposes of strength, economy and uniformity in manufacture. It has heretofore been proposed .to make fan blades of many varieties as to size, shape, conformation and numher, and to mount such bladesin various dispositi ns relative to their axis of rotation to form an impeller. The present improvements are in part directed to manufacturing considerations and they involve a novel geometrical system as a basis for producing satisfactorily operating blades in a variety of sizes peculiarly adapted for mounting upon a hollow dome-shaped hub of relatively large diameter in comparison to the overall size of the impeller.

Hubs of this type are particularly advantageous in their ability to partially or fully surround and enclose the stator and the rotor of the electric motor employed to motivate the impeller whereby compactness and greater beauty of the fan as a whole is afforded. Such hubs are obviously required to support carried blades on a larger circumference in relation to the overall diameter of the fan than would otherwise be the case and the annular space available for the working surfaces of the blades is of less radial extent than would otherwise be'the case in a fan of given overall diameter. For a given amount of air displacement the area of the working surface of the blade is consequently made larger than in the older types of fans and the problem arises of providing blades of the characteristics indicated which shall have maximum strength and minimum weight. Hence it is undesirable to resort to supporting brackets and castings to supply the desirable rigidity to the blade which, itself,

is preferably made of thin sheet material.

It is well known that sheet material flexed to conform to the surface of a cone possesses by virtue of that conformity a peculiar resistance to change of its surface curvature. It is further true of the characteristics of conical curvature that such curvature lends itself to a scooping effect which is the natural action of a fan blade. The curvature of a conical surface is otherwise adapted to join in a desirable manner with a hub of bullet-nose shape and so far as we are aware, these facts have not heretofore been recognized as expedient of application in the forming of blades for a fan.

Several advantages obtainable through the use of conical curvature in contrast to cylindrical curvature or planar disposition of blade surfaces will be apparent from the accompanying illustrations showing-practical applications of the conical principle in shaping fan blades.

Fig. 6 indicates diagrammatically a typical cone II which may be employed as a form against whose surface the flat blank of a fan blade l0- may be pressed to cause the sheet-metal of the blade to assume a curvature according with that of the cone. The converging straight lines, two of which are designated respectively as I! and I3, represent straight lines separated by equal angles extending on the surface of the cone from its apex to its base. Such lines are known to the science of solid geometry as elements. Fig. 6

represents all of these elementsas they would ap pear in a side elevation of the cone I I. The same elements appear in Fig. 5 as they would be related in a development of the surface of cone- I I. Parallel spaced broken lines, including the line M-M and the line m--m, represent circumferential lines drawn on the surface of the cone in respectively spaced planes perpendicular to the axis of the cone or parallel to its base, and which broken lines therefore appear as straight lines in Fig. 6 but in Fig. 5 appear as arcs struck from the apex of the cone at radii equal to the'distance from the apex of the cone to-the point where each corresponding broken line in Fig. 6 intersects the sloping edge of the cone. Hence the true shape of the blade, whose developed view is shown in Fig. 5, appears distorted or foreshortened as viewed in Fig. 6. The line R-R in both of Figs. 5 and 6 indicates approximately the direction of a radial line which would pass through the axis about which the blade is designed to revolve. Auxiliary air fanning projections l4 and a fastening tongue l5 are afforded by the shape to which the blade is blanked, as is also the fastening flange I6 pierced to accommodate holding rivets or screws ll.

The manner in which the fan blade l9 may be mounted upon a hub I8 will be plain from Figs. 1, 7, and 8 in which the hub is shown to be hollow and possessing a relatively thin wall contoured somewhat like a dome or the nose of a bullet. The holding screws Il may penetrate both the flange l6 of the blade and the wall of hub l8, and are retained by nuts I!) located inside the hub. Screws H and nuts l9 may be replaced by rivets, or the blade at this point may be spot welded to the metal of the hub or may have tongues penetrating through apertures in the hub wall to be twisted, bent over, or otherwise secured against the interior surface of the wall as alternative means for holding the blade on the hub. The pliant ear l5 projects through an aperture in the hub wall and is twisted close to the interior surface of said wall and into angular relationship to the lengthwise direction of the slot. This twisted distortion of ear l5 draws and holds the blade l0 firmly against the outer surface of the hub wall and also enables the ear l5 to be readily redrawn by the simple expedient of twisting ear l5 back into its original longitudinal alignment with the slot, in case it is desired to remove or replace a defective blade. Such twisting of ear l5 may be repeated without danger 'to the surface of the hub against which they abut.

Fig. 7 shows diagrammatically that the blade I0 may be so positioned'on the hub l8 that the conical surface to which it conforms falls approximately tangent to a plane perpendicular to the axis A--A of rotation of the hub at approximately its entering end E. This condition alone serves to determine the disposition of the rest of the blade relative to the hub l8 whose axis appears at A-A and some departure from this disposition is possible depending upon the air impelling performance desired. For instance, the entering end E of the blade may be inclined as indicated by broken line position E in Fig. 7 if it is desired to scoop a greater volume of air. For this purpose blade I0 may, or need not, depart slightly in this end portion from the conical curvature to which as a whole the blade substantially conforms.

In each of Figs. 5, 6, and 7 in addition to the blade l0 there is shown a smaller blade l0 de signed to be conformed to a different portion of the curved surface of the forming cone H. Fig. '7 further shows a second hub I8 which may be of diameter and. contour similar to the hub l8 but is shown as shorter along its axis and somewhat differently positioned with respect to the smaller blade' l0 than is the hub l8 with respect to-the larger blade III.

From these two examples of different sized blades there will be apparent the geometrical scheme of these improvements upon which may be built a wide variety of blades for impellers, all

possessing certain structural characteristics novel with this invention.

Fig. 7 is a view looking at the blades in a direction defined by the fact that the line element l3 of the forming cone l l is so disposed that it is exactly endwise to the eyes of the observer so that it appears as a point, instead of as a line. This point consequently is coincident with the apex of the cone since all elements of the cone pass through the apex of the cone.

Also in Fig. '7 if the bottom edge of hub It or I8 appeared as a straight line a relationship of blade to hub would be indicated wherein the curved surface of its conical form along the element l3 would be tangent to a plane perpendicular to the axis of rotation A-A. While this is a practical relationship for some types of fan performance it serves to check the centrifugal escape of air radially outward past the peripheral edge of the blade if the hub as appearing in Fig.

7 be slightly inclined in the direction indicated by the fact that its edges atv the open end appear as an ellipse.

Increasing such inclination will increase the degree of angle X in Fig. 8 which indicates the forward divergence of the blade from planes such as S--S truly perpendicular to the axis of rotation A-A. Within certain limits, more volume of air will be forced into the impeller generated stream as the angle X at various circumferential points in the blade is increased.

Another way of defining a suitable relation ship. of the blades to the hub is to note that if the converging straight lines in Fig. 5 which represent the'elements of the cone, nearest to element 12 at the left thereof, were shown as they would appear in Fig. 1, those of the said elements which are most nearly central of the length of the blade from entering end E to trailing end T would fall in approximately tangential relationship to the outer circumference of the hub I8 or l8. And this relationship is true of both the larger blade I!) and the smaller blade While a variety of sizes and shapes oi conical forms may be used to determine the surface curvature of blades and the inclination thereof relative to a hub all constructed in accordance with the invention, a helpful guide to worlrable specifications for such forms may be had from the actual proportions illustrated in Figs. 5, 6, and 7. The larger blade III measuring, say, six inches from entering end E to trailing end T as viewed in Fig. 1, and designed to be carried by a hub of approximately four inches diameter to comprise an impeller having an outside diameter of between eleven and twelve inches may be conformed to a cone whose line elements form an angle of forty-five degrees with its base, and

in the positional relation to such cone indicated in Fig. 6 wherein the diameter of the cone in the plane M--M may be, say, twelve inches or approximately equal to the diameter of the complete impeller. Likewise'the small blade H) designed for use with the same hub may be curved to conform to a difi'erent portion of the same cone wherein the cone diameter in the plane m-m is nine inches or again approximately equal -to the overall diameter of the complete impeller of smaller size if constructed by assembling the smaller blade to the shorter hub l8.

The outline of each of blades ill in Fig. 1 indicates that the peripheral edge of the blade as thus viewed may conform practically to a true circumferential are 0-0 (struck from the axis of rotation) in that portion of the edge extending from a radial line R-R (approximately bisecting the blade) forwardly to near the enter.- ing end E of the blade.

Also as extending toward the trailing end '1 of 5 the blade from its radial line R-R the outer edge of the blade is seen to decrease in radial distance from the axis, continuously and with increasing abruptness until it meets the hub. While the bladeoutline may be varied within the scope l0 of this invention, the outline as shown is found hub l8. This results in the convex entering edge E and the convex trailing edge T both sweeping 25 backwardly (with respect to the direction of rotation of the impeller) as they extend to join the hub. Arrows D indicate the direction of rotation of the impeller inall figures of the drawings.

The relationship of adjacent blades is further 330 seen to be such that all points on the entering edge of one blade and'all points on the trailing edge of the blade rotatively ahead of same and adjacent thereto, fallen opposite sides of a plane parallel to the axis A-A if such imaginary plane 35 be passed between the blades without touching either of them. In other words, adjacent blades as viewed in Fig. 1 are circumferentially spaced at all points and do not overlap-at any point, although many of the aspects of theseimprovements are not concerned with whether or not adjacent blades overlap as viewed in Fig. l.

While the blades of the impeller as here shown are four in number, the principles of these improvements may apply to impellers having a difhave outlines differing from that herein de- 9 scribed to illustrate the invention.

Attention is called to the purpose of the projections I4 best shown in Figs. 1 and 10 as protruding through separate apertures. in the wall of hub l8 to serve as air impelling fins interior 55 of the hub. It has been mentioned hereinbefore that the space within the hollow hub may be cccupied by the body of an electric motor, and the hub may be supported and rotated by the rotor of such motor by means of its mounting nipple 60 20 having the socket 2| and set screw 22 for securing the same upon the rotor shaft. A motor body so located within hub l8 will be appreciably cooled by the fanning action of the projecting fins I l operating in what otherwise would'be a washer 26 against which the shoulder 25 may be peaned over all around by a suitable swaging tool thus securing together in accurately directed alignment the hub l8 and the nipple 20 with great strength and rigidity. The peaned over portion of shoulder 25 is indicated at 21 in Figs. 1 and 9. In Fig. 8 the wall of hub I8 is shown to have the aperture 28 to receive the shank of a screw driver used for tightening and loosening the set screw 22. Because this set screw islocated substantially as far back of the nose of the hub as is located the front portions of the blades !0, the screw driver aperture 28 may be located correspondingly far back to render it less conspicuous because of its closeness to the blades, and also when so located, the set screw exerts 'its fastening pressure at a point nearer the center of gravity of the impeller as a whole which tends to lessen stresses and danger of vibration at high speeds of rotation.

We claim:

1. An air impeller comprising in combination, a dome-shaped hub and more than one sheetlike blade each blade being flexed to conform substantially with the curved surface of a cone and so mounted on said hub that an element of the cone which passes through a portion of the blade near its entering end lies in a plane substantially parallel with a plane containing the axis of rotation of the hub.

2. An air impeller comprising in combination, a dome-shaped hub and more than one sheetlike blade each blade being flexed to conform substantially with the curved surface of a cone and so mounted on said hub that an element of the cone which passes through a portion of the blade near its entering end lies in 'a plane substantially parallel with a plane containing the axis of rotation of the hub, but displaced therefrom a distance approximately equal to half the overall length of the blade from its entering end to its trailing end and in the direction of movement of the blade.

3. An air impeller as described in claim 1 in which the blade is so mounted on the hub that the said element of the cone inclines toward the front of the hub with respect to a plane perpendicular to the axis of the hub passing through the innermost edge of the blade which is closest to the hub.

4. An air impeller comprising in combination, a dome-shaped hub and more than one blade of conical curvature mounted thereon, each of said blades having an edge conforming near the entering end of the blade to an arc struck from the axis of rotation and having an edge comprising the trailing end of the blade of diminish bullet-nose shape apertured at its nose portion and having its wall depressed to form a recess around the aperture in said portion, a mounting nipple having a head portion seated in said recess and a shank portion integral with said head portion and protruding through the aperture in alignment with the axis of the hub for rotatively supporting the latter.

6. In fan rotor construction a hollow hub of bullet-nose shape having an aperture in its nose portion and having its wall depressed to form a recess around the aperture, a mounting nipple having a head portion shaped to seat in and fill said recess and having a shank portion integral with said head portion and protruding through the aperture to the inside of the hub, and means inside the hub to rigidly secure the mounting nipple to the hub.

7. In fan rotor'construction a hollow hub of 5 bullet-nose shape having an aperture through the wall of its nose portion, a shouldered mounting nipple projecting inwardly of the hub through said aperture and having a head exterior to the wall of the'hub of larger diameter 10 than the aperture, a washer surrounding the shouldered portion of the nipple interior of the hub wall and means comprising a projection swaged from the shouldered portion of the nipple against the washer to hold the nipple in rigid 15 relation to the hub.

8. An air impeller comprising in combination,

a hub, a sheet-like blade flexed to conform substantially with the curved surface of a cone and secured edgewise against the exterior surface of 20 the hub in such position relative to the hub that a radial line passing through the axis of the hub and approximately bisecting the blade forms an angle of approximately forty-five degrees with those elements of the cone which intersect 25' said radial line.

9. In fan rotor construction a hollow dome shaped hub having a perforated Wall, a blade of pliant sheet material having a portion of one edge bent over and conformed and fastened to 30 said wall and having a continuation of said edge shaped to provide a holding tongue adapted to project through the perforated hub wall and twisted in its portion interior of said wall to prevent its withdrawal therefrom. 35

10. As an article of manufacture, a fan blade comprised of sheet-like material designed to revolve about an axis outside itself, and having an air entering end and a trailing end both disposed in arcs struck from said axis at an equal radius. and blanked to a shape at least fifty percent longer from entering end to trailing end than is the width of said blade in directions radial to said-axis, and conformed to the curved surface of a cone with the longest dimensions of said 45 blade disposed approximately in planes which cut circular sections from said cone.

11. In combination with a fan blade as described in claim 10, a dome-shaped hub adapted to be rotated about the said axis of revolution of the blade and secured to and carrying said blade in such position that the conical curvature of the said entering end of the blade is approximately tangent to its plane of rotation and located nearest the end .of said hub having the largest circumference.

12. An air impeller embodying in combination,

a hollow dome-shaped hub having a closed nose portion forming one end of the hub and having an open opposite end, and more than one impeller blade conformed to the curved surface of a cone and secured edgewise against the said hub in such position that the elements of the cone to whose surface said blade is conformed which are most nearly central of the circumferential length of the blade are disposed in planes approximately tangential to the circumference of the hub at its said open end.

13. An air impeller embodying in combination,

a hollow dome-shaped hub constructed to define an axis of rotation for said impeller and having a closed nose portion forming one end of the hub and having an open opposite end, and more than one impeller blade secured edgewise against the said hub and having an air impelling surface bounded by the blade edge, a radially inward portion of which edge is shaped to conform to the outer surface of said hub, an outer peripheral portion of which edge is shaped to align approximately with circumferential arcs struck at an equal radius from the rotative axis of the hub, and entering and trailing end portions of which edge are convexly curved and extend to connect said inward and outward portions of the edge,

said blades each being so proportioned and disposed that the air impelling surfaces thereof in no portions overlap with relation to each other when projected in lines paralleling the axis of rotation of the impeller.

14. An air impeller embodying in combination, a hollow dome-shaped hub constructed to define an axis of rotation for said impeller and having a closed nose portion forming one end of the hub and having an open opposite end, and more than one.impeller blade secured edgewise against said hub and having an air impelling surface bounded by the edge of the blade, said edge including a peripheral portion substantially aligned with circumferential arcs struck at an equal radius from the axis of hub rotation and a hub joining portion conformed to the shape of the hub, the said peripheral portion being circ'umferentially advanced relative to the hub joining portion in the direction said impeller rotates to force air toward the said nose portion of the hub, said blades each being so proportioned and disposed that the air impelling surfaces thereof in no portions overlap with relation to each other when projected in lines paralleling the axis of rotation of the impeller.

15. An air impeller as described in claim 13 in which the said entering and trailing portions of the edge of the blade curve convexly backward from the said peripheral portion of the blade. edge with relation to the direction in which the impeller rotates for forcing air toward the nose portion of the hub thereby to join inward portion of the blade edge which is secured to said hub, said blades each being so proportioned and disposed that the air impelling surfaces thereof in no portions overlap with relation to each other when projected in lines paralleling the axis of rotation of the impeller.

16. In combination with a plurality of fan blades, each as described in claim 10', a domeshaped hub adapted to be rotated about the common axis of revolution of said blades and secured to and carrying said plurality of blades in such relative circumferential positions that all points on the said trailing edge of each blade and all points on the entering edge of the following blade lie on opposite sides 'ofa plane parallel to the said axis of revolution.

17. An air impeller embodying in combination, a hollow dome-shaped hub having a closed nose portion forming one end of the hub and having an open end, means to mount said hub for rotation about an axis central thereof, and more than one impeller blade secured edgewise against said hub and having an air impelling surface, said blades being so prt portioned and disposed that the air impelling surfaces thereof in no portions overlap when projected in lines paralleling the said axis of rotation, and each blade having an air impelling surface whose maximum extent along arcs of equal radius struck from said axis with the said of rotation is at least fifty per cent greater than is the radial width of an annular space bordered by the open end of said hub and extending to the radially outmost edge of the blade.

18. An air impeller embodying in combination, a hollow dome-shaped hub having a closed nose portion forming one end of the hub and having an open end, means to mount said hub for rotation about an axis central thereof, and more than one impeller blade conformed to the curved surface of a cone and secured edgewise against the said hub, said blades each being so proportioned and disposed that the air impelling surfaces thereof in no portions overlap with relation to each other when projected in lines paralleling the said axis of rotation, and each blade having an air impelling surface whose maximum extent along arcs of equal radius struck from said axis of rotation is at least fifty per cent greater than is the radial width of an annular space bordered by the open end of said hub and extending to the radially outermost edge of the blade.

19. In fan rotor construction, a hollow shell having a perforated wall with means rotatively to mount the same, a blade of sheet material carried externally by said shell, a plurality of ears rigid with said blade at the edge thereof and penetrating the perforated wall of the shell, one of said ears projecting inside the shell in a manner to impel air therewithin when the shell is rotated, and another of said ears projecting inside the shell and thereat being flexed to pre- ,vent its withdrawal and the withdrawal of the first said ear from the interior of the shell and to assist in holding the blade against the exterior surface of the shell.

20. In fan rotor construction, a hollow hub having a perforated wall contoured to form a dome-shapedv nose portion comprising one end of said hub, a blade of sheet-like material, an ear rigid with said blade and penetrating the perforated dome-shaped wall of the hub and projecting inside said hub in a. manner to effect cooling movement of the air within the hub whenthe hub is rotated, and to leave vacant within said hub a suflicient space to accommodate a prime mover' for rotating said hub While cooled by said movement of the air.

21. In fan rotor construction, a hollow hub having a wall perforated to provide a narrow slot,

an air impeller blade carried externally by said hub, an ear'rigid with said blade and made of pliant sheet metal and projecting through said slot into the hub interior and thereat twisted into angular relation to the length of the slot in a manner to hold the blade and hub firmly together by means of torsional distortion of said ear.

22. In fan rotor construction, a hollow hub having a wall perforated to provide a narrow slot, an air impeller blade made of pliant sheet metal a portion of which forms a protruding ear projecting through said slot into the hub interior and thereat twisted into angular relation to the length of the slot in a manner to hold the blade 65 firmly on the outside of the hub by means of torsional distortion of said ear.

ALFRED c. GILBERT.

JOHN LANZ.

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