[go: up one dir, main page]

US912362A - Centrifugal fan and pump. - Google Patents

Centrifugal fan and pump. Download PDF

Info

Publication number
US912362A
US912362A US36985507A US1907369855A US912362A US 912362 A US912362 A US 912362A US 36985507 A US36985507 A US 36985507A US 1907369855 A US1907369855 A US 1907369855A US 912362 A US912362 A US 912362A
Authority
US
United States
Prior art keywords
vane
blade
vanes
fan
fluid
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US36985507A
Inventor
George Marie Capell
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US36985507A priority Critical patent/US912362A/en
Application granted granted Critical
Publication of US912362A publication Critical patent/US912362A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/281Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers

Definitions

  • This invention relates to improvements in centrifugal fans and pump wheels for circulating fluids and has special reference to the type of fans shown in my Patent No. 867,874 granted OctoberB, 190?, wherein is shown, described and claimed broadly a tail-blade back of the main vanes, a series of radially stepped vanes, and a series of vanes between the main vanes.
  • centrifugal force has almost entirely been relied on as the urging force compelling the fluid to flow, though in some cases this has been supplemented by a scooping eifect derived by bending in a forward direction lateral extensions of the inner portions of the vanes, the gathering effect of the scoops augmenting the quantity of fluid which enters the zone of action in front of the revolving vanes.
  • a scooping eifect derived by bending in a forward direction lateral extensions of the inner portions of the vanes
  • I provide means for augmenting cavitation at the rear of the inner portions of the vanes and at the same time suppressing cavitation at the rear of the outer portions and thereby fill up'the cavity entirely from the interior of the fan small acldition to the inducement of fluid to enter the zone of action of the vanes because its evacuation by centrifugal force must be accompanied by replenishmentfrom the interior apart from the inducing effect of further cavitation. It is to the cumulative effect derived thereby that I attribute the.very greatly enhanced manomet-ric and volumetric elfect which I have derived from a fan constructed in accordance with the principle of this invention.
  • Figure I is a transverse section of a portion of a fan showing my invention applied thereto.
  • Fig. 2 is a sectional view of the same taken at right angles to that shown in Fig. 1, on the line 2 2 Fig. 1, and showing a double inlet construction.
  • Fig. 3 is a transverse section of the fan showanother form :of the invention. 4 is another view of the section, taken at right angles to that shown in Fig. 3, on the 4-4 Fig. 3, and showing an inlet construction.
  • the *fan wheel is formed with a number of principal vanes -0..a between which are interposed a number of secondary vanes 5.6 and 0.0 and, for a purpose to be presently explained, tail-blades dd at the rear of the exterior portions of the principal vanes an.
  • the portions of the principal wanes which extend within the periphery of the inlet orifice have scoop-shaped lateral extensions e..-c -projecting outwards and .for wardsland constitute a well known addition to a fan for augmenting thevolmne :of delivery of the fan.
  • the fan shown is designed to take advantage of the fact that a partial vacuum is produced at the rear of an advancing vane by utilizing that vacuum as an additional force inducing air to flow into 'the zone of action of the vanes.
  • the inner edge of the secondary vane 72 is stepped outwards relatively to the inner edge of the preceding principal vane a and the inner edge of the vane c is stepped outwards relatively to that of the vane b.
  • the result of such relative positions of the inner edges of the series of vanes a, b and c is to cause, by the relative remoteness from a of the next succeeding vane a, a great tendency to the production of a vacuum in the rear of the inner portion of a.
  • Also on account of the outward stepping of 0 there will be a pronounced tendency to the production of a vacuum at the rear of the inner portion of I; while at the rear of c the vacuum produced will be no more than in fans of normal construction.
  • the outer edge of the vane c is at a greater radial distance than the edge of b but less than that of the outer edge of the succeeding vane (1.
  • the outer edge of the vane c is at a greater radial distance than the edge of b but less than that of the outer edge of the succeeding vane (1.
  • this blade (1 is positioned with its outer edge short of the periphery of the wheel and divergent from the back of the vane as compared with the inner edge which is relatively close to the vane while leaving a space for the outward flow of the fluid between the vane and tailblade, and the inner edge of the said blade I between the vane and tail-blade and the 'Iproximity of the tail-blade will preclude to production of a vacuum at the rear of the any appreciable degree the tendency to the outer portion of the vane a and the backward slope ofthe outward extremity of the tail-blade will minimize any tendency to the production of a vacuum at the rear of the outward portion of that blade.”
  • the diverging of the inner edge of such blade (1 will assist in gathering fluid to pass between the vane and blade by avoiding the contraction of stream which results from a sharp edged entrance and thus augmenting the flow.
  • the different improvements may be employed separately from each other, as for example, the main vanes extending inwardly from the periphery together with the tailblades located at the back of them, as described, may be employed without intermediate vanes.
  • a centrifugal wheel for circulating fluids having a series ofvanes, and blades at the back of the vanes, each such blade extending inwardly in a direction to first converge towards its vane and afterwards to diverge therefrom, leaving a space between the blade and vane for the passage of fluid.
  • a centrifugal wheel or circulating fluids having a series of vanes,'and blades at the back of the vanes. each such blade extending inwardly in a direction to first converge towards its vane and afterwards to diverge therefrom, leaving a space between the erases twice the distance from the periphery as it is from the air inlet or inner circle, such blade first converging towards its vane and afterwards diverging therefrom leaving a space between the vane and blade for the passage of fluid.
  • a centrifugal wheel for circulating fluids having aseries of vanes and a single blade at't-he back of each vane, the nearest point of blade to vane being located about twice the distance from the periphery as it is flOD'l'tllB airinlet or inner circle, such blade first converging towards its vane and afterwards diverging therefrom leaving a space between the vane and blade for the passage of fluid the amount of the subsequent divergence being less than that of the preceding convergence.
  • a centrifugal wheel for circulating fluids having a series of vanes and a single blade at the back of each vane, the nearest point of blade to vane being located about twice the distance from the periphery as it is from the air inlet or inner circle, such blade first converging towards its vane and afterwards diverging therefrbm leaving a space between the vane and blade for the passage of fluid, the vane being convex relatively to the blade at the back thereof.
  • a centrifugal wheel for circulating fluids having a series of vanes and a single blade at the back of each vane, the nearest point of blade to vane being located about twice the distance from the periphery as it is from the air inlet or inner circle, such blade first converging toward its vane and afterwards diverging therefrom leaving a space between the vane and blade for the passage of fluid, the vane being convex relatively to the blade at the back thereof, and the blade at its outer portion concave, and at its inner portion convex relatively to the vane.

Landscapes

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

Description

e. M. CAPELL. GENTRIFUGAL FAN AND-PUMP.
APPLICATION FILED APR. 23. 1907.
912,362. Patented Feb. 16, 1909.
WITNESSES |NVENTOR NORRIS PETERS, INC" LITHO., WASHINGTON. D. C
clear, and exact description thereof.
known in relation to other matters, its utilior wheel. The effect will be great of even a GEORGE MARIE CAIELL, OF STON'Y STRATFDRD, ENGLAND.
CENTBIFUGAL FAN AND Pm.
Specification '01 Letters Patent.
Patented Feb; 16,1909.
Application filed April as, 1907. Serial No. 369,855.
To all whom it may concern:
Be it known that I, GEORGE MARE 'GAPELL, a resident of Passenham Rectory, Stony Stratford, Buckingham, England, have invented a new and useful Improvement in Centrifugal Fans and Pumps; and I do hereby declare the following to be a full,
This invention relates to improvements in centrifugal fans and pump wheels for circulating fluids and has special reference to the type of fans shown in my Patent No. 867,874 granted OctoberB, 190?, wherein is shown, described and claimed broadly a tail-blade back of the main vanes, a series of radially stepped vanes, and a series of vanes between the main vanes. Hitherto in such fans and wheels, centrifugal force has almost entirely been relied on as the urging force compelling the fluid to flow, though in some cases this has been supplemented by a scooping eifect derived by bending in a forward direction lateral extensions of the inner portions of the vanes, the gathering effect of the scoops augmenting the quantity of fluid which enters the zone of action in front of the revolving vanes. Over and above these two impelling forces there is a third which, although well zation for promoting the-outputof fans and centrifugal pumps has not hitherto been proposed.
It is Well known that at the rear of a linearly moving vane there is created a partial vacuum, the action being conveniently cal-led cavitation towards which, fluid in the neighborhood Wlll flow by reason of the higher pressure to which it is there sub jected. Under ordinary circumstances no useful effect is derivable from this cavitation inasmuch as fluid will flow to the vacated space behind the vane equally from the space outside the exterior edge of the vane as from that within the interior edge. Now according to this invention I provide means for augmenting cavitation at the rear of the inner portions of the vanes and at the same time suppressing cavitation at the rear of the outer portions and thereby fill up'the cavity entirely from the interior of the fan small acldition to the inducement of fluid to enter the zone of action of the vanes because its evacuation by centrifugal force must be accompanied by replenishmentfrom the interior apart from the inducing effect of further cavitation. It is to the cumulative effect derived thereby that I attribute the.very greatly enhanced manomet-ric and volumetric elfect which I have derived from a fan constructed in accordance with the principle of this invention.
The means for augmenting cavitation at the rear of the inner portions of the vanes and suppressing it at the rear of the outer portions, can best be explained by reference to a representative example as shown in the accompanying drawing which is that of a double inlet mine ventilating fan.
In the drawing :Figure I is a transverse section of a portion of a fan showing my invention applied thereto. Fig. 2 is a sectional view of the same taken at right angles to that shown in Fig. 1, on the line 2 2 Fig. 1, and showing a double inlet construction. Fig. 3 is a transverse section of the fan showanother form :of the invention. 4 is another view of the section, taken at right angles to that shown in Fig. 3, on the 4-4 Fig. 3, and showing an inlet construction.
' Referring to Fig. 1 it will be observed that the *fan wheel is formed with a number of principal vanes -0..a between which are interposed a number of secondary vanes 5.6 and 0.0 and, for a purpose to be presently explained, tail-blades dd at the rear of the exterior portions of the principal vanes an. The portions of the principal wanes which extend within the periphery of the inlet orifice have scoop-shaped lateral extensions e..-c -projecting outwards and .for wardsland constitute a well known addition to a fan for augmenting thevolmne :of delivery of the fan.
The fan shown is designed to take advantage of the fact that a partial vacuum is produced at the rear of an advancing vane by utilizing that vacuum as an additional force inducing air to flow into 'the zone of action of the vanes. For this purpose the inner edge of the secondary vane 72 is stepped outwards relatively to the inner edge of the preceding principal vane a and the inner edge of the vane c is stepped outwards relatively to that of the vane b. The result of such relative positions of the inner edges of the series of vanes a, b and c, is to cause, by the relative remoteness from a of the next succeeding vane a, a great tendency to the production of a vacuum in the rear of the inner portion of a. Also on account of the outward stepping of 0 there will be a pronounced tendency to the production of a vacuum at the rear of the inner portion of I; while at the rear of c the vacuum produced will be no more than in fans of normal construction.
To realize the inducing effect on the .flow due to the above described vacuum production, it will be'necessary to provide conditions which will prevent a counteracting effect at the outer portions of the vanes and so avoid as completely as possible a tendency to a back flow from the casing into the spaces vacated by the advancing vanes. For
this purpose the outer edge of the vane c is at a greater radial distance than the edge of b but less than that of the outer edge of the succeeding vane (1. Thus at the rear of the outer portions-of the vanes b and 0 there will be little or no tendency to the production of avacuum on account of the proximity of the vanes of greater radius which follow. But all this will be of no avail unless the production of a. vacuum at the rear of the outer portion of a is prevented. I havediscovered an efl'ectual means of attaining this desired result by the useof the tail-blade (Z. In Fig. 1 this blade (1 is positioned with its outer edge short of the periphery of the wheel and divergent from the back of the vane as compared with the inner edge which is relatively close to the vane while leaving a space for the outward flow of the fluid between the vane and tailblade, and the inner edge of the said blade I between the vane and tail-blade and the 'Iproximity of the tail-blade will preclude to production of a vacuum at the rear of the any appreciable degree the tendency to the outer portion of the vane a and the backward slope ofthe outward extremity of the tail-blade will minimize any tendency to the production of a vacuum at the rear of the outward portion of that blade." The diverging of the inner edge of such blade (1 will assist in gathering fluid to pass between the vane and blade by avoiding the contraction of stream which results from a sharp edged entrance and thus augmenting the flow.
In Fig. 3 the tail-blade is entirely convex to the vane, whereas in Fig. 1 the outer por tion is concave and both are efficient forms of the general form of tail-blade shown in said patent. I
It has been found that by placing the contracted portion of the opening between the vane and blade at about twice the distance from the periphery as it is from the air inlet or inner circle it will give the best results.
The figures show details of construction in respect to which no claim is made in this application. To strengthen the support 01 the portions of the principal vanes a.a which extend within the air-inlet orifice, circumferentially, disposed stay rods f.f are pro-.
vided and these are secured to arms--; ;-;g; n="
somewhat tangentially inclined, whereby a portion ofthe turning efiort is transmitted from the shaft to the vanes of the wheel. The drawing shows wheels adapted for operating on air. If water or other fluid is required to be circulated or pumped, the design will require some modification of detail, but such detail forms no portion of the present invention.
The different improvements may be employed separately from each other, as for example, the main vanes extending inwardly from the periphery together with the tailblades located at the back of them, as described, may be employed without intermediate vanes.
In fans of ordinary construction in which the outer edges of all the vanes are at equal radii and are equally spaced and also the inner edges, the greater spacing of the outer edges relatively to the inner edges consequent on the 'greater circumference of the circle along which they are disposed has the.
result of causing the cavitation effect of 0nward motion to be more pronounced at the rear of the outward portions of the vanes than at the rear of'the inward portions so that, in ordinary fans, the principle of action,
which bythe present invention is sought to be utilized for promoting the flow, has hitherto operated in a contrary manner and I claim by the present invention to have converted a feeble opponent into a potent ally whereby I have been able to obtain a greater volumetric and manometric discharge than has hitherto been possible with a given diameter and speed of revolution of fan.
I claim:
1. A centrifugal wheel for circulating fluids, having a series ofvanes, and blades at the back of the vanes, each such blade extending inwardly in a direction to first converge towards its vane and afterwards to diverge therefrom, leaving a space between the blade and vane for the passage of fluid.
2. A centrifugal wheel or circulating fluids, having a series of vanes,'and blades at the back of the vanes. each such blade extending inwardly in a direction to first converge towards its vane and afterwards to diverge therefrom, leaving a space between the erases twice the distance from the periphery as it is from the air inlet or inner circle, such blade first converging towards its vane and afterwards diverging therefrom leaving a space between the vane and blade for the passage of fluid.
4. A centrifugal wheel for circulating fluids having aseries of vanes and a single blade at't-he back of each vane, the nearest point of blade to vane being located about twice the distance from the periphery as it is flOD'l'tllB airinlet or inner circle, such blade first converging towards its vane and afterwards diverging therefrom leaving a space between the vane and blade for the passage of fluid the amount of the subsequent divergence being less than that of the preceding convergence.
5. A centrifugal wheel for circulating fluids having a series of vanes and a single blade at the back of each vane, the nearest point of blade to vane being located about twice the distance from the periphery as it is from the air inlet or inner circle, such blade first converging towards its vane and afterwards diverging therefrbm leaving a space between the vane and blade for the passage of fluid, the vane being convex relatively to the blade at the back thereof.
'6. A centrifugal wheel for circulating fluids having a series of vanes and a single blade at the back of each vane, the nearest point of blade to vane being located about twice the distance from the periphery as it is from the air inlet or inner circle, such blade first converging toward its vane and afterwards diverging therefrom leaving a space between the vane and blade for the passage of fluid, the vane being convex relatively to the blade at the back thereof, and the blade at its outer portion concave, and at its inner portion convex relatively to the vane.
In testimony whereof I have hereunto set my hand in the presence of two subscribing witnesses.
GEORGE MARIE CAPELL.
Vitnesses H. D. Jhairson, R L. RAM).
US36985507A 1907-04-23 1907-04-23 Centrifugal fan and pump. Expired - Lifetime US912362A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US36985507A US912362A (en) 1907-04-23 1907-04-23 Centrifugal fan and pump.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US36985507A US912362A (en) 1907-04-23 1907-04-23 Centrifugal fan and pump.

Publications (1)

Publication Number Publication Date
US912362A true US912362A (en) 1909-02-16

Family

ID=2980798

Family Applications (1)

Application Number Title Priority Date Filing Date
US36985507A Expired - Lifetime US912362A (en) 1907-04-23 1907-04-23 Centrifugal fan and pump.

Country Status (1)

Country Link
US (1) US912362A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5002461A (en) * 1990-01-26 1991-03-26 Schwitzer U.S. Inc. Compressor impeller with displaced splitter blades
US6139273A (en) * 1998-04-22 2000-10-31 Valeo Climate Control, Inc. Radial flow fan
WO2002090776A2 (en) * 2001-05-09 2002-11-14 Mtu Friedrichshafen Gmbh Rotor disk
US6695038B2 (en) * 1999-09-02 2004-02-24 Advanced Rotary Systems, Llc Heat exchanger type fan
WO2010048905A1 (en) * 2008-10-29 2010-05-06 Vysoké Učení Technické V Brně Impeller of hydraulic machines
US20120124985A1 (en) * 2009-06-01 2012-05-24 Lei Yuening Compressed-air wind turbine generator system having a substantially square, movable body
US10687440B1 (en) * 2019-01-24 2020-06-16 Dell Products L.P. Multi-radial-zone varying blade density fan system

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5002461A (en) * 1990-01-26 1991-03-26 Schwitzer U.S. Inc. Compressor impeller with displaced splitter blades
US6139273A (en) * 1998-04-22 2000-10-31 Valeo Climate Control, Inc. Radial flow fan
US6695038B2 (en) * 1999-09-02 2004-02-24 Advanced Rotary Systems, Llc Heat exchanger type fan
WO2002090776A2 (en) * 2001-05-09 2002-11-14 Mtu Friedrichshafen Gmbh Rotor disk
WO2002090776A3 (en) * 2001-05-09 2003-02-27 Mtu Friedrichshafen Gmbh Rotor disk
US20040202539A1 (en) * 2001-05-09 2004-10-14 Andreas Blank Rotor disk
WO2010048905A1 (en) * 2008-10-29 2010-05-06 Vysoké Učení Technické V Brně Impeller of hydraulic machines
CZ304593B6 (en) * 2008-10-29 2014-07-23 Vysoké Učení Technické V Brně Hydraulic machine impeller wheel
US20120124985A1 (en) * 2009-06-01 2012-05-24 Lei Yuening Compressed-air wind turbine generator system having a substantially square, movable body
US10687440B1 (en) * 2019-01-24 2020-06-16 Dell Products L.P. Multi-radial-zone varying blade density fan system

Similar Documents

Publication Publication Date Title
US912362A (en) Centrifugal fan and pump.
US885108A (en) Centrifugal pump.
US820399A (en) Inlet-opening or eye of centrifugal fans or pumps.
US867874A (en) Centrifugal fan and pump-wheel.
US801304A (en) Centrifugal fan or pump.
US2329696A (en) Centrifugal apparatus
US839273A (en) Centrifugal fan or pump and casing therefor.
US717096A (en) Centrifugal pump.
US909863A (en) Centrifugal fan.
US949150A (en) Centrifugal fan.
US963277A (en) Ventilating apparatus.
US787039A (en) Centrifugal pump.
US1535612A (en) Blading of axial turbines
US1390237A (en) Blower and exhauster for moving air and gas
US860465A (en) Centrifugal fan.
US1086754A (en) Rotary compressor, blower, and pump.
US1183075A (en) Centrifugal pump.
US1233275A (en) Air-compressor.
US1105967A (en) Centrifugal fan and pump.
US1553083A (en) Elastic-fluid turbine
US1099921A (en) Centrifugal pump.
US535483A (en) Centrifugal fan
US784371A (en) Elastic-fluid turbine.
US1771939A (en) Propeller, pump, or fan
US1208762A (en) Steam-turbine.