GB2051967A - Variable Pitch Axial Flow Fan Impeller - Google Patents
Variable Pitch Axial Flow Fan Impeller Download PDFInfo
- Publication number
- GB2051967A GB2051967A GB8016855A GB8016855A GB2051967A GB 2051967 A GB2051967 A GB 2051967A GB 8016855 A GB8016855 A GB 8016855A GB 8016855 A GB8016855 A GB 8016855A GB 2051967 A GB2051967 A GB 2051967A
- Authority
- GB
- United Kingdom
- Prior art keywords
- impeller
- blades
- blade
- actuator
- bearing
- 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.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/34—Blade mountings
- F04D29/36—Blade mountings adjustable
- F04D29/362—Blade mountings adjustable during rotation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D7/00—Rotors with blades adjustable in operation; Control thereof
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
- F05D2260/74—Adjusting of angle of incidence or attack of rotating blades by turning around an axis perpendicular the rotor centre line
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
- F05D2260/76—Adjusting of angle of incidence or attack of rotating blades the adjusting mechanism using auxiliary power sources
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
An impeller for a variable pitch axial flow fan having an actuator (25) arranged to rotate the blades (5) towards their maximum pitch angle, and in which the inherent blade tuning moment of the blades when the impeller is rotating provides the restoring force for moving the blades towards their minimum pitch angle, thus avoiding the need for blade counterweights and a heavy return spring. <IMAGE>
Description
SPECIFICATION
Impeller for a Variable Pitch Axial Flow Fan
This invention relates to impellers for variable
pitch axial flow fans, that is to say impellers in
which the pitch angle of the blades can be varied
while the impeller is rotating.
In such impellers the blades are commonly
supported in bearings carried by a hollow hub, so
as to be rotatable about respective axes extending
radially from the axis of rotation of the impeller,
the inner ends of the blades carrying arms which
extend outwardly with respect to the blade axes,
and which are coupled to an actuator movable
parallel to the impeller axis so as to effect a
rotation of the blades within the respective
bearings, and thereby vary their pitch angle. The
invention is concerned especially with impellers of this kind, which will hereinafter be referred to as of the kind specified.
It is well known that if a body, rotatable about its own axis, is rotated about a perpendicular axis, the centre of mass of the body will have a strong tendency to align itself with the plane of rotation of the body axis.
In a variable pitch axial flow fan this is manifested by a turning force which tends to reduce the blade pitch angle, that is to say the angle measured between the chord line and said plane of rotation.
It is common to compensate for this turning moment in impellers of the kind specified by attaching counterweights to the blade assembly within the hub. The actuator is then arranged to rotate the blades in either direction, a relatively strong return spring being provided for rotating the blades in the opposite direction. However in such arrangements the hub has to be sufficiently wide to accommodate the counterweights, and moreover since the counterweights add considerably to the weight of the blade assemblies, it must be made of suitably strong and heavy material to withstand the additional radial thrust developed under centrifugal force.
An object of the invention is to provide a form of impeller in which the use of counterweights can be provided.
According to the invention in an impeller of the kind specified for a variable pitch axial flow fan, the actuator is arranged to rotate the blades towards their maximum pitch angle, and the inherent blade turning moment provides the restoring force for moving the blades towards their minimum pitch angle.
Moreover the invention enables a relatively smaller and lighter hub to be used compared with those employed in counterweighted blade impellers.
In addition it has been found that the actuating forces in the planes of the blade bearings are very small compared with the centrifugal thrust forces exerted by the blades when the impeller is operating. Under these circumstances very simple axial thrust bearings can be utilised without recourse to the addition of journal bearings for the blades; the line of action of the resultant forces on the bearing remaining within the ball tracks.
The actuator is preferably arranged to be operated by pneumatic pressure from a suitable source via a rotary seal.
The invention will be further described by reference to Figures 1 and 2 of the accompanying drawings, in which Figure 1 illustrates an axial section through half of one impeller in accordance with the invention for an axial flow fan, and Figure 2 shows a transverse section of a part of the impeller.
In the drawing 1 represents the impeller hub shown bolted to a hollow boss 2 which is arranged to be secured to the shaft of an electric motor (not shown).
Around the periphery of the hub there are a number of uniformly spaced radially directed holes 3 into which are fitted the root portions 4 of respective aerofoil section blades 5 (shown only in part).
Each blade 5 is held in position by means of a circular retaining plate 6 which is secured to the inner end of the blade root 4 by means of a nut 7, which is screwed on to the protruding end of a threaded insert 8 captive within the blade root, a flange 10 at the outer end of the blade root being located in a recess around the outer end of the respective hole 3. A washer or pad 11 being located between the flange and the bottom of the recess.
Two dowels 1 5 are fitted between the blade 5 and the retaining plate 6 to provide location.
A thrust bearing 9 is clamped between the plate 6 and an inwardly facing surface of the hub 1 and, in use, when the impeller is rotating, the blades are urged outwardly under centrifugal force, the bearing 9 facilitating the rotation of the blade about its axis relative to the hub.
The thrust bearing 9 comprises a number of hardened steel balls 12 interposed between an annular inner race 13 adjacent the plate 6 and an outer race 14 adjacent the hub surface. The balls are arranged to roll in shallow annular grooves provided in the facing surfaces of the races 13 and 14 and are equidistantly spaced around the grooves by an annular bearing cage 16 having a relatively low mass, and formed, for example, from a suitable plastics material such as acetal resin or from nylon impregnated with graphite or molybdenum disulphide. The bearing cage 16 has a substantially channel shaped cross-section having in its base a plurality of uniformly spaced holes which accommodate the bearing balls 12, and is arranged so that in use either the base or the edges of its side walls bear against the surface of the outer race 14.The bearing 9 contains a lubricant having a density substantially the same as the material of the bearing cage 1 6.
The bearing 9 is enclosed by an annular housing 20 which is of channel-shaped crosssection having its mouth directed radially inwards towards the impeller axis, the depth of the walls of the housing being such that the bearing is accommodated entirely within the channel which thus serves to keep the balls and the cage of the bearing covered with lubricant despite the effect of centrifugal force when the impeller is in use.
Clearances are provided between the sides of the housing 20 and the inner ball race 13 and plate 6 to permit the blade to rotate freely.
Adjustment of the pitch angle of the blades 5 is effected by means of an arm 21 extending transversely from the plate 6 and supporting at its end a pin 22 carrying a roller 23 which locates within a channel 24 in the periphery of a common actuator 25. The actuator 25 is in the form of a shell formed in two parts 29, 30 joined around their periphery, the rear part 29 carrying a cylindrical flange 39 which surrounds the boss 2 but is free to move axially along it on a bearing 26.
The boss 2 carries coaxialiy at its end a circular plate 27 located within the actuator providing a backing for a diaphragm 28 which is clamped around its periphery between the two parts 29, 30 of the actuator 25 as shown. The plate 27 supports coaxially a stub shaft 31 which provides a guide for the front part 30 of the actuator which is free to slide axially along the shaft 31 on a bearing 32. The inner edge of the diaphragm 28 is secured to the plate 27 around the stub shaft 31, by an annular clamping plate 50 and screws 51.
The actuator is made rotationally fast with the hub, for example by means of a tension pin and screw 19 and 19.1 passing through the front and rear walls 29.1,42 of the actuator channel 24 on either side of a roller 23.
In use of the impeller the inherent blade turning moment will tend to rotate the blades to their minimum pitch angle position as shown in
Figure 1 of the drawing. In order to increase the pitch angle air under pressure is arranged to be admitted into the space between the front part 30 of the actuator and the diaphragm 28, via a rotatable coupling 35, and a duct formed by a gap or gaps (not shown) in the bearing 32. This produces a forward movement of the actuator 25 and so increases the pitch angle of the blades by an amount depending upon the admitted air pressure.
When the pressure is released the inherent blade turning moment causes the blades to be returned towards the minimum pitch angle position which is pre-determined by the positioning of the dowels 15 in the blade 5 and the retaining plate as described above. The minimum pitch angle is set before fitting the items 27, 30 and 41, by pulling the member 29 forward until it contacts adjusting nuts 1 7 carried on studs 18 screwed into the hub 1. The nuts 17 are adjusted until all the blades are at the desired pitch angie. Minimum pitch angle is adjustable by adjustment of the fan control equipment (not shown).
After assembly of the parts 27, 30 the impeller is completed by the attachment of a relatively thin-walled dome-shaped fairing 41 to the front of the hub 1 as shown.
The assembly of the impeller is facilitated by constructing the rear wall 42 of the actuator channel 24 in castellated form as shown more clearly in Figure 2, with the gaps 43 between the upstanding portions 44 of the wall of sufficient width to allow the passage of the rollers 23. After the rollers 23 have been located in the channel 24 the actuator is rotated relative to the hub to bring the upstanding portions opposite the rollers and is then secured against further rotation with respect to the hub by fitting a fixed dowel 19 and screw 19.1 as previously described or by any other convenient means.
Claims (10)
1. An impeller for a variable pitch axial flow fan incorporating a plurality of blades extending outwards from a hollow hub, and supported by respective bearings so that they can be rotated about their axes with respect to the hub, the inner ends of which blades carry arms which extend outwardly with respect to the blade axes and are coupled to an actuator which is movable parallel to the axis of the impeller to rotate the blades within their bearings and so vary their pitch angle, wherein the actuator is operable to rotate the blades towards their maximum pitch angle, and the inherent blade turning moment when the impeller is rotating provides a restoring force for moving the blades towards their minimum pitch.
angle.
2. An impeller according to Claim 1 having an adjustable stop which limits the movement of the actuator towards the maximum pitch angle position, adjustment of the stop enabling the maximum pitch angle of the blades to be set to a predetermined value.
3. An impeller according to Claim 1 or 2 wherein each blade has a root portion formed integrally with the blade and extending inwards through an opening in the wall of the hub, the blade being retained against radially inward movement by a flange at the outer end of the root portion, and against radially outward movement by a retaining member secured to the inner end of the root portion, a thrust bearing being located between said retaining member and the inner surface of the hub.
4. An impeller according to Claim 3 wherein each bearing comprises an outer race adjacent the hub, and inner race adjacent the retaining member, and a plurality of balls supported between the bearing races in a bearing cage, the bearing cage being arranged so that during rotation of the impeller centrifugal force acting on the bearing cage is taken by said outer race.
5. An impeller according to Claim 4 wherein the bearing cage is formed of a plastics material such as acetal resin or nylon impregnated with molybdenum disulphide or graphite.
6. An impeller according to Claim 3, 4 or 5 wherein each blade bearing is accommodated within an annular housing of channel-shaped cross-section having an open mouth directed towards the impeller axis, the walls of the housing extending inwards beyond the operative face of the inner bearing race.
7. An impeller according to any one of Claims 3 to 6 wherein the retaining member carries a said arm which is coupled to the actuator, said arm terminating in a roller which engages in a peripheral channel in the actuator.
8. An impeller according to Claim 7 wherein one wall of said peripheral channel is formed with uniformly spaced gaps for facilitating the introduction of the rollers into the channel during assembly of the impeller.
9. An impeller according to any preceding
Claim wherein the actuator is operable by pneumatic pressure.
10. An impeller substantially as shown in and as hereinbefore described with reference to
Figures 1 and 2 of the accompanying drawings.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8016855A GB2051967B (en) | 1979-05-22 | 1980-05-21 | Variable pitch axial flow fan impeller |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7917849 | 1979-05-22 | ||
GB8016855A GB2051967B (en) | 1979-05-22 | 1980-05-21 | Variable pitch axial flow fan impeller |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2051967A true GB2051967A (en) | 1981-01-21 |
GB2051967B GB2051967B (en) | 1982-11-17 |
Family
ID=26271616
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8016855A Expired GB2051967B (en) | 1979-05-22 | 1980-05-21 | Variable pitch axial flow fan impeller |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2051967B (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2254893A (en) * | 1991-04-18 | 1992-10-21 | Dowty Aerospace Gloucester | A variable pitch propeller assembley. |
US5281095A (en) * | 1990-12-20 | 1994-01-25 | Honda Giken Kogyo Kabushiki Kaisha | Variable-pitch mechanism for a propeller |
US5795132A (en) * | 1995-04-07 | 1998-08-18 | Something Else Limited Liability Co. | Variable pitch propeller |
US5931637A (en) * | 1996-01-22 | 1999-08-03 | Something Else Limited Liability Company | Propeller with variable rate of pitch change |
FR2942454A1 (en) * | 2009-02-23 | 2010-08-27 | Airbus France | BLADE RETENTION DEVICE FOR TURBOMACHINE PROPELLER. |
US20150361818A1 (en) * | 2014-06-16 | 2015-12-17 | Rolls-Royce Plc | Assembly |
-
1980
- 1980-05-21 GB GB8016855A patent/GB2051967B/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5281095A (en) * | 1990-12-20 | 1994-01-25 | Honda Giken Kogyo Kabushiki Kaisha | Variable-pitch mechanism for a propeller |
GB2254893A (en) * | 1991-04-18 | 1992-10-21 | Dowty Aerospace Gloucester | A variable pitch propeller assembley. |
US5795132A (en) * | 1995-04-07 | 1998-08-18 | Something Else Limited Liability Co. | Variable pitch propeller |
US5931637A (en) * | 1996-01-22 | 1999-08-03 | Something Else Limited Liability Company | Propeller with variable rate of pitch change |
FR2942454A1 (en) * | 2009-02-23 | 2010-08-27 | Airbus France | BLADE RETENTION DEVICE FOR TURBOMACHINE PROPELLER. |
US8496438B2 (en) | 2009-02-23 | 2013-07-30 | Airbus Operations Sas | Blade retaining device for turbo machine propeller |
US20150361818A1 (en) * | 2014-06-16 | 2015-12-17 | Rolls-Royce Plc | Assembly |
US9970313B2 (en) * | 2014-06-16 | 2018-05-15 | Rolls-Royce Plc | Unison ring assembly |
Also Published As
Publication number | Publication date |
---|---|
GB2051967B (en) | 1982-11-17 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19920521 |