EP0122726B1 - Fluid contacting surfaces and devices incorporating such surfaces - Google Patents

Fluid contacting surfaces and devices incorporating such surfaces Download PDF

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Publication number
EP0122726B1
EP0122726B1 EP84301804A EP84301804A EP0122726B1 EP 0122726 B1 EP0122726 B1 EP 0122726B1 EP 84301804 A EP84301804 A EP 84301804A EP 84301804 A EP84301804 A EP 84301804A EP 0122726 B1 EP0122726 B1 EP 0122726B1
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European Patent Office
Prior art keywords
axis
fluid
impeller
propeller
contacting surface
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EP84301804A
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German (de)
French (fr)
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EP0122726A1 (en
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Robert Davidson
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H1/00Propulsive elements directly acting on water
    • B63H1/02Propulsive elements directly acting on water of rotary type
    • B63H1/12Propulsive elements directly acting on water of rotary type with rotation axis substantially in propulsive direction
    • B63H1/14Propellers
    • B63H1/26Blades
    • 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
    • F04D29/18Rotors
    • F04D29/181Axial flow rotors

Definitions

  • This invention relates to fluid-contacting surfaces and devices incorporating such surfaces, and more particularly relates to fluid-contacting surfaces and devices which are arranged to affect, modify or control the flow of fluids, as for example the fluid-contacting surfaces of stationary deflectors or rotatable devices such as turbines, impellers or propellers and the like which may be used for a variety of purposes and applications e.g. as in the pneumatic and hydraulic applications.
  • an axial flow fluid impeller or propeller incorporating at least one fluid-contacting surface generated as aforesaid.
  • the invention further includes the methods of forming the said generating surface and the said stationary deflector and/or axial flow fluid impeller or propeller.
  • FIG. 1 of the drawings this diagrammatically illustrates how a fluid-contacting surface in accordance with the present invention may be generated about a point of origin O of an axis of rotation Z.
  • a generatrix point P defines a radius vector OP
  • transverse axis X extends at right angles to the axis of rotation Z and the angle ⁇ is formed between the X axis and the projection OQ of the radius vector OP onto the XY plane, with the angle Z being formed between the radius vector OP and the XY plane.
  • the parametric equations defining the curve generated by the point P are:
  • the surface may include the full 90° sweep between the transverse axis X and the true axis of rotation Z or a part thereof, or the full 180° sweep from adjacent the axis Z to one side of the point of origin 0 through the transverse axis X to lie adjacent the axis Z at the opposite side of the point of origin 0; and the surface thus formed may be duplicated or otherwise multiplied in providing a plurality of similar fluid-contacting surfaces in continuous or spaced relationship about the axis of rotation Z e.g. as in providing fluid-contacting surfaces on a twin or multi bladed impeller or propeller.
  • the rotatable impeller or propeller may be constructed with a blade 1 formed from such as a thin sheet of metal or other suitable material in initially flat circular disc form of radius equal to the length of the generating line OP and provided with either a single radial slit S or a small sector R, R' cut out, as illustrated by way of example in figure 5 of the drawings; and the whole or part disc form may then be twisted and bent into shape with the radial slit (or sector) edges R, R' disposed in opposition 180° apart to lie on or adjacent the axis of rotation Z of the impeller or propeller.
  • the blades 1' witt sweep through an imaginary sphere A.
  • the invention is not confined to impellers or propellers in which the fluid-contacting surface generating line OP is constant, but by varying the length of such line (e.g. by a gradual increase to a peak followed by a gradual decrease) during formation of the impeller, or by subsequent shaping of the impeller blades once initially formed as before described, impellers or propellers of different shapes and sweeping different shaped volumes can be provided to meet the desired situations.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Ocean & Marine Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Hydraulic Turbines (AREA)

Description

  • This invention relates to fluid-contacting surfaces and devices incorporating such surfaces, and more particularly relates to fluid-contacting surfaces and devices which are arranged to affect, modify or control the flow of fluids, as for example the fluid-contacting surfaces of stationary deflectors or rotatable devices such as turbines, impellers or propellers and the like which may be used for a variety of purposes and applications e.g. as in the pneumatic and hydraulic applications.
  • Conventional design of the fluid-contacting surfaces of such as impellers, propellers and like devices can be quite complex and involve relatively high design and production costs for such devices. It is accordingly an object of the present invention to provide an alternative means for generating or forming a fluid-contacting surface, and a device incorporating at least one such surface, in a relatively simple but effective and efficient manner.
  • Another object of this invention is to provide a fluid-contacting surface and/or device incorporating at least one such surface, which may have special purpose applications and provide more effective fluid flow control than at least many conventionally formed fluid-contacting surfaces and devices.
  • Other and more particular objects and advantages of the present invention will become apparent from the ensuing description.
  • According to one aspect of this invention therefor, a fluid-contacting surface comprises at least a part of that surface generated by a generating line extending radially from a point of origin on an axis and rotated about said axis from a said point of origin and radially position so as to sweep through a decreasing angle relative to the axis as rotation takes place.
  • In another aspect of the invention, there is provided a stationary fluid deflector incorporating the fluid-contacting surface generated as aforesaid.
  • In a further aspect of the invention, there is provided an axial flow fluid impeller or propeller incorporating at least one fluid-contacting surface generated as aforesaid.
  • The invention further includes the methods of forming the said generating surface and the said stationary deflector and/or axial flow fluid impeller or propeller.
  • Some preferred aspects of the invention will now be described by way of example and with reference to the accompanying drawings, in which:
    • Figure 1 is a diagram illustrating the principles involved in generating a fluid-contacting surface in accordance with the invention.
    • Figure 2 is an axial or end view of a first form of an impeller or propeller blade formed in accordance with the invention.
    • Figure 3 is a view in the direction of arrows III-III of figure 2.
    • Figure 4 is a view in the direction of arrows IV-IV of figure 2.
    • Figure 5 is an axial view of a blade part for forming the impeller or propeller of figures 2, 3 and 4, illustrated in a flat form prior to shaping.
    • Figure 6 is a perspective view of another form of the impeller or propeller form in accordance with the invention.
    • Figure 7 is a side view in the direction of arrow VII of figure 6.
    • Figure 8 is a side view in the direction of arrow VIII of figure 6.
    • Figure 9 is an axial or end view of the arrangement of figure 6 as viewed in the direction of arrow IX.
    • Figure 10 is an axial view of one blade part for forming the impeller or propeller of figures 6 to 9 inclusive, illustrated in the flat form prior to shaping.
    • Figure 11 is a side view of a further impeller or propeller similar to but including a modification of the impeller of figures 6 through to 9, and
    • Figure 12 is a view in the direction of arrows XII-XII of figure 11.
  • Referring firstly to figure 1 of the drawings, this diagrammatically illustrates how a fluid-contacting surface in accordance with the present invention may be generated about a point of origin O of an axis of rotation Z. A generatrix point P defines a radius vector OP, transverse axis X extends at right angles to the axis of rotation Z and the angle β is formed between the X axis and the projection OQ of the radius vector OP onto the XY plane, with the angle Z being formed between the radius vector OP and the XY plane. The parametric equations defining the curve generated by the point P are:
    • X=R . cos β cos z
    • Y=R . sin (3 cos z, and
    • Z=R . sin z

    Either of the angles (3 and z may be eliminated from the equations by expressing it as a function of the other.
  • As seen, in the XYZ co-ordinate system the point of origin 0 is at the intersection of point of origin of the three co-ordinate axes, and with the angle between the true axis of rotation Z and radius vector OP referred to as 0, the fluid-contacting surfaces generated in accordance with this invention is defined as the locus of the generatrix line OP where θ=f(β) i.e. is some function of the angle 13. For example, where
    Figure imgb0001
    Figure imgb0002
    Figure imgb0003
    or any other function, including tables of discrete values.
  • Simply put, the fluid-contacting surface in accordance with this invention, is any part of that surface generated by the radius vector or generating line OP rotated about the axis Z from the point of origin and swept between the transverse axis X through a decreasing angle to lie adjacent and parallel the axis Z. The surface may include the full 90° sweep between the transverse axis X and the true axis of rotation Z or a part thereof, or the full 180° sweep from adjacent the axis Z to one side of the point of origin 0 through the transverse axis X to lie adjacent the axis Z at the opposite side of the point of origin 0; and the surface thus formed may be duplicated or otherwise multiplied in providing a plurality of similar fluid-contacting surfaces in continuous or spaced relationship about the axis of rotation Z e.g. as in providing fluid-contacting surfaces on a twin or multi bladed impeller or propeller.
  • The angle through which the radius vector or generating line OP is swept and the angle of rotation about the axis Z may be unrelated or each may be a function of the other such as, for example, directly proportional, according to the use to which the fluid-contacting surface is to be put. Similarly the variance in the angle through which the generating line OP is swept may be unrelated or directly proportional to the speed of rotation of the line OP about the axis Z.
  • Further, it is envisaged that the generating line OP can remain of constant length throughout its rotational and angular sweep relative to the axis Z, so that the said surface, and any impeller or propeller blade formed thereby or incorporating such surface, may be swept through an imaginary sphere or spheroidal form, or the length of the generating line OP can be varied as it is swept through its prescribed angle and rotated about the axis Zfrbm its point of origin O in forming a fluid-contacting surface or device incorporating such surface arranged to sweep through an alternative required form as hereinafter described.
  • Referring now to figures 2, 3 and 4, the rotatable impeller or propeller may be constructed with a blade 1 formed from such as a thin sheet of metal or other suitable material in initially flat circular disc form of radius equal to the length of the generating line OP and provided with either a single radial slit S or a small sector R, R' cut out, as illustrated by way of example in figure 5 of the drawings; and the whole or part disc form may then be twisted and bent into shape with the radial slit (or sector) edges R, R' disposed in opposition 180° apart to lie on or adjacent the axis of rotation Z of the impeller or propeller.
  • In constructing the impeller or propeller in this manner, the slit S between the radial edges R, R' of the blade 1 may be a width such that it is substantially equal to the diameter of an axial shaft 2 for the impeller or propeller and to which the said radial edges R, R' can be secured such as by welding.
  • Conventional screw type impellers or propellers are formed with at least the inner parts of their fluid-contacting surfaces as true helix or substantially a true helix about the axis of rotation, with such helix being maintained perpendicular to the axis as it progresses longitudinally thereof; and many propellers are provided with a further helical twist along their radial axes towards their outer periphery. It will be seen that in the present invention there is a substantial difference in construction in that the blade is simply spirally formed from one point of origin 0 on the axis of rotation Z so that from the one medial position on the transverse axis X where the fluid-contacting surface generating line OP is disposed perpendicular to the axis of rotation Z, either side of such perpendicular position the angle of inclination 8 relative to the axis Z progressively decreases as it approaches the axis of rotation Z until it is positioned parallel and adjacent thereto i.e. adjacent the longitudinal surface of the axially disposed shaft 2.
  • In this form of the invention, a pitch value of n=2, has been selected, with the result that the blade 1 curves tightly into the main axis of rotation Z of the impeller or propeller. In figure 2, radial lines 3 represent equal increments of the angle (3 of figure 1 and the dashed lines 4 join sample points of equal displacement from the plane of the X and Y axes.
  • In this arrangement, with rotation of the impeller and shaft about axis Z a positive axial thrust on the fluid is exerted by the fluid-contacting surface of the blade 1 for efficient and effective operation either in moving the fluid coaxially or moving such as an aeroplane or boat relative to the respective fluid (air or water) in which it is located.
  • The arrangement shown in Figures 2, 3 and 4 illustrate a single blade, but a complementary second blade can be provided and mounted in complementary diametric opposition, as shown in broken outline; and it will be seen also that on rotation the blade 1 or blades 1 will sweep through an imaginary sphere A as indicated in broken outline in figure 4.
  • Referring now to figures 6 to 10 of the accompanying drawings, a twin bladed impeller or propeller is provided with different pitch and consequential different shape formed as a result of each blade l' being constructed from thin sheet metal initially of disc form as before but with a relatively large segment S' cut out between radial edges R and R', as shown in figure 10.
  • Again and with the two blades 1' and their common shaft 2' rotated about the said axis Z, the blades 1' witt sweep through an imaginary sphere A. It will be appreciated however that the invention is not confined to impellers or propellers in which the fluid-contacting surface generating line OP is constant, but by varying the length of such line (e.g. by a gradual increase to a peak followed by a gradual decrease) during formation of the impeller, or by subsequent shaping of the impeller blades once initially formed as before described, impellers or propellers of different shapes and sweeping different shaped volumes can be provided to meet the desired situations. For example, the impeller blades 1' can be shaped so that on rotation a substantially cylindrical volume may be swept as indicated in chain dot outline B in figure 7, or the blades 1' may be shaped so that an ellipsoidal form C is swept by the impeller blades. In other variations the basic spheroidal form may be in the main applicable to the medial part of the impeller or propeller, but segments of the sphere or spheroidal form at the opposite axial ends may be cut off, or the longitudinal axis of the impeller or propeller substantially shortened relative to the true diameter.
  • Referring now to figures 11 and 12 of the accompanying drawings, a twin bladed impeller or propeller may be provided which is substantially similar to the impeller or propeller previously described with reference to figures 6 to 10 of the drawings, except that in this arrangement whilst the two blades 1" are similarly formed from a thin flat disc arrangement, on assembly or prior to assembly axial end portions are cut out to more particularly separate the blades 1" at the shaft 2" each side of the medial portion.
  • Experiments with impellers and impeller blades formed as aforedescribed in accordance with this invention have shown that in many instances and on rotation in one direction the formed impellers will give a far more concentrated axial thrust than conventional impellers or similar overall size, similarly powered, and rotated at the same revolutions. The invention thus has particular applications in the construction of small and large air circulation, cooling and ventilating fans and the like; and it is further expected that the invention will have useful applications in marine propulsion for boats and the like, and/or the impelling or pumping of various kinds of fluids, and further have aeronautical applications.
  • As before indicated, the invention particularly lends itself to simplification of manufacture utilising sheet materials, but it will be appreciated that the invention is not confined in this respect and that the impeller, propeller or other blades or deflectors incorporating the fluid-contacting surface or surfaces in accordance with the invention can be manufactured and formed by other means.

Claims (12)

1. A fluid-contacting surface comprising at least a part of the surface which is generated by a generating line extending radially from a point of origin on an axis and rotated about said axis from said point and radial position so as to sweep through a decreasing angle relative to the axis as rotation takes place.
2. A fluid-contacting surface as claimed in claim 1 wherein the rate of decrease of said angle is directly proportional to the speed of rotation of the line about said axis.
3. A fluid-contacting surface as claimed in claim 1 or claim 2 wherein the length of the said generating line is constant through said rotational angular sweep.
4. A fluid-contacting surface as claimed in claim 1 or claim 2 wherein the length of the said generating line is varied by gradual increase to a peak and followed by a gradual decrease.
5. A fluid-contacting surface as claimed in claim 1 wherein the generating line is swept through substantially an angle of 90° from perpendicular to the axis adjacent to and parallel therewith.
6. A fluid-contacting surface as claimed in claim 1 wherein the generating line is swept through substantially 180° from a position adjacent and parallel with the axis to one side of said point of origin, through said radially extending position to a position adjacent and parallel with the axis at the other side of said point of origin.
7. A stationary fluid deflector having at least one fluid-contacting surface defined by at least part of the surface which is generated by a generating line extending radially from a point of origin on an axis and rotated about said axis from said point and radial position so as to sweep through a decreasing angle relative to the axis as rotation takes place.
8. An axial flow fluid impeller or propeller having at least one fluid-contacting surface defined by at least part of the surface which is generated by a generating line extending radially from a point of origin on an axis and rotated about said axis from said point and radial position so as to sweep through a decreasing angle relative to the axis as rotation takes place.
9. A fluid impeller as claimed in claim 8 and comprising two similar blade parts secured to and disposed in diametric opposition about a common axis, each of said blades having a fluid-contacting surface and said common axis being said axis about which the generating line is rotated.
10. A fluid impeller or propeller as claimed in claim 8 or claim 9 wherein the blade or blades is or are arranged to sweep through an imaginary co-axial spherical or spheroidal form on rotation of the impeller or propeller.
11. A fluid impeller or propeller as claimed in claim 8 or claim 9 wherein the blade or blades is or are arranged to sweep through all or part of an imaginary ellipsoidal form on rotation of the impeller or propeller.
12. A fluid impeller or propeller as claimed in claim 8 wherein the blade or blades is or are arranged to sweep through an imaginary co-axial cylindrical form on rotation of the impeller or propeller.
EP84301804A 1983-03-17 1984-03-16 Fluid contacting surfaces and devices incorporating such surfaces Expired EP0122726B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
NZ203600 1983-03-17
NZ203600A NZ203600A (en) 1983-03-17 1983-03-17 Generating a non-planar fluid working surface

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EP0122726A1 EP0122726A1 (en) 1984-10-24
EP0122726B1 true EP0122726B1 (en) 1986-07-09

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EP84301804A Expired EP0122726B1 (en) 1983-03-17 1984-03-16 Fluid contacting surfaces and devices incorporating such surfaces

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EP (1) EP0122726B1 (en)
JP (1) JPS59183001A (en)
AU (1) AU571200B2 (en)
CA (1) CA1229765A (en)
DE (1) DE3460275D1 (en)
MX (1) MX161273A (en)
NZ (1) NZ203600A (en)
ZA (1) ZA842009B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013115658A1 (en) * 2012-01-31 2013-08-08 Propeller Technology Ltd Propeller

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62500515A (en) * 1984-10-12 1987-03-05 ロリモント プロプライエタリー リミテッド marine propeller
DE3579914D1 (en) * 1984-10-12 1990-10-31 Lorimont Pty Ltd SCREW FOR BOATS.
CN111498049B (en) * 2020-04-10 2021-12-21 中船澄西扬州船舶有限公司 Mounting method of energy-saving stator

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1017915B (en) * 1955-06-02 1957-10-17 Bergedorfer Eisenwerk Ag Centrifugal pump for liquid food
JPS524940B1 (en) * 1970-02-20 1977-02-08
FR2187030A5 (en) * 1971-07-09 1974-01-11 Crambes Maurice
FR2359294A1 (en) * 1976-07-23 1978-02-17 Carrouset Pierre FLUID PREHENSION TURBINE
NL184075B (en) * 1978-06-30 1988-11-01 Hva Water Contractors B V METHOD FOR OPERATING A ROTARY PIVOT ROTATOR AND ROTOR INTENDED FOR CARRYING OUT SUCH A METHOD

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013115658A1 (en) * 2012-01-31 2013-08-08 Propeller Technology Ltd Propeller

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JPS59183001A (en) 1984-10-18
DE3460275D1 (en) 1986-08-14
AU2557884A (en) 1984-09-20
CA1229765A (en) 1987-12-01
AU571200B2 (en) 1988-04-14
NZ203600A (en) 1987-03-06
ZA842009B (en) 1984-10-31
MX161273A (en) 1990-08-27
EP0122726A1 (en) 1984-10-24

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