EP0346393A1 - Marine instrument - Google Patents

Marine instrument

Info

Publication number
EP0346393A1
EP0346393A1 EP88902996A EP88902996A EP0346393A1 EP 0346393 A1 EP0346393 A1 EP 0346393A1 EP 88902996 A EP88902996 A EP 88902996A EP 88902996 A EP88902996 A EP 88902996A EP 0346393 A1 EP0346393 A1 EP 0346393A1
Authority
EP
European Patent Office
Prior art keywords
paddlewheel
cavity
paddles
hull
sensor
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.)
Withdrawn
Application number
EP88902996A
Other languages
German (de)
English (en)
French (fr)
Inventor
Stephen G. Boucher
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.)
Airmar Technology Corp
Original Assignee
Airmar Technology Corp
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 Airmar Technology Corp filed Critical Airmar Technology Corp
Publication of EP0346393A1 publication Critical patent/EP0346393A1/en
Withdrawn legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/02Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring forces exerted by the fluid on solid bodies, e.g. anemometer
    • G01P5/06Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring forces exerted by the fluid on solid bodies, e.g. anemometer using rotation of vanes
    • G01P5/07Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring forces exerted by the fluid on solid bodies, e.g. anemometer using rotation of vanes with electrical coupling to the indicating device

Definitions

  • This invention is in the field of marine instrumentation for providing information with respect to the speed of marine vehicles through water.
  • U. S. Patent 4,555,938 describes a transom mounted marine speed sensor of the paddlewheel type, in which the paddles or blades are asymmetric in shape and formed of magnetized amorphous magnetic material.
  • the paddlewheel rotates about an axis which is transverse the direction of travel.
  • a Hall-effect device adjacent the paddlewheel senses the change in the magnetic field emanating from the paddles and generates an electrical signal directly proportional to the rotational speed of the paddlewheel.
  • the rotational speed of the paddlewheel is linearly related to the vessel speed, but this is not always the case; especially at the extremes of high and low speeds.
  • 3,457,782 employs a waterwheel having a plurality of buckets, closed at their side, and recessed in the peripheral edge of the wheel.
  • the slot within which the wheel rotates, is open on the downstream side. According to Maeder et al. , this provides a relief space which prevents a buildup of pressure on that side, which would vary the rotational characteristics of the wheel.
  • a boundary layer of water is formed on the hull of boats as the boat traverses the water.
  • the thickness of this layer varies principally with the speed of the boat and the distance of the layer from the leading edge of the water as it meets the bow or forward edge of the boat.
  • the fluid, i.e., water, within the boundary layer attaches to the vessel hull and flows at a lesser rate relative to the boat as compared with the water outside the layer. This rate varies throughout the thickness of the layer.
  • the boundary layer thickness ⁇ at the sensor is directly proportional to the distance "X" between the sensor and the leading edge. If the sensor paddles do not project beyond the thickness ⁇ £ , true speed is not sensed.
  • a new leading edge is obtained a known short distance away from the speed sensor.
  • This new leading edge may be conveniently obtained by providing a housing which projects below the hull.
  • the projecting portion of the housing has a pointed bow portion extending upstream which forms the new leading edge.
  • a pointed aft portion extends downstream.
  • the projecting section of the housing is horizontally aligned with the water surface by fairing blocks and projects a distance about equal to or greater than the largest anticipated thickness O of the new boundary layer formed by the new leading edge obtained at the bow of the projecting section at reasonable anticipated vessel speeds, i.e., about 3 miles per hour, or higher.
  • An intermediate portion of the projecting section houses the paddlewheel a predetermined, relatively short distance X 1 from the tip of the bow within a cavity formed therein.
  • the bow portion houses a sonar transducer element for sensing depth of water; while the aft portion houses a Hall-effect device for sensing the rotating magnetic field created as the paddlewheel revolves.
  • a thermal sensor in the form of a thermistor, may be located in the aft or bow portion, to sense water temperature.
  • is calculated to be about 0.1 inches at 5 miles per hour and becomes progressively thinner as speed is increased.
  • the paddle can be made with a minimum amount of projection, as compared to a system without a projecting housing, the bow of which forms a new leading edge.
  • Such a projecting sensor will produce substantially accurate water speed signals at low speeds while minimizing inaccuracy caused by changing boundary layer thickness at different speeds.
  • Paddle Shape The forward shape should have a relatively large coefficent of drag, as compared to the rearward shape, so as to minimize the force required to rotate the impeller within the cavity. As speed increases, i.e., at about 25-35 miles per hour, this force becomes greater due to turbulence in the enclosed cavity.
  • An acceptable fore-to-aft drag coefficient ratio is achieved in a preferred embodiment by forming the paddles in the shape of a half-hemisphere with the front of the paddle, presenting a blunt, or bluff, frontal surface and the shape at the rear of each paddle is formed as a curved half-hemispherical surface.
  • (ii) Hub Placement The paddlewheel should be vertically located within the cavity so that the periphery of the hub does not extend beyond the cavity. Pressure measurements, taken at several locations at the top of the paddlewheel cavity at various boat speeds, have shown that, as the hub is extended beyond the bottom of the cavity, negative pressure builds up within the cavity as speed is increased. The reason for this phenomena may be caused, in part, by the extended hub which deflects the water flow, creating an airfoil effect. I have found that by keeping the hub periphery level, or within the bottom of the cavity, reduces this tendency and increases the speed threshold before onset of cavitation.
  • Projection Ratio i.e., the ratio of paddle length (paddle projection), versus the overall radius of the paddlewheel. This minimizes negative pressure build-up within the cavity at increased speeds. Increasing negative pressure leads, eventually, to cavitation within the cavity, with resulting unpredictable behavior of the rotating paddlewheel. In accordance with the invention, a ratio of about 0.6, or less, has been found to be satisfactory for high speed operation.
  • Cross-Section Ratio i.e., the ratio of the cross-sectional shape of the paddles, taken in a plane transverse the direction of flow, versus the available cross-sectional space in the cavity, in the same plane, should be optimized within a range about 0.25 to 0.5.
  • this Cross-Section Ratio is in the order of 0.40. This ratio is achieved by symmetrically contouring, or rounding-off, the side walls of the paddles, at the tips and symmetrically removing material from the sidewalls as they join the hub.
  • the factors involved in optimizing the Cross-Section Ratio are paddle shape and material and slow speed slippage.
  • the paddle shape is constrained by the requirement for a high fore-to-aft drag ratio, the need ' to maximize paddle section near the outside diameter so as to generate maximum rotational force (torque) , and the need to have sufficient mass of amorphous magnetic material close to the cavity walls so as to generate sufficient magnetic field strength to switch commonly available Hall-cell devices.
  • Reducing the cross-section ratio allows the entrained water in the cavity to be laterally displaced at higher paddlewheel rotational speeds and allows some venting of the negative pressure buildup in the cavity.
  • the lower limit to cross-sectional ratio is dependent on the required linearity and accuracy of the paddlewheel at low boat speeds ( 5 miles per hour) .
  • the force applied to rotate the paddlewheel is proportionally reduced.
  • the profile drag may be somewhat reduced, due to the narrower section, the viscous drag (i.e., frictional drag) and bearing friction are not proportionally reduced. (The viscous drag remains nearly constant because the wetted surface of the paddlewheel is not reduced linearly with reduction in paddlewheel cross-section. )
  • Fig. 1 is an elevational frontal view of a high speed through-hull speed sensor in accordance with the invention in partial cut-away form including the hull 11 and shim and fairing 13 ⁇ and 13L, respectively.
  • Fig. 2 is a top view of the sensor of Fig. 1.
  • Fig. 3 is a cross-sectional view along the lines III-III of Fig. 1, which, for simplicity, omits the flanged nut 22 and the detail cross-section of transducer 60 and Hall-effect device 56.
  • Fig. 4 is an elevational plan view of paddlewheel 26 of the invention.
  • Fig. 5 is a side view of Fig. 4.
  • Fig. 6 is a cross-sectional view taken along lines VI-VI of Fig. 5.
  • Fig. " 7 is an elevational view of an alternate embodiment speed sensor in accordance with the invention with portions broken away.
  • Fig. 8 is a top view of Fig. 7.
  • Fig. 9 is a side view of Fig. 10.
  • Fig. 10 is an elevational plane view of a six-paddle paddlewheel used in the Fig. 7 embodiment.
  • Fig. 11 is a cross-sectional view taken along lines XI-XI of Fig. 9. Best Mode of Carrying Out the Invention
  • a preferred embodiment of the invention comprising a high speed through-hull tri-sensor device 10 for marine vessels.
  • the device 10 may be mounted through the hull 11 of a boat (not shown) .
  • the sensor has a housing designated, generally, by the numeral 12, comprising a vertically extending housing sleeve 12S, and lower body portion 12L, respectively.
  • the sleeve 12S is positioned in an opening through the hull 11.
  • Upper wedge or shim and lower fairing block 13U and 13L, respectively, are wedged between the top surface of lower body portion 12L, hull 11 and lock-nut 22, to position sensor 10 in a vertical plane.
  • Nut 22 preferably has a bottom skirt, or flange portion 22F, which rests against the upper shim 13U and a hexagonal nut portion 22 with internal threads, which engage a set of external threads 21 on the exterior periphery of the sleeve 12S.
  • a tubular body 52 the lower portion of which forms the paddlewheel cavity 30, is adapted to slideably insert into the sleeve 12S.
  • Seal rings 32 and 34 are disposed in grooves on the periphery of the body 52 and form a fluid-tight seal between the body and sleeve.
  • Body 52 is of tubular shape and is formed of metal or plastic.
  • a cable 16 containing wires 19 is coupled through a bored hole 27 formed in an enlarged wall of the sleeve 12S.
  • Wires 19 provide electrical connection to components, such as Hall-effect device 56, sonar transducer 60, and thermistor 62, affixed to the inner walls of lower body portion 12L.
  • the upper end of body 52 includes a tab 20, through which a pull ring 18 is attached.
  • a second pull ring 14 is affixed to pin 17 which extends through a bore in sleeve 12S and a transverse bore in body 52.
  • the relative location of the bores assures that when pin 17 is in place, the body 52 is vertically aligned so- hat the bottom wall 52B is coplanar, or flush, with the bottom of the housing.
  • Removable lock ring 15 is used to secure the pin 17 in place.
  • a paddlewheel 26 is rotatably mounted on axle 28 within the cavity 30 formed in the lower portion of body 52.
  • Paddlewheel 26 is an integral structure having a hub 38 from which four asymmetric shaped paddles extend about the periphery thereof.
  • the axle 28 rotates within bearings 37 disposed in a bore 39 which extends through a central opening in the hub 38, and into opposing recessed holes in the cavity side walls formed in body 52.
  • the paddlewheel 26 is thereby rotatably suspended within the cavity 30.
  • paddlewheel 26 is formed of amorphous magnetized material, such as barium ferrite.
  • the paddles 42 may be polarized with respect to the hub, or with respect to each other. As the paddles rotate about the shaft when the vessel traverses the water, ' the variation in magnetic field is sensed by a Hall-effect device 56 mounted on an interior wall 121 of housing 12.
  • the lower portion 12L of the housing extends about 1 inch, or more, (due to the fairing block) , into the water in operation, and thus may be more readily subjected to impact from objects than prior art flush mounted, or low profile flanged, through-hull sensors. If the housing breaks, water may enter the boat through the opening. Therefore, the housing should preferably be made of thick cast, non-corrosive metal.
  • housing 12 should be constructed of non-ferrous metal, so that it will be permeable to the magnet field emanating from the paddlewheel. Bronze is therefore a preferred material, since it meets all of the above criteria. '
  • Sonic transducer assembly 60, thermal sensing device 62, and Hall-effect device 56 are substantially " as described in U. S. Patent No. 4,555,938, and are electrically coupled via wires 19 to depth indicator 90, temperature display 80, and speed display 70, respectively; also as described therein.
  • the interior of the lower housing, at the bow end 12B, contains sensors 60 and 62 and is encapsulated in potting material 64, such as polyurethane.
  • potting material 64 such as polyurethane
  • the interior at the aft end 12A, containing Hall-effect device 66 is encapsulated with polyurethane 64.
  • the upper wall 44 of cavity 30 is an arched surface, closely spaced from the tip T of the four paddles 42 as they rotate about axle 28.
  • the periphery P of the hub 38 is approximately flush with the bottom surface B of the cavity.
  • the profile of the paddles is contoured as a bluff frontal surface F and a convex curve aft surface A to produce a high drag coefficent ratio (aft versus fore) of about 2.8.
  • a high fore-to-aft ratio is produced when the aft drag coefficient is low and the fore drag coefficient is high.
  • the fore shape is a flat, or near planar, surface and the high fore drag coefficent of the paddle is calculated as about 1.17.
  • the aft shape is a convex half-hemisphere producing a calculated low aft drag coefficient of about 0.42. This should be compared with the fore-to-aft ratio for the asymmetric paddles of U. S. Patent No. 4,555,938, which is ' calculated to be about 1.5.
  • the radius of the paddlewheel 26, measured from tip to center, is about 0.61 inches and the four paddles 42 project a distance of about 0.33 inches from- the cavity bottom B to produce a relatively low paddle projection to paddlewheel radius ratio
  • Projection Ratio of about 0.55.
  • Known prior art paddlewheel sensors such as that shown in U. S. 4,555,938, have had Projection Ratios as high as 0.8.
  • a ratio of 0.6, or less is required for high speed performance.
  • the cross-sectional shape of the paddles 42 taken in a plane transverse the direction of flow versus the available cross-sectioned space in the cavity in the same plane, i.e., Cross-Sectional Ratio, should be kept to a ratio of between 0.25 to 0.5. In accordance with the present invention, this ratio is in the order of 0.40.
  • This ratio is achieved by using a relatively thin cross-sectional paddle and by symmetrically rounding off the side walls W (See Fig. 4) of the paddles at the tips and symmetrically removing material from the sidewalls as they join the hub. This reduces the numerator of the ratio, i.e., paddle cross-section.
  • the paddlewheel diameter is about 1.22 inches and the hub diameter is about 0.50 inches, resulting in a paddle length of about 0.36 inches.
  • the paddle width is about 0.335 inches and the minimum gap between the paddle tips T and the top of the cavity is about .030 inches.
  • the cross-sectional ratio is computed as follows:
  • the paddle profile can be modelled as a circle with a diameter of 0.335 inches, which yields an area of about .088 square inches. Correcting for area mainly at the root (base) of the paddle adds about .008 square inches. Therefore, the cross-sectional ratio is:
  • Figs. 7 and 8 show an alternate embodiment of the invention, wherein corresponding parts carry the same numeral with a prime suffix.
  • a low profile through-hull speed-only-sensor 10' is provided, which mounts on a hull with the lower housing portion 12L' extending through the hull between wing nut 78 and lower flange 12F on housing 12'.
  • Tubular housing 12 may be formed of rigid plastic material with peripheral external threads 21' which engage with internal threads on cap 114 and nut 78.
  • a tubular body 52' is slideably insertable with O-rings 32', forming a fluid-tight seal between housing 12' and body 52.
  • Hall-effect device 56' is encapsulated in body 52' within the roof or arch above cavity 30' closely adjacent paddlewheel 26' rotatably mounted on axle 28' within cavity 30'.
  • Cable 16* is potted within body 52* and couples wires between the Hall-effect device 56' and a speed meter (not shown) .
  • Tab 20' is formed on body 52' and pull ring 18' is disposed in a transverse hole on tab 20' to enable body 52' to be removed from the housing 12 ' .
  • the arrow A indicates the bow direction in which the paddle would face when secured by cap 114.
  • the cavity 30' and paddlewheel 26' may be appropriately dimensioned, as described in the above referenced tri-sensor embodiment.
  • Figs. 9, 10 and 11 show the details of the paddlewheel 26', which has six paddles 42' extending from the hub 38'. Six paddles are preferred in some applications because of the high possible pulse rate produced. Also, a six paddle device has less tendency to stall at low speeds. The fore-to-aft ratio is about 2.8, as in the previous embodiment.
  • the Cross-Sectional Ratio of this embodiment is identical to the previous embodiment, i.e., 0.40.
  • the Projection Ratio is 0.45.
  • the periphery P of hub 38' is located at, or above, the lower surface of the cavity 30' .

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Measuring Volume Flow (AREA)
  • Transmission And Conversion Of Sensor Element Output (AREA)
  • Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)
  • Lubrication Of Internal Combustion Engines (AREA)
  • Geophysics And Detection Of Objects (AREA)
EP88902996A 1987-01-28 1988-01-27 Marine instrument Withdrawn EP0346393A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US752787A 1987-01-28 1987-01-28
US7527 1987-01-28

Publications (1)

Publication Number Publication Date
EP0346393A1 true EP0346393A1 (en) 1989-12-20

Family

ID=21726725

Family Applications (1)

Application Number Title Priority Date Filing Date
EP88902996A Withdrawn EP0346393A1 (en) 1987-01-28 1988-01-27 Marine instrument

Country Status (6)

Country Link
EP (1) EP0346393A1 (ko)
JP (1) JPH02501950A (ko)
KR (1) KR960014484B1 (ko)
AU (1) AU605281B2 (ko)
CA (1) CA1313775C (ko)
WO (1) WO1988005915A2 (ko)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0005872D0 (en) * 2000-03-10 2000-05-03 Tacktick Ltd Boat speed measuring apparatus

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4399695A (en) * 1980-02-12 1983-08-23 Peyton Ralph B Underwater sensing mechanism and method
DE3011531C2 (de) * 1980-03-21 1983-01-13 Trion Präzisionselektronik Herstellungs- und Verbriebs GmbH, 1000 Berlin Geschwindigkeitsmesser für Wasserfahrzeuge
DE3219393C1 (de) * 1982-05-24 1983-04-14 Dieter 8034 Germering Flasch Geschwindigkeitsmesser für strömende Medien
DE3238433A1 (de) * 1982-10-16 1984-04-19 Vdo Adolf Schindling Ag, 6000 Frankfurt Geschwindigkeitsmesser
US4555938A (en) * 1984-06-01 1985-12-03 Airmar Technology Corporation Marine instrument
JPS60145340A (ja) * 1984-08-06 1985-07-31 Res Inst Iron Steel Tohoku Univ シリコンカ−バイド繊維強化アルミニウム複合材料の製造方法
US4644788A (en) * 1985-12-06 1987-02-24 Airmar Technology Corporation Modular marine instrument

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO8805915A2 *

Also Published As

Publication number Publication date
AU605281B2 (en) 1991-01-10
WO1988005915A2 (en) 1988-08-11
JPH02501950A (ja) 1990-06-28
WO1988005915A3 (en) 1988-09-22
AU1495488A (en) 1988-08-24
KR960014484B1 (ko) 1996-10-16
CA1313775C (en) 1993-02-23
KR890700834A (ko) 1989-04-27

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