WO2006001747A1 - Foldable propeller - Google Patents

Foldable propeller Download PDF

Info

Publication number
WO2006001747A1
WO2006001747A1 PCT/SE2005/000918 SE2005000918W WO2006001747A1 WO 2006001747 A1 WO2006001747 A1 WO 2006001747A1 SE 2005000918 W SE2005000918 W SE 2005000918W WO 2006001747 A1 WO2006001747 A1 WO 2006001747A1
Authority
WO
WIPO (PCT)
Prior art keywords
blade
propeller
hub
boat
segment
Prior art date
Application number
PCT/SE2005/000918
Other languages
English (en)
French (fr)
Inventor
Jan Karlsson
Original Assignee
Ingeniosus Ab
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 Ingeniosus Ab filed Critical Ingeniosus Ab
Priority to EP05752541A priority Critical patent/EP1768892A1/en
Publication of WO2006001747A1 publication Critical patent/WO2006001747A1/en

Links

Classifications

    • 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
    • B63H1/20Hubs; Blade connections
    • B63H1/22Hubs; Blade connections the blades being foldable
    • B63H1/24Hubs; Blade connections the blades being foldable automatically foldable or unfoldable

Definitions

  • the present invention relates to a foldable propeller for a boat, comprising a hub for fitting to a driveshaft of the boat and at least two propeller blades pivotably arranged about a spindle of the hub between a substantially folded first position and a substantially deployed second position according to the preamble of the subsequent claim 1.
  • Such a propeller is usually adapted to being usable together with an engine to propel the boat forwards or rearwards.
  • propellers are made foldable, i.e. with propeller blades fastened to a hub pivotably so that they can be folded together (by the boat's movement through the water) in the direction defined by the propeller's driveshaft, to a position in which they extend in the longitudinal direction of the boat.
  • the blades are deployed by centrifugal force due to rotation of the driveshaft.
  • propeller blades are normally designed to constitute a streamlined body, thereby reducing drag resistance.
  • WO 93/01972 refers to a propeller comprising at least three blades which are arranged to pivot between a deployed position and a folded position.
  • propellers with blades which can be folded together usually result in little drag resistance, but the propulsive action of these known propellers is relatively poor when travelling forwards and, above all, when travelling rearwards.
  • a particular problem of previously known foldable propellers concerns propulsion power when travelling rearwards.
  • High propulsion power rearwards when the boat is moving forwards, e.g. when decelerating close to a landing, is usually achieved by increasing the weight at the blade tips and thereby increasing the centrifugal force which causes the blades to pivot about their pivot spindle. The angle of opening of the blades is thus increased.
  • increasing the weight at the blade tips entails problems either in the form of thick blade portions with bad cavitation characteristics, or in the form of long blade portions which tend to reduce propeller efficiency, particularly at increased boat velocity, when the propeller is acting in the forward direction.
  • a further problem of known foldable propellers is the relatively large forces which occur when propeller blades deployed by the propeller being caused to rotate reach their limit-position stop, resulting in undesirable noise and a "power shock" which is transmitted via the driveshaft and the engine to the hull.
  • a general problem of propellers is achieving both high propulsive force and high propeller efficiency when travelling forwards at any desired velocity.
  • the general solution to this problem is large propeller diameter combined with low driveshaft speed.
  • the propeller's radial load distribution needs to be optimum and the blade area large enough to prevent cavitation.
  • the blades need to have thin bent sections of the aerofoil type. Providing foldable propellers with thin blades is a particular problem in that doing so often conflicts with the need for the blades to be heavy enough to ensure that they will always deploy.
  • the object of the present invention is to provide a foldable propeller which solves the problems mentioned above. This object is achieved with a foldable propeller according to the present invention, whose characteristics are defined in the subsequent claim 1.
  • the invention thus relates to a foldable propeller for a boat, comprising a hub for fitting to a driveshaft of the boat and at least two propeller blades pivotably arranged about a spindle of the hub between a substantially folded first position and a substantially deployed second position.
  • the propeller is distinguished particularly by:
  • propeller blades take the form of a first and a second blade element, each of which elements comprises blade segments on opposite sides of said spindle, and by
  • the blade segments of each blade element are provided with different blade shapes on opposite sides of said spindle. More precisely, the blade shape of one blade segment, the main blade segment, is designed to cause greater drag resistance than the second blade segment, the secondary blade segment. The result is that the propeller folds together when it is not rotating and the boat is moving through the water, e.g. during sailing.
  • said greater drag resistance of the main blade segment is achieved by the latter' s blade area being so disposed as to cause more resistance than the blade area of the secondary blade segment. More precisely, the main blade segment is provided with a larger blade width at a radius (r) from said spindle than the secondary blade segment at the same radius (r).
  • the hub is provided with a recess for accommodating two of the secondary blade segments of the blade elements when the propeller is in its folded position.
  • the propeller thus meets the requirement of relatively low drag resistance when it is not being used for powering the boat, i.e. when it is not rotating.
  • said recess is provided by the hub being fork-shaped with two parallel fork limbs extending in the longitudinal direction of the hub, whereby said recess takes the form of an aperture running through between the fork limbs.
  • a limit-position stop against which the respective blade element abuts when the propeller is in its deployed position is provided on the inside of each of the fork limbs, i.e. in said recess. This enables accurate mutual positioning of the blade elements, thereby ensuring that an optimum propeller blade profile is always achieved.
  • Figure 1 shows a sideview of the propeller in its deployed position according to the present invention
  • Figure 2 shows the propeller as seen from directly behind in its deployed position with the propeller rotating and operating in the forward direction
  • Figure 3 shows the propeller as seen from directly behind in its deployed position with the propeller rotating and operating in the reverse direction
  • Figure 4 shows the propeller in a position halfway between its folded and deployed positions
  • Figure 5 shows a sideview of the propeller in ks folded position.
  • ref. 1 denotes generally a propeller with a hub 2 for fitting to a driveshaft 3 of a boat (not shown).
  • the propeller 1 in its deployed position has two substantially identical propeller blades 4, 5.
  • the propeller blades 4, 5 take the form of a first blade element 6 and a second blade element 7, each of which elements comprises, on opposite sides of a spindle 8, blade segments 9, 10, 11, 12 whereby a blade segment 9, 10 from one blade element 6 and a blade segment 11, 12 from a second blade element 7 together constitute a propeller blade 4, 5 in the deployed position.
  • Each blade element 6, 7 is made of, for example, bronze, aluminium bronze (containing 8-10% aluminium), steel or a plastic fibre composite.
  • the hub 2 may be made of similar material.
  • each of the blade elements 6, 7 is fastened, pivotably about said spindle 8, to the hub 2, said spindle 8 extending through cooperating holes 13 in the hub 2
  • the blade segments 9, 10, 11, 12 of a blade element 6, 7 are provided with different blade shapes on opposite sides of the spindle 8. More precisely, the blade shape of one blade segment 10, 11, the main blade segment, is designed to cause greater drag resistance than the second blade element 9, 12, the secondary blade segment. The result, when the propeller is not rotating and the boat is moving through the water, is a greater turning moment of the main blade segment 10, 11 about the spindle 8 than of the secondary blade segment 9, 12, thereby leading to the main blade segment 10, 11 being folded rearwards, i.e. folding together of the propeller 1, e.g. during sailing.
  • the blade area of the main blade segment 10, 11 is larger than the blade area of the secondary blade segment 9, 12 since the main blade segment 10, 11 is provided with a larger blade width at a radius (r) from said spindle than the secondary blade segment at the same radius (r).
  • the blade width of the secondary blade segment 9, 12 is about 0.3 to 0.4 times the blade width of the main blade segment 10, 11 at a radius (r), and a blade width 0.35 times the blade width of the main blade segment 10, 11 is particularly preferred.
  • the area of the main blade segment 10, 11 is 70-130% larger than the blade area of the secondary blade segment 9, 12, and a 90-110% relationship is particularly advantageous.
  • the two blade elements 6, 7 are identical, making it possible to simplify manufacturing and hence be able to ensure relatively low production costs.
  • the pressure centre 20, 21 shifts to a distance which corresponds to about one-third of the total deployed width of the propeller blade from the new front edge 15, 16.
  • the fact that the secondary blade segment 9, 12 is so designed that the pressure centre 20, 21 is situated on it results in the turning moment on the blade element 6, 7 about the spindle 8 being greater from the secondary blade segment 9, 12 than from the main blade segment 10, 11, thereby, in a manner similar to that described above, causing the blade element 6, 7 to abut against the limit-position stop 22.
  • Figure 5 depicts the propeller 1 in its folded position, i.e. with the blade elements 6, 7 substantially parallel with the longitudinal direction of the hub 2 and thereby constituting a streamlined body with low drag resistance.
  • the propeller may be provided with four propeller blades.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • Motor Power Transmission Devices (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
PCT/SE2005/000918 2004-06-24 2005-06-14 Foldable propeller WO2006001747A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP05752541A EP1768892A1 (en) 2004-06-24 2005-06-14 Foldable propeller

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SE0401652A SE526414C2 (sv) 2004-06-24 2004-06-24 Fällbar propeller
SE0401652-3 2004-06-24

Publications (1)

Publication Number Publication Date
WO2006001747A1 true WO2006001747A1 (en) 2006-01-05

Family

ID=32733682

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/SE2005/000918 WO2006001747A1 (en) 2004-06-24 2005-06-14 Foldable propeller

Country Status (3)

Country Link
EP (1) EP1768892A1 (sv)
SE (1) SE526414C2 (sv)
WO (1) WO2006001747A1 (sv)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104002946A (zh) * 2014-06-16 2014-08-27 国家海洋技术中心 可收放式螺旋桨推进装置
EP2888165A4 (en) * 2012-08-24 2016-04-13 Zee Aero Inc VARIABLE GEOMETRY SUSTENTATION BLOWER MECHANISM
US9540103B2 (en) 2014-06-24 2017-01-10 Kitty Hawk Corporation Passive deployment mechanism for lift fan

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2608257A (en) * 1951-09-29 1952-08-26 Bert O Godfrey Marine propeller
US3982853A (en) * 1975-07-23 1976-09-28 David Walter Beck Folding boat propeller
US4207028A (en) * 1979-06-12 1980-06-10 Ridder Sven O Extendable and retractable propeller for watercraft
US4242049A (en) * 1978-02-06 1980-12-30 Hasselfors Stainless Ab Foldable propeller
US4364711A (en) * 1980-01-16 1982-12-21 Ab Volvo Penta Folding boat propeller

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2608257A (en) * 1951-09-29 1952-08-26 Bert O Godfrey Marine propeller
US3982853A (en) * 1975-07-23 1976-09-28 David Walter Beck Folding boat propeller
US4242049A (en) * 1978-02-06 1980-12-30 Hasselfors Stainless Ab Foldable propeller
US4207028A (en) * 1979-06-12 1980-06-10 Ridder Sven O Extendable and retractable propeller for watercraft
US4364711A (en) * 1980-01-16 1982-12-21 Ab Volvo Penta Folding boat propeller

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2888165A4 (en) * 2012-08-24 2016-04-13 Zee Aero Inc VARIABLE GEOMETRY SUSTENTATION BLOWER MECHANISM
CN104002946A (zh) * 2014-06-16 2014-08-27 国家海洋技术中心 可收放式螺旋桨推进装置
US9540103B2 (en) 2014-06-24 2017-01-10 Kitty Hawk Corporation Passive deployment mechanism for lift fan

Also Published As

Publication number Publication date
EP1768892A1 (en) 2007-04-04
SE0401652L (sv) 2005-09-13
SE0401652D0 (sv) 2004-06-24
SE526414C2 (sv) 2005-09-13

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