EP0963315B1 - Mehrpropeller system mit ausgleichsgetriebe - Google Patents

Mehrpropeller system mit ausgleichsgetriebe Download PDF

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Publication number
EP0963315B1
EP0963315B1 EP98905432A EP98905432A EP0963315B1 EP 0963315 B1 EP0963315 B1 EP 0963315B1 EP 98905432 A EP98905432 A EP 98905432A EP 98905432 A EP98905432 A EP 98905432A EP 0963315 B1 EP0963315 B1 EP 0963315B1
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EP
European Patent Office
Prior art keywords
propeller
multipropeller
differential
drive wheel
drive shaft
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
EP98905432A
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English (en)
French (fr)
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EP0963315A1 (de
Inventor
Jouko Viljo Kalervo Niemi
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Individual
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Individual
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Publication date
Priority claimed from FI970778A external-priority patent/FI970778A0/fi
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Publication of EP0963315A1 publication Critical patent/EP0963315A1/de
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H5/00—Arrangements on vessels of propulsion elements directly acting on water
    • B63H5/07—Arrangements on vessels of propulsion elements directly acting on water of propellers
    • B63H5/08—Arrangements on vessels of propulsion elements directly acting on water of propellers of more than one propeller
    • B63H5/10—Arrangements on vessels of propulsion elements directly acting on water of propellers of more than one propeller of coaxial type, e.g. of counter-rotative type

Definitions

  • the invention relates to a differential multipropeller system that is suited to be used especially in watercraft propulsion devices, but also in other applications.
  • the invention relates to a multipropeller system in which the ratio of the rotational speeds of the propellers is not fixed.
  • Multipropeller systems where at least two propellers are arranged concentrically in succession and relatively near to each other, have several verified advantages, such as the elimination of torques caused by the rotation of the propellers, which torques tend to deviate a craft from its direction of motion.
  • the most common multipropeller systems designed for watercraft propulsion devices are provided with two propellers.
  • a first bevel gear that transmits the rotary motion of the drive shaft to the second and third bevel gears located at the front end of the propeller shafts, said second and third bevel gears being of equal sizes and located on different sides of the first bevel gear.
  • the equal size of the second and third bevel gears provided in the propeller shafts results in that the torques and angular velocities of the propeller shafts always have the same absolute values.
  • the location of the second and third bevel gear on opposite sides of the first bevel gear results in that the angular velocities of the propeller shafts always have opposite signs.
  • a system composed of a differential torque system and two propellers connected thereto can be called a differential double-propeller system.
  • this arrangement achieves many advantages in comparison with the equal torque system, but the structure of the differential double-propeller systems described in the US patent 5,009,621 is very complicated, wherefore their production costs rise high, and they contain several weak spots that are susceptible to damages.
  • the object of the present invention is to introduce a differential multipropeller system with a simple and solid structure.
  • the system according to the invention is characterized in that the drive shaft is concentric with the two propellers and extends through both of them.
  • the first propeller or a part immediately connected thereto is in a way assumed as part of the torque splitting device, which divides the torque obtained from the drive shaft between the first and the second propeller.
  • a first gear or friction wheel attached to the drive shaft moves one or several second gear or friction wheels, the motion of which rotates the first propeller in a direction perpendicular to the shaft(s) of the second gear or friction wheel(s).
  • the second gear or friction wheel(s) transmit part of the motion further to a third gear or friction wheel, which is advantageously located concentrically with the drive shaft, but is not attached thereto, but to the second propeller.
  • the splitting of the torques between the propellers according to the invention results in that on the average, the absolute value of the angular velocities of the propellers is only part of the angular velocity of the drive shaft, i.e. the system includes an integrated reduction gearing.
  • the absolute value of the angular velocities of the propellers is usually something like half of the angular velocity of the drive shaft.
  • the integrated reduction gearing is particularly advantageous in systems where the drive shaft is rotated by an electric motor, because the rotational speed of the electric motor may be made higher than without the reduction gearing, and consequently the diameter of the electric motor can be smaller.
  • the integrated gearing is also advantageous in applications where a propeller system according to the invention is used to rotate the drive shaft of a generator or a turbine, in which case it acts as a step-up gear: the rotational speed of the turbine axis is higher than the rotational speed of either one of the propellers.
  • Figure 1 is a schematical cross-section of a differential double-propeller system 100 comprising a first propeller 101 and a second propeller 102.
  • the drive shaft 103 extends throughout the whole system, and for rotating said shaft, there is provided a motor or a similar device which is not illustrated in the drawing.
  • a first bevel gear 104 which in this embodiment of the invention is installed in a position where its conical cogged surface tapers towards the outermost end of the drive shaft 103, i.e. to the left with respect to the position illustrated in the drawing.
  • the second bevel gears 105a and 105b are located at an angle of 90 degrees with respect to the first bevel gear 104, and so that while the first bevel gear turns around, it rotates the second bevel gears.
  • the shafts 106a and 106b of the second bevel gears are attached with bearings to the recesses 107a and 107b provided in the first propeller 101.
  • the third bevel gear 108 is like a mirror image of the first bevel gear 104 in relation to the plane where the shafts 106a and 106b of the second bevel gears are located.
  • the third bevel gear 108 is not attached to the part of the drive shaft 103 passing therethrough, but can freely rotate around it.
  • the third bevel gear 108 is attached to the second propeller 102 by intermediation of a tubular shaft 109.
  • the third bevel gear 108 could also be attached directly to the second propeller 102, without the tubular shaft, or it could even be part of the same piece.
  • a support cone 110 and a locking nut 111 At the outermost end of the drive shaft 103, there are provided a support cone 110 and a locking nut 111, the purpose whereof is to keep the propellers 101 and 102 attached to the drive shaft 103.
  • the locking nut 111 is opened, so that the support cone 110 and the propellers 101 and 102 can be pulled apart from the drive shaft 102.
  • All gear wheels illustrated in the structure, as well as the gear wheels illustrated below in connection with other preferred embodiments, could also be friction wheels. Gear wheels and friction wheels may be commonly designated as drive wheels.
  • first bevel gear 104 When the first bevel gear 104 turns around along with the drive shaft, it tends to rotate the second bevel gears 105a and 105b, each around its respective shaft 106a and 106b. It also tends to revolve the whole assembly of second bevel gears 105a and 105b and shafts 106a and 106b around the drive shaft.
  • Figure 1 illustrates two second bevel gears 105a and 105b.
  • the invention does not, however, restrict the number of these gear wheels; consequently, there can be one or two or as many gear wheels as can be fitted around the first and third bevel gears.
  • a natural alternative to attaching the shafts 106a and 106b of the second bevel gears with bearings to the recesses 107a and 107b provided in the first propeller 101 is to provide bearings between each second bevel gear and the respective shaft and to attach the shafts rigidly to the first propeller.
  • Figure 2 is a schematical cross-section of a preferred embodiment 200 of the invention, which embodiment in a way is a mirror image of the embodiment of figure 1.
  • the drive shaft 203 is rotated, with respect to the position illustrated in the drawing, at the left-hand end of the drive shaft, and the support cone 210 and locking nut 211 that keep the propellers locked in place are located at the right-hand end of the drive shaft.
  • the first bevel gear 204 is arranged so that its conical toothed surface tapers towards the inner end of the drive shaft 203.
  • the embodiment of figure 2 corresponds to that of figure 1, and in the light of the description given above, the operation of the embodiment of figure 2 is easily understood.
  • Figure 3 is a schematical cross-section of an embodiment 400 of the invention, where the gear wheel assembly formed by the bevel gears 404, 405a, 405b and 408 is not located inside the propellers but in a transmission housing 420, which may also contain other parts connected to power transmission and even a whole engine that rotates the drive shaft 403.
  • the shafts 406a and 406b of the second bevel gears 405a and 405b are attached with bearings to the recesses 407a and 407b provided in the propeller shaft 421, so that they transmit the rotary motion to the first propeller 401 by intermediation of the tubular propeller shaft 421.
  • the system according to this embodiment functions in similar fashion as the embodiment illustrated in figure 1.
  • Figure 4 illustrates a modification 600 of the invention comprising a total number of four propellers 601, 602, 603 and 604. From the bevel gear 606 arranged at the end of the drive shaft 605, power is transmitted to the first and second propeller 601 and 602 in similar fashion as in the embodiment of figure 1. To the drive shaft, there also is attached a fourth bevel gear 607 which transmits power to the third and fourth propeller 603 and 604.
  • the invention does not restrict the number of propellers that can be installed successively in the described manner, but the motional resistances caused by the bevel gears become a restricting factor at some stage.
  • This type of embodiment is suited for instance in an axial pump where the propellers 601 - 604 are located inside a cylindrical chamber, so that they push water or other medium contained in the cylinder towards the other end of said cylinder.
  • Figure 5 illustrates another preferred embodiment 700 of the invention in a partial cut-out diagram.
  • the first gear wheel 701 attached to the drive shaft 702, and the second gear wheels 703a and 703b operationally engaging with the first gear wheel 701 are not conical but cylindrical in shape with their outer cylindrical surfaces toothed.
  • the third gear wheel 704 is an inner-toothed cylindrical gear having an inner cylindrical toothed surface that operationally engages with the second gear wheels 703a and 703b; the general form of the third gear wheel 704 that of a "bowl” enclosing the second and first gear wheels, with a hole through the bottom of the "bowl” for the drive shaft 702 to pass through.
  • the toothed surface of the third gear wheel 704 is the inner surface of the walls of the "bowl". With respect to simple manufacturing it may be more appropriate to provide a simple ring-formed inner-toothed gear as the third gear wheel.
  • the shafts 705a and 705b of the second gear wheels 703a and 703b are parallel to the drive shaft 702 and have their other ends attached with bearings to the recesses 706a and 706b in the first propeller 707. Again the shafts 705a and 705b of the second gear wheels may be attached essentially rigidly to the first propeller 707 if there are bearings between each second gear wheel and the respective shaft.
  • the third gear wheel 704 is essentially rigidly connected to the second propeller 708.
  • the operation of the embodiment of figure 5 is analogous to that of the embodiments described above.
  • the first gear wheel 701 rotates along with the drive shaft 702, tending to rotate the second gear wheels 703a and 703b each around its corresponding shaft. If, for some reason, the third gear wheel 704 could not rotate, the second gear wheels 703a and 703b would roll between the rotating first gear wheel 701 on their inside and the stationary third gear wheel 704 on their outside, resulting in the shafts 705a and 705b being revolved around the drive shaft 701 like the cartridges in the cylinder of a revolver.
  • the revolving movement of the shafts 705a and 705b is synonymous to the rotation of the first propeller.
  • the rotation of the first propeller 707 be prevented while the third gear wheel 704 is allowed to rotate freely, the rotating movement of the drive shaft 701 would only rotate each second gear wheel 703a and 703b around its corresponding shaft 705a and 705b. This, in turn, would cause the third gear wheel 704 (and the second propeller 708 along with it) to rotate into the direction opposite to that of the drive shaft rotation.
  • bearings and/or lubrication must be provided in between all parts that slide against each other, and that the seepage of water or other surrounding medium to the gear wheels and bearings must be prevented by means of a suitable sealing.
  • bearings, lubrication and sealing represent known technology, and they are not significant as for the characteristic novel features of the invention, wherefore they are, for the benefit of both graphic and textual clarity, left out of the figures 1 - 5 and of the associated descriptions.
  • the invention does not require any particular propeller diameter or shape or number of blades, but also these structural parameters can be adjusted to be suitable by way of trial and by taking into account the power of the motor used at any given time, the size and desired velocity of the craft in question, as well as other affecting factors.
  • a particularly advantageous embodiment of the invention is such where at least one of the propellers is made adjustable.
  • adjustable propeller There are numerous known ways of producing an adjustable propeller; they are most commonly found in connection with airplane engines where the adjustable parameter is the blade angle. Adjustment of the propeller may be based on mechanics, pneumatics, hydraulics, electronics or any combination of these.
  • a popular and simple construction includes a toroidal, nonrotating part placed around the drive shaft movably in the longitudinal direction thereof.
  • a roller bearing communicates the linear movement of the toroidal part to a corresponding part in the propeller hub, where an arrangement of levers transforms the linear movement into a synchronised rotational movement of the propeller blades around their corresponding longitudinal axes.
  • An adjustable propeller known as such is easily fitted into a construction according to the invention, where it gives the user a large freedom to dynamically choose the operational parameters of the propeller system.
  • Figure 6 illustrates how the invention is applied in an azimuth propulsion device 500, which is a propulsion device that is attached to the bottom of a craft and turns around a pivoted-axis 501.
  • the housing 502 of the azimuth propulsion device may contain an electric motor that rotates the drive shaft, from which the motion is transmitted to the differential multipropeller system according to the invention, said system comprising in this embodiment the propellers 503 and 504. Because the system according to the invention comprises an integrated reduction gear, the propellers 503 and 504 each rotate approximately at a speed the absolute value of which is half of the rotational speed of the rotor of the electric motor.
  • the electric motor can be constructed so that the higher its rotational speed in normal use, the smaller its diameter; consequently, owing to the present invention, the housing 502 of the azimuth propulsion device can be made smaller in cross-sectional surface than in the known arrangements of the prior art, where the rotary motion is transmitted from the electric motor to the propeller without a reduction gear.
  • a small cross-sectional area means a low flow resistance, and it also means that the housing of the propulsion device is a lesser obstruction to the water flowing to the propellers, wherefore the efficiency of the propellers is improved.
  • the invention can also be applied in water jet propulsion devices, where the water is sucked in through a suction hole or holes, provided at the bottom of the craft, to a flow channel containing a propeller assembly that pushes the water out at a strong force through a blow aperture or apertures provided at the rear of the craft.
  • the advantage brought about by the invention is that the share of the motor and/or gear system in the transversal surface area of the flow channel is smaller than in prior art arrangements applying the multipropeller system, as well as the fact that the structure according to the invention is extremely solid.
  • Another application of the invention where the integrated gearing and propeller assembly would most advantageously be fitted in a tube would be a turbine of a hydro-electric power installation, operating either under the unidirectionally flowing conditions of a river power plant or the alternatingly flowing conditions of a tidal power station.
  • a turbine of a hydro-electric power installation operating either under the unidirectionally flowing conditions of a river power plant or the alternatingly flowing conditions of a tidal power station.
  • the integrated gearing inherent to the invention will act as a step-up gearing, giving the turbine shaft a higher angular velocity than in known multipropeller solutions.
  • the argument of smaller transversal surface area of the flow channel being taken by the gear system also applies.
  • the invention does not restrict the ways by which the drive shaft rotating the multipropeller system is set to rotate in the propulsion applications, wherefore the invention can be applied in propulsion devices driven both by combustion engines and electric motors as well as in hydraulic propulsion devices.
  • the simplicity of the invention ensures that the drive shaft extends through the propellers, which makes the structure very solid.
  • the invention can also be applied in assemblies where the rotation of the propellers by for example water or air flow rotates the drive shaft and not vice versa. For instance an electric generator can then be connected to the drive shaft.
  • Shafts in general should be understood in their widest meaning in the present patent application.
  • the shaft of a gear wheel is the part that gives mechanical support to the gear wheel and is essentially stationary with respect to the rotational motion of the gear wheel, irrespective of the design and mechanical details of the parts.
  • the invention does not require that the first and second propellers should be placed in immediate succession.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Gear Transmission (AREA)
  • Amplifiers (AREA)
  • Nitrogen And Oxygen Or Sulfur-Condensed Heterocyclic Ring Systems (AREA)
  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)
  • Hardware Redundancy (AREA)
  • Dc Digital Transmission (AREA)
  • Gears, Cams (AREA)

Claims (8)

  1. Ein Mehrpropeller System mit Ausgleichsgetriebe (100, 200, 400, 600, 700) bestehend aus einen Antriebswelle (103, 203, 403, 605, 702) zur Übertragung von Rotationskraft zu und/von dem Differentialmultipropellersystem, und einem ersten Propeller (101, 601, 707) und einem zweiten Propeller (102, 602, 708); die besagten Propeller (der erste und der zweite) sind konzentrisch in einer Nacheinanderfolge arrangiert, wobei die kennzeichnende Eigenart ist, dass
    es aus einem ersten Antriebsrad (104, 204, 404,701), aus einem zweiten Antriebsrad (105a, 105b, 405a, 405b, 703a, 703b), aus einer zweiten Antriebsradwelle (106a, 106b, 406a, 406b,705a, 705b) und einem dritten Antriebsrad (108, 408) besteht, wobei das erste Antriebsrad mit der dritten Antriebswelle (103, 203, 403, 605, 702) verbunden und das zweite Antriebsrad bei Betrieb mittdem ersten Antriebsrad und mit dem dritten Antriebsrad gekuppelt ist,
    der erste Propeller (101, 601) ist mit der zweiten Antriebsradwelle (106a, 106b, 406a, 705a, 705b) verbunden und der zweite Propeller (102, 602) ist mit dem dritten Antriebsrad (108, 408) verbunden, und
    die Antriebswelle (103, 203, 403, 605, 702) ist konzentrisch mit den zwei Propellern (101, 601, 707, 102, 602, 708) und läuft durch die beiden hindurch.
  2. Ein Mehrpropeller System mit Ausgleichsgetriebe (100, 200, 400, 600) entsprechend dem Anspruch 1, wobei die kennzeichnende Eigenart ist, dass das erste, zweite und dritte Antriebsrad Kegelradgetriebe sind, und dass die Welle des zweiten Antriebsrades im rechten Winkel zu den rotierenden Achsen des ersten und dritten Antriebsrades ist.
  3. Ein Mehrpropeller System mit Ausgleichsgetriebe (700) entsprechend dem Anspruch 1, wobei die kennzeichnende Eigenart ist, dass das erste und zweite Antriebsrad zylindrische mit Aussenzähnen versehene Antriebsräder sind und das dritte Antriebsrad ein mit Innenzähnen versehenes zylindrisches Antiebsrad ist und dass die Welle des zweiten Antriebsrades parallel mit den rotierenden Achsen des ersten und dritten Antriebsrades läuft.
  4. Ein Mehrpropeller System mit Ausgleichsgetriebe (100, 200, 700) entsprechend dem Anspruch 1, wobei die kennzeichnende Eigenart ist, dass sich das erste, zweite und dritte Antriebsrad innerhalb eines der Propeller befinden.
  5. Ein Mehrpropeller System mit Ausgleichsgetriebe (400) entsprechend dem Anspruch 1, wobei die kennzeichnende Eigenart ist, dass sich das erste, zweite und dritte Antriebsrad innerhalb eines Kraftübertragungsgehäuses befinden, welches sich nicht innerhalb keines der beiden Propeller befindet.
  6. Eine Azimutantriebsvorrichtung (500), deren kennzeichnende Eigenart ist, dass sie aus einem Differentialmultipropellersystem entsprechend dem Anspruch 1 besteht, worin die Antriebswelle so arrangiert ist, dass sie die Rotationskraft von einem Motor zu dem Differentialmultipropellersystem überträgt.
  7. Eine Wasserstrahlantriebsvorrichtung, deren kennzeichnende Eigenart ist, dass sie entsprechend dem Anspruch 1 aus dem Differentialmultipropellersystem besteht, wobei die Antriebswelle so arrangiert ist, dass sie die Rotationskraft von einem Motor zu dem Differentialmultipropellersystem überträgt.
  8. Eine Turbinenvorrichtung, deren kennzeichnende Eigenart ist, dass sie entsprechend dem Anspruch 1 aus einem Differentialmultipropellersystem besteht, wobei die Antriebswelle so arrangiert ist, dass sie die Rotationskraft von dem Differentialmultipropellersystem zu einem Generator überträgt.
EP98905432A 1997-02-25 1998-02-24 Mehrpropeller system mit ausgleichsgetriebe Expired - Lifetime EP0963315B1 (de)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
FI970778A FI970778A0 (fi) 1997-02-25 1997-02-25 Differential-dubbelpropellersystem
FI970778 1997-02-25
FI974256A FI974256A (fi) 1997-02-25 1997-11-17 Differentiaali-monipotkurijärjestelmä
FI974256 1997-11-17
PCT/FI1998/000162 WO1998038085A1 (en) 1997-02-25 1998-02-24 Differential multipropeller system

Publications (2)

Publication Number Publication Date
EP0963315A1 EP0963315A1 (de) 1999-12-15
EP0963315B1 true EP0963315B1 (de) 2002-12-18

Family

ID=26160341

Family Applications (1)

Application Number Title Priority Date Filing Date
EP98905432A Expired - Lifetime EP0963315B1 (de) 1997-02-25 1998-02-24 Mehrpropeller system mit ausgleichsgetriebe

Country Status (6)

Country Link
EP (1) EP0963315B1 (de)
AT (1) ATE229904T1 (de)
AU (1) AU6101498A (de)
DE (1) DE69810276T2 (de)
FI (1) FI974256A (de)
WO (1) WO1998038085A1 (de)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6220906B1 (en) * 1999-10-04 2001-04-24 The United States Of America As Represented By The Secretary Of The Navy Marine propulsion assembly
GB2368056B (en) * 2002-02-21 2002-09-04 Graham Miller Counter-rotating shaft drive mechanism
EP1900632A1 (de) * 2006-09-15 2008-03-19 Yellowfin Limited Schiffsantrieb und Ausführungseinzelheiten hierfür
ES2409113T3 (es) 2008-05-27 2013-06-25 Siemens Aktiengesellschaft Turbomáquina con al menos dos rotores contrarrotantes y equilibrio de momento mecánico
CN103202324B (zh) * 2013-02-05 2015-04-15 惠阳亚伦塑胶电器实业有限公司 一种食品搓揉设备

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE451191B (sv) * 1982-09-13 1987-09-14 Volvo Penta Ab Propellerdrev for batar
JPH06520B2 (ja) * 1988-11-30 1994-01-05 三菱重工業株式会社 舶用二重反転プロペラ駆動装置
US5009621A (en) * 1989-03-20 1991-04-23 Brunswick Corporation Torque splitting drive train mechanism for a dual counterrotating propeller marine drive system

Also Published As

Publication number Publication date
FI974256A (fi) 1998-08-26
AU6101498A (en) 1998-09-18
FI974256A0 (fi) 1997-11-17
ATE229904T1 (de) 2003-01-15
DE69810276D1 (de) 2003-01-30
EP0963315A1 (de) 1999-12-15
DE69810276T2 (de) 2004-04-22
WO1998038085A1 (en) 1998-09-03

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