US3895598A - Ship propulsion unit having a variable pitch propeller - Google Patents

Ship propulsion unit having a variable pitch propeller Download PDF

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Publication number
US3895598A
US3895598A US443316A US44331674A US3895598A US 3895598 A US3895598 A US 3895598A US 443316 A US443316 A US 443316A US 44331674 A US44331674 A US 44331674A US 3895598 A US3895598 A US 3895598A
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US
United States
Prior art keywords
hollow member
propeller
hub
servo motor
propulsion unit
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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
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US443316A
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English (en)
Inventor
Karl Blickle
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JM Voith GmbH
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JM Voith GmbH
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Publication date
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H3/00—Propeller-blade pitch changing
    • B63H3/06—Propeller-blade pitch changing characterised by use of non-mechanical actuating means, e.g. electrical
    • B63H3/08—Propeller-blade pitch changing characterised by use of non-mechanical actuating means, e.g. electrical fluid
    • B63H3/081—Propeller-blade pitch changing characterised by use of non-mechanical actuating means, e.g. electrical fluid actuated by control element coaxial with the propeller shaft
    • B63H3/082—Propeller-blade pitch changing characterised by use of non-mechanical actuating means, e.g. electrical fluid actuated by control element coaxial with the propeller shaft the control element being axially reciprocatable
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H3/00—Propeller-blade pitch changing
    • B63H3/06—Propeller-blade pitch changing characterised by use of non-mechanical actuating means, e.g. electrical
    • B63H3/08—Propeller-blade pitch changing characterised by use of non-mechanical actuating means, e.g. electrical fluid
    • B63H2003/088—Propeller-blade pitch changing characterised by use of non-mechanical actuating means, e.g. electrical fluid characterised by supply of fluid actuating medium to control element, e.g. of hydraulic fluid to actuator co-rotating with the propeller

Definitions

  • ABSTRACT A ship propulsion unit comprises a variable pitch pro- Foreign Application Priority Data peller supported in a hub mounted on the lower end of a hollow member which 1s plvotably supported In a Feb. 23, 1973 Germany 2308931 fixed housing Such that the hollow member and hub are both pivotable about a vertical axis.
  • a coaxial [52] U.S. Cl 115/35; 416/147 drive Shaft for the propeller is enclosed within the [51] Int. Cl B6311 1/14 low element.
  • a plurality of pairs of Sealing rings are [58] Fleld of Search 1 15/34 34 provided between the hollow member and a portion of 115/41 42416l1471 174; 114/150 said fixed housing to define a plurality of annular chambers through which pass a number of supply and [56] References Cited return lines for several fluid pressure systems which UNITED STATES PATENT lead to the propeller and a servo motor for adjusting 2,458,813 1/1949 Wanzer 115/35 the Pitch Of the Propeller blades- 3,266,454 8/1966 Sterling et al....
  • the present invention relates to a ship propulsion unit having a variable pitch propeller supported in a hub mounted on a hollow member such that both the hollow member and hub are pivotable about a vertical axis, more particularly, to the control and operation of the propeller and associated components through a plurality of hydraulic systems.
  • the propeller thrust can be varied infinitely with respect to both magnitude and direction while the prime mover or source of power could be operated always at a constant RPM and in the same direction of rotation. This would eliminate the necessity of providing reverse or reduction gearing.
  • a ship propulsion unit of the general type as described above wherein the unit is pivotable and the propeller is variable in pitch is disclosed in the German publication document 1,922,834. Varying the pitch of the conventional variable pitch propeller is achieved by hydraulic control systems in the hub. However, such hydraulic systems present difficulties in the connections between moving and stationary components because of the pivoting of the hub. In order to overcome this problem, this German publication document has disclosed a mechanical actuation device for varying the propeller pitch. This mechanical actuation device is disadvantageous in that the transmission of power by such a propulsion unit is limited and such a unit can be used only up to about 1,000 H.P. In addition, because of the mechanical transmission there are a number of components which are susceptible to possible failure.
  • a further disadvantage is that only a single oil filled chamber is provided for the object of lubrication in the control element.
  • a direct lubrication of the bearings, particularly with respect to an oil retaining packing which is effective for preventing the penetration of water is not possible.
  • the pivotable element possesses a double bearing arrangement which is also disadvantageous since this arrangement absorbs the pushing and tilting forces acting upon the propeller but the over-all height of the propeller unit is too great because of this construction.
  • FIG. 1 is an elevational view of a ship propulsion unit according to the present invention with the upper portion of the unit being shown in section;
  • FIG. 2 is a longitudinal view of the hub element of the unit of FIG. I but in enlarged scale;
  • FIG. 3 is a sectional view in enlarged scale of that portion of the unit wherein the hydraulic systems are introduced into the hollow member;
  • FIG. 4 is a sectional view taken along the line IV-IV of FIG. 3.
  • the ship propulsion unit comprises a variable pitch propeller 2 supported upon a hub l which is rigidly connected to a hollow member 3 positioned vertically with respect to the ship.
  • the hollow member 3 has a teardrop or streamline cross-section to reduce hydraulic flow resistance upon the propulsion uIIIt.
  • the propeller is driven by two bevel gear stages 4 and 5 that are generally arranged in the form of a Z as will be apparent from a study of FIGS. 1 and 2.
  • a drive shaft 6 is mounted coaxially within the hollow member 3 and drivingly connects the bevel gear stages.
  • the shaft is provided with an insertion coupling 7 which eliminates bending forces acting upon the gearing and also facilitates the disassembly of the propeller.
  • the insertion coupling is readily engaged and disengaged by suitable movement in an axial direction and may be constructed in a form of a gear coupling, a splined clutch, a bolt clutch or the like as known in the art.
  • the hollow member 3 is mounted within the hull of the ship by being supported by an anti-friction ball or anti-friction tapered roller bearing 8 which functions to absorb shearing and tilting forces. With this overhanging support such forces can be reliably controlled and transmitted to the hull of the ship.
  • the anti-friction bearing 8 has an inner race 13 which is formed by an internal ring gear 9 which is attached to the upper end or outwardly tapering portion of the hollow member 3. This construction of the inner bearing race not only reduces the costs of the installation but simplifies the structure.
  • the hollow member 3 together with the hub l are pivoted by means of a spur gear 10 which meshes with the internal gear 9 and is driven by a suitable motor as known in the art but not illustrated in the drawings.
  • the blades of the propeller are indicated at 11 and are adjusted with respect to pitch hydraulically by means of a piston rod 12.
  • the operative connection between the rod 12 and the blades 11 is known in the art.
  • Such a structure may comprise a displaceable cross element connected to the piston rod and coupling rods engaging the cross element.
  • a servo motor 15 is provided for displacing the piston rod 12 and is positioned between propeller bearings 16a and 16b for the purpose of reducing the total length of the hub l.
  • the pressure fluid which may be hydraulic fluid for the servo motor 15, is controlled by an auxiliary fluid pressure motor 17 having a cylinder from which extends a piston rod operatively connected by linkage 37 to a control pin 18.
  • the oil level in the hub l is always maintained constant by a pump 19 which draws the oil from the huh I through a suction tube 36' and allows the oil to flow through the various lubrication points back into the hub.
  • an oil retaining packing 20 is provided for the propeller shaft.
  • the internal pressure on packing 20, which is higher than the external pressure, is provided by an oil gravity tank 21 connected to the pressure of the lubricating oil and is located above the water line. Oil is introduced to the packing through the line 31.
  • FIGS. 3 and 4 The connection of the several hydraulic systems from the fixed housing to the pivotable hollow member 3 may be seen in FIGS. 3 and 4 and the lines of the separate hydraulic systems are shown in FIG. 3 as being slightly shifted for the purpose of clarifying the invention.
  • the peripheral relationship of the lines may be seen in FIG. 4.
  • a plurality of sealing rings 24 are positioned in pairs between the pivotable hollow member 3 and fixed housing 23 such that a pair of sealing rings 24 forms a number of annular chambers 2530.
  • the individual hydraulic systems can be connected through these annular chambers into the hub 1 independently of the position of the hollow member 3.
  • An oil supply line 31 for the packing 20 connects from fixed housing 23 into annular chamber 25 and the inner portion of this line indicated as 31' then continues in the interior of the hollow member 3.
  • Lubricating oil is introduced in the same manner through a lubricating oil line 32 into annular chamber 26 and then supplied through inner line 32' as may be desired.
  • the control fluid or oil for the auxiliary cylinder 17 is supplied through a supply line 33 into annular chamber 27 and the oil is returned from the cylinder 17 through return line 34 through annular chamber 28.
  • the oil for servo motor 15 is supplied through line 35 and annular chamber 29 and then through inner line 35' which connects directly to the servo motor.
  • Pump 19 is connected through a suction tube 36, annular chamber 30 and a suction tube 36 to the oil bath or sump in hub l.
  • the oil line 31 terminates at the propeller shaft packing 20 and enables the oil retaining packing to prevent the penetration of water at this point.
  • the auxiliary cylinder 17 is actuated through supply line 33 and return line 34'.
  • the actuation of the cylinder operates linkage 37 which controls the oil lines 38 and 39 to control the oil to the chambers 43 and 44 on both sides of the servo motor or piston 15.
  • the oil for the servo motor 15 as controlled by the auxiliary cylinder 17 is introduced into the desired chamber of the servo motor through oil line bores 40 and 41 and a recess 42 in the control pin 18.
  • the left end of bore 40 is plugged with respect to bore 46 after the manufacturing operation of boring bore 40 through pin 18.
  • the piston rod 12 is displaced forwardly or rearwardly to effect an adjustment of the pitch of the blades 11.
  • the two chambers 43 and 44 of the servo motor 15 are emptied in a suitable position of the control pin 18 through an annular chamber 45 located between the control pin 18 and piston rod 12 and through bores 46, 47 into the lower portion of the hub l.
  • the control pin 18 is so constructed that during filling of the chamber 43 through line 38 the chamber 44 is emptied simultaneously through line 39 and bores 46 and 47.
  • the chamber 43 is emptied in the same manner through line 38 into annular chamber 45 and chamber 44 is supplied simultaneously with oil under pressure.
  • the oil level in the hub is maintained constant by the suction tube 36' which opens close to the bottom of the hub l as may be seen in FIG. 2.
  • Lubricating oil is supplied to propeller bearings 16a and 16b through lubricating oil ine 32 that further divides into lines 32line and 321). If desired. the lubricating oil line 32 can be further subdivided into branch lines for lubricating additional bearing points.
  • the propulsion unit can be readily mounted and removed because of the axial insertion coupling 7 that divides drive shaft 6 into two separate components. After loosening connecting bolts 48, the hollow member 3 "together with hub 1 and propeller 2 can be removed in a downward direction as viewed in FIG. 1. The upper portion of the propulsion unit together with spur gear 10 is lifted upwardly in the same manner after bolts 49 are loosened.
  • a pretensioned coil spring 50 which functions to place the propeller blades in a predetermined pitch in the event the servo motor pressure should fail.
  • the adjusting of the blades to such a pitch insures that the ship is still maneuverable and can probably be guided to a port with the blades at a small pitch.
  • the propulsion unit and hydraulic connections according to the present invention is advantageous in that the unit can transmit power up to and above 30,000 'H.P.
  • the entire drive possesses relatively few moving parts and consequently is less susceptible to mechanical failure.
  • the hydraulic system connections as disclosed herein enable the hollow supporting member together with the hub to be pivoted as a unit as desired without any necessity of providing abutment or other means for limiting movement. Depending upon the number of sealing rings provided in accordance with the present invention any number of hydraulic lines can be introduced into the hub.
  • the overhanging or flying support or suspension of the hollow member and hub by the use of tapered antifriction roller bearings is also advantageous since this structure considerably reduces the overall size and weight of the installation.
  • a ship propulsion unit the combination of a fixed housing, a vertical hollow member pivotable on said housing about a vertical axis, anti-friction bearing means in said fixed housing for supporting said hollow member therefrom in overhanging relationship to absorb axial and vertical forces, a hub mounted on said hollow member and pivotable therewith, a variable pitch propeller on said hub.
  • means for driving said propeller comprising a drive shaft coaxially positioned within said hollow member.
  • servo motor means within said hub for adjusting the pitch of said propeller blades, packing means between said hollow member and a portion of said housing, said packing comprising a plurality of pairs of spaced sealing rings and an annular chamber being defined between each said pair of rings, a plurality of fluid pressure systems for said propeller and servo motor means and each system comprising a supply and a return line passing through an annular chamber of said packing means, each of said supply and return lines having an outer portion connected to a said annular chamber from outside of said fixed housing and an inner portion within said hollow member and connected to the said annular chamber.
  • a motor having an output shaft with a spur gear thereon and said gear meshing with said ring gear so that said hollow member and hub are rotated by said motor.
  • said servo motor means comprises a servo motor and a piston rod extending therefrom operatively connected to the blades of the propeller to adjust the pitch thereof.
  • a control pin to regulate the supply of pressure medium through the hydraulic system sup ply line connected to said servo motor means.
  • an auxiliary fluid pressure motor including a cylinder and a piston and said piston being connected to said control pin.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Actuator (AREA)
  • General Details Of Gearings (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
US443316A 1973-02-23 1974-02-19 Ship propulsion unit having a variable pitch propeller Expired - Lifetime US3895598A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2308931A DE2308931B2 (de) 1973-02-23 1973-02-23 Schiffsantrieb in Innenbordbauweise mit einem Verstellpropeller

Publications (1)

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US3895598A true US3895598A (en) 1975-07-22

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US (1) US3895598A (enrdf_load_stackoverflow)
JP (2) JPS5041295A (enrdf_load_stackoverflow)
DE (1) DE2308931B2 (enrdf_load_stackoverflow)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4028004A (en) * 1974-07-03 1977-06-07 Lips B.V. Feathering controllable pitch propeller
US4365937A (en) * 1979-11-26 1982-12-28 Hiebert Harold L Adjustable pitch propeller drive
US4643643A (en) * 1984-05-14 1987-02-17 Blohm & Voss Ag Apparatus for adjusting and locking pitch of a variable pitch propeller on a ship
US4747359A (en) * 1985-08-29 1988-05-31 Tokyo Keiki Co., Ltd. Apparatus for controlling the turn of ship
US4906213A (en) * 1989-04-18 1990-03-06 Bird-Johnson Company Apparatus for detecting the pitch of a marine controllable pitch propeller
US4907992A (en) * 1988-10-17 1990-03-13 Bird-Johnson Company Oil distribution box for a marine controllable pitch propeller
US5073134A (en) * 1990-01-04 1991-12-17 Mueller Peter Boat drive with adjustable pitch propeller
US10968882B2 (en) 2017-03-24 2021-04-06 Kabushiki Kaisha Toshiba Movable-blade operation system for hydraulic machine

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5220596A (en) * 1975-08-08 1977-02-16 Kawasaki Heavy Ind Ltd Pressurized oil introduction system for adjustment of revolving thrust er
ES465685A1 (es) * 1977-01-07 1978-09-16 Ferodo Sa Dispositivo de mando en rotacion y en orientacion de una he-lice-timon para vehiculo flotante.
JPH0442239Y2 (enrdf_load_stackoverflow) * 1985-03-07 1992-10-05
JPH0632480Y2 (ja) * 1985-03-07 1994-08-24 川崎重工業株式会社 旋回式スラスタ

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2458813A (en) * 1943-02-13 1949-01-11 Murray & Tregurtha Inc Outboard propeller mechanism for barges, scows, and the like
US3266454A (en) * 1964-10-22 1966-08-16 Richard J Sterling Inboard propulsion and steering means
US3376842A (en) * 1960-05-11 1968-04-09 Volvo Penta Ab Boat propulsion mechanism
US3534703A (en) * 1967-01-09 1970-10-20 Saab Scania Ab Outboard propelling system comprising an adjustable propeller
US3762359A (en) * 1971-10-20 1973-10-02 Mobil Oil Corp Marine propeller stern bearing-shaft design and seal arrangement

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH232017A (de) * 1943-03-06 1944-04-30 Sulzer Ag Propellerantriebsanlage an Schiffen.
CH279159A (de) * 1946-10-07 1951-11-15 Johannes Liaaen Nils Propellerverstelleinrichtung mit Servomotor für Schiffe, Pumpen oder Turbinen.
DE890610C (de) * 1951-10-17 1953-09-21 Theodor Klatte Fa Hydraulische Antriebsvorrichtung fuer Schiffsschrauben
DE1922834A1 (de) * 1969-05-05 1970-11-26 Kiyoshi Shima Steuervorrichtung fuer Schiffsschrauben

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2458813A (en) * 1943-02-13 1949-01-11 Murray & Tregurtha Inc Outboard propeller mechanism for barges, scows, and the like
US3376842A (en) * 1960-05-11 1968-04-09 Volvo Penta Ab Boat propulsion mechanism
US3266454A (en) * 1964-10-22 1966-08-16 Richard J Sterling Inboard propulsion and steering means
US3534703A (en) * 1967-01-09 1970-10-20 Saab Scania Ab Outboard propelling system comprising an adjustable propeller
US3762359A (en) * 1971-10-20 1973-10-02 Mobil Oil Corp Marine propeller stern bearing-shaft design and seal arrangement

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4028004A (en) * 1974-07-03 1977-06-07 Lips B.V. Feathering controllable pitch propeller
US4365937A (en) * 1979-11-26 1982-12-28 Hiebert Harold L Adjustable pitch propeller drive
US4643643A (en) * 1984-05-14 1987-02-17 Blohm & Voss Ag Apparatus for adjusting and locking pitch of a variable pitch propeller on a ship
US4747359A (en) * 1985-08-29 1988-05-31 Tokyo Keiki Co., Ltd. Apparatus for controlling the turn of ship
US4907992A (en) * 1988-10-17 1990-03-13 Bird-Johnson Company Oil distribution box for a marine controllable pitch propeller
US4906213A (en) * 1989-04-18 1990-03-06 Bird-Johnson Company Apparatus for detecting the pitch of a marine controllable pitch propeller
US5073134A (en) * 1990-01-04 1991-12-17 Mueller Peter Boat drive with adjustable pitch propeller
US10968882B2 (en) 2017-03-24 2021-04-06 Kabushiki Kaisha Toshiba Movable-blade operation system for hydraulic machine

Also Published As

Publication number Publication date
JPS54167993U (enrdf_load_stackoverflow) 1979-11-27
JPS5041295A (enrdf_load_stackoverflow) 1975-04-15
DE2308931A1 (de) 1974-09-05
DE2308931B2 (de) 1978-06-29

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