EP2676876A2 - Submersible - Google Patents

Submersible Download PDF

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Publication number
EP2676876A2
EP2676876A2 EP13172027.8A EP13172027A EP2676876A2 EP 2676876 A2 EP2676876 A2 EP 2676876A2 EP 13172027 A EP13172027 A EP 13172027A EP 2676876 A2 EP2676876 A2 EP 2676876A2
Authority
EP
European Patent Office
Prior art keywords
rudder
hull
iii
submarine
rudder blades
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.)
Granted
Application number
EP13172027.8A
Other languages
German (de)
English (en)
Other versions
EP2676876B1 (fr
EP2676876A3 (fr
Inventor
Randolf Teppner
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.)
ThyssenKrupp Marine Systems GmbH
Original Assignee
ThyssenKrupp Marine Systems GmbH
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 ThyssenKrupp Marine Systems GmbH filed Critical ThyssenKrupp Marine Systems GmbH
Publication of EP2676876A2 publication Critical patent/EP2676876A2/fr
Publication of EP2676876A3 publication Critical patent/EP2676876A3/fr
Application granted granted Critical
Publication of EP2676876B1 publication Critical patent/EP2676876B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63GOFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
    • B63G8/00Underwater vessels, e.g. submarines; Equipment specially adapted therefor
    • B63G8/14Control of attitude or depth
    • B63G8/18Control of attitude or depth by hydrofoils
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63GOFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
    • B63G8/00Underwater vessels, e.g. submarines; Equipment specially adapted therefor
    • B63G8/14Control of attitude or depth
    • B63G8/20Steering equipment

Definitions

  • the invention relates to a submarine with the features specified in the preamble of claim 1.
  • submarines which have at their rear a propeller as the main drive, wherein at the rear end, which tapers in the direction of the stern at a circular or oval cross-section, rudder blades for lateral and depth control are arranged.
  • the invention has the object to provide a submarine, in which an inhomogeneous flow of the arranged at the rear of the submarine propeller due to the previously arranged at the rear of the rudder blades prevented or at least reduced to a considerable extent in improving the rudder efficiency.
  • the submarine according to the invention has rudder blades arranged in a manner known per se on the outside of its hull.
  • the rudder blades can be either the front ailerons, which are arranged, for example, on the tower of the submarine or on a forward hull of the submarine in the normal direction of travel of the submarine, as well as the rear and side rudders.
  • the rudder blades behind the rudder blades arranged at the stern of the submarine propellers are the outside of the hull and the side facing the ship at least one of the rudder blades and preferably all rudder blades arranged and designed so that the rudder blade at least in the neutral position of the rudder blade adjacent pivot areas free space to the Outside of the boat body connects. Ie.
  • a wide angular range for example in an angular range of about ⁇ 30 ° to a neutral position of the rudder blades, in which the rudder blades can be pivoted during operation of the submarine, the geometric surface of the outside of the hull and the contour of the hull directly opposite Side of the rudder blades coordinated so that no or only forms a negligible in terms of turbulence freely flowed space between the rudder blades and the outside of the hull.
  • a preferred embodiment for avoiding free spaces between the rudder blades and the boat body is that the outer side of the hull is at least in parts of the areas over which the rudder blades are pivotally formed as a section of a surface of revolution and preferably spherically curved, wherein the outside of the hull facing the sides of the rudder blades have a curvature corresponding to the curvature of the outside of the hull.
  • the rudder axis of the rudder blades is suitably aligned normal to a voltage applied to the curvature of the hull tangent.
  • spherical curvature formed on the outside of the hull curvature can optionally be convex convex so convexly outwardly, in which case the boat body directly opposite side of the rudder blades is concave, or it may be negative so concave curved inward then the Hull directly opposite side has a corresponding convex curvature.
  • the radius of curvature of the spherically formed portion of the hull and the corresponding radius of curvature of the outer side of the hull directly opposite side of the rudder blade are selected such that the transitions from the spherically formed portions of the hull to the adjoining non-spherically curved portions of the hull as fluent as possible run so that no larger edges are formed, which could otherwise lead to stalls at worst.
  • the outer side of the hull each at least in the areas over which the rudder blades are pivotal, downstream of the rudder axes of the rudder blades a spherical curvature with a first radius of curvature and upstream of the rudder axes of the rudder blades has a spherical curvature with a second radius of curvature, wherein the sides of the rudder blades facing the outside of the hull have with the bulges of the outside of the hull corresponding bulges.
  • the hull may have a spherical shape with a first radius and in the areas beyond which one starts from the rudder axes the rudder blades is pivoted in the direction of the bow of the submarine pointing part of the rudder blades, having a spherical shape with a second radius, which is different from the first radius.
  • a further advantageous and particularly easy to implement measure to prevent free space between the rudder blades and the hull when pivoting the rudder blades is to form the outside of the hull in each case at least in parts of the pivoting areas of the rudder blades.
  • the areas of the outside of the hull, over which the rudder blades are flowed upstream and downstream of the rudder axis of these rudder blades may be formed as planes, which planes may be oriented at the rear of the boat in adaptation to its taper obliquely to the longitudinal axis of the submarine.
  • the hull directly facing sides of the rudder blades are straight, these straight sides are oriented relative to the rudder axes of the rudder blades so that these sides connect free space to the flat outer side portions of the hull.
  • the outer cross-sectional contour of the rear of the ship at least in the region of the arrangement of the rudder blades have the shape of a genuine or rounded polygon, ie, the cross section of the rear of the vessel may be formed at least in the area in which the rudder blades are arranged angular, the corners preferably rounded.
  • the polygonal cross section of the rear end depends on the number of rudder blades arranged on the stern.
  • the submarine according to the invention can have a genuine or rounded triangular cross-sectional contour at least in the region of the rear hull in which a rudder blade is arranged on each of the three outer sides thus formed is.
  • the submarine according to the invention has four rudder blades arranged at its rear end, the submarine can advantageously have a genuine or rounded quadrangular outer cross-sectional contour, at least in the region of the rear hull in which the rudder blades are arranged.
  • a rudder is understood to mean such an arrangement of the rudder blades, in which two rudder blades are aligned vertically in a common plane and two rudder blades are aligned horizontally in a common plane in normal horizontal floating or floating position of the submarine.
  • the submarine has a real or rounded quadrangular outer cross section in the region of its rear end, the outer sides of this cross section can be aligned in pairs horizontally and vertically.
  • the submarine according to the invention can have four rudder blades in the region of the rear ship, which form an X-rudder.
  • the rudder blades are at an angle of 30-60.degree.
  • at least a portion of the aft-hull may have a true or rounded quadrangular outer cross-section, with two horizontal corners of the true or rounded quadrangular cross-section on a vertical and the remaining two corners of the cross-section in the normal horizontal floating and floating position of the submarine a horizontal are arranged.
  • This embodiment is advantageous in that it complicates the sonar location of the submarine.
  • the Fig. 1 and 2 show a rear ship 2 of a submarine. This rear ship 2 goes into the stern 4 of the submarine. At the rear 4 a propeller 6 is arranged. On the outside of the rear of the ship 2 four rudder blades 8 are arranged, which are each pivotable about a rudder axis A.
  • the rudder blades 8 form a rudder, wherein in the horizontal floating or floating position of the submarine two rudder blades 8 are aligned in a common vertical plane and two rudder blades 8 are aligned in a common horizontal plane.
  • the rear of the ship 2 has in the region of the arrangement of the rudder blades 8 a curved rectangular cross-section, wherein the corners of the rectangle are rounded.
  • the four regions of the rear hull 2 lying between these corners have a spherical surface with a radius of curvature R corresponding to the radius of curvature of the rear hull in the longitudinal direction.
  • the four rudder blades 8 at a rear of the ship 2 directly opposite side 10 with a to the Buckling radius R complementary radius of curvature vaulted.
  • FIG. 3 illustrated Hinterschiff 2 I differs from that in the Fig. 1 and 2 illustrated Schuschiff 2 above all to the effect that the rudder blades 8 form an X-rudder and against the rudder blades 8 at the in the Fig. 1 and 2 Rear of the ship 2 are arranged offset by an angle of 45 °.
  • the rear of ship 2 I has in the area in which the rudder blades 8 are pivotable, a curved rectangular cross section.
  • the cross-sectional contour is such that two corners of the rectangular cross-section are arranged in a horizontal vertical plane of the submarine in a common vertical plane and the remaining two corners in a common horizontal plane.
  • the rear hull 2 "shown has a purely rectangular cross-section with rounded corners whose cross-sectional area is continuously reduced in the direction of the stern 4. Accordingly, the rear hull 2" has the shape of a quadrangular truncated pyramid converging in the stern 4 of the submarine.
  • the planar outer surfaces of the rear hull 2 ", on each of which a rudder blade 8" is arranged pivotable about a pivot axis A oriented normal to the respective outer surface, are aligned in such a way that The four rudder blades 8 "form a rudder 8.
  • the sides of the rudder blades 8" directly facing the rear vane 2 are straight and aligned normal to the rudder axles A corresponding to the planar configuration of the four outer sides of the aft ship 2".
  • FIG. 6 in a cross-sectional view illustrated Schuschiff 2 III differs from that in the Fig. 4 and 5 represented rear end 2 "only to the effect that the truncated pyramidal rear end 2 III relative to the rear end 2" relative to a center axis of the rear of the ship 2 III is rotated by an angle of 45 °, so that arranged on the four flat outer sides of the rear of the vessel 2 III rudder leaves "form an X-rudder.
  • FIGS. 7 and 8 show a rear hull 2 IV of a submarine with a cross-section in the shape of an equilateral triangle, which continuously decreases in the direction of the tail 4 of the submarine, so that the rear hull 2 IV essentially forms a stump of a tetrahedron.
  • the rear end 2 IV tapers in the direction of the stern 4 on its three outer sides with a curvature radius R I.
  • the same radius of curvature R I the outer sides of the cross section, on each of which a rudder blade 8 III is arranged, also to their limited rounded corners, so that the outer sides are curved in the area of the rudder blades 8 III spherically outward.
  • the rudder blades 8 III are arched at their rear side 2 IV directly facing sides in each case with a radius of curvature corresponding to the radius of curvature R I such that form no free spaces when pivoting the rudder blades 8 III between the rear end 2 IV and the rudder blades 8 III ,
  • rudder blade 8 IV has on its rear side of the ship, not directly facing side 10 I a curvature, which differs downstream of the rudder axis A of the curvature upstream of the rudder axis A.
  • the side 10 I in a portion upstream of the rudder axis A is arched with a curvature radius R "and vaulted downstream of the rudder axis A with a curvature radius R III , wherein the curvature radius R III is greater than the curvature radius R".
  • rudder blade 8 IV As well as the rudder blades 8, 8 II and 8 III in an angular range a of 60 ° pivotable. Accordingly, the rudder blade 8 IV on the outside of the rear of the ship in the Fig. 10 and 11 illustrated embodiment over an area X upstream of the rudder axis A and pivoted over a region Y downstream of the rudder axis.
  • the outer side of the rear end is therefore curved spherically outward in the region X with a radius complementary to the radius of curvature R" and spherical in the region Y with a radius complementary to the radius of curvature R III arched outwards.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laying Of Electric Cables Or Lines Outside (AREA)
  • Toys (AREA)
  • Hydraulic Turbines (AREA)
  • Electric Cable Installation (AREA)
EP13172027.8A 2012-06-21 2013-06-14 Submersible Active EP2676876B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102012210499A DE102012210499A1 (de) 2012-06-21 2012-06-21 Unterseeboot

Publications (3)

Publication Number Publication Date
EP2676876A2 true EP2676876A2 (fr) 2013-12-25
EP2676876A3 EP2676876A3 (fr) 2016-12-21
EP2676876B1 EP2676876B1 (fr) 2019-03-20

Family

ID=48669757

Family Applications (1)

Application Number Title Priority Date Filing Date
EP13172027.8A Active EP2676876B1 (fr) 2012-06-21 2013-06-14 Submersible

Country Status (3)

Country Link
EP (1) EP2676876B1 (fr)
KR (1) KR101614894B1 (fr)
DE (1) DE102012210499A1 (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109533259A (zh) * 2018-10-26 2019-03-29 北京精密机电控制设备研究所 一种auv用操纵一体化装置
CN113734392A (zh) * 2021-09-18 2021-12-03 深圳先进技术研究院 舵控操纵装置及方法
WO2021194565A3 (fr) * 2019-12-13 2021-12-23 Current Power Energy Systems, Inc. Systèmes d'énergie électrique à partir de courants marins
WO2023039876A1 (fr) * 2021-09-18 2023-03-23 深圳先进技术研究院 Appareil et procédé de commande de gouvernes
WO2023117617A1 (fr) * 2021-12-21 2023-06-29 Atlas Elektronik Gmbh Dispositif comprenant une coque présentant dans une zone de pivotement d'un gouvernail une section transversale non circulaire

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107792325B (zh) * 2017-10-12 2020-04-14 中国船舶重工集团公司第七一九研究所 适用于微型无人潜航器的尾部集成结构及其操舵方法

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3448714A (en) * 1968-01-22 1969-06-10 Us Navy Fin and revolving cylinder bidirectional steering actuator
GB2164612B (en) * 1979-09-10 1986-09-03 British Aerospace Vehicles fitted with thrust vector control systems
DE3242290C2 (de) * 1982-11-16 1986-03-20 Howaldtswerke - Deutsche Werft AG Hamburg und Kiel, 2300 Kiel Abweiser an Antriebs- und Steuereinrichtungen von Schiffen
US4919066A (en) * 1989-01-19 1990-04-24 Allied-Signal, Inc. Hydrodynamic configuration for underwater vehicle
US5487351A (en) * 1995-01-13 1996-01-30 The United States Of America As Represented By The Secretary Of The Navy Control surface for underwater vehicle
US6223676B1 (en) * 1999-11-23 2001-05-01 Newport News Shipbuilding And Dry Dock Company Control for X-stern vehicle
JP2007276609A (ja) * 2006-04-06 2007-10-25 Osaka Prefecture Univ 水中グライダー
DE102008031044B4 (de) * 2008-06-26 2014-08-21 Thyssenkrupp Marine Systems Gmbh Vorrichtung für U-Boote als Abweiser
ES2386442B1 (es) * 2009-11-27 2013-07-09 Airbus Operations S.L. Carena de timón de profundidad de aeronave.

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109533259A (zh) * 2018-10-26 2019-03-29 北京精密机电控制设备研究所 一种auv用操纵一体化装置
WO2021194565A3 (fr) * 2019-12-13 2021-12-23 Current Power Energy Systems, Inc. Systèmes d'énergie électrique à partir de courants marins
CN113734392A (zh) * 2021-09-18 2021-12-03 深圳先进技术研究院 舵控操纵装置及方法
WO2023039876A1 (fr) * 2021-09-18 2023-03-23 深圳先进技术研究院 Appareil et procédé de commande de gouvernes
WO2023117617A1 (fr) * 2021-12-21 2023-06-29 Atlas Elektronik Gmbh Dispositif comprenant une coque présentant dans une zone de pivotement d'un gouvernail une section transversale non circulaire

Also Published As

Publication number Publication date
EP2676876B1 (fr) 2019-03-20
DE102012210499A1 (de) 2013-12-24
KR101614894B1 (ko) 2016-04-22
KR20130143497A (ko) 2013-12-31
EP2676876A3 (fr) 2016-12-21

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